Engine exhaust systems: Recip. and Turbine Flashcards

1
Q

Approximately __________ percent of the heat energy in fuel burned is lost out the exhaust system.

A

50

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2
Q

Two problems caused be short exhaust stacks are
__________
__________

A

Excessive nose

Exhaust valve warpage

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3
Q

The large pipe into which all exhaust gases from a radial engine flow is called a/an __________.

A

Collector ring

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4
Q

The name of the exhaust system component through which exhaust gases leave the aircraft is the __________.

A

Tail pipe

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5
Q

Two uses for some of the heat taken from exhaust gasses are:

A

cabin heat

carburetor heat

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6
Q

Flexible ducting used for carrying the heated air from the shroud around the muffler to the carburetor heat box is __________ (red/black)

A

Red

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7
Q

The stainless-steel tube through which some of the exhaust gases pass after leaving the tail pipe is called a/an __________ tube,

A

Augmenter

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8
Q

Two devices used to recover some of the energy from exhaust gasses are:
__________
__________

A

Turbochargers

Power recovery turbines

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9
Q

Two methods of allowing exhaust system components to move relative to each other without leaking exhaust gases are:
__________
__________

A

Slip joints

Metal bellows

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10
Q

Energy extracted from exhaust gases by a power recovery turbine is coupled to the crankshaft through a ____________.

A

Fluid coupling

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11
Q

An exhaust system component must be protected from marks made by galvanized metal because the __________ deposits will defuse into the metal and cause cracking

A

Zinc

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12
Q

Exhaust systems must never be marked with a lead pencil because the _________ in the pencil mark will diffuse into the metal and cause cracking

A

Carbon

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13
Q

The air pressure used to pressure-check an exhaust system for leaks may be produced with the use of a/an __________.

A

Vacuum cleaner

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14
Q

Carbon monoxide detectors are packets of chemical crystals that change __________ in the presence of CO

A

color

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15
Q

The most common type of exhaust duct for the smaller turbojet and turbofan engines is a _________ duct.

A

Convergent

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16
Q

The exhaust cone is considered to be an __________ component

A

Engine

17
Q

Exhaust gasses leave the exhaust nozzle in most turbojet and low-bypass turbofan engines at the speed of __________

A

sound

18
Q

A convergent-divergent exhaust nozzle increases the thrust produced at supersonic flights by increasing the __________ of exhaust gases.

A

Velocity

19
Q

Exhaust gases enter a CD nozzle at a __________ speed

A

Subsonic

20
Q

In a CD nozzle that uses two sets of overlapping flaps to control gases as they leave an afterburner duct, the flaps are actuated hydraulicly and they are controlled by the___________.

A

Eletric Engine Control (EEC)

21
Q

A CD inlet duct and a CD exhaust nozzle serve a __________ function

A

Diferent

22
Q

Ture or False.

A noise suppressor used on a turbojet engine exhaust system decreases the total amount of sound the engine produces.

A

False

23
Q

The amount of noise a turbojet produces is related to the _________ of the exhaust gases

A

Velocity

24
Q

Low-frequency sound waves travel a __________ distance through the air than high-frequency wave

A

Greater

25
Q

Two reasons a turbofan engine produces less noise than a turbojet engine is:
__________
__________

A

The fan extracts extra energy from the exhaust gases

The exhaust gas velocities are lower

26
Q

A thrust reverser installed on a turbojet or turbofan engine produces a forward thrust that is between _________ and __________ percent of the engines rated forward thrust

A

40

50

27
Q

Two types of thrust reversers are those that use __________ doors and ___________ vaines

A

Clamshell

Cascade

28
Q

Thrust reversers are most effective on the ground when the speed is __________

A

High

29
Q

An afterburner is used on a supersonic commercial transport to decrease the time needed for the aircraft t reach its __________

A

Cruising altitude

30
Q

When the afterburner is being used, the area of the exhaust nozzle is __________

A

Increased

31
Q

The engine in a harrier jet produces a component of vertical thrust by vectoring the __________

A

Engine exhaust

32
Q

An augmented tube increases the flow of cooling through the engine cylinder fins because of low pressure caused by the high velocity___________ gases that flow through the tube

A

Exhaust