M6.2 Flashcards

1
Q

What is a non-ferrous metal?

A
  • Does not contain iron as it’s base material
  • non-magnetic
  • aluminium, copper, titanium, magnesium -> common in aircraft construction and repair
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2
Q

Advantages of aluminium alloyed with copper or zinc?

A
  • strong as steel
  • Only 1/3 of weight of steel
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3
Q

What are the 2 main classes of aluminium alloys?

A
  • Wrought aluminium alloys
  • cast aluminium alloys
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4
Q

Explain the 4 digit index of aluminium alloy?

A
  • 1st > Main alloying ingredient
  • 2nd > modification of alloy
  • 3rd > no special significance (alloy designator)
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5
Q

What is cladding?

A

-thin layer of pure aluminium applied at high temp

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6
Q

Common non-ferrous metals used in aircraft construction are?

A
  • magnesium
  • Titanium
  • Inconel
  • Monel
  • Copper
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7
Q

Properties of magnesium?

A
  • lightweight
  • Strong
  • non-magnetic
  • lower density compared to aluminium and weights 2/3 as much
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8
Q

Disadvantage of pure magnesium?

A
  • highly susceptibility to corrosion
  • easily cracked when form
  • burns readily
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9
Q

Where do they use magnesium alloys on an aircraft?

A
  • landing wheels
  • engine crankcases
  • valve bodies
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10
Q

Pure titanium is how much lighter than stainless steel approximately?

A
  • about 50% and equal in strength
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11
Q

What items are made using titanium on aircraft?

A
  • bolts + fasteners
  • flap tracks
  • engine compressor blades
  • firewalls
  • hydraulic pipes (that operate in high temp)
  • engine exhaust
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12
Q

Properties of pure titanium?

A
  • soft
  • ductile
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13
Q

What are the 2 common nickel alloys?

A
  • Monel
  • Inconel
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14
Q

Monel contains?

A
  • 68% nickel
  • 29% copper
  • small amounts of iron and manganese
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15
Q

Inconel contains?

A
  • 80% nickel
  • 14% chromium
  • small amounts of iron + other elements
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16
Q

What is heat treatment?

A
  • involvement of heating and cooling of metals in their solid state
  • increases properties
17
Q

What are the 2 types of heat treatment?

A
  • solution heat treatment
  • precipitation heat treatment
18
Q

What is solution heat treatment?

A
  • heating aluminium alloy to allow alloying element to mix with base metal
19
Q

What is precipitation heat treatment?

A
  • Soft when removed from quench bath
  • become hard and gain strength over time
20
Q

What is natural ageing?

A
  • alloy cooled at room temp
  • can take days/weeks
21
Q

What is annealing?

A
  • softens metal and decreases internal strength
  • opposite of hardening
22
Q

What does T stand for in temper designations?

A
  • alloy underwent solution heat treatment
23
Q

What does t3 stand for?

A
  • solution heat treated
  • followed by strain hardening
24
Q

What does t4 stand for?

A
  • underwent solution heat treatment
  • followed by natural ageing at room temp
25
Q

What does t6 stand for?

A
  • alloy underwent solution heat treatment
  • followed by artificial ageing
26
Q

Explain strain hardening (known as cold working or work hardening)?

A
  • mechanically working a metal at a temp below its critical range