Airframe Design and Materials Flashcards

(39 cards)

1
Q

Minor Failure

A

Probable

10^3

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2
Q

Major Failure

A

Remote

10^5

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3
Q

Hazardous Failure

A

Extremely Remote

10^7

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4
Q

Catastrophic Failure

A

Extremely Unprobable

10^9

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5
Q

Safe Life

A

The life of an aircraft which it will not suffer catastrophic failure.

May be used during a declared number of cycles or flight hours.

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6
Q

Fail Safe

A

The load is carried by other components if a part of the structure fails.

The limited amount of time that an aircraft can carry a failed load.

Can be carried until the next periodic inspection.

“PARALLEL LOAD PATHS”

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7
Q

Damage Tolerant structure

A

Load is spread over a large area.

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8
Q

Bending

A

The total combination of tension, compression and shear.

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9
Q

Tension

A

The outer edge stresses.

Can cause pulled rivets.

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10
Q

Compression

A

The inner edges squeezing together.

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11
Q

Shear

A

Occurs across the structure as forces try and tear it.

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12
Q

Stress

A

The internal force per unit area inside structural part, as a result of external loads

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13
Q

Strain

A
  • The quantifiable effects of stress

- The Deformation caused by the action of stress on a material

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14
Q

Buckling

A

Deformation occurring to a thin sheet after compressive forces.

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15
Q

What is a Stringer used for?

A

L shape metal that is bonded to skin.

Will PREVENT BUCKLING

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16
Q

Design Limit Load CS25

A

The maximum load the designer expects the aircraft to experience in service.

2.5g

Ultimate load = 2.5g x 1.5 = 3.75g

17
Q

Dynamic Load

A

Builds up quickly due to changes in flight conditions.

Produced when manoeuvring

Can be severe.

18
Q

Static Load

A

Build up slowly, fairly constant

19
Q

When does maximum stress occur at the wings?

A

Maximum stress occurs with empty wing tanks

20
Q

What provides bending relief at the wing roots?

A

Ailerons

Fuel in wings

Underslung engines.

21
Q

What does the Wohler Curve exhibit?

A

Relationship between stress and cycles to Failure

22
Q

Stress Corrosion

A

Combination of stress & corrosion.

Causes by fatigue.

Unpredictable and quick

23
Q

What determines the number of cycles to failure?

A

The amplitude or size of load

24
Q

Define an Alloy

A

A combination of two or more metals providing properties we didn’t have previously

25
Properties of an alloy
Elasticity Plasticity Strength Stiffness
26
Most common materials for alloys
Aluminium Titanium Magnesium Steel
27
What is the most common alloy used in today's modern manufacturing?
Duralumin
28
Properties of Duralumin
A copper-based aluminium alloy Good strength to weight ratio It's more susceptible to corrosion difficult to weld however
29
Alclad
Improvement to Duralumin Aluminium coating on its surfaces Duralumin gives it strength; Pure aluminium protects the Duralumin
30
What is steel composed of?
Iron and carbon
31
What are composite materials?
Two more materials with properties that are different to the original elements Consist of matrix, bulk, reinforcement The reinforcement is fibre.
32
Properties of composite materials?
Light weight Rigidity Strength
33
Why is the nosecone made from glass fibre?
Allows for radio waves to pass through, transparent.
34
Properties of Aramid/Kevlar
Impact proof
35
What is fibrelam used for
Flooring
36
Disadvantage of a honeycomb/sandwiched flooring
Not suitable for concentrated loads, loads must be spread.
37
Hard Time Maintenance
A component that is overhauled or replaced after a set number of hours, cycles or operations.
38
On Condition Maintenance
Visually check if performance is acceptable. Without disassembly, or removal from service.
39
Framework / Truss Fuselage
Frame takes all the loads