15.17 Turboshaft Enigines Flashcards

1
Q

what is a turbo shaft engine optimised to create?

A

shaft power, not thrust

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2
Q

how may the shaft be driven in a turbo shaft engine ?

A

coupled directly to the turbine or driven by its own free turbine located in the exhaust stream

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3
Q

how does the free turbine rotate ?

A

independently

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4
Q

what is a turbo shaft’s engine output measured in ?

A

shaft horse power

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5
Q

what are the two major part assemblies of a turboshaft engine ?

A

-gas generator
-power section

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6
Q

what does the gas generator section comprise of?

A

Compressor, combustion chambers, igniters, nozzles, and one or more sections of the turbines

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7
Q

what does the power section comprise of ?

A

additional stages of turbines, gear reduction system, and the shaft output

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8
Q

where might turboshaft engines be used?

A

where is sustained high power output ,high reliability, small size and light weight is needed such as helicopter engines and APU’s

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9
Q

why are Drive systems fitted turboshaft engines ?

A

to transfer the power produced within the engine

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10
Q

what are the two components used to reduce transmission speeds?

A
  • reduction gearbox
  • main rotor gearbox
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11
Q

when an aircraft uses two turboshaft engines, What must be fitted to stop one engine from driving the other?

A

a free wheel which automatically disconnects the slower engine

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12
Q

what is a free wheel also known as ?

A

a sprag clutch

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13
Q

what is the purpose of a universal joint being fitted to the output shaft?

A

it ensures driveshaft alignment between the engine and the main rotor gearbox.
and it also ensures the transmission of only the engines torque

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14
Q

what is the purpose of reduction gearing?

A

to slow the output shaft’s speed down

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15
Q

why is a universal joint connection provided on a turbo shaft engine ?

A

so that there is adequate movement of the transmission

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16
Q

what must couplings not be subjected to ?

A

Tension or compression loads

17
Q

why might drive shafts fitted with couplings require repetitive inspection?

A

they are subjected to distortion due to high RPM and fatigue stresses

18
Q

how is fuel control for a turboshaft engine received ?

A

via a signal from the flight crew for a given level of power

19
Q

what is adjusted when a level of power command is inputted ?

A

-engine fuel flow
- turbine inlet temperature

20
Q

how can large to medium sized helicopters fitted with FADEC control their engines ?

A

individually via a switch with options:
- off
- idle
- flight