Brayton Cycle: The Ideal Cycle for Gas-Turbine Engines
The Brayton cycle is the ideal thermodynamic cycle for gas turbine engines. This page introduces the cycle's key components, processes, and applications.
Components and Processes
The Brayton cycle consists of four main processes:
- Isentropic compression (1-2)
- Constant pressure heat addition (2-3)
- Isentropic expansion (3-4)
- Constant pressure heat rejection (4-1)
These processes occur in the compressor, combustion chamber, and turbine of a gas turbine engine.
Vocabulary: Isentropic - A process where entropy remains constant.
Key Equations
The Brayton cycle analysis involves several important equations:
-
Heat entering and exiting:
- Qin = H3 - H2 = CpT3−T2
- Qout = H4 - H1 = CpT4−T1
-
Work in compression and expansion:
- Wc = CpT2−T1
- WT = CpT3−T4
-
Pressure ratio: rp = P2 / P1
Definition: Pressure ratio is the ratio of the compressor outlet pressure to the inlet pressure.
Applications
The Brayton cycle has diverse applications, including:
- Military aviation
- Commercial aviation
- Electric power generation
- Transportation (ships, tanks)
- Industrial processes
Highlight: The Brayton cycle's versatility makes it crucial in both aerospace and power generation industries.