HAYNES^® 214^® alloy is normally final solution heat-treated at 2000°F (1095°C) for a time commensurate with section thickness. Solution heat-treating can be performed at temperatures as low as about 1950°F (1065°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 structure and properties. It is imperative that components be cooled as rapidly as possible from intermediate and final anneal operations in order to achieve maximum ductility.

Typical Hardness Properties for Sheet

Condition	Rockwell C Hardness

Solution Annealed	24.3
10% Cold Reduced	33.8
20% Cold Reduced	37.6
30% Cold Reduced	40.6
40% Cold Reduced	42.4
50% Cold Reduced	43.0

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)	Hardness
Percent Cold Reduction	Subsequent Anneal Temperature	Ksi	MPa	Ksi	MPa	%	R_C

0	None	144.7	1000	86.2	595	36.3	24.3
10		159.4	1100	121.9	840	22.5	33.8
20		176.5	1215	148.8	1025	12.9	37.6
30		194.1	1340	169.5	1170	8.1	40.6
40		208.6	1440	183.2	1265	5.3	42.4
50		219.8	1515	193.8	1335	4.0	43.0

0	1800° (982°C) for 5 min.	-	-
10		147.2	1015	90.8	625	33.1	27.4
20		150.3	1035	89.9	620	33.7	24.9
30		155.6	1075	94.2	650	33.5	27.1
40		154.3	1065	92.5	640	33.7	27.9
50		157.9	1090	95.1	655	33.7	29.3

0	1900° (1038°C) for 5 min.	-
10		145.5	1005	83.6	575	36.2	24.3
20		149.5	1030	88.5	610	34.6	25.1
30		151.8	1045	91.8	635	33.3	24.0
40		154.1	1060	95.2	655	32.9	24.3
50		152.0	1050	90.3	625	32.3	24.4

0	2000° (1093°C) for 5 min.	-
10		143.6	990	84.8	585	36.4	22.9
20		145.8	1005	87.2	600	34.4	24.0
30		146.2	1010	84.5	585	36.5	24.5
40		147.4	1015	86.1	595	36.5	22.5
50		148.3	1020	86.8	600	34.7	23.3

* Based upon rolling reductions taken upon 0.120-inch (3.0mm) thick sheet. Duplicate tests.

Haynes International, Inc. 800-354-0806 765-456-6012

HAYNES® 214® alloy Information

A nickel-chromium-aluminum-iron alloy with outstanding resistance to oxidation.

HAYNES^® 214^® alloy Information