6.2- Aircraft Materials- Non Ferrrous Flashcards

1
Q

Why is titanium used widely in the aircraft industry?

A

High strength, light weight, temp resistance and corrosion resistance.

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2
Q

The weight of titanium is approximately what of steel?

A

56% but has the same strength.

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3
Q

What temperature is the strength of titanium held too?

A

800°F or 427°C.

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4
Q

What methods can titanium be worked by?

A

It can be sheared, drawn, pressed, machined, routed, sawn and nibbled.

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5
Q

What must the cutting dies and shear blades be made of to machine titanium?

A

Good quality steel and kept very sharp.

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6
Q

Why must a fire extinguisher be kept on hand when working with titanium?

A

Because the swarf is extremely flammable if a spark gets to it. Its recommended to use a liquid coolant whilst machining.

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7
Q

Titanium is not a good conductor of heat so what happens during machining?

A

The built up heat doesn’t dissipate.

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8
Q

Name some of the methods developed to machine titanium?

A

Use low cutting speeds
Maintain high feed rates
Use plenty of cutting fluid
Use sharp tools and replace them at the first sign of wear.

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9
Q

With the presence of oxygen what temperature will titanium ignite?

A

1065°C (1950°F).

with nitrogen it ignites at 815°C.

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10
Q

Why is pure cast aluminium highly corrosion resistant?

A

It has a non porous oxide coating that forms on the surface.

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11
Q

Wrought and cast irons are identified by a four digit system, what are the designated by?

A

The Aluminium Association of America (AA number).

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12
Q

What does the first digit of the AA number show?

A

Main alloying element.

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13
Q

What does the second digit of the AA number show?

A

Alloy modification.
0-orginal alloy
1-9- modifications.

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14
Q

What is the melting point of aluminium?

A

660°C

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15
Q

Aluminium alloys such as 2024 and 7075 are susceptible to corrosion, how are they protected.

A

With aluminium cladding, sheets of aluminium and 1% zinc.

Thickness is 3-5% of core

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16
Q

If the first digit of the aluminium designation is 2 what alloy is it?

A

Copper.

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17
Q

If the first digit of the aluminium designation is 3 what alloy is it?

A

Manganese.

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18
Q

If the first digit of the aluminium designation is 4 what alloy is it?

A

Silicon.

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19
Q

If the first digit of the aluminium designation is 5 what alloy is it?

A

Magnesium

6 is magnesium and silicon.

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20
Q

If the first digit of the aluminium designation is 7 what alloy is it?

A

Zinc.

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21
Q

If the first digit of the aluminium designation is 8 what alloy is it?

A

Other elements.

22
Q

Give the characteristics of 1100 aluminium.

A

Pure
Soft and ductile
Excellent corrosion resistance

23
Q

Give the characteristics of 3003 aluminium.

A

Manganese
Most widely used
Higher strength than 1100

24
Q

What is work hardening?

A

Strengthening of metal by plastic deformation.

25
Q

What is the process of solution heat treatment

A

Heated in molten sodium or potassium nitrate or hot air furnace. Temp is then held at +/- 50°C. Then cooled or quenched.

26
Q

What is natural age hardening?

A

Occurs at room temperature and is the process of copper precipitating the grain boundaries.

27
Q

How can age hardening be slowed down?

A

By freezing the alloy immediately after quenching.

28
Q

What is artificial age hardening also know as?

A

Precipitation hardening.

29
Q

What does artificial age hardening do?

A

Locks all the particles together in the grain, increasing strength stability and resistance to corrosion.

30
Q

How many times can a clad material be heat treated?

A

3 times.

31
Q

In the temper designation what does a W mean?

A

Unstable temper, solution heat treated.

32
Q

In the temper designation what does a F mean?

A

As fabricated (no treatment).

33
Q

In the temper designation what does a O mean?

A

Annealed.

34
Q

In the temper designation what does a H mean?

A

Strain hardened.

35
Q

In the temper designation what does a T mean?

A

Heat treated to produce stable tempers other than F, O or H.

36
Q

The temper designation is followed by a number 1-10 what do they represent?

A

The different sequence of treatments.

37
Q

If you saw TX… (e.g.TX51) in the temper designation what would this represent?

A

That it has been stress relieved. The digits that follow designate how it has been relieved.

38
Q

Non-heat treatable alloys are given what letter for designation?

A

H and then digits follow.

39
Q

If you saw H26 what would it mean for the alloy treatment?

A

Indicates strain hardened and partially annealed to 3/4 hard condition.

40
Q

If you saw H24 for example what do the first and second digits indicate?

A

1st- Treatment

2nd- Degree of hardness.

41
Q

The second digits of the strain hardening represent the degree of hardness, what are they and whats the values?

A

2 is a quarter through to 8 which is full hard and 9 which is extra hard.

42
Q

Magnesium is lighter than aluminium and was used extensively in aircraft until what three detrimental qualities were discovered?

A

At high risk to corrosion.

Difficult to work with.

Highly Flammable.

43
Q

What is a huge benefit of magnesium?

A

It is non magnetic which makes it useful for making instrument casings.

44
Q

No classification system is internationally accepted for magnesium alloys however what is used most?

A

American society for testing materials (ASTM).

45
Q

Can magnesium alloys get the same heat treatments as aluminium alloys?

A

Yes, including solution heat treatment, annealing etc.

46
Q

What does the acronym GLARE stand for?

A

Glass Reinforced Laminate its from the family of FML’s (Fibre metal laminates).

47
Q

What is an FML?

A

Consists of thin layers of metal sheet and uni-directional fibre layers.

48
Q

What does Glare consist of?

A

Aluminium and glass fibre prepreg layers.

49
Q

How many different grades of glare are there?

A

Six, they all have the consistent use of Cytec FM 94 adhesive.

50
Q

What does Glare 4B-4/3-0.4 indicate?

A

4B- Fibre orientation
4/3- 4 layers of aluminium and 3 fibre
0.4- aluminium thickness mm.

51
Q

What are the common uses of GLARE?

A

Fuselage skin on A380’s, aircraft cargo bay doors and blast resistant containers.

52
Q

What are the properties of GLARE? (6 examples)

A
High strength
Fatigue resistant
Damage tolerant
Impact and blast resistant
Fire resistant
Thermal isolation.