9. Gas power cycle free study note

1. Introduction to Gas power cycle

A gas power cycle is a thermodynamic cycle in which a gas is used as the working fluid to produce mechanical power. In these cycles, the working fluid usually remains in the gaseous phase throughout the cycle.

Gas power cycles are widely used in:

  • Internal combustion engines
  • Gas turbines
  • Jet engines
  • Power generation systems

In these cycles, heat is supplied to the gas, which expands and produces work. After expansion, the gas is cooled or exhausted and the cycle repeats.

Basic Characteristics

  1. Working fluid is gas (air, combustion gases).
  2. Heat energy is converted into mechanical energy.
  3. Processes involve compression, heat addition, expansion, and heat rejection.

2. Types of Gas Power Cycles

The most important gas power cycles are:

  1. Otto Cycle
  2. Diesel Cycle
  3. Dual Combustion Cycle
  4. Brayton Cycle

1. Otto Cycle

Definition

The Otto cycle is the ideal thermodynamic cycle for spark ignition (SI) engines, such as petrol engines.

Processes in Otto Cycle

The cycle consists of four processes:

  1. Process 1โ€“2: Isentropic Compression
    • Air is compressed in the cylinder.
    • Pressure and temperature increase.
  2. Process 2โ€“3: Constant Volume Heat Addition
    • Fuel-air mixture burns.
    • Heat is added at constant volume.
  3. Process 3โ€“4: Isentropic Expansion
    • High-pressure gas expands.
    • Work is produced.
  4. Process 4โ€“1: Constant Volume Heat Rejection
    • Heat is rejected to surroundings.

Efficiency of Otto Cycle

ฮท=1โˆ’1rฮณโˆ’1\eta = 1 – \frac{1}{r^{\gamma -1}}

Where:

  • r = Compression ratio
  • ฮณ = Specific heat ratio

Applications

  • Petrol engines
  • Motorcycles
  • Small generators

2. Diesel Cycle

Definition

The Diesel cycle is the ideal cycle for compression ignition engines (diesel engines).

Processes of Diesel Cycle

  1. Process 1โ€“2: Isentropic Compression
    • Air is compressed in the cylinder.
  2. Process 2โ€“3: Constant Pressure Heat Addition
    • Fuel is injected and combustion occurs.
  3. Process 3โ€“4: Isentropic Expansion
    • High pressure gases expand producing work.
  4. Process 4โ€“1: Constant Volume Heat Rejection

Efficiency

Efficiency depends on:

  • Compression ratio
  • Cut-off ratio

Applications

  • Trucks
  • Buses
  • Heavy machinery
  • Diesel generators

3. Dual Combustion Cycle

Definition

The dual combustion cycle is a combination of Otto cycle and Diesel cycle.

Heat is added partly at:

  • Constant volume
  • Constant pressure

Processes

  1. Isentropic compression
  2. Constant volume heat addition
  3. Constant pressure heat addition
  4. Isentropic expansion
  5. Constant volume heat rejection

Advantages

  • More practical representation of real engines.
  • Used in modern diesel engines.

4. Brayton Cycle (Gas Turbine Cycle)

Processes of the Brayton Cycle

The Brayton cycle consists of four ideal thermodynamic processes.

1. Process 1โ€“2: Isentropic Compression

  • Air enters the compressor.
  • Pressure and temperature increase.
  • Entropy remains constant.
  • Compressor requires work input.

2. Process 2โ€“3: Constant Pressure Heat Addition

  • Compressed air enters the combustion chamber.
  • Fuel is injected and burned.
  • Heat is added at constant pressure.
  • Temperature rises significantly.
gas power cycle

3. Process 3โ€“4: Isentropic Expansion

  • High-temperature gases expand through the turbine.
  • Turbine produces mechanical work.
  • Pressure and temperature decrease.
  • Entropy remains constant.

4. Process 4โ€“1: Constant Pressure Heat Rejection

  • Exhaust gases reject heat to the surroundings.
  • Pressure remains nearly constant.
  • Cycle returns to its initial state.

Thermal Efficiency

For the ideal Brayton cycle,ฮท=1โˆ’1rp(ฮณโˆ’1)/ฮณ\eta = 1-\frac{1}{r_p^{(\gamma-1)/\gamma}}where:

  • rpr_prpโ€‹ = Pressure ratio
  • ฮณ\gammaฮณ = Ratio of specific heats (Cp/CvC_p/C_vCpโ€‹/Cvโ€‹)

The thermal efficiency increases as the pressure ratio increases (within practical limits).

Net Work Output

Wnet=WTโˆ’WCW_{net}=W_T-W_C

where:

  • WTW_TWTโ€‹ = Turbine work
  • WCW_CWCโ€‹ = Compressor work

Heat Added

Qin=Cp(T3โˆ’T2)Q_{in}=C_p(T_3-T_2)

Heat Rejected

Qout=Cp(T4โˆ’T1)Q_{out}=C_p(T_4-T_1)

Applications

  • Gas turbine power plants
  • Aircraft jet engines
  • Industrial turbines

5. Comparison of Gas Power Cycles

CycleHeat AdditionEngine Type
Otto CycleConstant VolumePetrol Engine
Diesel CycleConstant PressureDiesel Engine
Dual CycleVolume + PressureModern Diesel Engine
Brayton CycleConstant PressureGas Turbine

6. Advantages of Gas Power Cycles

  1. High power output
  2. Simple design
  3. Quick start and stop
  4. Used widely in transportation and power generation

7. Limitations

  1. Lower efficiency compared to steam power cycles
  2. High fuel consumption
  3. High operating temperatures

External References

  1. NPTEL Course

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