Gas turbines have these advantages over steam plants:
Gas Turbine Power Plant
They are small in size, mass, and initial cost per unit output. Their delivery time is relatively short and they can be installed quickly.
Dr. M. Zahurul Haq
They are quick starting (as low as 10 s), often by remote control.
Professor Department of Mechanical Engineering Bangladesh University of Engineering & Technology (BUET) Dhaka-1000, Bangladesh
They are smooth running and have a capacity factor (percent of time the unit is operating at full power) of 96 to 98 percent. They can use a wide variety of liquid and gaseous fuels including gasified coal and synthetic fuels.
[email protected] http://teacher.buet.ac.bd/zahurul/
They are subject to fewer environmental restrictions than other prime movers.
ME 403: Power Plant Engineering
c Dr. M. Zahurul Zahurul Haq Haq (BUE (BUET) T)
Gas Tu Turbine rbine
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c Dr. M. Zahurul Zahurul Haq Haq (BUE (BUET) T)
Gas Tu Turbine rbine
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T401
Schematic layout of a single-shaft gas turbine.
T371
A comparison between the working cycle of a turbo-jet engine and a piston engine. c Dr. M. Zahurul Zahurul Haq Haq (BUE (BUET) T)
Gas Tu Turbine rbine
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T402
Schematic layout of a two-shaft gas turbine. c Dr. M. Zahurul Zahurul Haq Haq (BUE (BUET) T)
Gas Tu Turbine rbine
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Thermodynamics of gas turbine cycles
T403
Thermodynamics of gas turbine cycles
T404
Representation of a simple cycle gas turbine.
Representation of gas turbine cycle on temperature-entropy diagram.
T405
Effect of pressure ratio on the temperature-entropy diagram for an ideal gas turbine cycle when T 3 is constant. c Dr. M. Zahurul Haq (BUET)
Gas Turbine
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c Dr. M. Zahurul Haq (BUET)
Thermodynamics of gas turbine cycles
Gas Turbine
T407
ME 403 ( 2015)
T408
Schematic representation of a regenerative cycle.
Variation of thermal efficiency and specific work with compressor pressure ratio.
Gas Turbine
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Thermodynamics of gas turbine cycles
T406
c Dr. M. Zahurul Haq (BUET)
ME 403 ( 2015)
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c Dr. M. Zahurul Haq (BUET)
Gas Turbine
Heat transfer for a regenerative gas turbine cycle.
ME 403 ( 2015)
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Thermodynamics of gas turbine cycles
Thermodynamics of gas turbine cycles
T409
Effect of T 4 and pressure ratio on the thermal efficiency of a regenerative cycle. The limiting pressure ratios when T 5 = T 2 are shown.
c Dr. M. Zahurul Haq (BUET)
Gas Turbine
ME 403 ( 2015)
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T410
Ideal and actual compression and expansion processes on the temperature-entropy diagram. c Dr. M. Zahurul Haq (BUET)
Thermodynamics of gas turbine cycles
Gas Turbine
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Thermodynamics of gas turbine cycles
T412 T411
Variation of the isentropic efficiency with pressure ratio for a polytropic efficiency of 0.87.
c Dr. M. Zahurul Haq (BUET)
Gas Turbine
ME 403 (2015)
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Combustion temperature rise versus fuel-air ratio.
c Dr. M. Zahurul Haq (BUET)
Gas Turbine
ME 403 (2015)
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Thermodynamics of gas turbine cycles
Thermodynamics of gas turbine cycles
T414
T413
Performance of a practical simple gas turbine cycle as a carpet plot for a series of maximum cycle temperatures and pressure ratios.
Simple gas turbine thermal efficiency varying with pressure ratio.
c Dr. M. Zahurul Haq (BUET)
Gas Turbine
ME 403 (2015)
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c Dr. M. Zahurul Haq (BUET)
Thermodynamics of gas turbine cycles
Gas Turbine
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Thermodynamics of gas turbine cycles
T418
Schematic representation of an intercooled gas turbine.
T417 T419
Carpet plot for a regenerative gas turbine cycle. c Dr. M. Zahurul Haq (BUET)
Gas Turbine
ME 403 (2015)
Two-stage intercooled compression process on the temperature-entropy diagram. 15 / 25
c Dr. M. Zahurul Haq (BUET)
Gas Turbine
ME 403 (2015)
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Thermodynamics of gas turbine cycles
Thermodynamics of gas turbine cycles
T420
Variation of thermal efficiency with specific work for a practical intercooled gas turbine when optimised for maximum thermal efficiency.
c Dr. M. Zahurul Haq (BUET)
Gas Turbine
ME 403 (2015)
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T421
Schematic representation of an intercooled, regenerative gas turbine cycle. c Dr. M. Zahurul Haq (BUET)
Thermodynamics of gas turbine cycles
Gas Turbine
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Thermodynamics of gas turbine cycles
T423
T422
Temperature-entropy diagram for the intercooled and nonintercooled, regenerative gas turbine cycles. c Dr. M. Zahurul Haq (BUET)
Gas Turbine
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Variation of thermal efficiency with specific work for a practical intercooled, regenerative gas turbine cycle
c Dr. M. Zahurul Haq (BUET)
Gas Turbine
ME 403 (2015)
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Thermodynamics of gas turbine cycles
Thermodynamics of gas turbine cycles
T427
T424
Variation of thermal efficiency with specific work when optimised for maximum thermal efficiency.
Schematic representation of a reheat gas turbine.
c Dr. M. Zahurul Haq (BUET)
Gas Turbine
ME 403 (2015)
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c Dr. M. Zahurul Haq (BUET)
Thermodynamics of gas turbine cycles
Gas Turbine
ME 403 (2015)
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Thermodynamics of gas turbine cycles
T429
Schematic representation of a reheat-regenerative gas turbine.
T430
Schematic representation of an intercooled, reheat and regenerative cycle. c Dr. M. Zahurul Haq (BUET)
Gas Turbine
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c Dr. M. Zahurul Haq (BUET)
Gas Turbine
ME 403 (2015)
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Thermodynamics of gas turbine cycles
T433
Variation of thermal efficiency with specific work for practical intercooled, reheat and regenerative (ICRHR) cycle. c Dr. M. Zahurul Haq (BUET)
Gas Turbine
ME 403 (2015)
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