unit 2 Flashcards

1
Q

A jet engine derives its name from its design in that it uses

A

an exhaust-gas driven turbine wheel to drive its compressor

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2
Q

A turbo-supercharger is essentially a

A

high-capacity air pump

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3
Q

The two forces that air is subjected to after it is drawn into the guide vanes of centrifugal compressor are

A

rotational and centrifugal

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4
Q

A constructional feature of the centrifugal compressor is that the impeller

A

is forged as a single unit

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5
Q

The jet engine compressor that is cheaper to manufacture is the

A

centrifugal type, because of its fewer parts

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6
Q

Which is a constructional feature of an axial-flow compressor casing?

A

Split along the horizontal centerline

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7
Q

The percentage of combustion efficiency of a gas turbine is usually between

A

95 and 100

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8
Q

What is the most probable cause of flameout of a jet engine flying at 40,000 feet with a constant engine revolution per minute (rpm) of 50 percent?

A

the rpm is too low

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9
Q

The excess airflow that is not burned in the combustion section is used to

A

mix with and cool the burned gases

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10
Q

The inner and outer surfaces of an annular-type combustion chamber are formed by

A

interlocking stainless-steel bands

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11
Q

Fuel that accumulates after a failed start is

A

drained overboard by a drain system

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12
Q

The parts on a can-annular combustion section must be removed in a specific order because of the

A

combustion chamber crossover tubes

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13
Q

What is the most common type of fuel nozzle system?

A

Pressure-atomizing

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14
Q

Three types of turbine and van assemblies used in jet engines are impulse, reaction, and

A

reaction-impulse

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15
Q

The “fir tree” method of attaching turbine blades (buckets) to the turbine rotor disc is preferred because

A

of the temperature differential between the turbine rotor disc and the blades.

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16
Q

In an non-afterburning engine, the exhaust duct connects the turbine outlet and the

A

jet nozzle

17
Q

The purpose of the exhaust duct is to

A

straighten exhaust gas-flow

18
Q

What is one common type of variable-area orifice that is used on augmentors?

A

Segmented-flap

19
Q

The purpose of an augmentor (afterburner) in a jet engine is to

A

augment the maximum thrust capability of the basic engine

20
Q

How many different types of loads can be imposed on a jet engine bearing?

A

three

21
Q

When you handle jet engine bearings, you must change cotton gloves frequently because they

A

get soaked with sweat

22
Q

Before inspecting new jet engine bearings, you should

A

remove the preservative coating

23
Q

Next to contamination and improper lubrication, what is the greatest enemy of antifriction bearings?

A

Improper removal

24
Q

The most commonly used bearing removal tools include

A

arbor presses and bearing pullers

25
Q

Which type of defect appears on bearings as a result of bearing parts striking together

A

nicks

26
Q

Which type of defect appears on bearings as a result of small particles of foreign material becoming lodged between the rollers?

A

Grooves

27
Q

Excessive bearing wear can usually be detected by

A

roughness of the metal

28
Q

Before you install separable bearings, you must ensure the

A

bearings are a matched set

29
Q

Of the following, the recommended method of expanding a bearing race before installation is to use a

A

hot-oil bath

30
Q

The reduction gearbox on an F100-PW-220 engine reduces speed between the main fuel gear pump and the engine-driven main gearbox by

A

52 percent