Siemens is developing hybrid electric propulsion systems for aircraft to reduce operating costs and environmental impact through distributed electric propulsion. Siemens has flight tested electric propulsion units on various aircraft, including setting world records on the Extra 330LE. Current projects include providing electric motors and inverters for the Eviation Alice nine-seat electric commuter aircraft and Airbus's CityAirbus electric air taxi.
Lattice Energy LLC- Report Reveals Boeing and NASA Investigating LENR-powered...Lewis Larsen
There is a recent NASA government contract report titled, “Subsonic Ultra Green Aircraft Research Phase II: N+4 Advanced Concept Development,” by Marty K. Bradley and Christopher K. Droney of Boeing Research and Technology, Huntington Beach, California. The document reveals that Boeing and NASA are now jointly investigating the possibility of using low energy nuclear reactions (LENRs) to power advanced versions of future “green aircraft.”
1. Ducts are sized using pressure drop and velocity criteria. The duct diameter is selected based on the air volume and desired constant pressure drop. Duct velocities are limited based on building type to control noise.
2. Elbows, T-branches, Y-branches, and reducers (transitions) are examples of duct fittings.
3. Volume dampers and fire dampers are examples of duct accessories.
4. Allowable duct velocities vary from 2-12 m/s depending on the building type, with typical office spaces around 6 m/s.
5. Supply ducts deliver conditioned air to spaces, return ducts remove air from spaces, and exhaust ducts remove
The document analyzes the ideal performance of a jet engine through three parts. It examines the propulsive, thermal, and overall efficiencies. The compressor compresses the air 10 times while the turbine expands it 10 times. With compressor and turbine efficiencies of 85%, the useful work is 14,100kJ. The combustion temperature is 1112K and heat supplied is 50,900kJ. The nozzle exhaust is choked with pressure of 129kPa and temperature of 664K. Specific fuel consumption is calculated based on the heat required to increase the air temperature. An afterburner is considered which further increases the exhaust temperature.
Enhancement of Heat Transfer Analysis and Optimization of Engine Fins of Vary...ijtsrd
The Engine cylinder is one of the major automobile components, which is subjected to high temperature variations and thermal stresses. In order to cool the cylinder, fins are provided on the cylinder to increase the rate of heat transfer. By doing thermal analysis on the engine cylinder fins, it is helpful to know the heat dissipation inside the cylinder. The principle implemented in this project is to increase the heat dissipation rate by using the invisible working fluid, nothing but air. As know, by increasing the surface area we can increase the heat dissipation rate, so designing such a large complex engine is very difficult. The main purpose of using these cooling fins is to cool the engine cylinder by air. The main aim of the project is to analyse the thermal properties by varying geometry, material, distance between the fins and thickness of cylinder fins. Parametric models of cylinder with fins have been developed to predict the transient thermal behaviour. The models are created by varying the geometry circular and also by varying thickness of the fins for both geometries. The 3D modelling software used is Pro/Engineer. Thermal analysis is done on the cylinder fins to determine variation temperature distribution over time. The analysis is done using ANSYS. Thermal analysis determines temperatures and other thermal quantities. In this thesis, using materials cast iron, Copper and Aluminium alloy 6082 are also for cylinder fin body. Thermal analysis is done using all the three materials by changing geometries, distance between the fins and thickness of the fins for the actual model of the cylinder fin body. K. Karthikeyan | C. Saravanan | Dr. T. Senthil Kumar"Enhancement of Heat Transfer Analysis and Optimization of Engine Fins of Varying Geometry" Published in International Journal of Trend in Scientific Research and Development (ijtsrd), ISSN: 2456-6470, Volume-2 | Issue-4 , June 2018, URL: http://www.ijtsrd.com/papers/ijtsrd14327.pdf http://www.ijtsrd.com/engineering/mechanical-engineering/14327/enhancement-of-heat-transfer-analysis-and-optimization-of-engine-fins-of-varying-geometry/k-karthikeyan
ALSTOM TECHNICAL PAPER - 2005 EPRI Pulliam #6 HP Rotor Forging Section Replac...Mike Jirinec, PMP
The document discusses the replacement of a high-pressure steam turbine rotor forging section due to severe creep damage. Inspections found cracking in the balance plane radius, and metallurgical examination revealed severe creep cracking. Material analysis and creep rupture testing allowed for temporary operation at a de-rated output and temperature until repair. In 2005, the forging section was replaced and a new section was join welded to the rotor between stages. The repair involved replacing the damaged section and welding a new one using deep groove submerged arc welding.
In ancient times, ships were used to travel and explore new lands, but required significant fuel storage which added weight. Later, steam engines and nuclear power were adopted for marine propulsion. Nuclear power provided significant advantages by using small amounts of fuel to power ships for long periods without refueling, helping address energy and range issues for naval vessels. Nuclear marine propulsion works by using a nuclear reactor to create steam that drives turbines and generators to power the ship. While allowing for long-range operation, nuclear marine propulsion requires extensive shielding and specially trained crews, and any failures could have severe environmental impacts.
The document describes the electrical system configuration of an Airbus A320 aircraft. In normal configuration, external power can supply the AC and DC ground/flight buses directly without powering the entire aircraft network when only ground services are required. The document also outlines failure scenarios for individual engine generators, AC bus 1, and transformer rectifiers TR1 and TR2, as well as flight operations using only battery power on the ground or in flight at speeds under 50 knots.
Lattice Energy LLC- Report Reveals Boeing and NASA Investigating LENR-powered...Lewis Larsen
There is a recent NASA government contract report titled, “Subsonic Ultra Green Aircraft Research Phase II: N+4 Advanced Concept Development,” by Marty K. Bradley and Christopher K. Droney of Boeing Research and Technology, Huntington Beach, California. The document reveals that Boeing and NASA are now jointly investigating the possibility of using low energy nuclear reactions (LENRs) to power advanced versions of future “green aircraft.”
1. Ducts are sized using pressure drop and velocity criteria. The duct diameter is selected based on the air volume and desired constant pressure drop. Duct velocities are limited based on building type to control noise.
2. Elbows, T-branches, Y-branches, and reducers (transitions) are examples of duct fittings.
3. Volume dampers and fire dampers are examples of duct accessories.
4. Allowable duct velocities vary from 2-12 m/s depending on the building type, with typical office spaces around 6 m/s.
5. Supply ducts deliver conditioned air to spaces, return ducts remove air from spaces, and exhaust ducts remove
The document analyzes the ideal performance of a jet engine through three parts. It examines the propulsive, thermal, and overall efficiencies. The compressor compresses the air 10 times while the turbine expands it 10 times. With compressor and turbine efficiencies of 85%, the useful work is 14,100kJ. The combustion temperature is 1112K and heat supplied is 50,900kJ. The nozzle exhaust is choked with pressure of 129kPa and temperature of 664K. Specific fuel consumption is calculated based on the heat required to increase the air temperature. An afterburner is considered which further increases the exhaust temperature.
Enhancement of Heat Transfer Analysis and Optimization of Engine Fins of Vary...ijtsrd
The Engine cylinder is one of the major automobile components, which is subjected to high temperature variations and thermal stresses. In order to cool the cylinder, fins are provided on the cylinder to increase the rate of heat transfer. By doing thermal analysis on the engine cylinder fins, it is helpful to know the heat dissipation inside the cylinder. The principle implemented in this project is to increase the heat dissipation rate by using the invisible working fluid, nothing but air. As know, by increasing the surface area we can increase the heat dissipation rate, so designing such a large complex engine is very difficult. The main purpose of using these cooling fins is to cool the engine cylinder by air. The main aim of the project is to analyse the thermal properties by varying geometry, material, distance between the fins and thickness of cylinder fins. Parametric models of cylinder with fins have been developed to predict the transient thermal behaviour. The models are created by varying the geometry circular and also by varying thickness of the fins for both geometries. The 3D modelling software used is Pro/Engineer. Thermal analysis is done on the cylinder fins to determine variation temperature distribution over time. The analysis is done using ANSYS. Thermal analysis determines temperatures and other thermal quantities. In this thesis, using materials cast iron, Copper and Aluminium alloy 6082 are also for cylinder fin body. Thermal analysis is done using all the three materials by changing geometries, distance between the fins and thickness of the fins for the actual model of the cylinder fin body. K. Karthikeyan | C. Saravanan | Dr. T. Senthil Kumar"Enhancement of Heat Transfer Analysis and Optimization of Engine Fins of Varying Geometry" Published in International Journal of Trend in Scientific Research and Development (ijtsrd), ISSN: 2456-6470, Volume-2 | Issue-4 , June 2018, URL: http://www.ijtsrd.com/papers/ijtsrd14327.pdf http://www.ijtsrd.com/engineering/mechanical-engineering/14327/enhancement-of-heat-transfer-analysis-and-optimization-of-engine-fins-of-varying-geometry/k-karthikeyan
ALSTOM TECHNICAL PAPER - 2005 EPRI Pulliam #6 HP Rotor Forging Section Replac...Mike Jirinec, PMP
The document discusses the replacement of a high-pressure steam turbine rotor forging section due to severe creep damage. Inspections found cracking in the balance plane radius, and metallurgical examination revealed severe creep cracking. Material analysis and creep rupture testing allowed for temporary operation at a de-rated output and temperature until repair. In 2005, the forging section was replaced and a new section was join welded to the rotor between stages. The repair involved replacing the damaged section and welding a new one using deep groove submerged arc welding.
In ancient times, ships were used to travel and explore new lands, but required significant fuel storage which added weight. Later, steam engines and nuclear power were adopted for marine propulsion. Nuclear power provided significant advantages by using small amounts of fuel to power ships for long periods without refueling, helping address energy and range issues for naval vessels. Nuclear marine propulsion works by using a nuclear reactor to create steam that drives turbines and generators to power the ship. While allowing for long-range operation, nuclear marine propulsion requires extensive shielding and specially trained crews, and any failures could have severe environmental impacts.
The document describes the electrical system configuration of an Airbus A320 aircraft. In normal configuration, external power can supply the AC and DC ground/flight buses directly without powering the entire aircraft network when only ground services are required. The document also outlines failure scenarios for individual engine generators, AC bus 1, and transformer rectifiers TR1 and TR2, as well as flight operations using only battery power on the ground or in flight at speeds under 50 knots.
This document provides an overview of gas turbine engines and their components. It discusses the fundamentals of gas turbine engines including the Brayton cycle and basic components like compressors, combustion chambers, and nozzles. Regarding compressors, it describes the advantages and disadvantages of radial/centrifugal and axial flow compressors. For combustion chambers, it discusses different chamber types (can, can-annular, annular) and factors affecting combustor design like temperature, stability, and pollution control. It also provides information on supersonic combustion challenges. Finally, it provides an introduction to nozzles and their objectives in jet propulsion.
The document discusses the zones of combustion in a jet engine combustion chamber. It explains that there are three main zones:
1) The primary combustion zone, where a portion of the incoming air mixes with fuel for combustion. Recirculation helps mix and stabilize the flame.
2) The dilution zone, where the remaining air is mixed with the combustion gases to lower the temperature before the turbine.
3) The cooling zone, where the remaining air is used to cool the combustion chamber walls and stabilize the flame. Without these zones, the flame would not remain lit through different operating conditions of the engine.
MIL-1760 Aerospace & Defense Engineering Training : Tonex TrainingBryan Len
Price: $1,699.00
Course Number: 1760
Length: 2 Days
MIL-STD-1760 Aircraft/Store Electrical Interconnection System defines a standardized electrical interface between a military aircraft and its carriage stores. Carriage stores range from weapons, such as GBU-31 JDAM, to pods, such as AN/AAQ-14 LANTIRN, to drop tanks. Prior to adoption and widespread use of MIL-STD-1760, new store types were added to aircraft using dissimilar, proprietary interfaces.
This greatly complicated the aircraft equipment used to control and monitor the store while it was attached to the aircraft: the stores management system, or SMS.
The course includes description of MIL-STD-1760 signals including:
MIL-STD-704 power connections;
MIL-STD-1553 data communications interface;
high and low bandwidth analog signals;
discrete signals; and
fiber optics
Course Objectives:
Upon successful completion of this course , all the attendees will have the capability to do :
MIL-STD-1760 defines the electrical characteristics of the signals at the interface, as well as the connector and pin assignments of all of the signals used in the interface Upon completion of this course, the attendees are be able to:Describe what MIL-STD-1760 is
Understand MIL-STD-1760 characteristics
Describe MIL-STD-1760 architecture
Explain requirements, design and, testing aspects of MIL-STD-1760
Course Outline:
This course will focus on points mentioned at below:
Introduction to MIL-STD-1760
Aircraft/store Configurations
Aircraft Requirements
Mission store Requirements
Carriage store Requirements
Umbilical cable requirements
Power Interface Interrupts
MIL-STD-1760 MIL-STD-1760 Systems Engineering: Requirements, Design, Implementation and Testing
MIL-STD-1760 Requirements
Ask for more information. Visit Tonex.com
https://www.tonex.com/training-courses/mil-1760-training/
Wind tunnels come in several types depending on their design and airflow characteristics. The document describes blow down, atmospheric entry, high enthalpy, and continuous flow wind tunnels. Continuous flow wind tunnels can be open circuit for subsonic or supersonic testing, or closed circuit. Open circuit tunnels work by drawing in air and exhausting it, while closed circuit wind tunnels recirculate the air through a compressor. The different wind tunnel types are used to simulate various flow conditions for testing aircraft and missile components.
The document provides an overview of aircraft structures and their key components. It discusses the fuselage, wings, empennage, landing gear, and powerplants. For each component, it describes the basic design and functions. It also covers important aircraft structural concepts like stressed skin construction, monocoque vs semi-monocoque design, and choices of lightweight metal materials. Overall the document serves as a high-level introduction to aircraft structures and the major structural components of airplanes.
This is Part 1 of 3 covering my work on my Future Deep Strike Aircraft project, to inspire interest in aerospace engineering for the RAeS, the A&SPA(UK) and AIAA.
The document discusses vortex theory and Prandtl's lifting-line theory for analyzing the aerodynamics of finite wings. It introduces key concepts like downwash, trailing vortices, Helmholtz's vortex theorems, and the Biot-Savart law. The lifting-line theory models the wing as a bound vortex filament with varying circulation strength. This allows determining the induced downwash and angle of attack distributions. Prandtl's fundamental equation relates the circulation distribution to the wing geometry and twist. The lifting-line theory provides insights into the relationship between wing shape and lift distribution.
This document provides an overview of materials used in transparent armour systems. It discusses various types of glass like borosilicate glass, fused silica, laminated glass, and toughened glass. It also covers glass ceramics and how they are produced. Transparent ceramics like aluminium oxynitride spinel, single crystal aluminium oxide, and magnesium aluminate spinel are introduced. Polymeric materials such as thermoplastics and thermosets that can be used are mentioned. Finally, it provides a brief overview of the design of transparent armour systems including strike face layer, intermediate layer, and spall layer, and discusses ballistic performance considerations.
The document describes the process of calculating the cooling load of a room using the Cooling Load Temperature Difference (CLTD) Method. It involves calculating the transmission load through the walls and roof by determining their areas, U-values, and CLTD corrections. The solar heat gain through windows is also calculated. Internal loads from lighting, equipment, and occupancy are estimated. The total cooling load is calculated by summing the transmission load, solar gain, internal load, and occupancy load, which comes out to be 9170.97 watts or around 2.5 to 3 tons for air conditioning unit selection.
The document discusses inspection and maintenance procedures for aircraft piston engines. It begins by listing different engine classifications and components like dynamic dampers. It describes steps like checking for oil pressure after starting, performing dimensional inspections to check for wear. Visual inspections are used to find defects. The document then discusses classification of piston engines and components like master articulated rods. It outlines the basic overhaul process and non-destructive testing methods. Finally, it describes inspecting and maintaining engine controls during 100-hour inspections to check for wear and smooth operation.
The document discusses the black box, which consists of the flight data recorder (FDR) and cockpit voice recorder (CVR). It provides a brief history, explaining the first FDR prototype was created in 1956. It describes the construction of black boxes, including their heat-resistant red paint and mounting in the aircraft's tail section. The inside contains the FDR, which records aircraft performance parameters, and the CVR, which records audio from the cockpit. Black boxes use magnetic tapes or solid state technology to store data. They aid in accident investigations by providing audio and data to help determine causes.
Pressure Coefficients on Building Facades for Building SimulationSimScale
While accurate wind pressure coefficients are critical to evaluating building design, most engineering software for energy and thermal analysis oversimplifies treatment of wind pressure, which can adversely impact cooling, ventilation, overheating, and fresh air rates assessments. This presentation shows how SimScale provides accurate calculations of wind pressures, quickly and cost-efficiently, to deliver a more comprehensive evaluation of building performance.
Watch the webinar recording here: https://www.youtube.com/watch?v=VU4-PN9PYDM
Cryogenic rocket engines use cryogenic fuels such as liquid hydrogen and liquid oxygen that are stored at very low temperatures. They provide several advantages including high energy density and producing only water exhaust, but also have challenges like boil off and leakage due to the extreme cold temperatures required. India's first unmanned lunar mission in 2008 failed when the indigenous cryogenic upper stage engine did not ignite as planned. Future rocket technologies being researched include ion engines, nuclear thermal engines, and other alternatives to further space exploration.
The document provides information about gas turbine engines, including their basic mechanics and operation. It discusses the classification of engines, principles of jet propulsion, theories of jet propulsion and gas turbine engines. It also covers the working cycle of gas turbine engines, factors that affect thrust, types of gas turbine engines like turbojet engines, and changes in velocity and pressure during operation.
This document discusses aerospace fasteners from an manufacturing perspective. It describes the types of rivets used in aircraft assembly, including solid and blind rivets. Solid rivets are used when access is available to both sides, while blind rivets are used when one side is inaccessible. The document outlines rivet identification codes and the process for installing solid rivets. Material selection and testing of aerospace fasteners is also summarized.
1. Many factors must be considered when estimating heating and cooling loads for a building, including size, materials, windows, occupancy, equipment, and air infiltration.
2. Sensible heat is direct heat that raises air temperature, while latent heat involves moisture changing phase. Total heat load is the sum of sensible and latent loads.
3. Effective room loads account for bypass air and determine supply air conditions and equipment capacity needs.
Sistem komunikasi merupakan unsur penting dalam pesawat terbang untuk memfasilitasi komunikasi antara pilot dengan menara kontrol darat maupun antar pesawat. Terdapat berbagai jenis sistem komunikasi yang digunakan seperti High Frequency, Very High Frequency, dan Ultra High Frequency untuk berkomunikasi jarak jauh dan dekat. Sistem komunikasi internal juga digunakan untuk memfasilitasi komunikasi antar awak pesawat dan penumpang melalui Public Address system dan Intercom system. Peralatan darur
The document summarizes the evolution of aircraft structures from early designs using wooden ribs and fabric to modern aluminum and composite designs. It describes key structural components such as those that produce lift (wings, airfoils), control (elevators, ailerons, rudders), modify lift (flaps, slats), and hold other components. Early aircraft had open wooden frameworks and fabric coverings while later warplanes used metal tubing and stressed skin construction. Modern jets widely use semi-monocoque construction.
The document provides information about Frankfinn Institute Of Airhostess Training and a student's research project on the current aviation industry scenario. It discusses sources used like the aviation faculty, newspapers, magazines and the internet. It describes Airbus aircraft models from A300 to A380 and their features. It highlights the growth prospects of the Indian aviation sector and ongoing trends. The student gains knowledge about the industry through this research project.
IDTechEx Research: Manned Electric AircraftIDTechEx
About 20 companies make or will soon make electric aircraft. Nearly all are pure electric and fixed wing, the motorised hang glider and the self-launching sailplane being typical, with one hour endurance. A bigger value market being addressed is training planes and bigger still will be hybrid fixed wing and vertical takeoff aircraft hybrid and pure electric with the pure electric ones only managing 30 minutes. In these slides we discuss possible uses, improvements and other types too.
For more information, see http://www.idtechex.com/aircraft.
Slides by Dr. Peter Harrop of IDTechEx.
This document provides an overview of gas turbine engines and their components. It discusses the fundamentals of gas turbine engines including the Brayton cycle and basic components like compressors, combustion chambers, and nozzles. Regarding compressors, it describes the advantages and disadvantages of radial/centrifugal and axial flow compressors. For combustion chambers, it discusses different chamber types (can, can-annular, annular) and factors affecting combustor design like temperature, stability, and pollution control. It also provides information on supersonic combustion challenges. Finally, it provides an introduction to nozzles and their objectives in jet propulsion.
The document discusses the zones of combustion in a jet engine combustion chamber. It explains that there are three main zones:
1) The primary combustion zone, where a portion of the incoming air mixes with fuel for combustion. Recirculation helps mix and stabilize the flame.
2) The dilution zone, where the remaining air is mixed with the combustion gases to lower the temperature before the turbine.
3) The cooling zone, where the remaining air is used to cool the combustion chamber walls and stabilize the flame. Without these zones, the flame would not remain lit through different operating conditions of the engine.
MIL-1760 Aerospace & Defense Engineering Training : Tonex TrainingBryan Len
Price: $1,699.00
Course Number: 1760
Length: 2 Days
MIL-STD-1760 Aircraft/Store Electrical Interconnection System defines a standardized electrical interface between a military aircraft and its carriage stores. Carriage stores range from weapons, such as GBU-31 JDAM, to pods, such as AN/AAQ-14 LANTIRN, to drop tanks. Prior to adoption and widespread use of MIL-STD-1760, new store types were added to aircraft using dissimilar, proprietary interfaces.
This greatly complicated the aircraft equipment used to control and monitor the store while it was attached to the aircraft: the stores management system, or SMS.
The course includes description of MIL-STD-1760 signals including:
MIL-STD-704 power connections;
MIL-STD-1553 data communications interface;
high and low bandwidth analog signals;
discrete signals; and
fiber optics
Course Objectives:
Upon successful completion of this course , all the attendees will have the capability to do :
MIL-STD-1760 defines the electrical characteristics of the signals at the interface, as well as the connector and pin assignments of all of the signals used in the interface Upon completion of this course, the attendees are be able to:Describe what MIL-STD-1760 is
Understand MIL-STD-1760 characteristics
Describe MIL-STD-1760 architecture
Explain requirements, design and, testing aspects of MIL-STD-1760
Course Outline:
This course will focus on points mentioned at below:
Introduction to MIL-STD-1760
Aircraft/store Configurations
Aircraft Requirements
Mission store Requirements
Carriage store Requirements
Umbilical cable requirements
Power Interface Interrupts
MIL-STD-1760 MIL-STD-1760 Systems Engineering: Requirements, Design, Implementation and Testing
MIL-STD-1760 Requirements
Ask for more information. Visit Tonex.com
https://www.tonex.com/training-courses/mil-1760-training/
Wind tunnels come in several types depending on their design and airflow characteristics. The document describes blow down, atmospheric entry, high enthalpy, and continuous flow wind tunnels. Continuous flow wind tunnels can be open circuit for subsonic or supersonic testing, or closed circuit. Open circuit tunnels work by drawing in air and exhausting it, while closed circuit wind tunnels recirculate the air through a compressor. The different wind tunnel types are used to simulate various flow conditions for testing aircraft and missile components.
The document provides an overview of aircraft structures and their key components. It discusses the fuselage, wings, empennage, landing gear, and powerplants. For each component, it describes the basic design and functions. It also covers important aircraft structural concepts like stressed skin construction, monocoque vs semi-monocoque design, and choices of lightweight metal materials. Overall the document serves as a high-level introduction to aircraft structures and the major structural components of airplanes.
This is Part 1 of 3 covering my work on my Future Deep Strike Aircraft project, to inspire interest in aerospace engineering for the RAeS, the A&SPA(UK) and AIAA.
The document discusses vortex theory and Prandtl's lifting-line theory for analyzing the aerodynamics of finite wings. It introduces key concepts like downwash, trailing vortices, Helmholtz's vortex theorems, and the Biot-Savart law. The lifting-line theory models the wing as a bound vortex filament with varying circulation strength. This allows determining the induced downwash and angle of attack distributions. Prandtl's fundamental equation relates the circulation distribution to the wing geometry and twist. The lifting-line theory provides insights into the relationship between wing shape and lift distribution.
This document provides an overview of materials used in transparent armour systems. It discusses various types of glass like borosilicate glass, fused silica, laminated glass, and toughened glass. It also covers glass ceramics and how they are produced. Transparent ceramics like aluminium oxynitride spinel, single crystal aluminium oxide, and magnesium aluminate spinel are introduced. Polymeric materials such as thermoplastics and thermosets that can be used are mentioned. Finally, it provides a brief overview of the design of transparent armour systems including strike face layer, intermediate layer, and spall layer, and discusses ballistic performance considerations.
The document describes the process of calculating the cooling load of a room using the Cooling Load Temperature Difference (CLTD) Method. It involves calculating the transmission load through the walls and roof by determining their areas, U-values, and CLTD corrections. The solar heat gain through windows is also calculated. Internal loads from lighting, equipment, and occupancy are estimated. The total cooling load is calculated by summing the transmission load, solar gain, internal load, and occupancy load, which comes out to be 9170.97 watts or around 2.5 to 3 tons for air conditioning unit selection.
The document discusses inspection and maintenance procedures for aircraft piston engines. It begins by listing different engine classifications and components like dynamic dampers. It describes steps like checking for oil pressure after starting, performing dimensional inspections to check for wear. Visual inspections are used to find defects. The document then discusses classification of piston engines and components like master articulated rods. It outlines the basic overhaul process and non-destructive testing methods. Finally, it describes inspecting and maintaining engine controls during 100-hour inspections to check for wear and smooth operation.
The document discusses the black box, which consists of the flight data recorder (FDR) and cockpit voice recorder (CVR). It provides a brief history, explaining the first FDR prototype was created in 1956. It describes the construction of black boxes, including their heat-resistant red paint and mounting in the aircraft's tail section. The inside contains the FDR, which records aircraft performance parameters, and the CVR, which records audio from the cockpit. Black boxes use magnetic tapes or solid state technology to store data. They aid in accident investigations by providing audio and data to help determine causes.
Pressure Coefficients on Building Facades for Building SimulationSimScale
While accurate wind pressure coefficients are critical to evaluating building design, most engineering software for energy and thermal analysis oversimplifies treatment of wind pressure, which can adversely impact cooling, ventilation, overheating, and fresh air rates assessments. This presentation shows how SimScale provides accurate calculations of wind pressures, quickly and cost-efficiently, to deliver a more comprehensive evaluation of building performance.
Watch the webinar recording here: https://www.youtube.com/watch?v=VU4-PN9PYDM
Cryogenic rocket engines use cryogenic fuels such as liquid hydrogen and liquid oxygen that are stored at very low temperatures. They provide several advantages including high energy density and producing only water exhaust, but also have challenges like boil off and leakage due to the extreme cold temperatures required. India's first unmanned lunar mission in 2008 failed when the indigenous cryogenic upper stage engine did not ignite as planned. Future rocket technologies being researched include ion engines, nuclear thermal engines, and other alternatives to further space exploration.
The document provides information about gas turbine engines, including their basic mechanics and operation. It discusses the classification of engines, principles of jet propulsion, theories of jet propulsion and gas turbine engines. It also covers the working cycle of gas turbine engines, factors that affect thrust, types of gas turbine engines like turbojet engines, and changes in velocity and pressure during operation.
This document discusses aerospace fasteners from an manufacturing perspective. It describes the types of rivets used in aircraft assembly, including solid and blind rivets. Solid rivets are used when access is available to both sides, while blind rivets are used when one side is inaccessible. The document outlines rivet identification codes and the process for installing solid rivets. Material selection and testing of aerospace fasteners is also summarized.
1. Many factors must be considered when estimating heating and cooling loads for a building, including size, materials, windows, occupancy, equipment, and air infiltration.
2. Sensible heat is direct heat that raises air temperature, while latent heat involves moisture changing phase. Total heat load is the sum of sensible and latent loads.
3. Effective room loads account for bypass air and determine supply air conditions and equipment capacity needs.
Sistem komunikasi merupakan unsur penting dalam pesawat terbang untuk memfasilitasi komunikasi antara pilot dengan menara kontrol darat maupun antar pesawat. Terdapat berbagai jenis sistem komunikasi yang digunakan seperti High Frequency, Very High Frequency, dan Ultra High Frequency untuk berkomunikasi jarak jauh dan dekat. Sistem komunikasi internal juga digunakan untuk memfasilitasi komunikasi antar awak pesawat dan penumpang melalui Public Address system dan Intercom system. Peralatan darur
The document summarizes the evolution of aircraft structures from early designs using wooden ribs and fabric to modern aluminum and composite designs. It describes key structural components such as those that produce lift (wings, airfoils), control (elevators, ailerons, rudders), modify lift (flaps, slats), and hold other components. Early aircraft had open wooden frameworks and fabric coverings while later warplanes used metal tubing and stressed skin construction. Modern jets widely use semi-monocoque construction.
The document provides information about Frankfinn Institute Of Airhostess Training and a student's research project on the current aviation industry scenario. It discusses sources used like the aviation faculty, newspapers, magazines and the internet. It describes Airbus aircraft models from A300 to A380 and their features. It highlights the growth prospects of the Indian aviation sector and ongoing trends. The student gains knowledge about the industry through this research project.
IDTechEx Research: Manned Electric AircraftIDTechEx
About 20 companies make or will soon make electric aircraft. Nearly all are pure electric and fixed wing, the motorised hang glider and the self-launching sailplane being typical, with one hour endurance. A bigger value market being addressed is training planes and bigger still will be hybrid fixed wing and vertical takeoff aircraft hybrid and pure electric with the pure electric ones only managing 30 minutes. In these slides we discuss possible uses, improvements and other types too.
For more information, see http://www.idtechex.com/aircraft.
Slides by Dr. Peter Harrop of IDTechEx.
The document provides information about various Airbus aircraft models from the A300 launched in 1974 to the A380 launched in 2007. It describes the key features and technologies of each aircraft model, including seating configurations, cabin amenities, and flight deck innovations. It also discusses the advantages and disadvantages faced by the aviation industry.
This article discusses the design features of modern Airbus Industry A320neo aircraft, and is the study of the mechanism, directions on the patterns of the impact of new technologies on the emergence and development of a class of long haul passenger aircraft. Ruzmatov P. A. "Design Features of Modern A320PEO Aircraft" Published in International Journal of Trend in Scientific Research and Development (ijtsrd), ISSN: 2456-6470, Volume-6 | Issue-3 , April 2022, URL: https://www.ijtsrd.com/papers/ijtsrd49881.pdf Paper URL: https://www.ijtsrd.com/engineering/aeronautical-engineering/49881/design-features-of-modern-a320peo-aircraft/ruzmatov-p-a
This document is a project report on a car operating on an air motor. It includes chapters on the air motor, its principle of working, material selection and requirements, design, cost estimation, fabrication, maintenance, and future scope. The project was completed by three students under the guidance of a professor, as a practical fulfillment of their mechanical engineering degree.
Newswatch Volume 11 issue 35 - september 16benjacques
The document summarizes several news stories related to the airline industry:
1) Air France KLM approved an order for 110 new long-haul aircraft from Airbus and Boeing that will replace older planes and support growth. This is the first joint order by Air France and KLM and will include A350 and 787 planes.
2) Skymark Airlines selected Rolls-Royce Trent 900 engines to power 6 Airbus A380s on order, citing the engine's superior fuel efficiency and reliability.
3) The International Air Cargo Association urged the EU to suspend its emissions trading scheme for aviation, arguing it oversteps sovereign authority and will impose massive new taxes on the industry without guaranteeing funds will
As environmental and economic reasons drive us towards sustainable transport solutions, Aviation is no different. This presentation introduces you to the reasons, history and technology behind the exciting and fast paced world of E-Flight.
The document provides information on various Airbus aircraft models from the A300 to the A380. It discusses the key features and technological advances of each plane. The A380 in particular is highlighted as the world's largest passenger airliner, capable of carrying 555 passengers. Safety is also emphasized, noting that all Airbus aircraft meet international certification standards and that the A380 can evacuate over 800 passengers within 80 seconds during emergency tests.
The document discusses the air car, a vehicle that runs on compressed air. It stores approximately 90 cubic meters of compressed air in carbon fiber tanks. When the air is released, it pushes the pistons and powers the motor. This provides a zero emissions option for transportation. Some benefits are no pollution, low refueling costs, and not relying on hazardous fuels. Challenges include a limited driving range due to the air tanks heating up and losing pressure over time. However, it could help reduce emissions and fuel costs in the future.
Developing Commercial Vehicles Inspired by NatureAltair
As Germany's largest independent engineering partner to the worldwide automotive industry, EDAG is continuously seeking for new technologies and innovative processes to streamline vehicle development. EDAG has a profound expertise in integrated development and the optimization of vehicles, production facilities, derivatives, and modules. To meet fuel efficiency and emission reduction goals, structurally efficient lightweight designs are demanded in the development of passenger cars and commercial vehicles alike. To fulfill customer demands and to deliver lighter and yet fully functional and validated components in shorter time, EDAG is leveraging its engineering knowledge to combine state-of-the-art computer aided engineering tools, in this case Altair's OptiStruct, with new production technologies such as additive manufacturing. OptiStruct enabled the EDAG engineers to design lightweight and, by being inspired by nature, yet stiff structures of a cabin and a chassis. The components were then manufactured using additive manufacturing methods. To find the optimal solution for the final design the engineers later also conducted multi-physical optimizations, combining strength and crash demands of the vehicle, using an equivalent linear approach. The entire development and manufacturing process for the cabin and chassis structures will be subject of this presentation, showing how a combination of topology optimization and additive manufacturing leads to lighter and stiffer products. The project is a prime example of how mature CAE technology can be adjusted and used in combination with new manufacturing methods to introduce revolutionary structural enhancements within the transportation sector.
Speakers
Andreas Pfeiffer, Development Engineer, EDAG
Detailed program of EUROPEAN DRONE SUMMIT 2019
The EUROPEAN DRONE SUMMIT is an international conference for the European drone industry to explore strategies for the efficient use of UAS. Key figures from the fields of politics, law-making, research, industry and business come together to discuss the way forward for achieving acceptance and devising solutions for the safe and effective commercial use of unmanned aircraft in Europe.
The EUROPEAN DRONE SUMMIT is the European platform for discussing the current needs of the UAS industry, both for newcomers with an interest in the industry as well as long-time experts. Meetings on special topics cover business models and strategies as well as use cases, whereby the highlights will be
- Safety and security using UAS as well as counter drone systems
- Integrating UAS into airspace
- Vertical mobility using UAS in urban environments
- Services backed up by UAS – rescue and emergency response services
Our top speakers will present different opportunities to connect existing business concepts with boosting new technologies.
The EUROPEAN DRONE SUMMIT is the place to learn how to implement best the advantages of UAS in your business and avoid common mistakes. Start a dialogue with an eminent network of distinguished drone experts.
Electric flight – Potential and Limitations (2012)Andrew Gelston
This document discusses the potential and limitations of electric flight. It begins by providing historical context on electric flight dating back to 1940. It then compares conventional propulsion systems that burn fuel to electric propulsion systems, noting batteries and fuel cells as two main energy storage options for electric systems. Batteries currently have much lower mass-specific energy density than kerosene-based fuels, presenting a major challenge. While electric propulsion systems can have higher efficiencies than combustion systems, the mass of current battery technology limits its application for aircraft. Advances in battery technology would be needed to overcome this limitation.
PNEUMATICALLY DRIVEN VEHICLE WITH RECHARGEABLE BATTERY DURING DRIVE- AN EXPLO...IAEME Publication
Energy can be stored in compressed air form at very high pressures running to a few dozens of atmospheres. The compressed air properly controlled, timed, released through pressure regulators etc., can be used to run Pistons that in turn can drive an engine. This compressed air can be furnished through already available accumulator as well as through an on board compressor. A battery which gets duly charged as per needs on line in a running vehicle through solar energy depending on availability or offline when the vehicle is stationary can support to run a d.c motor too which in turn can drive the vehicle. This works as a redundant system to attend the drive power needs or in managing to reach destinations
Curtis Tomlinson is a highly qualified and experienced aircraft project engineer with over 30 years of experience working on a wide variety of commercial and military aircraft. He has extensive experience managing projects and working on maintenance, modifications, and repairs of aircraft. Some of his most recent projects include working as a subject matter expert on projects to develop training modules for aircraft maintenance and converting Lynx helicopters into Wildcat replicas.
Yin Sun Shell - Shell (Projects & Technology)GuidoBacker1
This document discusses the concept of a flexible offshore wind hydrogen power plant module. It proposes using offshore wind farms to produce hydrogen through electrolysis, which could help balance the grid and provide energy storage. The key challenges addressed are developing an optimal electrical architecture and controllable electrolysis for hydrogen production. Various transmission options like high voltage AC and DC are considered. The goal is an integrated system that can flexibly control multiple energy flows to meet grid needs.
The document discusses potential future innovations in aircraft design and technology over multiple paragraphs. Some of the key innovations discussed include:
1) Assisted take-offs using electromagnetic motors or inductive circuits to accelerate aircraft on a track system, removing the need for landing gear.
2) The development of detachable passenger cabins with parachutes for emergency scenarios.
3) The use of bionic structures and biopolymer membranes that could make aircraft lighter, more fuel efficient, and provide passengers with panoramic views.
4) Integrated neural networks and smart/self-cleaning materials that could make aircraft systems more efficient and reduce weight.
5) Engine technologies like those being developed by Reaction
What will air travel look like in 2035 and beyond? Learn more about the latest trends in the aviation industry and how your flying experience will change over the next few decades.
Comparative analysis between traditional aquaponics and reconstructed aquapon...bijceesjournal
The aquaponic system of planting is a method that does not require soil usage. It is a method that only needs water, fish, lava rocks (a substitute for soil), and plants. Aquaponic systems are sustainable and environmentally friendly. Its use not only helps to plant in small spaces but also helps reduce artificial chemical use and minimizes excess water use, as aquaponics consumes 90% less water than soil-based gardening. The study applied a descriptive and experimental design to assess and compare conventional and reconstructed aquaponic methods for reproducing tomatoes. The researchers created an observation checklist to determine the significant factors of the study. The study aims to determine the significant difference between traditional aquaponics and reconstructed aquaponics systems propagating tomatoes in terms of height, weight, girth, and number of fruits. The reconstructed aquaponics system’s higher growth yield results in a much more nourished crop than the traditional aquaponics system. It is superior in its number of fruits, height, weight, and girth measurement. Moreover, the reconstructed aquaponics system is proven to eliminate all the hindrances present in the traditional aquaponics system, which are overcrowding of fish, algae growth, pest problems, contaminated water, and dead fish.
KuberTENes Birthday Bash Guadalajara - K8sGPT first impressionsVictor Morales
K8sGPT is a tool that analyzes and diagnoses Kubernetes clusters. This presentation was used to share the requirements and dependencies to deploy K8sGPT in a local environment.
Use PyCharm for remote debugging of WSL on a Windo cf5c162d672e4e58b4dde5d797...shadow0702a
This document serves as a comprehensive step-by-step guide on how to effectively use PyCharm for remote debugging of the Windows Subsystem for Linux (WSL) on a local Windows machine. It meticulously outlines several critical steps in the process, starting with the crucial task of enabling permissions, followed by the installation and configuration of WSL.
The guide then proceeds to explain how to set up the SSH service within the WSL environment, an integral part of the process. Alongside this, it also provides detailed instructions on how to modify the inbound rules of the Windows firewall to facilitate the process, ensuring that there are no connectivity issues that could potentially hinder the debugging process.
The document further emphasizes on the importance of checking the connection between the Windows and WSL environments, providing instructions on how to ensure that the connection is optimal and ready for remote debugging.
It also offers an in-depth guide on how to configure the WSL interpreter and files within the PyCharm environment. This is essential for ensuring that the debugging process is set up correctly and that the program can be run effectively within the WSL terminal.
Additionally, the document provides guidance on how to set up breakpoints for debugging, a fundamental aspect of the debugging process which allows the developer to stop the execution of their code at certain points and inspect their program at those stages.
Finally, the document concludes by providing a link to a reference blog. This blog offers additional information and guidance on configuring the remote Python interpreter in PyCharm, providing the reader with a well-rounded understanding of the process.
Software Engineering and Project Management - Introduction, Modeling Concepts...Prakhyath Rai
Introduction, Modeling Concepts and Class Modeling: What is Object orientation? What is OO development? OO Themes; Evidence for usefulness of OO development; OO modeling history. Modeling
as Design technique: Modeling, abstraction, The Three models. Class Modeling: Object and Class Concept, Link and associations concepts, Generalization and Inheritance, A sample class model, Navigation of class models, and UML diagrams
Building the Analysis Models: Requirement Analysis, Analysis Model Approaches, Data modeling Concepts, Object Oriented Analysis, Scenario-Based Modeling, Flow-Oriented Modeling, class Based Modeling, Creating a Behavioral Model.
Discover the latest insights on Data Driven Maintenance with our comprehensive webinar presentation. Learn about traditional maintenance challenges, the right approach to utilizing data, and the benefits of adopting a Data Driven Maintenance strategy. Explore real-world examples, industry best practices, and innovative solutions like FMECA and the D3M model. This presentation, led by expert Jules Oudmans, is essential for asset owners looking to optimize their maintenance processes and leverage digital technologies for improved efficiency and performance. Download now to stay ahead in the evolving maintenance landscape.
CHINA’S GEO-ECONOMIC OUTREACH IN CENTRAL ASIAN COUNTRIES AND FUTURE PROSPECTjpsjournal1
The rivalry between prominent international actors for dominance over Central Asia's hydrocarbon
reserves and the ancient silk trade route, along with China's diplomatic endeavours in the area, has been
referred to as the "New Great Game." This research centres on the power struggle, considering
geopolitical, geostrategic, and geoeconomic variables. Topics including trade, political hegemony, oil
politics, and conventional and nontraditional security are all explored and explained by the researcher.
Using Mackinder's Heartland, Spykman Rimland, and Hegemonic Stability theories, examines China's role
in Central Asia. This study adheres to the empirical epistemological method and has taken care of
objectivity. This study analyze primary and secondary research documents critically to elaborate role of
china’s geo economic outreach in central Asian countries and its future prospect. China is thriving in trade,
pipeline politics, and winning states, according to this study, thanks to important instruments like the
Shanghai Cooperation Organisation and the Belt and Road Economic Initiative. According to this study,
China is seeing significant success in commerce, pipeline politics, and gaining influence on other
governments. This success may be attributed to the effective utilisation of key tools such as the Shanghai
Cooperation Organisation and the Belt and Road Economic Initiative.
Optimizing Gradle Builds - Gradle DPE Tour Berlin 2024Sinan KOZAK
Sinan from the Delivery Hero mobile infrastructure engineering team shares a deep dive into performance acceleration with Gradle build cache optimizations. Sinan shares their journey into solving complex build-cache problems that affect Gradle builds. By understanding the challenges and solutions found in our journey, we aim to demonstrate the possibilities for faster builds. The case study reveals how overlapping outputs and cache misconfigurations led to significant increases in build times, especially as the project scaled up with numerous modules using Paparazzi tests. The journey from diagnosing to defeating cache issues offers invaluable lessons on maintaining cache integrity without sacrificing functionality.
Electric vehicle and photovoltaic advanced roles in enhancing the financial p...IJECEIAES
Climate change's impact on the planet forced the United Nations and governments to promote green energies and electric transportation. The deployments of photovoltaic (PV) and electric vehicle (EV) systems gained stronger momentum due to their numerous advantages over fossil fuel types. The advantages go beyond sustainability to reach financial support and stability. The work in this paper introduces the hybrid system between PV and EV to support industrial and commercial plants. This paper covers the theoretical framework of the proposed hybrid system including the required equation to complete the cost analysis when PV and EV are present. In addition, the proposed design diagram which sets the priorities and requirements of the system is presented. The proposed approach allows setup to advance their power stability, especially during power outages. The presented information supports researchers and plant owners to complete the necessary analysis while promoting the deployment of clean energy. The result of a case study that represents a dairy milk farmer supports the theoretical works and highlights its advanced benefits to existing plants. The short return on investment of the proposed approach supports the paper's novelty approach for the sustainable electrical system. In addition, the proposed system allows for an isolated power setup without the need for a transmission line which enhances the safety of the electrical network