HAYNES® 556® alloy Site
Principal Features
Sulfidation Resistance
Carburization Resistance
Oxidation Resistance
Applications
Resistance to Chlorine-Bearing Environments
Other Environments
Physical Properties
Modulus of Elasticity
Tensile Properties
ASME Vessel Code
Creep and Rupture Properties
Impact Properties
Thermal Stability
Fabrication Characteristics
Welding
Health and Safety
Machining
HAYNES®556® alloy
Technical Briefs
HAYNES®556® alloy
Wire Information
Metallurgist Support
Sales Office Addresses
Tubular Products
Fittings & Flanges
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ASME Vessel Code Allowable Stresses |
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| HAYNES® 556® alloy is approved for ASME Vessel Code Section I construction to 1200°F (650°C) under Code Case No. 2010 and Section VIII Division 1 construction to 1650°F (900°C). Allowable stresses are reprinted here by permission of the ASME. |
ASME Vessel Code Allowable Stresses |
Metal
Temperatures
Not Exceeding |
Maximum Allowable Stress Values |
Standard |
Note(1) |
°F |
°C |
Ksi |
(MPa) |
Ksi |
(MPa) |
|
100 |
37 |
25.0 |
(172) |
25.0 |
(172) |
200 |
93 |
25.0 |
(172) |
25.0 |
(172) |
300 |
149 |
23.1 |
(159) |
24.5 |
(168) |
400 |
204 |
21.3 |
(146) |
23.7 |
(163) |
500 |
260 |
20.1 |
(138) |
23.1 |
(159) |
600 |
315 |
19.3 |
(133) |
22.8 |
(157) |
650 |
343 |
19.0 |
(131) |
22.7 |
(156) |
700 |
371 |
18.7 |
(129) |
22.5 |
(155) |
750 |
398 |
18.5 |
(127) |
22.4 |
(154) |
800 |
426 |
18.2 |
(125) |
22.3 |
(153) |
850 |
454 |
18.0 |
(124) |
22.2 |
(153) |
900 |
482 |
17.8 |
(122) |
22.1 |
(152) |
950 |
510 |
17.6 |
(121) |
21.8 |
(150) |
1000 |
537 |
17.4 |
(120) |
21.6 |
(148) |
1050 |
565 |
17.2 |
(118) |
21.4 |
(147) |
1100 |
593 |
17.1 |
(118) |
20.8 |
(143) |
1150 |
621 |
16.9 |
(116) |
16.9 |
(116) |
1200 |
648 |
13.6 |
(93) |
13.6 |
(93) |
1250 |
676 |
10.9 |
(75) |
10.9 |
(75) |
1300 |
704 |
8.8 |
(60) |
8.8 |
(60) |
1350 |
732 |
7.0 |
(48) |
7.0 |
(48) |
1400 |
760 |
5.6 |
(38) |
5.6 |
(38) |
1450 |
787 |
4.5 |
(31) |
4.5 |
(31) |
1500 |
815 |
3.6 |
(25) |
3.6 |
(25) |
1550 |
843 |
2.8 |
(19) |
2.8 |
(19) |
1600 |
871 |
2.2 |
(15) |
2.2 |
(15) |
1650 |
898 |
1.8 |
(12) |
1.8 |
(12) |
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NOTE(1)
Due to the relatively low yield strength of this material, these higher stress values were established at temperatures where the short time tensile properties govern to permit the use of these alloys where slightly greater deformation is acceptable. These higher stress values exceed 67%, but do not exceed 90% of the yield strength at temperature. Use of these stress values may result in dimensional changes due to permanent strain. These stress values are not recommended for flanges of gasketed joints or other applications where slight amounts of distortion can cause leakage or malfunction. |
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