The Airframe Flashcards

(45 cards)

1
Q

What material usually forms the skin of an aircraft?

A

Aluminium

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2
Q

The fuselage is of what kind of construction?

A

Semi-monocoque

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3
Q

What is a monocoque construction?

A

No internal structure
Stress carried by the skin

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4
Q

What is a strut-type construction?

A

Internal framework carries all the stress

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5
Q

Semi-monocoque construction is a compromise between what two types?

A

Strut-type and monocoque

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6
Q

The windscreen typically consists of what material?

A

Perspex

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7
Q

Properties of perspex?

A

Easily scratched

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8
Q

In a wing, what attaches to the fuselage and extends to the wing tip?

A

Spar

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9
Q

What carries the major loads in a wing?

A

Spars

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10
Q

What wing structure provides external strength by transmitting extra loads to the fuselage?

A

Struts

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11
Q

What does a strut do?

A

Transmits extra loads of the fuselage

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12
Q

What structures run roughly perpendicular to the spars? in a wing

A

Ribs

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13
Q

What do ribs transmit?

A

Loads between the skin and the spars

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14
Q

What transmits loads between skins and spars?

A

Ribs

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15
Q

What calculation identifies the physical loads that an aircraft will undergo?

A

Stress analysis

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16
Q

What is stress caused by?

A

External forces acting on a material

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17
Q

What is stress?

A

Internal force that opposes deformation

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18
Q

What is strain?

A

The degree by which a material has been defroemd from a force or load

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19
Q

How are stress and strain different?

A

Stress is resistance to deformation
Strain is the degree of deformation

20
Q

What are the 5 major stresses?

A

Compression
Tension
Shear
Torsion
Bending

21
Q

What is tension?

A

Pulling apart

22
Q

What is compression?

A

Pushing together

23
Q

What is torsion?

A

Twisting apart

24
Q

What is shear?

A

Laterally shifting layers about a point

25
What occurs at the outside of a bend?
Tension
26
What occurs at the inside of a bend?
Compression
27
What stresses are aircraft meant to avoid?
Bending
28
Instead of bending, what are aircraft parts meant to undergo?
Tension and compression
29
Why is nylon better than manila rope (for tying down aircraft)?
It is more elastic and less likely to shrink when wet
30
How does carbon monoxide affect the body?
Displaces oxygen from the bloodstream
31
What can be fitted to the flight control system to prevent excessive movement?
Stops
32
The flight control system on most light training aircraft are of what type?
Mechanical flight control system
33
What is the Elastic Limit?
The limit of distortion at which the structure returns to its original shape and dimensions
34
What is the limit of distortion at which the structure returns to its original shape and dimensions?
Elastic limit
35
What is the Yield Point?
The point at which deformations become permanent
36
What is the point at which deformations become permanent
Yield Point
37
What is the Ultimate Load?
The load at which failure of the structure occurs
38
What is the load at which failure of the structure occurs?
Ultimate Load
39
What does Fail Safe mean?
If one part fails, the remaining parts in the system will continue to operate
40
What does Safe Life mean?
A component is released with a specific 'life' of hours or cycles, until replacement
41
If one part fails, the remaining parts in the system will continue to operate. This is given what term?
Fail Safe
42
A component is released with a specific 'life' of hours or cycles, until replacement. This is given what term?
Safe Life
43
The main weight of the aircraft is supported by what structures?
The main spar, connected to the undercarriage
44
What are fuselage formers?
Components that provide only 'shape' to the fuselage
45