Non Ferrous Flashcards
What is the most widely used non ferrous material used in aircraft
Titanium
Advantages of Titanium
High strength to weight ratio
Temperature resistance
Corrosion resistance
Disadvantages of titanium
Horrible to work with
Flammable
When exposed at high temperatures in the presence of oxygen or nitrogen it will ignite
Pure Aluminium
Extremely malleable - to soft for aircraft use
Alloyed with other metals to increase strength
Excellent corrosion resistance
Very lightweight
Cast aluminium
Cast aluminium has a grain structure that is very coarse, thus the metal is brittle. Cast aluminium is used in construction of aircraft wheels and engine crankcases.
Wrought aluminium
Wrought, its grain structure is compressed and tightened as it is forced into shapes of plates, rods, extrusions or skins. Wrought aluminium (used extensively in aircraft construction) is either non-heat- treated or heat-treated.
Identification of Aluminium
Four digit number
1st digit - major alloying element
2nd digit - Alloy modification
Last two digits - different alloys in the group
Clad
A layer of pure aluminium with 1% zinc as a means of corrosion protection
3-5% thickness of the material
Ink print corresponds to material grain structure
1100 Pure aluminium
Commercially pure Soft Ductile Good workability Corrosion resistance NON HEAT TREATABLE
3003 Manganese aluminium
Most widely used
In trades strength up to 20%
Good corrosion resistance and workability
NON HEAT TREATABLE
5052 Magnesium aluminium
Most common High strength Good fatigue strength Good workability NON HEAT TREATABLE
2011 Copper aluminium
Most free-machining
Corrosion resistance
Good strength and hardness
HEAT TREATABLE
2017 Aluminium
Good machinablity High strength Tough Ductile HEAT TREATABLE
2024 Aluminium
Best known High strength Excellent fatigue resistance Low corrosion resistance Usually anodised finish or in clad form
7075 Zinc aluminium
High strength - density ratio
Non-weldable
Poor corrosion resistance
Normally clad