Solution-annealed and Age-hardened Plate*
Temperature
|
Yield Strength
0.2% Offset |
Ultimate Tensile
Strength
|
Elongation
|
Reduction of Area
|
°F |
°C |
ksi |
MPa |
ksi |
MPa |
% |
%
|
RT |
RT |
103.7 |
715 |
166.4 |
1147 |
30 |
31
|
1000 |
538 |
94.1 |
649 |
143.8 |
991 |
34 |
36
|
1200 |
649 |
93.2 |
643 |
152.0 |
1048 |
31 |
31
|
1300 |
704 |
94.2 |
649 |
141.8 |
978 |
29 |
28
|
1400 |
760 |
91.1 |
628 |
124.2 |
856 |
22 |
24
|
1500 |
816 |
83.4 |
575 |
102.8 |
709 |
28 |
31
|
1600 |
871 |
73.6 |
507 |
82.1 |
566 |
31 |
42
|
1700 |
927 |
44.9 |
310 |
52.1 |
359 |
50 |
69
|
1800 |
982 |
19.1 |
132 |
25.3 |
174 |
71 |
91
|
*Solution Annealing: Sheet at 2100°F (1149°C), Plate at 2075°F (1135°C)
Age-Hardening: 1850°F (1010°C)/2h/AC + 1450°F (788°C)/8h/AC
RT= Room Temperature
Comparative Yield Strengths of Age-hardened* Sheet Material at Room Temperature and 1600°F (871°C)
At room temperature, HAYNES® 282® alloy has a higher yield strength than 263 alloy, but is not as strong as R-41 and Waspaloy alloys, which contain higher gamma-prime phase contents. However, at higher temperatures typical of gas turbine component applications, 282 alloy exhibits excellent yield strength, surpassing that of 263 and Waspaloy, and approaching that of the less fabricable R-41 alloy.

*Age-hardened (263 alloy: 1472°F (800°C)/8h/AC, Waspaloy alloy : 1825°F (996°C)/2h/AC + 1550°F (843°C)/4h/AC + 1400°F (760°C)/16h/AC, R-41 alloy: 1650°F (899°C)/4h/AC, 282® alloy: 1850°F (1010°C)/2h/AC + 1450°F (788°C)/8h/AC)