An iron-nickel-chromium-cobalt alloy that combines effective resistance to sulfidizing, carburizing and chlorine-bearing environments with good oxidation resistance, fabricability and excellent high-temperature strength.
HAYNES® 556® alloy is normally final solution heat-treated at 2150°F (1175°C) for a time commensurate with section thickness. Solution heat-treating can be performed at temperatures as low as about
2125°F (1165°C), but resulting material properties will be altered accordingly. Annealing during fabrication can be performed at even lower temperatures, but a final, subsequent solution heat treatment is needed to produce optimum properties and structure. Please refer to the following sections and publication H-3159 for additional information.
Typical Hardness Properties
Solution Annealed
Room Temperature Hardness
Form
RB
Sheet
91
Plate
96.5
Effect of Cold Reduction upon Room-Temperature Tensile Properties*
Percent Cold Reduction
Subsequent Anneal Temperature
Ultimate
Tensile Strength
Yield Strength
at 0.2% Offset
Elongation in
2 in. (50.8 mm)
Ksi
MPa
Ksi
MPa
%
0
None
115.0
795
52.9
365
50.7
10
127.8
880
93.3
645
34.8
20
142.1
980
113.3
780
23.5
30
172.6
1190
144.1
995
12.0
40
189.3
1305
155.8
1075
10.1
50
204.2
1410
169.7
1170
8.0
0
1850°F
(1010°C)
for 5 min.
114.7
790
52.6
365
44.8
10
121.6
840
76.9
530
34.3
20
127.0
875
88.8
610
30.3
30
135.2
930
92.7
640
26.6
40
133.3
920
80.0
550
30.6
50
135.0
930
83.0
570
31.7
0
1950°F
(1065°C)
for 5 min.
115.8
800
52.9
365
45.2
10
122.2
845
76.8
530
36.9
20
124.7
860
76.8
530
34.8
30
125.1
865
66.0
455
38.3
40
128.1
885
71.4
490
36.7
50
131.0
905
77.9
535
33.4
0
2050°F
(1121°C)
for 5 min.
117.0
805
54.3
375
47.0
10
117.4
810
55.3
380
48.0
20
120.1
830
58.4
405
45.4
30
123.6
850
63.5
440
43.0
40
124.7
860
66.9
460
42.4
50
126.6
875
70.8
485
35.0
* Based upon rolling reductions taken upon 0.120-inch (3.0mm) thick sheet. Duplicate tests.
Typical Microstructure
(ASTM 5 grain size) Annealed at 2150°F (1175°C) Etchant:95ml
HCL plus 5gm oxalic acid, 4 volts