Turbine Engines Flashcards

1
Q

Explain the main difference and advantage of turbofan over turbojet engines

A

A turbofan engine uses a fan to bypass some air around the engine core and to provide thrust. The advantage is that
this provides additional thrust without increasing fuel flow

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2
Q

Name the major components in a gas turbine engine

A

Air Inlet, Compression Section, Combustion Section,Turbine Section,Exhaust Section, Gearbox and Accessory Section

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3
Q

What determines the amount of airflow through a turbine engine

A

The forward speed of the the aircraft, compressor speed, and air density

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4
Q

Name two types of compressors commonly used in turbine engines

A

Axial and Centrifugal

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5
Q

Name two different methods for attaching turbine engine rotor blades to the rotor disk

A

Dovetail, Bulb and FiR-Tree Type Root

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6
Q

What is a split compressor system

A

Also called dual or twin spool compressors, these are connected to the turbine section, one inside the other

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7
Q

What prevents the combustion chambers from burning

A

Cooling air along the inside of the liner

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8
Q

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

A

Flame propagation during start

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9
Q

What are carbon seals used for in turbine engines

A

They are used as oil seals for the rotor shaft bearings

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10
Q

What are the different types of combustion chambers used in turbine engines

A

Can, annular, can-annular, and reverse flow annular

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11
Q

What functions do axial flow turbine nozzles perform

A

They direct the mass airflow to drive the turbine rotor at a specific angle

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12
Q

How is thermal stress relieved on a turbine disc

A

By directing bleed air onto the face of the disk, or by grooves being cut in the disk

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13
Q

What is the purpose of turbine engine compressor field cleaning

A

Remove contaminant deposits and improve performance

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14
Q

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

A

Fluid flush and abrasive grit blast

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15
Q

How can you tell if a turbofan or turbojet is out of trim

A

High EGT at target EPR

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16
Q

What would the possible cause be for a turbojet or turbofan engine having high exhaust gas temperature, low RPM and high fuel flow at ALL engine pressure ratio settings

A

Possible turbine damage or loss of turbine efficiency

17
Q

Name types of compressor blade damage

A

Dents, galling, pitting, cracks, scratches, burrs, burns and gouges

18
Q

What is used to mark hot and cold section parts

A

Dye, felt tip marker, or chalk 4-26

19
Q

What is the effect of relative humidity on turbine power

A

Negligible effect