Light Alloys- Introduction Flashcards

1
Q

What are light elements?

A

Defined as those with density less than 5g/cm3

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2
Q

Narrowing down the light elements to use

A

31 light elements
14 are metals
8 are alkali or alkaline earth metals which are not suitable for engineering metals
Of remaining 6 Sc and Y are too rare and costly to use as alloy bases
Leaves Be, Mg, Al, Ti

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3
Q

Physical properties that are service limiting

A

Density ρ, Mg lowest
Melting point Tm, Ti highest
Modulus E, Be highest

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4
Q

Deformability and strength of Al

A

Only one with FCC
Easily drawn, extruded, rolled at low temperatures
Can be strengthened without loss in ductility

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5
Q

Deformability and strength of Ti, Mg, Be

A

When all HCP difficult to deform due to restricted slip modes
Pure Ti BCC above 882°C but needs alloying to stabilise this at room temperature (increases density)
Limitation of Be is brittleness and toxicity

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6
Q

Dimensional changes with temperature of Al and Mg

A

Both have high solidification contractions (so high shrinkage) compared to Fe. Can rectify by adding Si to Al castings to reduce αT and reduce solidification contraction to about zero at eutectique (13% Si) composition.

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7
Q

Conductivity of Al

A

Pure Al has 2/3 electrical conductivity and 1/2 density of Cu. Used for heavy applications in overhead wires and busbars. Cu mainly restricted to internal wiring

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8
Q

Fabrication of light metals

A

Mg has exceptional machinability (2x Al and 10x steel) because of high conductivity and low ductility. Combined with high castability makes Mg attractive. Ti shows poor machinability, formability, castability and conductivity.

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9
Q

Surface characterisation of light metals

A

All 4 form stable thin oxide films
High reflectivity and corrosion resistance of Al
Film can be thickened by anodising

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10
Q

Beryllium characteristics and uses

A

High specific modulus and melting point
Limited formability and high cost
Toxic
Low x-ray and neutron absorption
Limited to P/M and special applications
X-ray windows, satellite antennae, heat sinks for brakes, Cu-Be alloys, nuclear

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11
Q

Magnesium characteristics

A

Main competitor is Al
Processed mainly into castings
Good machinability
Lower latent heat per volume than Al
Weight advantage over Al
Worse formability and corrosion resistance
Production is only 2% of Al, 1/3 of it goes into Al alloys

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12
Q

Aluminium characteristics and uses

A

Good corrosion resistance and conductivity
Low weight
1/3 stiffness of steel, lower atom and higher cost
Poor fatigue resistance
Processed as wrought, cast or powder products
Building and domestic, transport and containers
Ti better in some high T applications
Compares favourably to plastics and is recyclable

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13
Q

Titanium characteristics and uses

A

Corrosion resistance food
Strength to weight ratio good
High Tm and good fatigue resistance
Biocompatible
High cost
Aerospace and aircraft engines/airframe
Non-aero uses depend mainly on corrosion resistance
Hip replacements, competes with stainless steel
Special melting procedures and equipment

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14
Q

Properties to consider when selecting light alloy

A

Cost, strength, density, stiffness,
Ductility, fracture toughness, fatigue resistance,
Creep resistance, corrosion, stress corrosion cracking

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15
Q

What is materials cost made up of?

A

Cost of purchase
Cost of ownership

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16
Q

How to minimise cost of ownership

A

Save weight (and fuel cost for transport)
Minimise cost of repair and part replacement (very high for PMSs and low for traditional light alloys)

17
Q

Order of material cost lowest to highest

A

Mild steel
Al alloys
Stainless and maraging steels
Ti alloys
Ni based superalloys
Carbon fibre reinforced polymer

18
Q

Extracting Ti data

A

TiO2 -> Ti + O2
ΔH0 224900
ΔS0 42.44
Total energy cost 125000 kWh/tonne

19
Q

Extracting Al data

A

1/2Al2O3 -> Al + 3/4O2
ΔH0 201630
ΔS0 39.06
Total energy cost 75000 kWh/tonnes (14000 from electrolysis)

20
Q

Extracting iron data

A

1/2Fe2O3 -> Fe + 3/4O2
ΔH0 97290
ΔS0 29.96
Total energy cost 15000 kWh/tonne (for steel)

21
Q

Problem of machining

A

Can be very material wasteful
In airbus wing skin panel 80% is machined away
Ti forgings for bulkheads in mid fuselage (not airbus) have about 90% machined away

22
Q

Super plastic forming and diffusion bonding

A

SPFDB of Ti and Al components is highly material efficient and can produce highly mechanically efficient components with significant weight savings

23
Q

Specific stiffness

A

E/ρ
Almost constant between engineering metals
Relevant for bending resistance
Be actually has much higher than rest

24
Q

Buckling resistance

A

E^1/3/ρ
This is specific elastic buckling resistance parameter
Represents performance of long thin panels of material
Low density alloys outperform heavy ones in terms of buckling resistance