Materials Flashcards

1
Q

Stiffness

A

Young’s Modulus

Early elastic deformation

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2
Q

Strength

A

Ultimate load bearing capacity prior to failure

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3
Q

Toughness

A

Energy absorbed before fracture

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4
Q

Ductility

A

Ability to deform

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5
Q

Brittle

A

Opposite to ductile

Low deformation before fracture

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6
Q

Hardness

A

Resistance to surface deformation

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7
Q

Ductility test

A

A bar of the material is bent in the middle with force applied in the middle and at the ends.

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8
Q

Fatigue test

A

A cyclic load is applied below UTS

Tests crack initiation, growth and tensile overload failure

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9
Q

Steel- pros and cons

A

Pros
UTS
Good elevated temperature properties
Cheap and readily available

Cons
Relatively high density
Poor Strength/weight
Corrosion problematic
Difficult to fabricate
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10
Q

Aluminium

A
Pros
Low density
Good strength/weight
Easily fabricated by many routes
Relatively inexpensive

Cons
Low hardness
Poor Corrosion resistance
Relatively poor fatigue performance

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11
Q

Titanium

A
Pros
Relatively lightweight
Excellent corrosion resistance
High strength/weight
Good high temperature properties
Demonstrates super-plasticity-complex forms

Cons
Relatively high price
Difficult to form at room temp
Expensive to machine

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12
Q

Types of Composites

A
Fibreglass
Carbon fibre reinforced polymer
Wood
MMC's
CMC's
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13
Q

Fibre orientation and loading

A

Fibre orientation matched to principal stresses

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14
Q

GLARE Technology

A

Hybrid material
Alternating layers of aluminium foils and unidirectional glass fibres
Impregnated with adhesive

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15
Q

Jet engine work cycle

A

Suck-Squeeze-Bang-Blow

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16
Q

Fan in a jet engine

A

Intakes a large volume of air

17
Q

Compressor

A

Reduces air volume and raises pressure

18
Q

Combustor

A

Air+Fuel mixed and ignited

19
Q

Turbine

A

Exhaust gases expelled, turbines rotates fan and compressor via shaft/gears

20
Q

How much thrust is produced by air directly expelled around the outside of a high bypass gas turbine?

A

Up to 50%

21
Q

How many flight cycles are engines typically designed for?

A

30,000 flights

22
Q

Temperature at fan intake

A

-60 degrees celsius

23
Q

Temperature at IP compressor

A

300 degrees celsius

24
Q

Temperature at the HP compressor

A

600 degrees celsius

25
Q

Temperature at the combustor

A

1200 degrees celsius

26
Q

Temperature at the turbine/exhaust

A

> 1200 degrees celsius

27
Q

Fan/Compressor material

A

Titanium

28
Q

Combustor/Turbine material

A

Nickel

29
Q

Why is having a single crystal turbine blade desired?

A

Excellent mechanical properties in longitudinal axis and improved heat resistance

30
Q

How are the HP turbine blades cooled?

A

Blade temperature would exceed melting point of Nickel so cooling air plus ceramic thermal barrier coatings are used to prevent this

31
Q

Engine Tests

A

Bird strike (impact)
Fan blade off (containment)
Hail and water ingestion