Turbojet Engine Principles: EASA Part-66 Module 15 Essentials
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Turbojet Engine Fundamentals
A turbojet engine, as outlined in the EASA Part-66 Module 15 (Gas Turbine Engines) syllabus, is the simplest form of aircraft gas turbine engine. It generates all of its thrust through the high-speed ejection of exhaust gases from its nozzle. It is one of four main turbine engine types studied in the EASA syllabus: turbojet, turbofan, turboprop, and turboshaft.
Fundamental Principle
The turbojet operates on the Brayton cycle, which involves continuous intake, compression, combustion, and expansion. Air is compressed, mixed with fuel, burned at nearly constant pressure, and expelled at high velocity to produce thrust. The reaction of this high-speed exhaust jet propels the aircraft forward.
Construction and Components
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