A gas turbine uses a gaseous working fluid to generate mechanical power that can power industrial devices. It has three main parts - an air compressor, combustion chamber, and turbine. The air is compressed in the compressor, mixed with fuel and ignited in the combustion chamber, and the hot gases spin the turbine to generate power. Some applications of gas turbines include aviation, power generation, and the oil and gas industry. The efficiency of gas turbines is typically 20-30% compared to 38-48% for steam power plants.
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
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The document discusses gas turbine technology. It begins by defining a gas turbine as a machine that delivers mechanical power using a gaseous working fluid. It then discusses the main components of a gas turbine - the compressor, combustion chamber, and turbine. The document covers various gas turbine cycles including open and closed cycles. It also discusses ways to improve gas turbine efficiency such as intercooling, reheating, and regeneration. The document provides an overview of gas turbine applications and operating principles.
The document discusses various factors that affect the efficiency of internal combustion engines such as specific heat, dissociation, premixed vs non-premixed fuel charges, and different types of losses in actual engine cycles compared to ideal cycles. It notes that the actual efficiency of a good engine is around 25% of the estimated efficiency from the ideal air standard cycle due to losses from factors like heat transfer, combustion, pumping, and blow-by. Fuel-air ratio can impact maximum power output due to chemical equilibrium losses. Variable specific heats can increase maximum pressure but decrease maximum temperature compared to constant specific heats.
This document discusses steam power plant cycles, including ideal cycles and actual cycles. It covers the Carnot cycle, limitations of the Carnot cycle, the Rankine cycle, analysis of the ideal Rankine cycle, deviations of the actual cycle from the ideal cycle, ways to increase the efficiency of the Rankine cycle such as lowering condenser pressure, superheating steam, and increasing boiler pressure. It also discusses reheat cycles, methods of reheating such as gas reheating and live steam reheating, and regenerative cycles using open and closed feedwater heaters.
The document discusses different methods of governing steam turbines to maintain a constant rotational speed despite varying loads. Throttle governing reduces steam pressure through a restricted passage before entering the turbine. Nozzle governing opens and closes sets of nozzles to control steam flow. Bypass governing introduces steam into later turbine stages during overloads. Combination governing uses two methods, typically bypass and nozzle. Electro-hydraulic governing uses electronic, hydraulic, and mechanical components to precisely control steam flow and allow synchronization to power grids for load and frequency regulation.
This document presents information on gas turbine cycles. It discusses open and closed cycle gas turbines, with open cycle directly discharging exhaust to the atmosphere and closed cycle recirculating working medium. It also describes how intercooling, reheating, and regeneration can increase the net work output of gas turbine cycles by reducing compressor work and increasing turbine work. A T-S diagram is included to illustrate an ideal gas turbine cycle with these modifications.
This document provides an overview of the key principles covered in the textbook "Principles of Turbomachinery" by R.K. Turton. It discusses fundamental concepts like the Euler equation and its applications to different turbomachines. It also introduces compressible flow theory and illustrates examples of how to apply the principles to radial outflow machines, axial pumps/turbines, and compressible flow problems. The overview concludes by noting that subsequent chapters will apply these principles to specific machine types and cover additional topics like scaling laws, cavitation, blade design of axial and radial machines, and special applications.
A gas turbine uses a gaseous working fluid to generate mechanical power that can power industrial devices. It has three main parts - an air compressor, combustion chamber, and turbine. The air is compressed in the compressor, mixed with fuel and ignited in the combustion chamber, and the hot gases spin the turbine to generate power. Some applications of gas turbines include aviation, power generation, and the oil and gas industry. The efficiency of gas turbines is typically 20-30% compared to 38-48% for steam power plants.
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
The document discusses gas turbine technology. It begins by defining a gas turbine as a machine that delivers mechanical power using a gaseous working fluid. It then discusses the main components of a gas turbine - the compressor, combustion chamber, and turbine. The document covers various gas turbine cycles including open and closed cycles. It also discusses ways to improve gas turbine efficiency such as intercooling, reheating, and regeneration. The document provides an overview of gas turbine applications and operating principles.
The document discusses various factors that affect the efficiency of internal combustion engines such as specific heat, dissociation, premixed vs non-premixed fuel charges, and different types of losses in actual engine cycles compared to ideal cycles. It notes that the actual efficiency of a good engine is around 25% of the estimated efficiency from the ideal air standard cycle due to losses from factors like heat transfer, combustion, pumping, and blow-by. Fuel-air ratio can impact maximum power output due to chemical equilibrium losses. Variable specific heats can increase maximum pressure but decrease maximum temperature compared to constant specific heats.
This document discusses steam power plant cycles, including ideal cycles and actual cycles. It covers the Carnot cycle, limitations of the Carnot cycle, the Rankine cycle, analysis of the ideal Rankine cycle, deviations of the actual cycle from the ideal cycle, ways to increase the efficiency of the Rankine cycle such as lowering condenser pressure, superheating steam, and increasing boiler pressure. It also discusses reheat cycles, methods of reheating such as gas reheating and live steam reheating, and regenerative cycles using open and closed feedwater heaters.
The document discusses different methods of governing steam turbines to maintain a constant rotational speed despite varying loads. Throttle governing reduces steam pressure through a restricted passage before entering the turbine. Nozzle governing opens and closes sets of nozzles to control steam flow. Bypass governing introduces steam into later turbine stages during overloads. Combination governing uses two methods, typically bypass and nozzle. Electro-hydraulic governing uses electronic, hydraulic, and mechanical components to precisely control steam flow and allow synchronization to power grids for load and frequency regulation.
This document presents information on gas turbine cycles. It discusses open and closed cycle gas turbines, with open cycle directly discharging exhaust to the atmosphere and closed cycle recirculating working medium. It also describes how intercooling, reheating, and regeneration can increase the net work output of gas turbine cycles by reducing compressor work and increasing turbine work. A T-S diagram is included to illustrate an ideal gas turbine cycle with these modifications.
This document provides an overview of the key principles covered in the textbook "Principles of Turbomachinery" by R.K. Turton. It discusses fundamental concepts like the Euler equation and its applications to different turbomachines. It also introduces compressible flow theory and illustrates examples of how to apply the principles to radial outflow machines, axial pumps/turbines, and compressible flow problems. The overview concludes by noting that subsequent chapters will apply these principles to specific machine types and cover additional topics like scaling laws, cavitation, blade design of axial and radial machines, and special applications.
Turbines work by converting the kinetic energy of a moving fluid like water, steam, gas or wind into mechanical rotational energy. There are different types of turbines that are designed based on how the fluid interacts with the turbine blades including impulse turbines where the fluid hits the blades at high speed, and reaction turbines where the pressure of the fluid changes as it passes through the rotor blades. Common types of turbines include water turbines like the Pelton, Francis and Kaplan turbines, steam turbines used in power plants, gas turbines that power aircraft and generators, and wind turbines that convert wind energy into electricity.
1) A reciprocating compressor takes in air or gas at low pressure and compresses it using pistons moving back and forth in cylinders.
2) It is classified based on design, number of stages, pressure ratio, capacity, number of cylinders, type of fluid, and cooling method.
3) In single stage reciprocating compression, air is drawn into the cylinder on the inward stroke and compressed on the outward stroke through inlet and outlet valves.
Gas turbines have three main parts - an air compressor, combustion chamber, and turbine. The air compressor increases the pressure of air that is mixed with fuel in the combustion chamber and ignited. This powers the turbine, which can generate mechanical power or thrust. There are two main types - open cycle gas turbines that exhaust air to the atmosphere, and closed cycle gas turbines that recirculate the working fluid through a cooler before returning it to the compressor. Methods to improve gas turbine efficiency include intercooling the compressed air between compression stages, reheating the gas before a secondary expansion turbine, and regenerating heat from the exhaust to preheat the incoming compressed air.
This document provides information about steam turbines, including:
- Steam turbines convert the thermal energy of steam into rotational mechanical energy through a series of stages, with modern turbines invented by Charles Parsons in 1884.
- About 90% of electricity in the US is generated using steam turbines, as the rotary motion produced is well-suited to drive electrical generators.
- Steam turbines come in a wide range of sizes, from small <0.75 kW units for pumps and compressors, to large 1,500 MW turbines for electricity generation. They can be classified in various ways such as by flow direction, number of stages, steam pressure, or governing method.
The Whitworth quick return mechanism is used in slotters to convert the rotary motion of an electric motor into reciprocating motion of the ram. It allows the return stroke of the ram to be faster than the cutting stroke. The mechanism uses a bull gear connected to a crank plate through an eccentrically mounted pin. As the bull gear rotates, the sliding movement of the crank pin along the crank plate's slot converts it into reciprocating motion of the connecting rod and ram. The return stroke angle is less than the cutting stroke angle, allowing the ram to move faster on its return. Quick return mechanisms are widely used in machines like shapers, screw presses, and saws.
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.
The document discusses combustion in diesel engines. It describes the four stages of combustion: ignition delay period, rapid combustion period, controlled combustion period, and after-burning period. It explains factors that affect the ignition delay period such as compression ratio, engine speed, fuel quality, and intake conditions. The document also discusses knock in diesel engines and different combustion chamber designs for diesel engines, including direct injection and indirect injection types.
Simple description about gas turbine. Where you are going to know about its classification,advantages and disadvantages also.Here also you can find-out where it is actually usages.
Pneumatics: Shuttle, Twin pressure, Quick Exhaust, Time Delay, FRLAbhishek Patange
The document discusses various components used in pneumatic systems including logic gates, valves, and FRL units. It begins with explanations of shuttle valves and twin pressure/dual pressure valves that can function as OR and AND logic gates respectively. Various valves are then discussed such as time delay valves, quick exhaust valves, and their applications. Speed control methods and the stick-slip effect in pneumatics are also covered. Finally, the construction and working of the main components of an FRL (filter, regulator, lubricator) unit are explained in detail with diagrams.
Natural draught is produced by a chimney and provides ventilation for boiler systems. The height and diameter of a chimney can be calculated based on factors like flue gas temperature, ambient temperature, and air-fuel ratio. For maximum discharge of hot gases, the flue gas temperature should be slightly higher than ambient temperature. Chimneys provide advantages like no external power requirements but have limitations like low efficiency below 1%. Boiler performance is quantified by equivalent evaporation and efficiency, which allow standardization based on feed water temperature and pressure.
This document appears to be a submission from a student named Saurabh Negi to an unknown recipient for a B.Tech (M.E.) program. It discusses thermal efficiency, which is defined as the ratio of work to heat in thermodynamics calculations.
The document presents information on a bootstrap air cooling system suitable for aircraft. It consists of two heat exchangers, a secondary compressor driven by a turbine, and uses ram air and compression to cool and circulate air. Ambient air is compressed by the main aircraft compressor then cooled in an air cooler before further compression and cooling. It is then expanded through a turbine to provide cooled air to the aircraft cabin. Advantages are that air is readily available, non-toxic, and pressures are low. A limitation is that it requires aircraft flight for ram air cooling and is not suitable for ground use without an additional fan.
This document provides an overview of a presentation on root blowers. It defines an air compressor as a device that takes in gas or vapor, increases its pressure, and delivers it at high pressure. It notes that a blower is one type of air compressor. The document then focuses on root blowers, describing their working mechanism where lobes trap air and increase its pressure before delivery. It includes videos demonstrating two-lobe and three-lobe root blowers. The document outlines advantages of root blowers like quick attainment of full revolutions and lower partial-load power demand. It also lists some applications for root blowers such as in drying, paper industry processes, and dust collection systems.
Fectors Affecting the efficiency of Rankine cycleRushikesh Raval
This document discusses three thermodynamic variables that affect the efficiency and work output of a Rankine cycle: (1) superheating of steam, (2) boiler pressure, and (3) exhaust steam pressure. Superheating steam increases efficiency by raising the average heat addition temperature while keeping the average heat rejection temperature the same. Increasing boiler pressure raises net work and lowers heat rejected, improving efficiency. Reducing condenser pressure raises net work and efficiency by lowering the average heat rejection temperature.
Boiler draught refers to the pressure difference between the air inside a boiler furnace and the outside air, which causes the flow of air and flue gases through the boiler. This pressure difference is necessary for proper combustion of fuel and removal of flue gases. Draught can be produced naturally through the use of a chimney, or artificially through mechanical fans or steam jets. Forced draught uses a fan before the furnace to push air and gases through, while induced draught uses a fan at the chimney to pull gases through. Balanced draught combines the two. Mechanical draught allows better control of the pressure but has higher costs than natural or steam jet draught.
The document provides lecture notes on steam nozzles and power plants. It discusses:
1) The basic components and energy conversion process in thermal power plants, including the Rankine cycle in which water is heated to steam to power a turbine and generator.
2) The history and development of steam turbines, from early aeolipile devices to modern turbines invented by Charles Parsons in 1884.
3) How energy is converted in steam turbines via nozzles that accelerate steam to high velocity to impulse turbine blades and produce rotation.
4) Details on nozzle types, flow properties, relationships between area, velocity and pressure, and equations for calculating velocity from enthalpy change.
This document discusses different types of steam turbines and their operating principles. It describes impulse turbines where steam expands within nozzles and does not change pressure as it passes over blades. Reaction turbines gradually decrease pressure as steam passes over fixed and moving blades. Compounding methods are also presented, including velocity compounding using multiple blade rings, pressure compounding with nozzle stages, and pressure-velocity compounding combining both methods. The document aims to explain steam turbine design and operation.
This document provides information about axial flow compressors including:
- They consist of multiple rows of fixed and moving blades that continuously pressurize gas flowing parallel to the axis of rotation, achieving high efficiency and mass flow.
- Each pair of rotor and stator blades constitutes a pressure stage, with typical single stage pressure increases of 15-60% and multiple stages used to achieve higher overall pressure ratios.
- Stalling and surging refer to unstable flow conditions that reduce compressor performance and must be avoided through proper design and operation.
- They find applications in industries like oil refining and power generation as well as aircraft engines due to their high performance capabilities.
The various forces acts on the reciprocating parts of an engine.
The resultant of all the forces acting on the body of the engine due to inertia forces only is known as unbalanced force or shaking force.
This document discusses various types of machine balancing. It begins by defining static and dynamic balancing. Static balancing deals with balancing forces when a machine is at rest, while dynamic balancing deals with balancing forces during motion. It then discusses balancing of single and multiple rotating masses, as well as reciprocating masses. Methods for analytically and graphically balancing multiple masses are provided. The document also covers balancing of engines with different cylinder configurations, including inline, V-shaped, radial, and locomotive engines. Partial balancing techniques are discussed for reducing unbalanced forces in locomotives.
Brayton or Joule cycle -P-V diagram and thermal efficiency. Construction and working of gas turbine i] Open cycle ii] Closed cycle gas turbine, simple circuit, Comparison, P-V & T-S diagramTurbojet and Turboprop Engine and Application
power generation using stirling engine and solar energyabhishek sharma
This document describes a project to generate electricity using a beta Stirling engine powered by solar energy. It discusses how Stirling engines work using the expansion and compression of gases, and how a beta Stirling engine was designed. Parabolic dishes would be used to concentrate solar rays to heat the engine. The document outlines the process for analyzing and designing the Stirling engine, including first and second order analyses and optimization of parameters. Software images show designs of the parabolic dishes and engine components. Analysis results predict efficiencies from 31-50% and power outputs ranging from 210-627 watts.
Turbines work by converting the kinetic energy of a moving fluid like water, steam, gas or wind into mechanical rotational energy. There are different types of turbines that are designed based on how the fluid interacts with the turbine blades including impulse turbines where the fluid hits the blades at high speed, and reaction turbines where the pressure of the fluid changes as it passes through the rotor blades. Common types of turbines include water turbines like the Pelton, Francis and Kaplan turbines, steam turbines used in power plants, gas turbines that power aircraft and generators, and wind turbines that convert wind energy into electricity.
1) A reciprocating compressor takes in air or gas at low pressure and compresses it using pistons moving back and forth in cylinders.
2) It is classified based on design, number of stages, pressure ratio, capacity, number of cylinders, type of fluid, and cooling method.
3) In single stage reciprocating compression, air is drawn into the cylinder on the inward stroke and compressed on the outward stroke through inlet and outlet valves.
Gas turbines have three main parts - an air compressor, combustion chamber, and turbine. The air compressor increases the pressure of air that is mixed with fuel in the combustion chamber and ignited. This powers the turbine, which can generate mechanical power or thrust. There are two main types - open cycle gas turbines that exhaust air to the atmosphere, and closed cycle gas turbines that recirculate the working fluid through a cooler before returning it to the compressor. Methods to improve gas turbine efficiency include intercooling the compressed air between compression stages, reheating the gas before a secondary expansion turbine, and regenerating heat from the exhaust to preheat the incoming compressed air.
This document provides information about steam turbines, including:
- Steam turbines convert the thermal energy of steam into rotational mechanical energy through a series of stages, with modern turbines invented by Charles Parsons in 1884.
- About 90% of electricity in the US is generated using steam turbines, as the rotary motion produced is well-suited to drive electrical generators.
- Steam turbines come in a wide range of sizes, from small <0.75 kW units for pumps and compressors, to large 1,500 MW turbines for electricity generation. They can be classified in various ways such as by flow direction, number of stages, steam pressure, or governing method.
The Whitworth quick return mechanism is used in slotters to convert the rotary motion of an electric motor into reciprocating motion of the ram. It allows the return stroke of the ram to be faster than the cutting stroke. The mechanism uses a bull gear connected to a crank plate through an eccentrically mounted pin. As the bull gear rotates, the sliding movement of the crank pin along the crank plate's slot converts it into reciprocating motion of the connecting rod and ram. The return stroke angle is less than the cutting stroke angle, allowing the ram to move faster on its return. Quick return mechanisms are widely used in machines like shapers, screw presses, and saws.
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.
The document discusses combustion in diesel engines. It describes the four stages of combustion: ignition delay period, rapid combustion period, controlled combustion period, and after-burning period. It explains factors that affect the ignition delay period such as compression ratio, engine speed, fuel quality, and intake conditions. The document also discusses knock in diesel engines and different combustion chamber designs for diesel engines, including direct injection and indirect injection types.
Simple description about gas turbine. Where you are going to know about its classification,advantages and disadvantages also.Here also you can find-out where it is actually usages.
Pneumatics: Shuttle, Twin pressure, Quick Exhaust, Time Delay, FRLAbhishek Patange
The document discusses various components used in pneumatic systems including logic gates, valves, and FRL units. It begins with explanations of shuttle valves and twin pressure/dual pressure valves that can function as OR and AND logic gates respectively. Various valves are then discussed such as time delay valves, quick exhaust valves, and their applications. Speed control methods and the stick-slip effect in pneumatics are also covered. Finally, the construction and working of the main components of an FRL (filter, regulator, lubricator) unit are explained in detail with diagrams.
Natural draught is produced by a chimney and provides ventilation for boiler systems. The height and diameter of a chimney can be calculated based on factors like flue gas temperature, ambient temperature, and air-fuel ratio. For maximum discharge of hot gases, the flue gas temperature should be slightly higher than ambient temperature. Chimneys provide advantages like no external power requirements but have limitations like low efficiency below 1%. Boiler performance is quantified by equivalent evaporation and efficiency, which allow standardization based on feed water temperature and pressure.
This document appears to be a submission from a student named Saurabh Negi to an unknown recipient for a B.Tech (M.E.) program. It discusses thermal efficiency, which is defined as the ratio of work to heat in thermodynamics calculations.
The document presents information on a bootstrap air cooling system suitable for aircraft. It consists of two heat exchangers, a secondary compressor driven by a turbine, and uses ram air and compression to cool and circulate air. Ambient air is compressed by the main aircraft compressor then cooled in an air cooler before further compression and cooling. It is then expanded through a turbine to provide cooled air to the aircraft cabin. Advantages are that air is readily available, non-toxic, and pressures are low. A limitation is that it requires aircraft flight for ram air cooling and is not suitable for ground use without an additional fan.
This document provides an overview of a presentation on root blowers. It defines an air compressor as a device that takes in gas or vapor, increases its pressure, and delivers it at high pressure. It notes that a blower is one type of air compressor. The document then focuses on root blowers, describing their working mechanism where lobes trap air and increase its pressure before delivery. It includes videos demonstrating two-lobe and three-lobe root blowers. The document outlines advantages of root blowers like quick attainment of full revolutions and lower partial-load power demand. It also lists some applications for root blowers such as in drying, paper industry processes, and dust collection systems.
Fectors Affecting the efficiency of Rankine cycleRushikesh Raval
This document discusses three thermodynamic variables that affect the efficiency and work output of a Rankine cycle: (1) superheating of steam, (2) boiler pressure, and (3) exhaust steam pressure. Superheating steam increases efficiency by raising the average heat addition temperature while keeping the average heat rejection temperature the same. Increasing boiler pressure raises net work and lowers heat rejected, improving efficiency. Reducing condenser pressure raises net work and efficiency by lowering the average heat rejection temperature.
Boiler draught refers to the pressure difference between the air inside a boiler furnace and the outside air, which causes the flow of air and flue gases through the boiler. This pressure difference is necessary for proper combustion of fuel and removal of flue gases. Draught can be produced naturally through the use of a chimney, or artificially through mechanical fans or steam jets. Forced draught uses a fan before the furnace to push air and gases through, while induced draught uses a fan at the chimney to pull gases through. Balanced draught combines the two. Mechanical draught allows better control of the pressure but has higher costs than natural or steam jet draught.
The document provides lecture notes on steam nozzles and power plants. It discusses:
1) The basic components and energy conversion process in thermal power plants, including the Rankine cycle in which water is heated to steam to power a turbine and generator.
2) The history and development of steam turbines, from early aeolipile devices to modern turbines invented by Charles Parsons in 1884.
3) How energy is converted in steam turbines via nozzles that accelerate steam to high velocity to impulse turbine blades and produce rotation.
4) Details on nozzle types, flow properties, relationships between area, velocity and pressure, and equations for calculating velocity from enthalpy change.
This document discusses different types of steam turbines and their operating principles. It describes impulse turbines where steam expands within nozzles and does not change pressure as it passes over blades. Reaction turbines gradually decrease pressure as steam passes over fixed and moving blades. Compounding methods are also presented, including velocity compounding using multiple blade rings, pressure compounding with nozzle stages, and pressure-velocity compounding combining both methods. The document aims to explain steam turbine design and operation.
This document provides information about axial flow compressors including:
- They consist of multiple rows of fixed and moving blades that continuously pressurize gas flowing parallel to the axis of rotation, achieving high efficiency and mass flow.
- Each pair of rotor and stator blades constitutes a pressure stage, with typical single stage pressure increases of 15-60% and multiple stages used to achieve higher overall pressure ratios.
- Stalling and surging refer to unstable flow conditions that reduce compressor performance and must be avoided through proper design and operation.
- They find applications in industries like oil refining and power generation as well as aircraft engines due to their high performance capabilities.
The various forces acts on the reciprocating parts of an engine.
The resultant of all the forces acting on the body of the engine due to inertia forces only is known as unbalanced force or shaking force.
This document discusses various types of machine balancing. It begins by defining static and dynamic balancing. Static balancing deals with balancing forces when a machine is at rest, while dynamic balancing deals with balancing forces during motion. It then discusses balancing of single and multiple rotating masses, as well as reciprocating masses. Methods for analytically and graphically balancing multiple masses are provided. The document also covers balancing of engines with different cylinder configurations, including inline, V-shaped, radial, and locomotive engines. Partial balancing techniques are discussed for reducing unbalanced forces in locomotives.
Brayton or Joule cycle -P-V diagram and thermal efficiency. Construction and working of gas turbine i] Open cycle ii] Closed cycle gas turbine, simple circuit, Comparison, P-V & T-S diagramTurbojet and Turboprop Engine and Application
power generation using stirling engine and solar energyabhishek sharma
This document describes a project to generate electricity using a beta Stirling engine powered by solar energy. It discusses how Stirling engines work using the expansion and compression of gases, and how a beta Stirling engine was designed. Parabolic dishes would be used to concentrate solar rays to heat the engine. The document outlines the process for analyzing and designing the Stirling engine, including first and second order analyses and optimization of parameters. Software images show designs of the parabolic dishes and engine components. Analysis results predict efficiencies from 31-50% and power outputs ranging from 210-627 watts.
Gas turbines work by compressing air, combusting fuel with the compressed air, and expanding the hot combustion gases through turbine blades to produce power. The expanded gases then exit through a nozzle. The turbine drives the compressor. Common applications include aircraft jet engines, power generation, and marine propulsion. Gas turbines can be open or closed cycle. Closed cycle turbines circulate the working fluid through the system while open cycle turbines exhaust the gases to the atmosphere after expansion. Regeneration and reheating can improve the efficiency of gas turbines. Jet engines like turbojets and turbofans use gas turbine principles to provide propulsive thrust. Ramjets rely solely on ram compression for combustion instead of using a compressor.
This document provides information about a green engine, which is a type of internal combustion engine that aims to reduce emissions. It has a six-phase working principle of intake, compression, mixing, combustion, power, and exhaust. This allows for complete fuel mixing and burning, resulting in near-zero emissions. The green engine has higher efficiency than conventional engines and can run on multiple fuel types. It has benefits like reduced size, weight, emissions, and noise compared to piston engines. Research is ongoing but it shows potential for use in various industries and applications.
1) Gas turbine power plants work by compressing air, mixing it with fuel and igniting it to spin a turbine. The turbine powers a generator and compressor.
2) Open cycle plants draw in air, exhaust it out. Closed cycle plants circulate a working fluid. Improving open cycle efficiency involves regeneration, reheating, or intercooling.
3) Combining gas turbines with steam plants improves efficiency by using exhaust heat to generate steam. Combining with diesels involves turbocharging, a gas generator, or a compound engine configuration.
The document discusses the history and working principles of the Stirling engine, an external combustion engine invented in 1816 by Robert Stirling as a safer alternative to steam engines. It describes the ideal Stirling cycle of isothermal expansion and compression processes separated by constant volume heat transfer. The key components of Stirling engines are identified as the working gas, heat exchangers, displacer mechanism, regenerator, and expansion/compression mechanism. Different types of Stirling engines - alpha and beta - are also summarized. Applications highlighted include using solar-powered Stirling engines for water pumping in rural areas.
Gas turbines work by compressing air, mixing it with fuel, and igniting the mixture to produce hot gases. These gases are used to spin a turbine, generating mechanical power. There are two main types - open cycle plants which exhaust gases to the atmosphere, and closed cycle plants which circulate working fluid. Gas turbines find application in aviation, power generation, and marine propulsion due to their compact size and ability to use various fuels.
This document provides an overview of a gas turbine power station in Uran, India. It discusses the key components of the power plant including the filter house, compressor, combustion chamber, gas turbine, generator, waste heat recovery plant, boiler, steam turbine, air cooled condenser, and transformer. It also discusses the starting frequency converter, gas skid, fuel management, and concludes by thanking those involved in the training project.
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.
The document discusses strategies to increase the efficiency of combined cycle power plants beyond 60% without new gas turbine technology. It proposes optimizing heat recovery steam generators (HRSGs) with dual or triple pressure levels, increasing steam turbine output by up to 13%. Regeneration and reheat cycles for the gas turbine are also suggested to further improve efficiency to 65%. The paper analyzes these methods for maximizing combined cycle plant efficiency.
This document describes a proposed system to generate electricity from industrial waste heat or heat generated from burning waste materials. The system uses a heat engine that operates in a closed cycle to convert thermal energy to mechanical energy. Key aspects include:
- It uses a piston inside a cylinder filled with gas to harness expansion and compression as the gas is heated and cooled.
- Reciprocating motion from the piston is converted to rotational motion via a crankshaft to power a generator.
- Advantages are it can generate electricity from otherwise wasted heat sources and uses simple design without valves.
- Applications include use by farmers and industries to harness waste heat, though limitations are variable power output is difficult and systems can be
The document discusses gas turbine power plants. It describes the key components of a gas turbine - the air compressor, diffuser, combustion chamber, and turbine. Gas turbines operate using the Brayton cycle and can be open or closed cycle. They have higher efficiency than steam plants but require specialized alloys due to high operating temperatures. Major applications include aviation, power generation, oil and gas industries, and marine propulsion.
This document summarizes the key differences between open cycle and closed cycle gas turbines. It explains that open cycle gas turbines involve irreversible compression and expansion processes, while closed cycle gas turbines involve ideal isentropic compression and expansion. The document also discusses gas turbine cycles with intercooling and reheat to increase output, as well as regenerative cycles to improve efficiency. Additional sections cover the advantages of gas turbines over internal combustion engines and steam turbines.
This document summarizes the closed cycle of a gas turbine. It works by compressing a working fluid like air or gases using a compressor mounted on a common shaft with a turbine. The compressed fluid is then heated in an external heater before passing through the turbine to generate power. This power is used to drive the compressor. The fluid is then cooled before repeating the cycle. Key advantages are high efficiency over a range of temperatures and pressures. Disadvantages include higher costs due to working under pressure and needing large heat exchangers. Applications include power generation, marine propulsion, and industrial uses.
A gas turbine uses a gaseous working fluid to generate mechanical power that can power industrial devices or generate thrust. It has three main parts - an air compressor, combustion chamber, and turbine. The compressed air is mixed with fuel and ignited in the combustion chamber, and the hot gases spin the turbine to generate power. Some applications of gas turbines include aviation, power generation, and marine propulsion. Gas turbines have lower efficiency than steam turbines but are simpler and can use cheaper fuels.
To study the behaviour of nanorefrigerant in vapour compression cycle a revieweSAT Journals
Abstract Nanofluid is an advanced kind of fluid, which contain nanometer sized (10-9 m) solid particles that are known as nanoparticles. Nanoparticles enhance the property of normal fluid. In past five years, nanorefrigerant has become the input for large number of experimental and vapour compression systems because of shortage of energy and environmental considerations. The conventional refrigerants have major role in global warming and depletion of the ozone layer. Therefore, there is need to improve the performance of vapour compression refrigeartion system with the help of using suitable refrigerant. Nearly all the works carried out in relation with nanofluids in vapour compression is regarding their applications in systems like domestic refrigerators and industrial purposes etc. The present paper investigate the performance of the nanorefrigerant in vapour compression cycle and the challenges of using nanorefrigerants in vapour compression cycle. Keywords: Nanofluids, nanoparticles, nanometer, nanorefrigerants, vapour compression, ecofriendly, domestic refrigerator
A gas turbine works by compressing air in a compressor and adding fuel which is burned, heating the air. The hot air then expands through turbine blades, providing power. Gas turbines are used for aircraft, locomotives, power generation and more. They have high power-to-weight ratios but low thermal efficiency compared to steam plants. Various techniques can improve efficiency, such as regeneration which recovers heat from the exhaust to preheat the incoming air.
Similar to Method to improve the Efficiency of Gas Turbine Power Plant (20)
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A SYSTEMATIC RISK ASSESSMENT APPROACH FOR SECURING THE SMART IRRIGATION SYSTEMSIJNSA Journal
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3. INTRODUCTION
G A S T u r b i n e P o w e r P l a n t
• Gas turbines have been used for electricity generation in the periods
of peak electricity demand.
• Gas turbines can be started and stopped quickly enabling them to be
brought into service as required to meet energy demand peaks.
• Small unit sizes and their low thermal efficiency restricted the
opportunities for their wider use for electricity generation.
• The Thermal efficiency of the gas turbine is 20 to 30% compared with
the modern steam power plant 38 to 40%.
3
4. CLASSIFICATION
G A S T u r b i n e P o w e r P l a n t
By Application:
• Air craft
• Stationary
• Locomotive
• Marine
• Transport
By Cycle:
• Open
• Closed
• Semi closed
By Fuel:
• Solid fuel
• Liquid fuel
• Gaseaos fuel
4
According to Arrangement:
• Simple
• Single Shaft
• Multi Shaft
• Inter cooled
• Reheat
• Regenerative
• Combination
According to combustion:
• Continuous combustion
• Intermittent combustion
5. EFFICIENCY IMPROVEMENT
G A S T u r b i n e P o w e r P l a n t
There are three method to improve efficiency of gas turbine power plant
• Intercooling
A compressor utilizes the major percentage of power developed by the
gas turbine. The work required by the compressor can be reduced by
compressing the air in two stages and incorporation a intercooler
between the two.
• Reheating
The output of gas turbine can be improved by expanding the gasses in two
stages with a reheater between the two.
The H.P. turbine drives the compressor and the LP turbine provides
useful power output
• Regeneration
The exhaust gasses from the turbine carry a large quantity of heat with
them since their temperature is far above the ambient temperature.
They can be used to heat air coming from the compressor there by
reducing the mass of fuel supplied in the combustion chamber.
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6. GAS TURBINE POWER PLANT
W i t h I n t e r c o o l i n g
• In Intercooling a heat exchanger is used to cool the
compressor gases at the time of compression process.
• When the compressor involves the high and low
pressure unit in it, the intercooler could be installed
between them to cool down the flow.
• This cooling process will decrease the work needed for
the compression in the high pressure unit. The cooling
fluid can be water , air.
• In marine gas turbines the sea water is used to cool the
fluid. It is observed that a successful implementation of
the intercooler can improve the gas turbine output .
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7. GAS TURBINE POWER PLANT
W i t h R e h e a t i n g
• Reheating is applied in a gas turbine in such a way that it
increases the turbine work without increasing the
compressor work or melting the turbine materials.
• When a gas turbine plant has a high pressure and low
pressure turbine a reheater can be applied successfully.
• Reheating can improve the efficiency up to 3 % .
• A reheater is generally is a combustor which reheat the
flow between the high and low pressure turbines.
• In jet engines an afterburner is used to reheat. It is
attached at the exhaust of the turbine. As a result the
thrust is increased. But it takes a lot of fuel to increase
the thrust .
7
8. GAS TURBINE POWER PLANT
W i t h R e g e n e r a t i o n
• Regeneration process involves the installation of a heat
exchanger in the gas turbine cycle.
• The heat-exchanger is also known as the recuperater.
• This heat exchanger is used to extract the heat from the
exhaust gas .
• This exhaust gas is used to heat the compressed air.
• This compressed and pre-heated air then enters the
combustors.
• When the heat exchanger is well designed , the effectiveness is
high and pressure drops are minimal.
• when these heat exchangers are used an improvement in the
efficiency is noticed. Regenerated Gas turbines can improve the
efficiency more than 5 % .
8
9. Conclusion
Methods presented in previous slides can enable us to develop
highly efficient models for Gas Turbines Power Plants.
9
10. REFERENCES
[ 1 ] h t t p s : / / n p t e l . a c . i n / c o n t e n t / s t o r a g e 2 / c o u r s e s / 1 0 1 1 0 1 0 0
2 / d o w n l o a d s / L e c t - 0 6 . p d f
[ 2 ] h t t p s : / / t w u g b c n . f i l e s . w o r d p r e s s . c o m / 2 0 1 1 / 0 3 / t h e -
b r a y t o n - c y c l e - w i t h - r e g e n e r a t i o n . p d f
[ 3 ] h t t p s : / / b a s i c m e c h a n i c a l e n g i n e e r i n g . c o m / g a s - t u r b i n e -
p o w e r - p l a n t - w i t h - r e g e n e r a t i o n - r e h e a t -
i n t e r c o o l i n g / # G a s _ T u r b i n e _ o r _ B r a y t o n _ C y c l e _ W i t h _ R e h e a t
_ , _ R e g e n e r a t i o n _ a n d _ I n t e r c o o l i n g
[ 4 ] h t t p s : / / w w w . e n g i n e e r i n g e n o t e s . c o m / m e c h a n i c a l -
e n g i n e e r i n g / g a s - t u r b i n e / t o p - 6 - m e t h o d s - t o - i m p r o v e - t h e -
e f f i c i e n c y - o f - g a s - t u r b i n e / 5 0 5 0 3
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