Brayton Cycle

Brayton Cycle is a thermodynamic cycle used in gas turbine engines and airbreathing jet engines. It consists of four processes: isentropic compression, constant pressure heat addition, isentropic expansion, and constant pressure heat rejection. The cycle is named after George Brayton, an American engineer who developed the first commercial gas turbine engine. The Brayton cycle is used to convert the chemical energy of fuel into mechanical energy, which is used to power aircraft engines, electric generators, and other machinery. The cycle is highly efficient and can achieve high power-to-weight ratios, making it ideal for aerospace applications.

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Brayton Cycle

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