These slides show how the falling costs of energy and transportation systems have been primarily from increases in scale. Increases in the scale of steam, internal combustion, and jet engines along with steam turbines and other electrical generating plants drove dramatic reductions in the cost of energy in the 19th and early 20th centuries. Similar cost reductions occurred as the scale of locomotives, ships, vehicles, and planes were increased. However, now that the limits to this scaling have been reached and carbon emissions have become a major problem, new sources of energy must be found. Electric vehicles, magnetic levitating trains, and fusion are some of the new concepts that may become economically feasible. Another set of slides addresses solar cells and wind turbines. These slides are based on a forthcoming book entitled “Technology Change and the Rise of New Industries and they are the ninth session in a course entitled “Analyzing Hi-Tech Opportunities.”
The document provides information about sections and voters in an election. It lists the following sections and number of voters in each:
Section 1: Abdulhamid Ibrahim Jamal Ibrahim: 1 voter
Section 2: Abdelraziq Nabil Ahmad: 1 voter
Section 3: Ahmad Mahmoud Shihata Ahmad Abdallah: 2 voters
Section 1: Ahmad Said Hussein Abdelrahman: 1 voter
1) The document discusses gas turbine combustion systems and provides an overview of the speaker's background working in the gas turbine industry.
2) It then covers various topics related to gas turbine combustors such as design requirements, combustion chemistry, alternative fuels, and challenges with variable load conditions.
3) Finally, it discusses the speaker's current role at Solar Turbines and provides technical details about gas turbine cycles, components, and performance parameters.
This document provides a training report from an internship at Rajghat Power House. It includes an acknowledgements section thanking those who supported the training. It also includes a preface describing how practical experience is important for engineering students to develop hands-on knowledge. The bulk of the document consists of sections on power plant basics, control and instrumentation, and conclusions from the learning experience. It aims to impart knowledge of fundamentals and applications gained during the industrial training placement.
The document provides an overview of the gas turbine engines market, including aviation gas turbines and industrial gas turbines. It states that the aviation gas turbine engines market was worth $64 billion in 2015 and is projected to reach $82 billion by 2020, growing at a CAGR of 4.13%. The main segments are turbofan engines, turboprop engines, turboshaft engines, and auxiliary power units. The key drivers are the re-equipment of modern aviation and increasing demand for commercial aircraft. The largest players are Rolls-Royce, Pratt & Whitney, GE Aviation, and CFM International. The industrial gas turbines market was worth $34.8 billion in 2015 and is projected to reach $37.7
A gas turbine, also called a combustion turbine, is a type of internal combustion engine. It has an upstream rotating compressor coupled toa downstream turbine, and a combustion chamber in-between. Energy is added to the gas stream in the combustor, where fuel is mixed with air and ignited. In the high-pressure environment of the combustor, combustion of the fuel increases the temperature. The products of the combustion are forced into the turbine section
Visit https://www.topicsforseminar.com to Download
GE ADGT Application CHP-Cogen-CC
GE코리아 뉴스레터를 구독하세요! http://goo.gl/IE8WS8
GE코리아 YouTube 채널을 구독하세요! http://goo.gl/M2gc8m
상상을 현실로 만듭니다. Imagination at work.
GE가 꿈꾸는 가치입니다. 아니, GE는 단지 꿈만 꾸고 있는 것이 아닙니다. 상상을 현실로 만들기 위해, 불가능했던 것을 가능하게 만들기 위해 쉬지 않고 움직이고 있습니다. GE는 에너지, 의료, 항공, 수송, 금융 등의 여러 분야에서 고객과 인류사회의 진보를 위해 더 편리하고 빠르며 친환경적인 솔루션을 찾아냅니다.
Connect with GE Online:
GE코리아 웹사이트: http://www.ge.com/kr/
GE리포트코리아: http://www.gereports.kr/
GE코리아 페이스북 페이지: hhttps://www.facebook.com/GEKorea
GE코리아 슬라이드쉐어: http://www.slideshare.net/GEKorea
This report reviews current turbofan engine noise and engine noise reduction technology, specifically focusing on the engine technology of larger passenger jetliners which have entered into service within the last ten (10) years.
Important factors in turbofan engine design from a community noise perspective and the sources of noise along with their relative importance are also presented. A review of different engine noise reduction technologies is presented, as well as an estimate of the technology’s readiness level.
Finally, potential trade-offs, challenges, and future technology directions are outlined.
Gas Turbine , CCPP, Operation& Maintenance, spare part supply, Manpower service for Power Plant, GE LM6000 ,GE LM2500, GE FRAME 6,... P&W, MAN, RR, Turbine commisioning and start up,......
The document provides information about sections and voters in an election. It lists the following sections and number of voters in each:
Section 1: Abdulhamid Ibrahim Jamal Ibrahim: 1 voter
Section 2: Abdelraziq Nabil Ahmad: 1 voter
Section 3: Ahmad Mahmoud Shihata Ahmad Abdallah: 2 voters
Section 1: Ahmad Said Hussein Abdelrahman: 1 voter
1) The document discusses gas turbine combustion systems and provides an overview of the speaker's background working in the gas turbine industry.
2) It then covers various topics related to gas turbine combustors such as design requirements, combustion chemistry, alternative fuels, and challenges with variable load conditions.
3) Finally, it discusses the speaker's current role at Solar Turbines and provides technical details about gas turbine cycles, components, and performance parameters.
This document provides a training report from an internship at Rajghat Power House. It includes an acknowledgements section thanking those who supported the training. It also includes a preface describing how practical experience is important for engineering students to develop hands-on knowledge. The bulk of the document consists of sections on power plant basics, control and instrumentation, and conclusions from the learning experience. It aims to impart knowledge of fundamentals and applications gained during the industrial training placement.
The document provides an overview of the gas turbine engines market, including aviation gas turbines and industrial gas turbines. It states that the aviation gas turbine engines market was worth $64 billion in 2015 and is projected to reach $82 billion by 2020, growing at a CAGR of 4.13%. The main segments are turbofan engines, turboprop engines, turboshaft engines, and auxiliary power units. The key drivers are the re-equipment of modern aviation and increasing demand for commercial aircraft. The largest players are Rolls-Royce, Pratt & Whitney, GE Aviation, and CFM International. The industrial gas turbines market was worth $34.8 billion in 2015 and is projected to reach $37.7
A gas turbine, also called a combustion turbine, is a type of internal combustion engine. It has an upstream rotating compressor coupled toa downstream turbine, and a combustion chamber in-between. Energy is added to the gas stream in the combustor, where fuel is mixed with air and ignited. In the high-pressure environment of the combustor, combustion of the fuel increases the temperature. The products of the combustion are forced into the turbine section
Visit https://www.topicsforseminar.com to Download
GE ADGT Application CHP-Cogen-CC
GE코리아 뉴스레터를 구독하세요! http://goo.gl/IE8WS8
GE코리아 YouTube 채널을 구독하세요! http://goo.gl/M2gc8m
상상을 현실로 만듭니다. Imagination at work.
GE가 꿈꾸는 가치입니다. 아니, GE는 단지 꿈만 꾸고 있는 것이 아닙니다. 상상을 현실로 만들기 위해, 불가능했던 것을 가능하게 만들기 위해 쉬지 않고 움직이고 있습니다. GE는 에너지, 의료, 항공, 수송, 금융 등의 여러 분야에서 고객과 인류사회의 진보를 위해 더 편리하고 빠르며 친환경적인 솔루션을 찾아냅니다.
Connect with GE Online:
GE코리아 웹사이트: http://www.ge.com/kr/
GE리포트코리아: http://www.gereports.kr/
GE코리아 페이스북 페이지: hhttps://www.facebook.com/GEKorea
GE코리아 슬라이드쉐어: http://www.slideshare.net/GEKorea
This report reviews current turbofan engine noise and engine noise reduction technology, specifically focusing on the engine technology of larger passenger jetliners which have entered into service within the last ten (10) years.
Important factors in turbofan engine design from a community noise perspective and the sources of noise along with their relative importance are also presented. A review of different engine noise reduction technologies is presented, as well as an estimate of the technology’s readiness level.
Finally, potential trade-offs, challenges, and future technology directions are outlined.
Gas Turbine , CCPP, Operation& Maintenance, spare part supply, Manpower service for Power Plant, GE LM6000 ,GE LM2500, GE FRAME 6,... P&W, MAN, RR, Turbine commisioning and start up,......
Jet engines produce thrust by channeling the explosion of fuel combustion rearward using a gas turbine. They operate based on Newton's third law, which states that for every action force there is an equal and opposite reaction force. The key parts of a jet engine are the fan, compressor, combustor, turbine, mixer, and nozzle. Air is sucked into the compressor and increases in pressure and temperature before being mixed with fuel and ignited in the combustor. The expanding hot gases power the turbine, which drives the compressor. The gases then exit through the nozzle at high speed, producing thrust that propels the aircraft forward. Jet engines provide advantages of high speed and power-to-weight ratio but have disadvantages of high fuel consumption
A gas turbine works by compressing air, mixing it with fuel and igniting it to produce hot exhaust gases that drive the turbine and generate power. It has an upstream compressor coupled to a downstream turbine with a combustion chamber in between. Gas turbines operate on the Brayton cycle and may be open or closed systems. They are used in power plants, vehicles, and other applications due to their high power-to-weight ratio and ability to operate on different fuels.
This document summarizes an innovative internal combustion engine concept for UAV applications. The engine uses stratified charge combustion with rich and lean zones to improve efficiency. It also incorporates a turbo compound configuration with multiple expansion stages to recover exhaust energy. Initial CFD analysis shows the stratified combustion and scavenging processes work as intended. The concept could enable high efficiency engines across a wide range of sizes, from 100 HP automotive engines to 7000 HP engines for UAVs.
Gas turbines operate by compressing air, adding fuel and igniting it to generate high-temperature gas, and expanding this gas through a turbine to power the compressor and provide output shaft work. There are various types including turbojets used in aircraft, turboprops which drive propellers via reduction gears, and turbofans which have a large fan at the front and achieve higher efficiency. Ramjets have no moving parts and rely solely on forward speed for compression, making them unable to produce static thrust.
Final Year Project report (Jet Engine)Pramod Pawar
The document describes a student project to design and construct a jet engine using an automotive turbocharger. The project involves modeling and analyzing engine components using software, and fabricating the engine. The project is divided into two sections - design of the jet engine, and construction of the jet engine. In the design section, the document outlines the approach, provides block diagrams of the engine systems, and describes the design of key components like the combustion chamber. The construction section will cover building the engine components and assembling the full engine. The goal is to build a working scaled model of a jet engine that can operate independently without external power.
Alstom provides gas power plant solutions that are reliable, versatile, and environmentally friendly. They have over 70 years of experience in designing, constructing, and commissioning gas power plants around the world. Their gas power plant experts are committed to meeting customer needs for retrofitting existing plants or designing new plants from the ground up.
Gas Turbine Theory - Principle of Operation and ConstructionSahyog Shishodia
This presentation tells all about basic principle behind Gas Turbine, their working, operation and construction. How they came into existence and where are they used.
Jet propulsion works by discharging a fluid to generate thrust in the opposite direction of the jet. There are two types of jet engines: air-breathing and non-air breathing. Air-breathing engines like turbojets, turbofans, ramjets, and pulsejets use atmospheric air, while non-air breathing rocket engines contain their own oxidizer and fuel. Rocket engines provide thrust through momentum change and pressure difference of the exhaust gases. They are self-contained and can operate in a vacuum but require a large amount of propellant.
Gas turbine plants use compressed air and combustion to drive a turbine and generate power. They have high efficiency, quick start-up times, and can use different fuels. The key components are an air compressor, combustor, and turbine connected by a common shaft. Air is compressed then mixed with fuel and ignited in the combustor. The hot gases drive the turbine which powers the compressor and generator. Axial compressors are commonly used due to their ability to deliver large air volumes at moderate pressures.
This document contains questions about various mechanical engineering topics including: internal combustion engines and their components; differences between two-stroke and four-stroke engines; thermal power plants and their working; differences between impulse and reaction turbines; rolling mills; air compressors; refrigeration systems; AC and DC power supplies for welding; friction clutches; couplings; centrifugal and reciprocating pumps; casting; heat transfer; Bernoulli's theorem; venturimeter; pitot tube; welding; and turning.
This document provides an overview of gas turbine engines. It discusses the history of gas turbine engines, including early developments in England, Germany, and the United States. It then describes the basic process of how gas turbine engines work, including the compressor, combustion chamber, and turbine. Finally, it discusses the different types of gas turbine engines, such as centrifugal flow, axial flow, and centrifugal-axial flow engines.
The document discusses combined cycle power plants (CCPP) which use natural gas more efficiently than other power generation technologies by consuming one-third less natural gas per kW.h of electricity generated. CCPPs allow countries like France to reduce CO2 emissions while modernizing their electricity production. However, natural gas has disadvantages such as limited supply that must be considered along with the higher costs of transport and treatment compared to other fuels.
This document provides an introduction to gas turbine engines. It discusses the working principle of jet propulsion based on Newton's third law of motion. It describes the basic components and functions of a gas turbine propulsion system, including compressing air, mixing and igniting fuel, and accelerating the gases to produce thrust. It also discusses different types of gas turbine engines such as turbojets, turbofans, turboprops, and ramjets as well as their applications in aircraft, marine, industrial, and launch vehicles.
This document summarizes a marine propulsion conference held in 2011 in Japan. It discusses Japan's national initiative to reduce ship emissions through 22 research projects funded by the Ministry of Land, Infrastructure, Transport and Tourism. The projects involve developing technologies to reduce CO2 emissions from ships by 30% compared to existing ships. Some highlighted projects include micro-bubble lubrication systems to reduce hull friction, low resistance coatings, improvements to propulsive efficiency, waste heat recovery systems, hybrid turbochargers, renewable energy technologies like solar and wind, and large capacity batteries. The conference provided details on these various emission reduction technologies and efforts.
The gas turbine is an internal combustion engine that uses air as the working fluid. The engine extracts chemical energy from fuel and converts it to mechanical energy using the gaseous energy of the working fluid (air) to drive the engine and propeller, which, in turn, propel the airplane.
The document provides an overview and goals for analyzing different types of gas turbine engines including turbojet, turbofan, and ramjet engines. It outlines the planned analysis of individual engine components including inlets, combustors, compressors, turbines, and control volume analysis. The analysis will use thermodynamic cycles and definitions of efficiency to evaluate performance parameters like propulsion efficiency, thermal efficiency, and thrust specific fuel consumption. Both ideal and non-ideal analyses are discussed for ramjet and turbojet engines.
This document discusses various basic terminology related to engine power, including:
- Spark ignition and compression ignition engines
- Definitions of bore, stroke, swept volume, clearance volume, and piston displacement
- Explanations of compression ratio, volumetric efficiency, and horsepower
- Descriptions of indicated horsepower, brake horsepower, SAE horsepower, belt horsepower, PTO horsepower, drawbar horsepower, maximum horsepower, and net horsepower
- Discussions of mean effective pressure, torque, and methods of measuring horsepower
1. Gas turbine power plants work by compressing air which is then mixed with fuel and ignited, producing hot exhaust gases that spin a turbine to generate electricity. They have advantages over steam plants like lower costs and less water use.
2. Key factors in selecting a gas turbine plant site include proximity to load centers to minimize transmission costs, available cheap land, accessible fuel sources, transportation access, and distance from populated areas due to noise.
3. Gas turbines compress air, combust fuel in it, and harness the expanding hot gases to drive a turbine coupled to a generator. While more efficient than earlier designs, over half the power produced is still used to drive the compressor.
The document describes a pistonless pump designed by NASA to pump rocket fuel. Some key points:
- The pump has fewer rotating parts than piston or turbo pumps, resulting in less friction and higher efficiency.
- It is lighter weight and easier to install in a rocket than turbo pumps.
- NASA testing found the pistonless pump works conveniently and is 80-90% more economical than other pump types.
Multi-Frequential Harmonic Balance Approach for the Simulation of Contra-Rotating Open Rotors: Application to Aeroelasticity
April 14, 2014 at CERFACS (Toulouse, France)
JURY:
P. FERRAND (President), LMFA, (Lyon, France)
C. CORRE (Referee), ENSE3, (Grenoble, France)
L. HE (Referee), University of Oxford, (Oxford, United-Kingdom)
J-C. CHASSAING (Member), UPMC, (Paris, France)
P. CINNELLA (Member), Università del Salento, (Lecce, Italy)
F. SICOT (Member), CERFACS, (Toulouse, France)
C. DEJEU (Invited), Snecma (Safran), (Villaroche, France)
ABSTRACT: Computational Fluid Dynamics (CFD) has allowed the optimization of many configurations among which aircraft engines. In the aeronautical industry, CFD is mostly restricted to steady approaches
due to the high computational cost of unsteady simulations. Nevertheless, the flow field across the rotating parts of aircraft engines, namely turbomachinery blades, is essentially periodic in time. Years ago, Fourier- based time methods have been developed to take advantage of this time periodicity. However, they are, for the most part, restricted to mono-frequential flow fields. This means that only a single base-frequency and its harmonics can be considered. Recently, a multi-frequential Fourier-based time method, namely the multi-frequential Harmonic Balance (HB), has been developed and implemented into the elsA CFD code, enabling new kinds of applications as, for instance, the aeroelasticity of multi-stage turbomachinery.
The present PhD thesis aims at applying the HB approach to the aeroelasticity of a new type of aircraft engine: the contra-rotating open rotor. The method is first validated on analytical, linear and non-linear numerical test problems. Two issues are raised, which prevent the use of such an approach on arbitrary aeroelastic configurations: the conditioning of the multi-frequential HB source term and the convergence of the method. Original methodologies are developed to improve the condition number of the simulations and to provide a priori estimates of the number of harmonics required to achieve a given convergence level. The HB method is then validated on a standard configuration for turbomachinery aeroelasticity. The results are shown to be in fair agreement with the experimental data. The applicability of the method is finally demonstrated for aeroelastic simulations of contra-rotating open rotors.
ESOS Transportation energy consumption-eco3 partnership brochureEco3 Partnership
Energy and Strategic Cost Management Solutions
ESOS Energy-Strategic Cost Management
The Eco3Partnership focuses on providing advice and guidance on the design and implementation of sustainable business solutions in the energy efficiency and renewables sector.
Our innovative solutions are designed to identify practical and cost efficient ways of reducing energy consumption and carbon emissions.
We can help deliver clear insight into energy consumption across your business, driving increased efficiency and reduced costs by providing a unique managed service and helping you implement our eco3 Smart Cloud Software that allows you to measure, manage and monitor your energy and carbon effectively.
These solutions reduce business operational costs whilst ensuring compliance with new legislation. We also provide guidance on energy procurement, low energy lighting and controls and combined heat and power initiatives.
Where required we can assist with the preparation of carbon management and carbon reduction programmes.
Jet engines produce thrust by channeling the explosion of fuel combustion rearward using a gas turbine. They operate based on Newton's third law, which states that for every action force there is an equal and opposite reaction force. The key parts of a jet engine are the fan, compressor, combustor, turbine, mixer, and nozzle. Air is sucked into the compressor and increases in pressure and temperature before being mixed with fuel and ignited in the combustor. The expanding hot gases power the turbine, which drives the compressor. The gases then exit through the nozzle at high speed, producing thrust that propels the aircraft forward. Jet engines provide advantages of high speed and power-to-weight ratio but have disadvantages of high fuel consumption
A gas turbine works by compressing air, mixing it with fuel and igniting it to produce hot exhaust gases that drive the turbine and generate power. It has an upstream compressor coupled to a downstream turbine with a combustion chamber in between. Gas turbines operate on the Brayton cycle and may be open or closed systems. They are used in power plants, vehicles, and other applications due to their high power-to-weight ratio and ability to operate on different fuels.
This document summarizes an innovative internal combustion engine concept for UAV applications. The engine uses stratified charge combustion with rich and lean zones to improve efficiency. It also incorporates a turbo compound configuration with multiple expansion stages to recover exhaust energy. Initial CFD analysis shows the stratified combustion and scavenging processes work as intended. The concept could enable high efficiency engines across a wide range of sizes, from 100 HP automotive engines to 7000 HP engines for UAVs.
Gas turbines operate by compressing air, adding fuel and igniting it to generate high-temperature gas, and expanding this gas through a turbine to power the compressor and provide output shaft work. There are various types including turbojets used in aircraft, turboprops which drive propellers via reduction gears, and turbofans which have a large fan at the front and achieve higher efficiency. Ramjets have no moving parts and rely solely on forward speed for compression, making them unable to produce static thrust.
Final Year Project report (Jet Engine)Pramod Pawar
The document describes a student project to design and construct a jet engine using an automotive turbocharger. The project involves modeling and analyzing engine components using software, and fabricating the engine. The project is divided into two sections - design of the jet engine, and construction of the jet engine. In the design section, the document outlines the approach, provides block diagrams of the engine systems, and describes the design of key components like the combustion chamber. The construction section will cover building the engine components and assembling the full engine. The goal is to build a working scaled model of a jet engine that can operate independently without external power.
Alstom provides gas power plant solutions that are reliable, versatile, and environmentally friendly. They have over 70 years of experience in designing, constructing, and commissioning gas power plants around the world. Their gas power plant experts are committed to meeting customer needs for retrofitting existing plants or designing new plants from the ground up.
Gas Turbine Theory - Principle of Operation and ConstructionSahyog Shishodia
This presentation tells all about basic principle behind Gas Turbine, their working, operation and construction. How they came into existence and where are they used.
Jet propulsion works by discharging a fluid to generate thrust in the opposite direction of the jet. There are two types of jet engines: air-breathing and non-air breathing. Air-breathing engines like turbojets, turbofans, ramjets, and pulsejets use atmospheric air, while non-air breathing rocket engines contain their own oxidizer and fuel. Rocket engines provide thrust through momentum change and pressure difference of the exhaust gases. They are self-contained and can operate in a vacuum but require a large amount of propellant.
Gas turbine plants use compressed air and combustion to drive a turbine and generate power. They have high efficiency, quick start-up times, and can use different fuels. The key components are an air compressor, combustor, and turbine connected by a common shaft. Air is compressed then mixed with fuel and ignited in the combustor. The hot gases drive the turbine which powers the compressor and generator. Axial compressors are commonly used due to their ability to deliver large air volumes at moderate pressures.
This document contains questions about various mechanical engineering topics including: internal combustion engines and their components; differences between two-stroke and four-stroke engines; thermal power plants and their working; differences between impulse and reaction turbines; rolling mills; air compressors; refrigeration systems; AC and DC power supplies for welding; friction clutches; couplings; centrifugal and reciprocating pumps; casting; heat transfer; Bernoulli's theorem; venturimeter; pitot tube; welding; and turning.
This document provides an overview of gas turbine engines. It discusses the history of gas turbine engines, including early developments in England, Germany, and the United States. It then describes the basic process of how gas turbine engines work, including the compressor, combustion chamber, and turbine. Finally, it discusses the different types of gas turbine engines, such as centrifugal flow, axial flow, and centrifugal-axial flow engines.
The document discusses combined cycle power plants (CCPP) which use natural gas more efficiently than other power generation technologies by consuming one-third less natural gas per kW.h of electricity generated. CCPPs allow countries like France to reduce CO2 emissions while modernizing their electricity production. However, natural gas has disadvantages such as limited supply that must be considered along with the higher costs of transport and treatment compared to other fuels.
This document provides an introduction to gas turbine engines. It discusses the working principle of jet propulsion based on Newton's third law of motion. It describes the basic components and functions of a gas turbine propulsion system, including compressing air, mixing and igniting fuel, and accelerating the gases to produce thrust. It also discusses different types of gas turbine engines such as turbojets, turbofans, turboprops, and ramjets as well as their applications in aircraft, marine, industrial, and launch vehicles.
This document summarizes a marine propulsion conference held in 2011 in Japan. It discusses Japan's national initiative to reduce ship emissions through 22 research projects funded by the Ministry of Land, Infrastructure, Transport and Tourism. The projects involve developing technologies to reduce CO2 emissions from ships by 30% compared to existing ships. Some highlighted projects include micro-bubble lubrication systems to reduce hull friction, low resistance coatings, improvements to propulsive efficiency, waste heat recovery systems, hybrid turbochargers, renewable energy technologies like solar and wind, and large capacity batteries. The conference provided details on these various emission reduction technologies and efforts.
The gas turbine is an internal combustion engine that uses air as the working fluid. The engine extracts chemical energy from fuel and converts it to mechanical energy using the gaseous energy of the working fluid (air) to drive the engine and propeller, which, in turn, propel the airplane.
The document provides an overview and goals for analyzing different types of gas turbine engines including turbojet, turbofan, and ramjet engines. It outlines the planned analysis of individual engine components including inlets, combustors, compressors, turbines, and control volume analysis. The analysis will use thermodynamic cycles and definitions of efficiency to evaluate performance parameters like propulsion efficiency, thermal efficiency, and thrust specific fuel consumption. Both ideal and non-ideal analyses are discussed for ramjet and turbojet engines.
This document discusses various basic terminology related to engine power, including:
- Spark ignition and compression ignition engines
- Definitions of bore, stroke, swept volume, clearance volume, and piston displacement
- Explanations of compression ratio, volumetric efficiency, and horsepower
- Descriptions of indicated horsepower, brake horsepower, SAE horsepower, belt horsepower, PTO horsepower, drawbar horsepower, maximum horsepower, and net horsepower
- Discussions of mean effective pressure, torque, and methods of measuring horsepower
1. Gas turbine power plants work by compressing air which is then mixed with fuel and ignited, producing hot exhaust gases that spin a turbine to generate electricity. They have advantages over steam plants like lower costs and less water use.
2. Key factors in selecting a gas turbine plant site include proximity to load centers to minimize transmission costs, available cheap land, accessible fuel sources, transportation access, and distance from populated areas due to noise.
3. Gas turbines compress air, combust fuel in it, and harness the expanding hot gases to drive a turbine coupled to a generator. While more efficient than earlier designs, over half the power produced is still used to drive the compressor.
The document describes a pistonless pump designed by NASA to pump rocket fuel. Some key points:
- The pump has fewer rotating parts than piston or turbo pumps, resulting in less friction and higher efficiency.
- It is lighter weight and easier to install in a rocket than turbo pumps.
- NASA testing found the pistonless pump works conveniently and is 80-90% more economical than other pump types.
Multi-Frequential Harmonic Balance Approach for the Simulation of Contra-Rotating Open Rotors: Application to Aeroelasticity
April 14, 2014 at CERFACS (Toulouse, France)
JURY:
P. FERRAND (President), LMFA, (Lyon, France)
C. CORRE (Referee), ENSE3, (Grenoble, France)
L. HE (Referee), University of Oxford, (Oxford, United-Kingdom)
J-C. CHASSAING (Member), UPMC, (Paris, France)
P. CINNELLA (Member), Università del Salento, (Lecce, Italy)
F. SICOT (Member), CERFACS, (Toulouse, France)
C. DEJEU (Invited), Snecma (Safran), (Villaroche, France)
ABSTRACT: Computational Fluid Dynamics (CFD) has allowed the optimization of many configurations among which aircraft engines. In the aeronautical industry, CFD is mostly restricted to steady approaches
due to the high computational cost of unsteady simulations. Nevertheless, the flow field across the rotating parts of aircraft engines, namely turbomachinery blades, is essentially periodic in time. Years ago, Fourier- based time methods have been developed to take advantage of this time periodicity. However, they are, for the most part, restricted to mono-frequential flow fields. This means that only a single base-frequency and its harmonics can be considered. Recently, a multi-frequential Fourier-based time method, namely the multi-frequential Harmonic Balance (HB), has been developed and implemented into the elsA CFD code, enabling new kinds of applications as, for instance, the aeroelasticity of multi-stage turbomachinery.
The present PhD thesis aims at applying the HB approach to the aeroelasticity of a new type of aircraft engine: the contra-rotating open rotor. The method is first validated on analytical, linear and non-linear numerical test problems. Two issues are raised, which prevent the use of such an approach on arbitrary aeroelastic configurations: the conditioning of the multi-frequential HB source term and the convergence of the method. Original methodologies are developed to improve the condition number of the simulations and to provide a priori estimates of the number of harmonics required to achieve a given convergence level. The HB method is then validated on a standard configuration for turbomachinery aeroelasticity. The results are shown to be in fair agreement with the experimental data. The applicability of the method is finally demonstrated for aeroelastic simulations of contra-rotating open rotors.
ESOS Transportation energy consumption-eco3 partnership brochureEco3 Partnership
Energy and Strategic Cost Management Solutions
ESOS Energy-Strategic Cost Management
The Eco3Partnership focuses on providing advice and guidance on the design and implementation of sustainable business solutions in the energy efficiency and renewables sector.
Our innovative solutions are designed to identify practical and cost efficient ways of reducing energy consumption and carbon emissions.
We can help deliver clear insight into energy consumption across your business, driving increased efficiency and reduced costs by providing a unique managed service and helping you implement our eco3 Smart Cloud Software that allows you to measure, manage and monitor your energy and carbon effectively.
These solutions reduce business operational costs whilst ensuring compliance with new legislation. We also provide guidance on energy procurement, low energy lighting and controls and combined heat and power initiatives.
Where required we can assist with the preparation of carbon management and carbon reduction programmes.
This so called PPT for propulsion study for Shenyang Aerospace University. This PPT right protected by Dr. divinder K. Yadav. Its using in SAU by Lale. For all students of Aeronautical Engineering must memorize each & every words from this PPT. If you miss a single words you must fail in the Exam. Remember there is no chance to be creative or use sense you just need to use the power of memorizing.
Toward a sustainable transportation network in the northeast 20160428 v2rwilliams9999
The nation needs to modernize its transportation system to enhance the mobility of all citizens and enable more efficient goods movement while transforming into a clean, sustainable sector of a vibrant economy. What strategies can be used by to achieve that goal? How are federal programs changing and engaging state, regional and local government agencies, and the private sector? This presentation discusses these issues.
All natural energy on Earth comes from solar radiation, heat from the Earth's mantle, and gravity. Fossil fuels like coal, oil, and natural gas are limited, non-renewable sources that have formed from ancient organic matter over millions of years. Energy can also be generated renewably from solar, wind, hydroelectric, geothermal, and biomass sources. Nuclear fission of uranium and thorium isotopes in the Earth's crust is another non-renewable source of energy. Hydrogen may become a sustainable energy source in the future.
The document discusses various energy conservation measures that can be implemented in hotels to reduce energy costs and improve profitability. Some key measures mentioned include installing energy efficient machines, implementing auto controls and timers for HVAC and lighting systems, improving insulation and installing efficient windows, replacing incandescent bulbs with CFLs and LEDs, using occupancy sensors and natural light where possible, and educating guests and staff to turn off lights in unoccupied rooms. Taking these measures can help cut a hotel's energy costs by 10-15% and improve the bottom line.
A power station or power plant generates electric power by converting other forms of energy into electrical energy. The most common types are thermal power plants, which burn fossil fuels to power steam turbines, and nuclear power plants, which use nuclear reactions to power steam turbines. Power plants are also classified by their prime mover, such as steam turbines, gas turbines, or hydroelectric turbines. When an imbalance occurs between power generation and load, it can cause power outages or failures across an electrical grid. Utilities take measures to protect against outages and restore power through monitoring, analytics of power usage and generation, and preventative maintenance of infrastructure.
A jet engine is a reaction engine discharging a fast-moving jet that generates thrust by jet propulsion. These slides will help out to understand the phenomenon of jet engines. their working and structure.
An overview of Energy & utilities industry. In the future, civilization will be forced to research and develop alternative energy sources. Our current rate of fossil fuel usage will lead to an energy crisis this century. In order to survive the energy crisis, many companies in the energy industry are inventing new ways to extract energy from renewable sources. While the rate of development is slow, mainstream awareness and government pressures are growing.
The deck talks about the needs of energy awareness and consumer education about the terminologies and technologies within the industry value chain so, energy can be consumed efficiently and smartly.
Abu Dhabi has a rich seafaring heritage that is still reflected in its culture today. One example is the symbolism of geometric round shapes, which pay homage to the circular designs seen on traditional dhow boats that were historically used for trade and travel across the sea.
This document provides an overview of jet engines, including their history, key parts, types, and comparisons to other propulsion systems. It discusses the main developers of the first jet engine in the early 1900s. The main types of jet engines are then outlined, including ramjet, turbojet, turbofan, turboprop, and turboshaft. Advantages of jet engines over internal combustion engines are higher mechanical efficiency and better weight to power ratios, while disadvantages include lower thermal efficiency and challenges with high temperature turbine blades. The document concludes with suggestions for future engine improvements and a vision of decreased aircraft weight enabling greater safety and flexibility.
The document discusses energy management system (EMS) development and implementation. It outlines the key components of an EMS, including establishing an energy policy, organizing responsibilities, planning initiatives, implementing programs, evaluating performance, and continually reviewing and improving the system. The goal is for organizations to systematically manage their energy use to reduce costs, increase efficiency, and meet regulatory requirements through a structured EMS.
This document summarizes several renewable energy sources: hydropower from falling water used for irrigation and machinery; solar power from the sun used for heating and generating electricity; bioenergy from biological material such as plant matter used directly or converted to biofuels; geothermal energy from the Earth's heat used for heating; and wind power from wind turbines converting kinetic energy to electricity or doing mechanical work.
The document defines renewable energy as energy from natural resources that can be reused sustainably without depleting the source. It lists several types of renewable energy resources: solar energy, wind power, hydropower, biomass, biofuels, and geothermal energy. For each type, it provides a brief definition and examples of technologies used to capture and convert the energy. It concludes by stating that renewable energy capacity, especially for solar and wind, grew significantly between 2004 and 2008.
Water jet cutting is a versatile and precise cutting process that uses a high-pressure stream of water, with or without an abrasive material, to cut materials. It can cut almost any material and produces no heat-affected zone. There are two main types - pure water jets which are used for softer materials, and abrasive water jets which use abrasives mixed with water to cut harder materials. The process involves forcing water or a water-abrasive mixture through a nozzle at extremely high pressure to cut materials. It has many advantages over other cutting methods like lasers or EDM such as being safer, faster, and producing less heat and burrs.
Energy is a property of objects that can be transferred or converted into different forms. There are two main types of energy: potential energy, which is the stored energy of position, and kinetic energy, which is the energy of motion. Mechanical energy is the sum of potential and kinetic energy and represents the energy from an object's motion and position. Energy can be transformed from one form to another, such as mechanical energy transforming to other forms like thermal, radiant, or electrical energy, which then become useful sources of energy for applications.
This document discusses energy management and ISO 50001, an international standard for energy management systems. It provides an overview of global energy trends showing increasing demand, the benefits organizations have realized from effective energy management in cost savings, and the key elements of an energy management system based on ISO 50001 including establishing baselines and goals, implementing action plans, monitoring performance, and continually improving the system. ISO 50001 provides a framework to help organizations systematically improve energy efficiency and reduce costs.
Sustainable transportation involves evaluating three components: vehicles, energy sources, and infrastructure to meet mobility needs while minimizing environmental and social impacts. A sustainable system allows basic access needs to be met safely and equitably, operates efficiently through diverse affordable modes, limits emissions within planetary boundaries, and integrates transportation and land use planning. Achieving sustainability requires considering a variety of objectives like affordable options, efficient use of resources, compact development, and comprehensive, inclusive planning across sectors.
Improved efficiency of gas turbine by Razin Sazzad MollaRazin Sazzad Molla
This document discusses ways to improve the efficiency of gas turbine engines through various design modifications and upgrades. It describes how increasing turbine inlet temperatures, improving compressor and turbine components, adding modifications like intercooling and regeneration, and utilizing advanced cooling techniques can boost efficiency. Other methods covered include inlet air cooling systems, compressor and turbine coatings, supercharging, and comprehensive component replacements. The goal of ongoing research is to enhance power output while reducing emissions and fuel consumption.
This document discusses gas turbine power generation. It begins by defining a gas turbine as a machine that extracts mechanical power from flowing gases. It then discusses the key components of a gas turbine - the compressor, combustion chamber, and turbine. The compressed air is heated in the combustion chamber before expanding through the turbine. The document provides diagrams of open and closed gas turbine cycles. It discusses applications of gas turbines such as aircraft engines and power generation. It also covers topics like emissions, efficiency, and the needs for future gas turbine development.
The document discusses methods for improving the efficiency of gas turbine engines. It describes the basic components and mechanism of gas turbines, including an air compressor, combustion chamber, and turbine. The document then reviews several specific techniques for boosting power output and heat rate, such as increasing inlet air density through cooling or boosting pressure. These efficiency upgrade options include ceramic coatings, inlet air cooling methods like fogging or refrigeration, and supercharging. While some upgrades are more expensive than others, the best option depends on the turbine's age, location, and operating cycle.
GAS TURBINES IN SIMPLE CYCLE & COMBINED CYCLE APPLICATIONSAbdelrhman Uossef
1. Gas turbines can operate in simple cycle mode, where the turbine directly drives a generator or compressor, or in combined cycle mode.
2. In simple cycle power generation, the gas turbine shaft is directly coupled to the generator to produce electricity.
3. Gas turbines used in simple cycle applications include models from Siemens, Alstom, Rolls Royce and General Electric ranging from 10-300 MW electrical output.
GAS TURBINES IN SIMPLE CYCLE & COMBINED CYCLE APPLICATIONSAbdelrhman Uossef
1. Gas turbines can operate in simple cycle mode, where the turbine directly drives a generator or compressor, or in combined cycle mode.
2. In simple cycle power generation, the gas turbine shaft is directly coupled to the generator to produce electricity.
3. Gas turbines used in simple cycle applications include models from Siemens, Alstom, Rolls Royce and General Electric ranging from 10-300 MW electrical output.
1. The document discusses gas turbines used in simple cycle applications and combined cycle applications for power generation. It provides examples of various gas turbine models from manufacturers like GE, Siemens, Rolls Royce, and describes their specifications and uses.
2. Gas turbines can be used for direct drive power generation or mechanical drive applications to power compressors, pumps, and other industrial equipment. Aeroderivative gas turbines adapted from aircraft engines are commonly used in offshore power generation due to their lighter weight.
3. The document outlines the basic components and operating principles of gas turbine systems. It also compares gas turbines to reciprocating engines and discusses factors like fuel type, electrical output, efficiency and emissions of different gas turbine models
This document presents information about a dual combustion engine. It was presented to Sir Qazi Shehzad by five students. The document defines a dual combustion engine as a four-stroke internal combustion engine where combustion occurs in two parts, first at constant pressure and then at constant volume. This makes it more efficient than a diesel engine. It also describes the key parts of the engine, the combustion cycle process, an equation for calculating its thermal efficiency, and its applications in vehicles, generators, and potentially future energy systems.
Rolls-Royce is a world leader in aero-engines and marine propulsion systems. The Trent engine family uses a three-shaft design that allows for higher pressure ratios and temperatures needed for long-haul flights. Material and design advances like single crystal alloys and ceramic composites have improved efficiency. Future concepts may use electric engines and contra-rotating fans to further reduce emissions and fuel consumption.
This document provides an overview of different types of power plants, with a focus on combined cycle power plants. It describes the basic components and operation of conventional steam plants, simple cycle peaking plants, and combined cycle plants. Combined cycle plants are the most efficient, using exhaust from gas turbines to power a steam turbine for additional electricity generation. They typically have overall efficiencies over 50% and heat rates under 7,700 BTU/kWh. The document also discusses the author's experience with a combined cycle plant project over 24 months that included installing gas turbines, ancillary equipment, and commissioning the system.
Use of Process Analyzers in Fossil Fuel PlantsIves Equipment
In spite of all efforts concerning energy savings and efficiency, the growing world population and the aspired higher 'standard of living' will lead to a further in- crease of world energy demand. In this context, almost half of the primary energy demand will continue to be covered by solid fuels, particularly by coal, until 2020 and many years beyond.
1. Gas turbine power plants use gas turbines to generate electricity and have advantages over steam plants like lower capital costs and reduced space requirements.
2. There are two main types - open cycle plants which exhaust combustion gases directly to the atmosphere, and closed cycle plants which recirculate working gases to improve efficiency.
3. Various methods can be used to recover waste heat from gas turbine exhaust to further improve efficiency, such as economizers, recuperators, regenerators, heat wheels, and heat pipes.
1. The document discusses gas turbine power plants, including their working principles, components, types (open vs closed cycle), and methods to improve efficiency like intercooling, reheating, and regeneration.
2. It also covers the ideal Brayton cycle that gas turbines undergo and compares the characteristics of open and closed cycle plants.
3. Combinations of gas turbines with steam and diesel power plants are described to further improve overall efficiency.
Gas Turbine Engine For Automotive ApplicationHASSAN ALESSA
This document summarizes the history and development of gas turbine engines for automotive applications. It discusses how gas turbines work, providing diagrams of key components like compressors and turbines. It also covers common gas turbine applications in vehicles, aircraft, power generation and more. The document then analyzes the thermodynamics and efficiencies of gas turbine engines compared to piston engines. It discusses Chrysler's experiments with gas turbine cars in the 1960s, including specifications of the engines. Finally, it outlines advantages and challenges of gas turbines for automotive use.
This document analyzes the cooling of an internal combustion (IC) engine using water cooling. It discusses key aspects of engine cooling systems including:
- IC engines reach high temperatures during combustion, so cooling is needed to avoid overheating. Water cooling and thermosyphon circulation are common cooling methods.
- Thermosyphon cooling works via natural convection as hot water rises and is replaced by cold water, circulating through the engine and radiator.
- Heat transfer equations are provided to calculate the quantity of water needed for cooling based on factors like surface area, temperature difference, and heat transfer coefficients.
- The performance of water-cooled engines is evaluated based on parameters like indicated power, mechanical
Various student project themes are proposed and being implemented in Centre for Advanced Studies in
Cryogenics related to Analysis/design/modeling/simulation/CFD/coding/computer program package/
prototyping/experimentation or its combinations (in collaboration and along with other departments of NIT
and reputed institutes/organizations in India and abroad) which benefits advanced research, technology,
scientific society and developing indigenous technologies and products.
1) The document discusses gas turbine engines, which are used to power commercial jets, helicopters, tanks, and power plants. They work by compressing air, mixing it with fuel, igniting it to create hot gases, and using those expanding gases to power turbines and produce thrust or rotation.
2) Engineering advancements in the early 1900s led to the development of gas turbines. They revolutionized airplane propulsion in the 1940s and have since been used for power generation and ships.
3) While powerful and compact, gas turbines are also expensive to design and manufacture due to their high operating temperatures and speeds. They consume more fuel when idling and prefer constant loads.
Similar to Energy and Transportation Systems: How might Technological Change be Creating New Opportunities in Them? (20)
The "Unproductive Bubble:" Unprofitable startups, small markets for new digit...Jeffrey Funk
This article will show that the current bubble has produced few profitable startups and involved few if any new digital technologies, nor technologies involving recent scientific advances, and thus it is unlikely that much that is productive will be left once the dust settles. There is a growth in old technologies such as e-commerce but little in new technologies such as AI. The startup losses are also much larger than in the past suggesting that fewer of today’s startups will still exist in a few years than those of 20 years ago.
Commercialization of Science: What has changed and what can be done to revit...Jeffrey Funk
This paper several changes that I believe may have reduced America’s ability to develop science-based technologies. I make no claims about the completeness. I begin with the growth of university research and then cover several changes it engendered, including an obsession with papers, hyper-specialization of researchers, and huge bureaucracies, also using the words of Nobel Laureates and other scientists to make my points.
2000, 2008, 2022: It is hard to avoid the parallels How Big Will the 2022 S...Jeffrey Funk
These slides summarize the recent share price declines for new startups, declines that are driven by huge annual and cumulative losses and it contrasts today's bubble with those of 2000 and 2008. It shows that today's bubble involves bigger startup losses than those of the 2000 bubble and that the markets of new technologies have not grown to the extent that those of past decades did. Many hedge funds, VCs, and pension funds are heavily invested in these startups. Some of them are also highly leveraged.
The Slow Growth of AI: The State of AI and Its ApplicationsJeffrey Funk
The failure of IBM Watson, disappointments of self-driving vehicles, slow diffusion of medical imaging, small markets for AI software, and scorching criticisms of Google’s research papers provide evidence for hype and disappointment in AI, which is consistent with negative social impact of Big Data and AI algorithms. There are some successes, but they are much smaller than the predictions, with virtual applications (advertising, news, retail sales, finance and e-commerce) having the largest success, building from previous Big Data usage in the past. Looking forward, AI will augment not replace workers just as past technologies did on farms, factories, and offices. Robotic process automation and natural language processing are likely to play important roles in this augmentation with RPA automating repetitive work, natural language processing summarizing information, and RPA also putting the information in the right bins for engineers, accountants, researchers, journalists, and lawyers. Big challenges include reductions in training time depending on faster computers, exponentially rising demands on computers for high accuracies in image recognition, a slowdown in supercomputer improvements, datasets riddled with errors, and reproducibility problems.
Behind the Slow Growth of AI: Failed Moonshots, Unprofitable Startups, Error...Jeffrey Funk
Smaller than expected markets, money-losing startups, failure of Watson, slow-diffusion of self-driving vehicles and medical imaging, and scorching criticisms of Google’s research papers are some of the examples used to characterize the hype of AI. There are some successes, but they are much smaller than the predictions, with advertising, news, and e-commerce having the biggest success stories. Looking forward, #AI will augment not replace workers just as past technologies did on farms, factories, and offices. Robotic process automation and natural language processing are likely to play important roles in this augmentation with #RPA automating repetitive work, natural language processing categorizing information, and RPA also putting the information in the right bins for engineers, accountants, researchers, journalists, and lawyers. The big challenges include exponentially rising demands on computers for high accuracies in images, a slowdown in supercomputer improvements, datasets riddled with errors, and reproducibility problems. See either this podcast or my slides, whose URL is shown in comments. #technolgy #innovation #venturecapital #ipo #artificialintelligence
The Troubled Future of Startups and Innovation: Webinar for London FuturistsJeffrey Funk
These slides show how the most successful startups of today (Unicorns) are not doing as well as the most successful of 20 to 50 years ago. Today's startups are doing worse in terms of time to profitability and time to top 100 market capitalization status. Only one Unicorn founded since 2000 has achieved top 100 market capitalization status while six, nine, and eight from the 70s, 80s, and 90s did so. It is also unlikely that few or any of today's Unicorns will achieve this status because their market capitalizations are too low, share prices increases since IPO are too small, and profits remain elusive. Only 14 of 45 had share price increases greater than the Nasdaq and only 6 of 45 had profits in 2019. The reasons for the worse performance of today's Unicorns than those of 20 to 50 years ago include no breakthrough technologies, hyper-growth strategies, and the targeting of regulated industries. The slides conclude with speculations on why few breakthrough technologies, including science-based technologies from universities are emerging. We need to think back to the division of labor that existed a half a century ago.
Where are the Next Googles and Amazons? They should be here by nowJeffrey Funk
Great startups aren’t being founded like they were in the 1970s (Microsoft, Apple, Oracle, Genentech, Home Depot, EMC), 1980s (Cisco, Dell, Adobe, Qualcomm, Amgen, Gilead Sciences), and 1990s (Amazon, Google, Netflix, Salesforce.com, PayPal). All of these startups reached the top 100 for market capitalization, but Facebook is the only startup founded since 2000 which has entered the top 100. Tesla and Uber are often discussed as highly successful but they have many times higher cumulative losses than did Amazon at its time of peak losses and neither has had a profitable year despite being older than Amazon was when it achieved profits. Furthermore, few of the recent Unicorn IPOs have experienced shareprice increases greater than those of the Nasdaq (14 of 45), only 3 of these 14 have profits, and only six of them have a
market capitalization over $30 (Zoom), $20 (Square), and $10 billion (Twilio, DocuSign, Okta). America’s venture capital system isn’t working as well as it once did, and the coronavirus will make things worse before the VC system gets better.
Start-up losses are mounting and innovation is slowing, but venture capitalists, entrepreneurs, consultants, university researchers, and business schools are hyping new technologies more than ever before. This hype is facilitated by changes in online media, including the rise of social media. This paper describes how the professional incentives of experts and the changes in online media have increased hype and how this hype makes it harder for policy makers, managers, scientists, engineers, professors, and students to understand new technologies and make good decisions. We need less hype and more level-headed economic analysis and this paper describes how this economic analysis can be done. Here is a link to the journal, Issues in Science & Technology: www.issues.org
Irrational Exuberance: A Tech Crash is ComingJeffrey Funk
These slides apply Nobel Laureate Robert Schiller's concept of irrational exuberance (and a book) title to the current speculative bubble of 2019. Over investments in startups and a lack of profitability in them are finally starting to catch up with the venture capital industry and the tech sector that relies on it. Investments by US venture capitalists have risen about six times since 2001 causing the total invested in 2018 to exceed by 40% the peak of 2000, the last big year of the dotcom bubble. But the number of IPOs has never returned to the peak years of 1993 to 2000; only about 250 were carried out between 2015 and 2017 vs. about 1,200 between 1995 and 1997.
The reason is simple: startups are taking longer to go public because they are not profitable. Consider the data. The median time to IPO has risen from 2.8 years in 1998 to 7.7 years in 2016 and the ones going public are less profitable than they were in the past. Although only 22% of startups going public in 1980 were unprofitable, 82% were unprofitable in 2018. The same high percentages of unprofitability have only been achieved twice before, in 1998 and 1999 right before the dotcom bubble burst. Furthermore, startups that have recently done high profile IPOs such as Snap, Dropbox, Blue Apron, Fitbit, Trivago, Box, and Cloudera are still not profitable.
Ride Sharing, Congestion, and the Need for Real SharingJeffrey Funk
Current ride sharing services are not financially sustainable. Although they provide more convenience than do taxi services, they are experiencing massive losses because they have the same cost structure as do taxis and thus must compete through subsidies and lower wages. After all, they use the same vehicles, roads, and drivers, and only GPS algorithms and phones are new.
They also increase congestion. Just as more private vehicles or taxis on the road will increase congestion, more ride sharing vehicles also increase congestion.
These slides describe new ways to use the technologies of ride sharing to reduce congestion along with costs while at the same time keeping travel time low. This can be done through changing public transportation systems or allowing private companies to offer competing services. For instance, current bus services, whether they are private or public, need to use the algorithms, GPS, phones and other technologies of ride sharing to revise routes, schedules and the premises that currently underpin public transportation. There is no reason a bus should be certain size, stop every 200 meters, or follow the same route all day. Algorithms and phones enable new types of routes in which designers simultaneously minimize time travel and maximize number of passengers transported per vehicle.hour.
Using the percent of top managers in IPOs (initial public offering) as a proxy for an industry’s/technology’s scientific intensity, this paper shows that the percentage of IPOs and of venture capital financing for science-based technologies has been declining for decades. Second, the percentage of PhDs among the top managers in science intensive industries is also declining, suggesting that their scientific intensities are falling. Third, the age of these top managers rose during the same period suggesting that the importance of experiential knowledge has increased even as the importance of PhDs and thus educational knowledge has decreased. Fourth, the numbers of IPOs and of venture capital funding are not increasing for newer science-based industries such as superconductors, solar cells, nanotechnology, and GMOs. Fifth, there are extreme diseconomies of scale in the universities that produce the PhD-holding top managers, suggesting that universities are far less effective at doing research than are companies. These results provide a new understanding of science and technology, and they offer new prescriptions for reversing slowing productivity growth.
This paper addresses the types of knowledge that are needed in entrepreneurial firms using a unique data base of executives and directors for all IPOs filed between 1990 and 2010. Using highest educational degrees as a proxy for educational knowledge, it shows that 85% of those with PhDs are concentrated in the life sciences and ICT (information and communication technology) industries and second, that those in the ICT industries are concentrated at lower layers in a “digital stack” of industries, ranging from semiconductors and other electronics at the bottom layer to computing and Internet infrastructure at the middle layer and Internet content, commerce, and services in the top layer. Third, industries with fewer PhDs have more bachelor’s and MBA degrees suggesting that PhDs are being replaced by them and not M.S. degrees. Fourth, age is higher for industries with the most PhDs thus suggesting a greater need for experiential knowledge in industries with greater needs for educational knowledge. Fifth, the number of Nobel Prizes tracks industries with high fractions of PhDs.
beyond patents:scholars of innovation use patenting as an indicator of innova...Jeffrey Funk
This paper discusses the problems with using patents as a measure of innovation and papers as a measure of science. It also uses data to show the problems. for example, the number of patent applications and awards have grown by six times since 1984 while productivity growth has slowed.
LED lighting has improved dramatically due to two mechanisms: creating new materials that better exploit electroluminescence, and geometrical scaling. New semiconductor materials like GaInN emit different colors with higher efficiency. Larger wafer sizes and production equipment lower costs. LED efficiency has increased from 0.0001 to over 100 lumens per watt, costs have plummeted, and the Department of Energy projects further increases. Both smaller LED sizes and larger scales drive these ongoing improvements.
These slides discuss how to put context back into learning. Farm and other work at home once provided a context for learning, but this context has become much weaker as work at home as mostly disappeared Students once learned mostly from parents because they worked on farms, fixed things at home, and prepared meals. These activities provided a "context" for school learning, a context that has been mostly lost. These slides discuss how this context can be put back into learning and the implications for the types of people best suited for teaching and the way to train them.
Technology Change, Creative Destruction, and Economic FeasibiltyJeffrey Funk
After showing that the costs of most electronic products are from electronic components, these slides show how the iPhone and iPad became economically feasible through improvements in microprocessors, flash memory, and displays.
These slides show that the demand for most professions is growing steadily in spite of continued improvements in productivity enhancing tools for them. They also show that AI will have a largely incremental effect on the professions, in combination with Moore's Law, cloud computing, and Big Data. They do this accounting, legal, architects, journalists, and engineers.
Solow's Computer Paradox and the Impact of AIJeffrey Funk
These slides show why IT has not delivered large improvements in productivity and why new forms of IT like AI will also not deliver large improvements, except in selected sectors. The main reason is that the improvements in AI are over-hyped and because most sectors do not have large inefficiencies in the organization of people, machinery, and materials.
What does innovation today tell us about tomorrow?Jeffrey Funk
1) The document discusses two processes of technological innovation - the science-based process and the Silicon Valley process.
2) Analysis of successful startups found that few cited scientific papers in their patents, indicating few innovations arose from the science-based process.
3) Predicted breakthrough technologies from MIT's Technology Review also showed that most science-based predictions led to small market sizes, while technologies not predicted became very large markets.
Creative destrution, Economic Feasibility, and Creative Destruction: The Case...Jeffrey Funk
This paper shows how new forms of electronic products and services such as smart phones, tablet computers and ride sharing become economically feasible and thus candidates for commercialization and creative destruction as improvements in standard electronic components such as microprocessors, memory, and displays occur. Unlike the predominant viewpoint in which commercialization is reached as advances in science facilitate design changes that enable improvements in performance and cost, most new forms of electronic products and services are not invented in a scientific sense and the cost and performance of them are primarily driven by improvements in standard components. They become candidates for commercialization as the cost and performance of standard components reach the levels necessary for the final products and services to have the required levels of performance and cost. This suggests that when managers, policy makers, engineers, and entrepreneurs consider the choice and timing of commercializing new electronic products and services, they should understand the composition of new technologies, the impact of components on a technology's cost, performance and design, and the rates of improvement in the components.
Part 2 Deep Dive: Navigating the 2024 Slowdownjeffkluth1
Introduction
The global retail industry has weathered numerous storms, with the financial crisis of 2008 serving as a poignant reminder of the sector's resilience and adaptability. However, as we navigate the complex landscape of 2024, retailers face a unique set of challenges that demand innovative strategies and a fundamental shift in mindset. This white paper contrasts the impact of the 2008 recession on the retail sector with the current headwinds retailers are grappling with, while offering a comprehensive roadmap for success in this new paradigm.
The Genesis of BriansClub.cm Famous Dark WEb PlatformSabaaSudozai
BriansClub.cm, a famous platform on the dark web, has become one of the most infamous carding marketplaces, specializing in the sale of stolen credit card data.
[To download this presentation, visit:
https://www.oeconsulting.com.sg/training-presentations]
This PowerPoint compilation offers a comprehensive overview of 20 leading innovation management frameworks and methodologies, selected for their broad applicability across various industries and organizational contexts. These frameworks are valuable resources for a wide range of users, including business professionals, educators, and consultants.
Each framework is presented with visually engaging diagrams and templates, ensuring the content is both informative and appealing. While this compilation is thorough, please note that the slides are intended as supplementary resources and may not be sufficient for standalone instructional purposes.
This compilation is ideal for anyone looking to enhance their understanding of innovation management and drive meaningful change within their organization. Whether you aim to improve product development processes, enhance customer experiences, or drive digital transformation, these frameworks offer valuable insights and tools to help you achieve your goals.
INCLUDED FRAMEWORKS/MODELS:
1. Stanford’s Design Thinking
2. IDEO’s Human-Centered Design
3. Strategyzer’s Business Model Innovation
4. Lean Startup Methodology
5. Agile Innovation Framework
6. Doblin’s Ten Types of Innovation
7. McKinsey’s Three Horizons of Growth
8. Customer Journey Map
9. Christensen’s Disruptive Innovation Theory
10. Blue Ocean Strategy
11. Strategyn’s Jobs-To-Be-Done (JTBD) Framework with Job Map
12. Design Sprint Framework
13. The Double Diamond
14. Lean Six Sigma DMAIC
15. TRIZ Problem-Solving Framework
16. Edward de Bono’s Six Thinking Hats
17. Stage-Gate Model
18. Toyota’s Six Steps of Kaizen
19. Microsoft’s Digital Transformation Framework
20. Design for Six Sigma (DFSS)
To download this presentation, visit:
https://www.oeconsulting.com.sg/training-presentations
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Taurus Zodiac Sign: Unveiling the Traits, Dates, and Horoscope Insights of th...my Pandit
Dive into the steadfast world of the Taurus Zodiac Sign. Discover the grounded, stable, and logical nature of Taurus individuals, and explore their key personality traits, important dates, and horoscope insights. Learn how the determination and patience of the Taurus sign make them the rock-steady achievers and anchors of the zodiac.
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Energy and Transportation Systems: How might Technological Change be Creating New Opportunities in Them?
1. How Might Technological Change be
Creating New Opportunities in
Energy and Transportation Systems?
9th Session of MT5009
A/Prof Jeffrey Funk
Division of Engineering and Technology
Management
National University of Singapore
2. Objectives
• What has and is driving improvements in cost and
performance of energy & transportation systems?
• Can we use such information to
– identify new types of energy & transportation systems?
– analyze potential for improvements in these new
systems?
– compare new and old systems now and in future?
– better understand when new systems might become
technically and economically feasible?
– analyze the opportunities created by these new
systems?
– understand technology change in general
3. This is the Ninth Session in MT5009
Session Technology
1 Objectives and overview of course
2 Four methods of achieving improvements in performance and cost: 1)
improving efficiency; 2) radical new processes; 3) geometric scaling; 4)
improvements in “key” components (e.g., ICs)
3 Semiconductors, ICs, new forms of transistors, electronic systems
4 Bio-electronics, tissue engineering, and health care
5 MEMS, nano-technology and programmable matter
6 Telecommunications and Internet
7 Human-computer interfaces, virtual and augmented reality
8 Lighting and displays
9 Energy and transportation
10 Solar cells and wind turbines
4. Outline for Tonight
• Engines
– Efficiency of engines
– Jet engines
– Benefits from increasing the scale of these engines
• Transportation Equipment
– Trains
– Ships
– Aircraft
– Vehicles
• Electricity Generation
– Fossil fuels and steam turbines
– Other sources (of electricity) and issues
5. Technology Paradigms for Engines
Type of Basic Operation Basic Methods of
Engine Improvement within
Technology Paradigm
Steam engine Power is generated and work Increase efficiency
(from early done by pressurized steam
1700s) pushing against a piston Higher temperature,
pressure, and size
Internal Power is generated and work (geometric scaling)
combustion done by an explosion and
engine (from subsequent expansion of Better controls over fuel, air,
mid-1800s) gaseous fuel pushing against a and heat
piston
Jet engine Combustion of high
(from mid- temperature and pressure fuel
1900s) provides thrust
6. Efficiency of Engines
• Efficiency of heat engine = 1 – Tout/Tin
• Increased temperatures often require
– better materials
– often higher pressures
– often larger scale
• These engines propel transportation device. For
them, we are often interested in power density or
miles per gallon. This also requires reductions in
– weight
– friction
– etc.
7. Figure 2.2 Improvements in Maximum Efficiency of Engines and Turbines
Combined
50% cycle gas
turbine
Source:
adapted
from (Smil,
2010, Figure
40% 1.2) and
Thermal (Edwards et
al, 2010) Diesel
Efficiency engines
30%
Gas
turbine
20%
Steam
turbine
10%
Steam
Engines Gasoline internal
combustion engines
0
1700 1750 1800 1850 1900 1950 2000
8. Progress of energy transportation (Watts per kg)
Source: Koh and Magee, Technology Forecasting and Social Change 75(6): 735-758
9. Progress of energy transportation (Watts per liter).
Source: Koh and Magee, Technology Forecasting and Social Change 75(6): 735-758
11. Increases in Scale: Larger Scale Often Leads to Higher
Temperatures, Pressures, and thus Efficiencies
1010
Power Steam
turbines
(W)
108
Source:
adapted
from
(Smil,
2010 Gas
106 Figure turbines
2.11)
104 Steam Internal
Engines combustion
engines
102
1700 1750 1800 1850 1900 1950 2000
12. Outline for Tonight
• Engines
– Efficiency of engines
– Jet engines
– Benefits from increasing the scale of these engines
• Transportation Equipment
– Trains
– Ships
– Aircraft
– Vehicles
• Electricity Generation
– Fossil fuels and steam turbines
– Other sources and issues
13. Jet Engines
• Combustion of high temperature and pressure fuel
provides thrust
– in accordance with Newton's laws of motion
• This broad definition of jet engines includes
– Turbojets, turbofans, rockets, ramjets, pulse jets, pump-jets
• Jet engines replaced piston ones partly because
– pistons can only move so fast
– propellers are limited by speed of sound and require dense air
– air causes friction (higher altitudes have thinner air and thus
less friction)
– thus jet engines (and rockets) can potentially go much faster
than piston engines
14. Jet Engines
Low-Bypass High-Bypass
Low-bypass ratio leads to high exhaust High bypass ratio leads to low exhaust
speed, high flight speeds, and low speed, lower flight speeds, and higher
fuel efficiency fuel efficiency
About 1.5 for fighter jets About 17 for commercial airliners
15. Jet Engines
• Overall Efficiency =
thermal efficiency x
propulsive efficiency
• Propulsive Efficiency
= 2Vf/(Vf + Ve)
where
Vf = flight velocity
Ve = exhaust velocity
Vf and Ve are
determined by the
bypass ratio
Source: Intergovernmental Panel on Climate Change, Aviation and the Global Atmosphere, Chapter 7
16. Increases in pressure
and temperature led
to higher efficiencies
(see next slide) and
lower fuel consumption
Source: Intergovernmental Panel on Climate Change,
Aviation and the Global Atmosphere, Chapter 7
17. Past and Future Efforts to Increase Efficiency
Thermal Efficiency
Propulsive Efficiency
Unducted fans (UDF) are needed to increase bypass ratios
Source: Intergovernmental Panel on Climate Change, Aviation and the Global Atmosphere, Chapter 7
18. Outline for Tonight
• Engines
– Efficiency of engines
– Jet engines
– Benefits from increasing the scale of these engines
• Transportation Equipment
– Trains
– Ships
– Aircraft
– Vehicles
• Electricity Generation
– Fossil fuels and steam turbines
– Other sources and issues
19. Larger Scale Often Leads to Higher Temperatures and
Pressures: Maximum Scale of Engines and Turbines
1010
Power Steam
(W) Source: turbines
adapted
108 from
(Smil,
2010
Figure
2.11)
Gas
106 turbines
104 Steam Internal
Engines combustion
engines
102
1700 1750 1800 1850 1900 1950 2000
20. From 10 HP (horse power)
in 1817
To 1,300,000 HP today
(1000 MW)
Steam engine
Their modern day
equivalent: steam
turbine
21. From ¾ horsepower in 1885 (Benz)
to world’s largest internal
combustion engine (90,000 HP)
Produced by Wartsila-Sulzer
and used in the Emma Maersk
(a ship)
22. Benefits of Larger Scale in Engines
Cost of cylinder
or piston is function
of cylinder’s surface
area (πDH) Height
of
Output of engine
cylinder
is function of
cylinder’s (H)
volume (πD2H/4)
Result: output rises
faster than costs as
diameter is increased
Diameter of cylinder (D)
23. Benefits from Larger Engines
• Not just internal combustion engines (ICE), any
form of engine that has pistons and cylinders
• Steam engines may benefit more from increases
in scale than do ICE since they have a boiler and
boilers benefit from increases in scale
– Like reaction vessels, costs increase as a function of
surface area and output increases as a function of
volume
• Other benefits of scaling
– Higher temperatures and pressures have higher
efficiencies
– Larger engines enable higher temperatures and higher
pressures
24. Comparing Price Per Horsepower for Smaller
and Larger Engines
• In terms of price per horsepower (HP),
– A 20 HP steam engine was 1/3 that of a 2 HP engine
in 1800 (Source: von Tunzelman)
– Honda’s 225 HP marine engine is currently 26% of its
2.3 HP engine (price per HP)
• Extrapolating to the complete range of engines
– largest steam engines in locomotives had thousands of
HP and largest steam turbines have 1.3 million HP
– the first (3/4 HP) and now largest (90,000 HP) ICE
– the largest engine would be less than 1% the price per
HP of the smallest engine
25. Limits to Paradigms for Engines
• Limits to thermal efficiencies (as defined by
thermodynamics) have almost been reached
• Limits to scaling (Higher temperature, pressure,
and size) have almost been reached
• Limits to complexity
– First jet engine in 1936: a few hundred parts
– Modern jet engines: as many as 22,000 parts
– This complexity raises costs!
• But problems with emissions (carbon dioxide,
lead, nitrous and sulfur dioxides) drive the need for
new technologies – what could they be?
26. Outline for Tonight
• Engines
– Efficiency of engines
– Jet engines
– Benefits from increasing the scale of these engines
• Transportation Equipment
– Trains
– Ships
– Aircraft
– Vehicles
• Electricity Generation
– Fossil fuels and steam turbines
– Other sources and issues
27. Technology Paradigms for Transportation Technologies
Technology Basic Operation Basic Methods of
Improvement within
Technology Paradigm
Locomotive Output from steam engine turns Geometric Scaling
wheels and wheels run on track
Steam ship Output from steam engine (and later Aerodynamic designs
ICE) turns propeller
Lighter materials
Electric trains Electricity powers the rotation of
wheels through motors
Automobiles Output from ICE or electric motor
turns wheels and wheels move over
ground
Aircraft Pushed forward by output from
internal combustion engine (later by
jet engine) and wings provide “lift”
ICE: internal combustion engine
28. Reaching Limits for Transportation Speed
Exploring and Shaping International Futures, Hughes & Hillebrand, 2006, p. 37
29. Scaling in Transportation Equipment
• In trains, ships, planes, and vehicles
– Basically long cylinder
– Construction/production cost is proportional to surface area
while output (people miles) is proportional to volume (and
speed)
– Benefits from increasing the scale of engines supports
increases in scale of transportation equipment
– Although operating cost rise with increases in weight and
speed, initially they don’t rise as fast as output does (but
diseconomies usually emerge)
• Results from increases in scale
– Cost of transportation dropped dramatically in the 1800s
and 1900s as large trains, ships, planes and buses were
constructed (also information technology and other factors)
30. From tens of horsepower, miles
per hour in single digits, and 70
passengers in 1804
To thousands of horsepower,
thousands of passengers, and
126 miles per hour in 1938
31. A New Concept (Lighter Electric Trains) and a Big Train:
8000 KW of Power, 236 miles per hour, and
thousands of passengers
It appears that the limits of scale have been reached.
32. Outline for Tonight
• Engines
– Efficiency of engines
– Jet engines
– Benefits from increasing the scale of these engines
• Transportation Equipment
– Trains
– Ships
– Aircraft
– Vehicles
• Electricity Generation
– Fossil fuels and steam turbines
– Other sources and issues
34. From 1,340 tons in 1838, 10 miles
per hour, and 48 passengers in 1838
(28 Tons per passenger)
To 225,000 tons in 2009, 26 miles
per hour, and 5300 passengers in 2009
(42 Tons per passenger)
Ocean-
Travelling
Steamships
35. From 1807 tons in 1878
To 500,000 tons in 2009
Oil Tankers
36. Benefits of Scaling in Oil Tankers and
Freight Vessels
Scale Dimension Oil Tankers Freight Vessels
Large Scale Price $120 Million $59 Million
Capacity 265,000 tons 170,000 tons
Price per capacity $453 per ton $347 per ton
Small Scale Price $43 Million $28 Million
Capacity 38,500 tons 40,000 tons
Price per capacity $1,116 per ton $700 per ton
Source: UN study of shipping equipment, 2009
37. Outline for Tonight
• Engines
– Efficiency of engines
– Jet engines
– Benefits from increasing the scale of these engines
• Transportation Equipment
– Trains
– Ships
– Aircraft
– Vehicles
• Electricity Generation
– Fossil fuels and steam turbines
– Other sources and issues
38. Geometric Scaling in Jet Engines (1)
• Combustion chambers (basically a cylinder)
benefit from larger scale
– costs rise with surface area
– output rises with volume
39. Jet Engines
I-A
From 1,250 pounds of thrust in 1942 (GE’s I-A) to
127,000 pounds of thrust today (GE90-115B)
Power (horsepower) = thrust (lbf) x speed (feet/second) / 550
From 660 (at 200mph) to 170,000 (at 500 mph) horsepower
40. Geometric Scaling in Jet Engines (2)
• Other benefits from larger scale were discussed
earlier tonight:
– Larger engines enable higher temperatures, pressures
– Higher temperatures enable higher thermal efficiencies
• Larger engines are also needed because aircraft
benefits from increases in scale
– Aircraft cost per passenger is lower for larger than
smaller planes
– Labor costs are lower and fuel efficiencies are higher
for larger aircraft
41. From DC-1 in 1931
(12 passengers, 180 mph)
To A-380 in 2005
(900* passengers, 560 mph)
*Economy only mode
42. Current Prices per Capacity for Large and
Small Scale Oil Tankers and Aircraft
Scale Dimension Oil Tankers Aircraft
Large Price $120 Million $346.3 Million
Scale (A380)
Capacity 265,000 tons 900 passengers
Price per $453 per ton $384,777 per
capacity passenger
Small Price $43 Million $62.5 Million
Scale (A318)
Capacity 38,500 tons 132 passengers
Price per $1,116 per ton $473,348 per
capacity passenger
43.
44. Outline for Tonight
• Engines
– Efficiency of engines
– Jet engines
– Benefits from increasing the scale of these engines
• Transportation Equipment
– Trains
– Ships
– Aircraft
– Vehicles
• Electricity Generation
– Fossil fuels and steam turbines
– Other sources and issues
45. From First Benz in 1885 (1600 cc, ¾
hp, 8 mph, 13 km/h, 1 passenger)
To: Model T (2900 cc, 20 hp) in 1909
And: BMW mini-coupe (218 HP,
1600 cc, 120 mph)
Not benefiting from scaling because
automobiles are designed only for a
few passengers!!!
46. From First Benz in 1885 (single
passenger, ¾ hp, 8 mph)
To 300 passenger bus in China with
over 300 horsepower
Buses do benefit
from scaling!!
But have limits
been reached?
47. From First Benz in 1885 (single
passenger, ¾ hp, 8 mph)
To 300 tons of material with 3000
horsepower in 21st century
Trucks also benefit
from scaling
But have limits
been reached?
48. Results from benefits of geometric
scaling for land, sea, and air
transportation in U.S.
• Transportation share of U.S. GDP dropped by
factor of 10
• Freight bill divided by U.S. GDP dropped by 50%
• Dollars per ton-mile for rail in U.S. dropped
almost by factor of 10
• Globalization is partly a result of scaling in
transportation equipment (and IT, containerized
shipping, and changes in political systems)
49. (for U.S.)
Source: Cities, regions and the decline of transport costs, Papers in Regional Science
83: 197–228 (2004), Edward L. Glaeser, Janet E. Kohlhase
50. For U.S.
Source: Cities, regions and the decline of transport costs, Papers in Regional Science
83: 197–228 (2004), Edward L. Glaeser, Janet E. Kohlhase
51. (only for rail in U.S.)
Source: Cities, regions and the decline of transport costs, Papers in Regional Science
83: 197–228 (2004), Edward L. Glaeser, Janet E. Kohlhase
52. But Increasing the Scale of Transportation Equipment
Required Better Components and Advances in Science
• Bigger locomotives and steam ships required
– Bigger rail lines, ports, and canals
– Lighter and stronger materials for them and their engines
– Better tolerances for engines
• Electric trains required
– Cheaper electricity, better motors (from the late 19th century)
• Automobiles and aircraft required
– Lighter materials for them and their engines
– Better tolerances for engines
– For aircraft,
• expensive composites for the fuselage and engines
• larger aircraft have required larger terminals
53. Limits to Efficiencies and Scaling
• Are limits to improvements in efficiencies being
approached?
• Are limits to physical spaces being approached for
– rail lines and terminals?
– shipping lanes and ports?
– air space and terminals?
– roads and parking?
• Are limits to making transportation equipment
lighter being approached?
• If there are fewer opportunities than how can we
solve problems with emissions?
54. How About Electric Vehicles?
• The main difference between conventional
and electric vehicles is the
– replacement of the internal combustion
engine and the gasoline tank
– with a battery and a motor
• How much can a battery’s
– energy storage density be improved?
– cost be reduced through increases in scale of
production equipment?
57. Source: Tarascon, J. 2009. Batteries for Transportation Now and In the Future,
presented at Energy 2050, Stockholm, Sweden, October 19-20.
58. Batteries
• Can better materials be found?
• Materials with
– higher energy or power densities per volume or weight?
– lower costs per volume or weight?
• Will these better materials enable the cost and
performance (e.g., range and acceleration) of
electric vehicles to be rapidly improved?
• Or will the costs fall as the scale of production is
increased (Lowe, M, Tokuoka, S, Trigg, T, Gereffi, G 2010. Lithium-ion Batteries for Electric
Vehicles, Center on Globalization, Governance & Competitiveness, Duke University, October 5)
– Lithium-ion batteries for cars are different from those for
electronic products
– Also have lower production volumes and higher costs
59. What About Batteries that Benefit from
Reductions in Scale
• Thin-film ones that benefit from geometric scaling in the
same that solar cells do
• Nano-scale ones
– While conventional batteries separate the two electrodes by thick
barrier, nano-scale batteries place the electrodes close to each
other with nano-wires and other nano-devices
– By reducing the diameter of the electrode or catalyst particles, the
ratio of surface area-to volume goes up and thus the rate of
exchange between particles increases
• Remember the discussion of nano-technology where
surface area-to volume ratio was emphasized
– Some technologies (phenomenon) benefit from increases in this
ratio
Sources: 1) Economist, 2011. The power of the press. January 20, 2011, p. 73; 2) Scientists Reveal Battery Behavior at
the Nanoscale, Science News, September 15, 2010, http://www.sciencedaily.com/releases/2010/09/100914151043.htm.
3) Building Better Batteries from the Nanoscale Up, Scientific computing,
http://www.scientificcomputing. com/news-DS-Building-Better-Batteries-from-the-Nanoscale -Up-121010.aspx,
60. What About Flywheels?
• Energy densities are already high, have steeper
slopes and improvements projected to continue
• Energy is function of mass times velocity squared,
lighter materials (carbon fiber) enable higher
speeds: Rapid improvements are occurring
• Better for hybrids than are batteries because twice
as much energy is converted during braking than
with batteries
• Also cheaper: One-fourth the price?
• Now used in Formula 1 cars
• Challenge is reliability with required vacuums
Source: The Economist Technology Quarterly, December 3, 2011
61. How About Magnetic Levitating
(MagLev) Trains?
• A magnetic field enables a train to float above the
tracks, thus eliminating friction
• Problem is high cost of magnets
• Potential solution is superconducting magnets
– Need higher temperature superconducting materials
(currently best are about 90 degrees Kelvin)
– Difficult to mold ceramic materials into wires
• nano-techniques help, prices have fallen by 90% since 1990s
• they remain ten times higher than copper cables ($15-
25/kiloamp per meter)
• Best applications are in places where laying new cables is
expensive
62. Outline for Tonight
• Engines
– Efficiency of engines
– Jet engines
– Benefits from increasing the scale of these engines
• Transportation Equipment
– Trains
– Ships
– Aircraft
– Vehicles
• Electricity Generation
– Fossil fuels and steam turbines
– Other sources and issues
63. Technology Paradigms for Electricity Generation
Technology Basic Operation Basic Methods of
Improvement within
Technology Paradigm
Battery Transforms chemical energy into More reactive, higher current
electrical energy carrying, and lighter materials
Generators Movement of a loop of wire Higher temperature, pressure,
and Turbines between poles of magnet by and scale
turbine generates electricity Higher energy density of fuels
Turbine rotation driven by water,
wind or steam where steam is
generated by many sources
Photovoltaic Absorption of photon releases Thinner materials that absorb
energy equal to “band-gap” of more solar radiation, have less
material recombination of electrons
and holes, and have band-gaps
matching solar spectrum
64. Electricity Generation
• Most electricity is generated via
– Steam, boilers, and steam turbines
• The steam can be generated by different
fuels
– Coal
– Oil
– Nuclear
– Geothermal
– Solar thermal
65. Costs Fell as the Scale was Increased
• Larger steam boilers and turbines
– led to cheaper turbines and
– thus lower costs of electricity generation
• Higher voltages led to lower transmission losses and thus
facilitated more centralized generation of electricity
• Result
– price of electricity in U.S. dropped from $4.50 to $0.09 between 1892
and 1970 in constant dollars
– little since then so diminishing returns to scale have probably been
reached
– Some argue US implemented too much scale
67. Scale of Coal-Fired Power Plants was Increased
Source:
Hirsh R (1989). Technology
and Transformation in the
Electric Utility Industry,
Cambridge University
Press.
71. Transmission Systems
• Also benefit from increases in scale
• But here scale is measured in terms of voltage
• Higher voltages reduce energy loss
– HVAC: high voltage alternating current
– HVDC: high voltage direct current
• How about superconductors for transmission
systems?
72.
73. Fig. 3. Progress of energy transportation; (a) powered distance
and (b) powered distance per unit cost.
74. Better transmission systems and lower capital
costs per output (from increases in efficiency and
scale) led to lower electricity costs per kilowatt
hour: From $4.50 to $0.09 in 1996 USD
Source: Hirsh R (1989). Technology and Transformation in the Electric Utility Industry, Cambridge University Press.
75. Outline for Tonight
• Engines
– Efficiency of engines
– Jet engines
– Benefits from increasing the scale of these engines
• Transportation Equipment
– Trains
– Ships
– Aircraft
– Vehicles
• Electricity Generation
– Fossil fuels and steam turbines
– Other sources and issues
77. Even Higher Energy Densities Exist
Storage type Specific energy (MJ/kg)
Indeterminate matter and antimatter 89,876,000,000 *
Deuterium-tritium fusion 576,000,000
Uranium-235 used in nuclear weapons 88,250,000
Natural uranium (99.3% U-238, 0.7% U-235) in fast breeder reactor 86,000,000
Reactor-grade uranium (3.5% U-235) in light water reactor 3,456,000
30% Pu-238 α-decay 2,200,000
Hf-178m2 isomer 1,326,000
Natural uranium (0.7% U235) in light water reactor 443,000
30% Ta-180m isomer 41,340
Source: http://en.wikipedia.org/wiki/Energy_density
*about 4740 kg of antimatter could have supplied humans with all their energy needs in 2008. for more information
on anti-matter, see Michio Kaku, Physics of the Impossible, New York: Doubleday, 2008
78. Another way to look at energy density; Source: Vaclav Smil
79. Fusion (1)
• The sun’s temperature can be created with
– high energy lasers impacting on fuel pellet
– high magnetic field
• Challenges
– high accuracy of laser beams and spherical
uniformity of pellets are needed in order to achieve
consistent heating across the pellet
– extremely precise magnetic field is needed so that
the gas is compressed evenly
• very difficult when done inside a dipole
• supercomputer plots the magnetic and electric fields
• Superconducting magnets may be needed
80. Fusion (2)
• “When I started in this field as a graduate
student we made 1/10 of a Watt of fusion heat
in a pulse of 1/100 of second. Now the record
is in the range of 10 million Watts for a second.
That is an improvement by an overall factor of
10 billion. The international ITER project will
produce 500 million Watts of fusion heat for
periods of at least 300 - 500 seconds.
• Rob Goldston, Director of the Princeton
Plasma Physics Laboratory, 2009?
81. Fusion (3)
• According to Michio Kaku (2011)
• The current record is 16 MW, created by the
European Joint European Trust
• The target date for breakeven in energy is now
set to be 2019
• DEMO is expected to continually produce
energy and begin doing so in 2033. It will
produce two billion watts of power (2 GW) or
25 times more energy than it consumes
82. Fusion (4)
• But what will the costs be?
• Will increases in scale lead to sufficient
reductions in cost?
• Will benefits from increases in scale be similar
to those experienced with coal-fired plants?
83. Conclusions (1)
• Energy and transportation equipment have
benefited from
– Improvements in efficiency
– increases in scale
– and new technologies (and science)
• These changes created opportunities for new and
existing firms
• But limits to scale have probably been reached for
most existing technologies
• Thus, improvements in cost and performance,
including reducing global warming, probably require
new technologies
84. Conclusions (2)
• Many new technologies are decades away
– or are they? Can you identify technological trends that
suggest otherwise?
– What about fusion, electric vehicles or magnetic levitating
trains ?
• In the next session, we look at two technologies
(solar cells and wind turbines) that are experiencing
rapidly falling costs