Turbine Engines Flashcards

1
Q

What are the major components of a typical gas turbine engine?

A

Air inlet, compressor, combustion section, turbine section, exhaust section, and accessory section.

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2
Q

What determines the amount of air passing through a turbine engine?

A

Compressor speed, forward speed of the aircraft, and air density.

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2
Q

What prevents burning of combustion chambers

A

The cooling secondary air inside of the liner.

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2
Q

What are the two principal types of compressors currently used in turbine engines?

A

Centrifugal and axial compressors

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2
Q

Name at least three types of combustion chamber systems.

A

Can, Annular, and Can Annular.

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2
Q

How are turbine engine rotor blades attached to rotor disks?

A

Bulb type, Fir tree type, or dovetail type

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2
Q

What are carbon seals used for in turbine engines.

A

Used as oil seals for the rotor shaft bearings.

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2
Q

What is the purpose of the interconnect tubes attached between can-type combustion chambers?

A

For flame propagation during starting, the way the flame moves through the combustion chamber.

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3
Q

What are the desired effects of turbine engine compressor field cleaning?

A

Increase engine efficiency and removal of contaminants from the interior surfaces of the engine.

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4
Q

What is the main operating difference between turbofan and turbojet engines?

A

The air that flows through the fan section of a turbofan engine bypasses or flows around the outside of the core engine instead of through it.

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5
Q

What methods are commonly used to accomplish turbine engine compressor field cleaning?

A

Fluid wash and abrasive grit blast.

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6
Q

Name an advantage of a turbofan over a turbojet.

A

A turbofan provides additional thrust without increase fuel flow.

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7
Q

What are the functions of axial flow turbine nozzles?

A

They prepare the mass airflow for driving the turbine rotor and deflect the gasses to a specific angle.

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8
Q

What are some ways of relieving thermal stress on a turbine disk?

A

By directing bleed air on the face of the disk, or by the grooving in the turbine disk

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8
Q

What type of compressor blade damage may be found when inspecting compressor blades?

A

Burns, burrs, cracks, dents, galling, gouges, pitting, and scratches.

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9
Q

What is used to mark both hot and cold section parts for repair?

A

Layout dye, commercial felt tip marker, or chalk.

10
Q

What is the effect of relative humidity on turbojet or turbofan power?

A

Negligible effect on either engine type.

11
Q

What may be the indications if a turbojet or turbofan engine is out of trim?

A

The engine has high exhaust gas temperature at the target engine pressure ratio for takeoff power.

12
Q

What would be the possible cause for a turbojet or turbofan engine having high EGT, low RPM, and high fuel at all engine pressure ratio settings?

A

Possible turbine damage or loss of turbine efficiency.