Module 5 Non-Ferrous Alloys Objective Two

Question 1

Temper Designations: F

Answer 1

as-fabricated

Question 2

Temper Designations: O

Answer 2

Annealed

Question 3

Temper Designations: H11 to H19

Answer 3

strain hardened only

Question 4

Temper Designations: H21 to H29

Answer 4

strain hardened and partially annealed

Question 5

Temper Designations: H31 to H39

Answer 5

strain hardened and thermally stabilized

Question 6

Temper Designations: W

Answer 6

solution heat treated

Question 7

Temper Designations: T1

Answer 7

cooled from an elevated-temperature shaping process (naturally aged)

Question 8

Temper Designations: T2

Answer 8

cooled from an elevated temperature shaping process, cold worked, and naturally aged

Question 9

Temper Designations: T3

Answer 9

solution heat treated, cold worked and naturally aged

Question 10

Temper Designations: T4

Answer 10

solution heat treated (naturally aged)

Question 11

Temper Designations: T5

Answer 11

cooled from an elevated-temperature shaping process and then artificially aged

Question 12

Temper Designations: T6

Answer 12

solution heat treated and then artificially aged

Question 13

Temper Designations: T7

Answer 13

solution heat treated and stabilized

Question 14

Temper Designations: T8

Answer 14

solution heat treated, cold worked and then artificially aged

Question 15

Temper Designations: T9

Answer 15

solution heat treated, artificially aged, and then cold worked

Question 16

Temper Designations: T10

Answer 16

cooled from an elevated-temperature shaping process, cold worked, and then artificially aged

Question 17

Anodizing

Answer 17

an electrolytic oxidation process that thickens the protective surface oxide film to improve the corrosion and wear resistance

Question 18

Cladding

Answer 18

gives the corrosion resistance of pure aluminium with the strength of strong alloy, done by placing a pure aluminium plate onto an alloy and then hot rolling.

Question 19

Aluminium/Lithium alloys

Answer 19

have good fatigue crack propagation resistance and are useful in aerospace applications