Ge10 Gas Turbine - QnA (2023)

Table of Contents
1. what is gas turbine describe it. ​ 2. it is used in gas turbines and jet engines 3. 1. Explain the advantages of Gas Turbine ​ 4. The gas turbine portion of a combined power plant has a pressure ratio of 5. At what stage in a turbine engine are gas pressures the greatest 6. An ideal gas mixture has a volumetric composition of 25% N2, 50% O2, and 25% CO2. The mixture flows through an insulated turbine at a rate of 12 kg/s. The mixture enters the turbine at 2 MPa and 500°C, and exits the turbine at 300 kPa. The turbine has an isentropic efficiency of 0.85. Assuming that the changes in kinetic and potential energy are negligible, and that the mixture has constant specific heats (evaluated at 600 K), determine the power produced by the turbine and the entropy generation rate for the process. 7. reflection how this kind of gas turbine engine works?​ 8. 1. The _____________________energy from the gas, oil or coal provides _____________ (2) _______________ energy to water and produce steam. A turbine changes the energy of the steam into __ (3) ________________energy of the rotating turbine and generator. The generator converts this energy into (4) _______________energy. The lamp is an energy converter changing (5) __________________energy to (6) ______________energy.​ 9. In air-standard analysis of a gas turbine, the temperature rise that would be brought about by combustion is accomplished by heat transfer from an external source. as such, air-standard analyses are of little value when studying combustion gas turbine performance. 10. How is thrust generated in a gas turbine engine? 11. difference of turbine and tesla turbine 12. Make a comparison in between single-shaft and split-shaft gas turbine engine in terms of their construction and operating principle.​ 13. which of the following is an example of nonrenewable resourcea. solar panelb. wind turbinesc. natural gasd. geothermal​ 14. A stream of ethylene gas at 300c and 45 bar is expanded adiabatically in a turbine to 2 bar. calculate the isentropic expansion work produced. assumed ideal gas condition 15. why power , isentropic efficiency is veru important factors og a gas turbine​ 16. Thus a Gas turbine feasible to be a independent electrical power source in Bohol?.​ 17. Air, behaving as an ideal gas with constant specific heats, enters a turbine at 1000 kPa and 700 K, and exits at 100 kPa and 425 K. Determine the isentropic efficiency of the turbine. 18. 2. Which is NOT an example of renewable resources?a. geothermalb. natural gasC. solar panelsd. wind turbines​ 19. Accessory section of the gas turbine engine 20. Nitrogen gas is used as the working fluid in a reversed Brayton refrigeration cycle. The cycle operates as a closed loop, with the nitrogen entering the compressor at 100 kPa and 10°C, and entering the turbine at 600 kPa and 50°C. The cycle is to be used as a refrigerator and is to remove 20 kW of heat from a cold region. Assume the N2 behaves as an ideal gas with constant specific heats. Determine the mass flow rate of the N2 through the cycle and the coefficient of performance of the cycle if (a) the compressor and turbine are isentropic, and (b) the isentropic efficiencies of both the turbine and compressor are 0.78. 21. The turbine section of a brayton cycle gas turbine receives the hot compressed air at 150 psia 22. 1. The ______ energy from the gas, oil or coal provides (2) ______ energy to water and produce steam. A turbine changes the energy of the steam into (3) _____ energy of the rotating turbine and generator. The generator converts this energy into (4) ______ energy. The lamp is an energy converter changing (5) ______ energy to (6) ______ energy.​​ 23. which is not an example of renewable resources a geothermal b natural gas c solar panels the wind turbines​ 24. 1.If you are about to build an aircraft, what type of gas turbine engine will you use and why? ​ 25. what are the types of gas turbine and what are the difference between them​ 26. essay about the reason why the unit measurements of fuel consumption for gas turbine engine is in mass flow or weight, rather than in volumes (gallons or litres)?​ 27. The compressor inlet air temperature in a gas turbine plant is 100oc. 28. what are the types of gas turbine and what are the difference between them​ 29. what are the types of gas turbine and what are the difference between them​ 30. What are the main 3 components of gas turbine?

Ge10 Gas Turbine - QnA (1)

what is gas turbine describe it. ​

Daftar Isi

1. what is gas turbine describe it. ​


Answer:

A gas turbine is a combustion engine that can convert natural gas or other liquid fuels to mechanical energy. This energy then drives a generator that produces electrical energy.


2. it is used in gas turbines and jet engines


Answer:

axial compressors

Explanation:

Modern large turbojet and turbofan engines usually use in axail compressors.


3. 1. Explain the advantages of Gas Turbine ​


Answer:

1. They are small in size, weigh less and have low initial cost per unit output.

2.They are easy to install within short periods.

3.They are quick-starting and smooth running.

4.They offer flexibility by supplying electricity for power generation as well as by supplying compressed air for process needs.

5.They are capable of using a range of liquid and gaseous fuels including synthetic fuels.

6.They are subjected (put) to fewer environmental restrictions than other prime movers.

7.Water consumption is less compared to steam power plant.


4. The gas turbine portion of a combined power plant has a pressure ratio of


Explanation:

16

Thegas-turbine portion of a combined gas-steampower plant has a pressure ratioof 16.

Answer:

16

The gas-turbine portion of a combined gas-steam power plant has a pressure ratio of 16.

Explanation:

hope it's help


5. At what stage in a turbine engine are gas pressures the greatest


Answer:

From stage 1 (row 1 of the compressor blade-vane sets) leading towards the burner, air pressure increases and air temperature increases. So, for this UUNBURNED air, the highest “air pressure” is right before the entrance to the burners.

Inside the burners, high pressure fuel is injected (usually either jet fuel (aircraft and Navy ships) or natural gas (industrial and electric power turbines) , mixed, and then burned. The now extremely hot, extremely high pressure exhaust gases then leave the burner and are directed right into the first stage of the exhaust turbine - which is where power is extracted in subsequent exhaust stages until it leaves the gas turbine exhaust.

So the highest “gas pressure” (and highest gas temperature) is right at the top of the burner, just before the gas enters the first row of the exhaust turbine blades.


6. An ideal gas mixture has a volumetric composition of 25% N2, 50% O2, and 25% CO2. The mixture flows through an insulated turbine at a rate of 12 kg/s. The mixture enters the turbine at 2 MPa and 500°C, and exits the turbine at 300 kPa. The turbine has an isentropic efficiency of 0.85. Assuming that the changes in kinetic and potential energy are negligible, and that the mixture has constant specific heats (evaluated at 600 K), determine the power produced by the turbine and the entropy generation rate for the process.


See the attached images.

An ideal gas mixture has a volumetric composition of 25% N2, 50% O2, and 25% CO2. The mixture flows through an insulated turbine at a rate of 12 kg/s. The mixture enters the turbine at 2 MPa and 500°C, and exits the turbine at 300 kPa. The turbine has an isentropic efficiency of 0.85. Assuming that the changes in kinetic and potential energy are negligible, and that the mixture has constant specific heats (evaluated at 600 K), determine the power produced by the turbine and the entropy generation rate for the process.


7. reflection how this kind of gas turbine engine works?​


Answer:

A gas turbine engine operates by compressing air to high pressure, combusting fuel in the air stream which increases pressure and temperature, then expanding the high-pressure exhaust gases through a turbine to produce work. Some or all of the work produced by the turbine is used to power the compressor.

Fan, compressor isentropic efficiency: 0.9

Turbine inlet temperature: 1500 K

Combustion chamber pressure loss: 1.3 bar


8. 1. The _____________________energy from the gas, oil or coal provides _____________ (2) _______________ energy to water and produce steam. A turbine changes the energy of the steam into __ (3) ________________energy of the rotating turbine and generator. The generator converts this energy into (4) _______________energy. The lamp is an energy converter changing (5) __________________energy to (6) ______________energy.​


Answer:

1. chemical

2. heat

3. mechanical

4. electrical

5. electrical

6. light


9. In air-standard analysis of a gas turbine, the temperature rise that would be brought about by combustion is accomplished by heat transfer from an external source. as such, air-standard analyses are of little value when studying combustion gas turbine performance.


Answer:

study hard ambition success


10. How is thrust generated in a gas turbine engine?


Answer:

In a jet engine the turbine is designed to provide just enough output to drive the compressor and auxiliary devices. The stream of gas then leaves the turbine at an intermediate pressure (above local atmospheric pressure) and is fed through a nozzle to produce thrust.

#READYTOHELP

Answer:

In a jet engine the turbine is designed to provide just enough output to drive the compressor and auxiliary devices. The stream of gas then leaves the turbine at an intermediate pressure (above local atmospheric pressure) and is fed through a nozzle to produce thrust.

#CarryOnLearning

Explanation:


11. difference of turbine and tesla turbine


Answer:

oni chan your so kawaiii

Answer:

The main difference between the Tesla turbine and the turbines used nowadays to propel jet planes, for example, is that instead of using curved blades like those of a windmill, it generates movement through smooth and parallel disks placed evenly across a shaft, like CD's placed along a pole.


12. Make a comparison in between single-shaft and split-shaft gas turbine engine in terms of their construction and operating principle.​


Answer:

If the load speed is constant, as in the case of an electric generator, a single-shaft unit is often specified; an engine specifically designed for electric power generation would make use of a single-shaft configuration.

An alternative, however, is the use of a two-shaft engine. If the load needs to be driven with varying speeds (compressors, pumps), two-shaft engines are advantageous.

Explanation:

single-shaft

In single-shaft turbines, controls speed by regulating the gas control valve or the liquid fuel valve.

split-shaft

In two-shaft gas turbines, it is driven from the power turbine shaft but regulates the fuel input to the gas generator


13. which of the following is an example of nonrenewable resourcea. solar panelb. wind turbinesc. natural gasd. geothermal​


KASAGUTAN:

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which of the following is an example of nonrenewable resource

a. solar panel

b. wind turbines

c. natural gas

d. geothermal

[tex]\huge\color{blue}{jayrenenicolenaba}[/tex]


14. A stream of ethylene gas at 300c and 45 bar is expanded adiabatically in a turbine to 2 bar. calculate the isentropic expansion work produced. assumed ideal gas condition


Answer:

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15. why power , isentropic efficiency is veru important factors og a gas turbine​


Answer:

As the isentropic efficiency of the turbine increases , the irreversibilities decrease. Hence, a turbine with a higher isentropic efficiency is capable of producing more power that's why isentropic efficiency is very important factors of a gas turbine


16. Thus a Gas turbine feasible to be a independent electrical power source in Bohol?.​


Answer:

hsjxsoqjspsys6shywhsbsjh

Explanation:

beeg .com and porn hub


17. Air, behaving as an ideal gas with constant specific heats, enters a turbine at 1000 kPa and 700 K, and exits at 100 kPa and 425 K. Determine the isentropic efficiency of the turbine.


See the attached image.

Air, behaving as an ideal gas with constant specific heats, enters a turbine at 1000 kPa and 700 K, and exits at 100 kPa and 425 K. Determine the isentropic efficiency of the turbine.


18. 2. Which is NOT an example of renewable resources?a. geothermalb. natural gasC. solar panelsd. wind turbines​


2. Which is NOT an example of renewable resources?

a. geothermal

b. natural gas

C. solar panels

d. wind turbines


19. Accessory section of the gas turbine engine


Answer:

ACCESSORY OF GAS ENGINE


20. Nitrogen gas is used as the working fluid in a reversed Brayton refrigeration cycle. The cycle operates as a closed loop, with the nitrogen entering the compressor at 100 kPa and 10°C, and entering the turbine at 600 kPa and 50°C. The cycle is to be used as a refrigerator and is to remove 20 kW of heat from a cold region. Assume the N2 behaves as an ideal gas with constant specific heats. Determine the mass flow rate of the N2 through the cycle and the coefficient of performance of the cycle if (a) the compressor and turbine are isentropic, and (b) the isentropic efficiencies of both the turbine and compressor are 0.78.


See the attached images.

Nitrogen gas is used as the working fluid in a reversed Brayton refrigeration cycle. The cycle operates as a closed loop, with the nitrogen entering the compressor at 100 kPa and 10°C, and entering the turbine at 600 kPa and 50°C. The cycle is to be used as a refrigerator and is to remove 20 kW of heat from a cold region. Assume the N2 behaves as an ideal gas with constant specific heats. Determine the mass flow rate of the N2 through the cycle and the coefficient of performance of the cycle if (a) the compressor and turbine are isentropic, and (b) the isentropic efficiencies of both the turbine and compressor are 0.78.


21. The turbine section of a brayton cycle gas turbine receives the hot compressed air at 150 psia


Answer:

The turbine section of a Brayton cycle gas turbine receives the hot compressed air at 150 psia and 2100°R and expands it to 15 psia and develops a gross output of 15000 hp . Air enters the compressor section at 15 psia and 500°R.

Explanation:

#CarryOnLearning


22. 1. The ______ energy from the gas, oil or coal provides (2) ______ energy to water and produce steam. A turbine changes the energy of the steam into (3) _____ energy of the rotating turbine and generator. The generator converts this energy into (4) ______ energy. The lamp is an energy converter changing (5) ______ energy to (6) ______ energy.​​


Answer:

1. chemical

2. heat

3. mechanical

4. electrical

5. electrical

6. light


23. which is not an example of renewable resources a geothermal b natural gas c solar panels the wind turbines​


Answer:

A. Geothermal

Explanation:

Renewable resources include biomass energy (such as ethanol), hydropower, geothermal power, wind energy, and solar energy.

Answer:

B. Natural Gas

- It is a non-renewable fossil fuel formed from the remains of tiny sea plants and animals that died 300-400 MILLION YEARS AGO.

(so, it takes a very, very long time to create, making it a non-renewable resource)

24. 1.If you are about to build an aircraft, what type of gas turbine engine will you use and why? ​


Answer:Turbofans are the most widely used gas turbine engine for air transport aircraft. The turbofan is a compromise between the good operating efficiency and high thrust capability of a turboprop and the high speed, high altitude capability of a turbojetA gas turbine is a rotary engine that extracts energy from a flow of combustion gases. Ambient air is drawn into the engine intake where an axial or a centrifugal compressor (or both) increases both the pressure and temperature of the air before feeding it into the combustion chamber.

Explanation:pa brainliest po


25. what are the types of gas turbine and what are the difference between them​


sorry eto lang ako, igop


26. essay about the reason why the unit measurements of fuel consumption for gas turbine engine is in mass flow or weight, rather than in volumes (gallons or litres)?​


Explanation:

. DESCRIBES THE REASON WHY THE UNIT MEASUREMENTS OF FUEL CONSUMPTION FOR GAS TURBINE ENGINE IS IN MASS FLOW OR WEIGHT, RATHER THAN IN VOLUMES (GALLONS OR LITRES)?


27. The compressor inlet air temperature in a gas turbine plant is 100oc.


Answer:

The power output and efficiency rating of gas turbines are usually based on ISO conditions (inlet air temperature 288 K and 65% relative humidity).

Explanation:


28. what are the types of gas turbine and what are the difference between them​


Answer:

turbojet, turbofan, turboprop, and turboshaft.


29. what are the types of gas turbine and what are the difference between them​


Answer:

Four types of gas turbine engines are used to propel and power aircraft. They are the Turbo jet , Turbo fan, Turbo fan and Turbo shaft


30. What are the main 3 components of gas turbine?

1. An Air Compressor
2. A Combustor
3. A Power TurbineANSWER:

Compressor
Combustor
Power Turbine

^_^

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