Brayton Cycle
Brayton Cycle for Gas Turbine Power Generation · Also known as: Joule cycle, gas turbine cycle
The Brayton Cycle (also called Joule Cycle) describes the thermodynamic process in gas turbines and jet engines. It consists of four processes: isentropic compression in a compressor, isobaric combustion (heat addition), isentropic expansion in a turbine, and isobaric heat rejection. The Brayton Cycle is the foundation for analyzing aircraft propulsion, ground-based power generation, and simple-cycle gas turbine plants.
Read the full method
Sign in with a free account to read this section.
Method map
The neighbourhood of related methods — select a node to explore.
When to use it
Use the Brayton Cycle for analyzing gas turbine power plants, jet engines, and industrial turbomachinery. It is particularly suited to high-temperature applications and systems where rapid response to load changes is important. Avoid using when working fluid properties deviate significantly from ideal gas behavior.
Strengths & limitations
- Simple cycle structure with only two pressure levels
- All processes involve flowing streams, avoiding phase change complexity
- High maximum operating temperatures possible with gas turbines
- Fast response to load changes for grid support applications
- Relatively low thermal efficiency compared to Rankine Cycle for given inlet/outlet temperatures
- Efficiency highly dependent on achieving high pressure ratios and temperatures
- Material temperature limits restrict turbine inlet temperature
- Compression power is substantial and temperature-dependent, reducing net work
Frequently asked
Why is Brayton Cycle efficiency so dependent on pressure ratio?
Higher pressure ratio increases the temperature after compression, requiring more heat addition for a fixed turbine inlet temperature. The work extracted is nearly proportional to pressure ratio, but compression work grows faster, reducing net work. Optimal pressure ratio balances these competing effects.
What is the purpose of regeneration in a Brayton Cycle?
Regeneration uses hot turbine exhaust to preheat the compressor discharge before combustion, reducing fuel needed for heat addition. This significantly improves efficiency, especially at lower pressure ratios where turbine exhaust temperature is high.
How does intercooling improve Brayton Cycle performance?
Intercooling reduces compressor work by cooling the gas between compressor stages before further compression. This lowers the average compressor inlet temperature, reducing work input while maintaining the same final pressure, improving net cycle work.
Sources
- Moran, M. J., Shapiro, H. N., Boettner, D. D., & Bailey, M. B. (2014). Fundamentals of Engineering Thermodynamics (8th ed.). Wiley. ISBN: 978-1118412947
- Cohen, H., Rogers, G. F. C., & Saravanamuttoo, H. I. H. (1996). Gas Turbine Theory (4th ed.). Longman. ISBN: 978-0582234994
How to cite this page
ScholarGate. (2026, June 3). Brayton Cycle for Gas Turbine Power Generation. ScholarGate. https://scholargate.app/en/thermodynamics/brayton-cycle
Which method?
Set this method beside its closest kin and read them side by side — the library lays the books on the table; the choice is yours.
- Finite-Time ThermodynamicsThermodynamics↔ compare
- Rankine CycleThermodynamics↔ compare
- Vapor Compression CycleThermodynamics↔ compare