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Aerospace Engineering Laboratory II

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Presentation on theme: "Aerospace Engineering Laboratory II"— Presentation transcript:

1 Aerospace Engineering Laboratory II 2145392
Gas Turbine Scp

2 Introduction Fluid machinery
Fluid machine that adds energy to the fluid is called, pump, compressor, blower and fan. Fluid machine that extracts energy from the fluid is called turbine.

3 Introduction Fluid machinery
For fluid machines of dynamic type, the machines can be further divided according to the flow direction (respect to the rotating shaft) as The radial flow machine: radial flow compressor, radial flow turbine. The axial flow machine: axial flow compressor, axial flow turbine. The mixed flow machine.

4 Introduction Gas Turbine
Gas Turbine is usually referred to a unit consisted of compressor, combustion chamber and turbine. Gas Turbine convert heat energy of a fuel into mechanical energy.

5 Introduction

6 Introduction Turboprop

7 Introduction Turbofan

8 Introduction Turbojet

9 Introduction Gas turbine in power plant

10 Introduction Gas turbine in power plant

11 Introduction Gas turbine engine, road vehicles, racing car, train, motorcycle , ship M1 tank

12 Piston engine vs Gas turbine engine

13 Piston engine vs Gas turbine engine

14 Piston engine vs Gas turbine engine
Advantages: Gas turbine engines have a great power-to-weight ratio compared to reciprocating engines. The flow of the fluid in the process can be classified as steady flow. Disadvantages: The main disadvantage of gas turbines is that, compared to a reciprocating engine of the same size, they are expensive, and they prefer a constant rather than a fluctuating load.

15 Performance of gas turbine unit
Study the actual working cycle of the gas turbine unit. Study the performance of the gas turbine unit.

16 Performance of gas turbine unit


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