BGT Flashcards

1
Q

Expansion would be in reference to what sort of duct?

A

Convergent

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2
Q

In axial flow compressor, reduction in annulus area between rotor shaft and stator causing would do what ?

A

Reduce area where compressed air held

Manintain constant air stream velocity

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3
Q

In turbo prop power plant, what is the proportion of prop to jet exhaust thrust contribution?

A

Prop 90%

J.E.T 10%

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4
Q

What is the main purpose of the compressor?

A

Supply large mass of compressed air to combustion chambers

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5
Q

What is the purpose of water or water methanol injection?

A

Increase mass flow through engine to increase thrust at takeoff

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6
Q

What is the purpose of variable inlet nozzle guide vanes?

A

Reduce chance of HIGH pressure compressor surging, especially during engine start

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7
Q

On a two spool turbofan engine, the fan and low pressure compressor are drive by what?

A

The last stage turbine

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8
Q

Which spins faster, N1 or N2 blades? Why?

A

N2 blades rotate at higher speeds

They are shorter than N1 and operate in higher temp air

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9
Q

What is high output igniters used for and how often do they discharge compared to low output?

A

Starting and in-flight re-lighting

Discharge less that low output

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10
Q

What is low output igniters used for and how often do they discharge compared to high output?

A

Flying in rain, turbulence, icing conditions and take off

Discharge more often then high

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11
Q

What happens to N1 rpm and N2 rpm as twin spool gas turbine aircraft gains height?

A

Both increase

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12
Q

What would you expect engine compressor rpm to be on a hotter day

A

Higher

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13
Q

EPR is measured between which two point?

A

First stage compressor inlet and Last stage TURBINE outlet

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14
Q

During take off run, what happens to EPR?

A

Drops

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15
Q

Thermo-dynamic rating of an engine describes what ratio?

A

Power output delivered at max turbine limit temperature

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16
Q

In the axial compressor what does the rotor and stator do?

A

Rotor accelerates air

Stator diffuses it