What are the main components of a gas turbine engine?

Prepare effectively for the Gas Turbine Systems (GS) A School Test. Access multiple choice questions, detailed explanations, and tips to enhance your readiness for the exam!

The main components of a gas turbine engine are the compressor, combustion chamber, and turbine. Each of these components plays a critical role in the overall operation of the engine.

The compressor is responsible for drawing in ambient air and compressing it, which significantly increases the air pressure before it enters the combustion chamber. This increase in pressure is essential for the efficient combustion of fuel.

The combustion chamber, also known as the combustor, is where the compressed air mixes with fuel and is ignited. This combustion process generates high-temperature, high-pressure gases that expand rapidly.

The turbine then extracts energy from these expanding gases, converting thermal energy into mechanical energy to drive the compressor. Additionally, the turbine helps produce thrust for propulsion in jet engines.

This configuration—comprising the compressor, combustion chamber, and turbine—is fundamental to the functionality of a gas turbine engine, making it the correct answer.

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