Airframe Structures Flashcards

1
Q

The group of metals with have iron as their principal constituent, is?

A

Ferrous metals(steel)

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2
Q

If ferrous metals contain small quantities of other metals such as nickel, chromium and manganese, as steel alloy is formed such as -

A

stainless steel

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3
Q

The group of metals having elements other than iron as their principal constituent, is?

A

non ferrous metals

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4
Q

where small quantities of other metals have been added to the base metal, an -

A

alloy is formed

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5
Q

Define tension -

A

the stress that resists the force that tends to pull apart

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6
Q

Define compression -

A

the stress that tends to resist a “crushing” force

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7
Q

Define torsion -

A

The force that produces twisting

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8
Q

Define shear -

A

The stress that resists the force tending to slide one layer of material over another

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9
Q

Define bending -

A

The combination of compression and tension

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10
Q

Hoop and axial stress is the result of -

A

pressurisation within an aircraft

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11
Q

considering hoop and axial stress, which one is the radial stress within a tube?

A

hoop stress

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12
Q

considering hoop and axial stress, which one is the longitudinal stress within a tube?

A

axial stress

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13
Q

the three causes of a direct chemical attack -

A
  1. Battery acid
  2. Residual flux deposits from welding or brazing
  3. Caustic cleaning solutions that have become trapped
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14
Q

The cause of electrochemical attack is -

A

usually water

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15
Q

Ribs are used to -

A

form the wing shape

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16
Q

A single shell type structure, where all the flight loads are carried by the outer skin, is a -

A

Monocoque

17
Q

A stressed skin structure, usually an aluminium alloy, where the outer skin supports some of the load, but is also supported internally by formers and stringers to give both shape and rigidity to the structure, is a?

A

Semi-monocoque

18
Q

An oscillation affecting the whole wing structure -

A

torsional flexural flutter

19
Q

An oscillation affecting the wing structure due to the twisting effect on the wing by aileron -

A

torsional aileron flutter

20
Q

loads imposed on the wing while it is flexing due to the tendency of the aileron to lag behind the up and down movement of the wing as it is flexing. This is called?

A

Flexural aileron flutter

21
Q

The component that provides the main structural strength in the wing, running laterally, is called a?

A

Main spar

22
Q

The component that gives the aerofoil its shape, in the wing, is called a?

A

Rib

23
Q

In the wing Stringers run -

A

Laterally, or span wise from root to tip.

24
Q

The material that is conductive in order to heat aircraft windscreens, is called?

A

Stannic oxide

25
Q

An aircraft windscreen normally comprise of how many layers?

A

3 layers

26
Q

On an aircraft windscreen, the material that separates the tempered class and the stannic oxide is?

A

A sheet of transparent vinyl

27
Q

With an aircraft windscreen, what is included to prevent shatter?

A

A sheet of transparent vinyl

28
Q

The layer that provides the most strength in a windscreen?

A

The centre layer

29
Q

A centilever wing is one that requires -

A

no external bracing via struts

30
Q

Bending loads imposed on the fuselage are supported by -

A

longerons

31
Q

Bending loads on the wings are supported by -

A

frames, formers and stingers,

32
Q

Ribs are assisted in supporting torsional loads by internal -

A

struts

33
Q

The primary force is weight, acting vertically from the centre of gravity. On the ground, with the total mass of the aeroplane supported by its undercarriage, this causes -

A

tension on the upper surface of the wings and compression on the lower surface.

34
Q

During flight, lift tends to pull the wings up, resulting in -

A

compression on the upper surface and tension on the lower surface

35
Q

Stringers run longitudinally and serve to locate the frames and formers as well as provide -

A

support for the skin, preventing buckling and bending.