Aircraft Materials - Non-Ferrous Flashcards

1
Q

What is the effect of precipitation heat treatment on aluminium?

A

It speeds up age hardening process

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2
Q

Aluminium exposed to air will

A

Oxidise and become electrically insulated

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3
Q

What care should you take with 2024-T3?

A

Do not scratch or make nicks in it

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4
Q

If aluminium alloy is not quenched within minimum time allowed after heat treatment is it will be

A

Brittle

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5
Q

Anodising protects alloy metal from corrosion and does what else?

A

Makes a good surface for paint to adhere to

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6
Q

Pure aluminium is

A

Highly resistant to corrosion

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7
Q

Precipitation treating makes the metal

A

Harder, stronger and less ductile

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8
Q

A material has the code 2024-T6 on it. Which part of the code indicates the percentage of he alloying element?

A

24

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9
Q

Aluminium alloyed primarily with magnesium is numbered

A

50xx

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10
Q

Non heat treatable materials

A

Can be hardened by strain hardening or cold workings

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11
Q

Cold working of a material is used to reduce

A

Wear of manufacturing tools

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12
Q

The main metal in Monel is

A

Nickel

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13
Q

Why is nickel chromium used in many exhaust systems?

A

Corrosion resistant and low expansion Coefficient

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14
Q

Titanium alloys

A

Have a high strength to weight ratio

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15
Q

Which part of the 2017-T36 aluminium alloy designation indicates the primary alloying agent used in its manufacture?

A

20

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16
Q

Clad aluminium alloys are used in aircraft because they

A

Are less subject to corrosion than uncharted aluminium alloys

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17
Q

Non heat treatable aluminium alloys

A

Can be hardened by strain hardening

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18
Q

When buffing surface of Aluminium Alloy, what material are you removing?

A

Oxide layer

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19
Q

Why is clad alloy preferred to pure Aluminium?

20
Q

Why are aluminium alloys used on aircraft, instead of pure aluminium?

21
Q

Age hardening of aluminium is

A

Never carried out

22
Q

Alcad is

A

Duralumin with aluminium coating

23
Q

The oxide film on the surface of aluminium is

A

Non porous

24
Q

The process of rolling a layer of pure aluminium over an aluminium alloy is

25
The critical aspects of heat treatment are
Temperature, method of heating and cooling
26
What is generally true for titanium alloy?
It is stronger than aluminium
27
Malleable materials are
Easy to forge
28
If material has to undergo deep cold forming operation, the essential property would be
Malleability
29
When two or more metallic materials are fused together, the combination is known as
An alloy
30
Malleable materials are normally
Easily forged
31
How does large grain size effect the mechanical properties of metal?
Materials with large grain size are more prone to creep
32
The cracking of structural members under repeated stress lower than the ultimate tensile load is known as
Fatigue failure
33
A sheet of metal is designated 2024-T4, the code tells us that the material is a copper based aluminium alloy which has been
Solution treated and naturally aged
34
Money metal consists of approximately
66% nickel and 33% copper
35
The ease with which a material can be forged, rolled and extruded without fracture is an indication of a material's
Malleability
36
What is fatigue?
Cyclic stressing of a part
37
Annealing of aluminium
Removes stresses caused by forming
38
In the Brinell hardness test, you would measure the indentation's
Diameter
39
The impact testing technique is used on a material to test for
Toughness
40
What is a fusible material?
The ability of a metal to melt
41
Brittleness is
The property of inability to deform before cracking
42
Hooke's law states that, within the elastic region, elastic strain is
Directly proportional to stress
43
The given of stress for a given material can be derived by
Load / Cross sectional area
44
A material's yield strength is the ability to
Resist deformation
45
What type of a test involves stretching material until it breaks?
Tensile testing
46
How many times can clad alloy be heat treated?
3 times