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These flashcards cover key concepts related to types of turbine engines, their operation, and distinctions between different engine types.
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What is the primary function of a propulsion system in aviation?
To produce thrust to push an object forward.
What principle explains how thrust is generated in a jet engine?
Newton's third law of action and reaction.
How do jet engines and rocket engines differ?
Jet engines are air-dependent, while rocket engines are air-independent.
What are the four basic operations of a gas turbine engine?
Intake, compression, power, and exhaust.
What component of a turbine engine compresses the intake air?
The compressor.
What role does the combustor play in a gas turbine engine?
It mixes compressed air with high-pressure fuel for combustion.
What is the outcome of the combustion process in a turbine engine?
The production of heat and pressure.
What is the core of a gas turbine engine composed of?
An inlet, a compressor section, combustion section, a turbine section, and an exhaust nozzle.
What is the main purpose of the turbine in a turbojet engine?
To turn the compressor.
What distinguishes a turbofan engine from a turbojet engine?
A turbofan engine has a fan that generates thrust, whereas a turbojet primarily uses exhaust energy.
What does the bypass ratio indicate in a turbofan engine?
The ratio of airflow that bypasses the core to the airflow that goes through the core.
How does a turboprop engine produce thrust?
By using a propeller that extracts energy from the exhaust gases.
What is the difference between fixed-turbine and free-turbine engines?
Fixed-turbine engines have the added turbine mechanically connected to the core, while free-turbine engines do not.
What type of turbine engine delivers power through a shaft to operate other machinery?
Turboshaft engine.
What is a key advantage of turbofans regarding fuel energy conversion?
They convert more fuel energy into pressure, improving efficiency.
What is the typical thrust contribution of the propeller in a turboprop engine?
Approximately 85 percent of the total thrust.