HITEALLOY

GH3536 is a Fe Ni Cr based solid solution strengthened deformation high-temperature alloy, which has moderate durability and creep strength at high temperatures of 900 ℃. It has good oxidation and corrosion resistance, good cold and hot processing formability, and welding performance, suitable for making components such as aviation engine combustion chambers that are used for a long time below 900 ℃, as well as high-temperature components that can work at temperatures up to 1080 ℃ for short-term use. Mainly including plates, strips, pipes, rods, forgings, and castings. Widely used in civil industry and aviation engines, for manufacturing steam turbines (combustion chambers, rectifiers, structural covers), industrial furnace components, support rollers, grid plates, ribbons and radiation tubes, and spiral tubes in petrochemical furnaces.

Corresponding brand:

UK	ASTM	UNS、SAE	DIN	EN	Grade	Old Grade
Nimonic PE13	Hastelloy X	No6002	NiCr22FEMO	K4536	GH3536	GH536
				K536		SG-5

Chemical composition:

%	C	Cr	Ni	W	Mo	Fe	B	S	Mn	Si	P	Cu	Ti	Al	Co
Min	0.05	20.5	-	0.2	8	17	-	-		-		-		-	0.5
Max	0.15	23	Remainder	1	10	20	0.01	0.015	1	1	0.015	0.5	0.15	0.5	2.5

Physical performance:

density g/cm³	magnetism	Thermal conductivity/w/(m.k)	resistivity	Specific heat capacity	linear expansion coefficient
		100~900℃	C)/(Ω.mm2/m)	℃)/kg/(kj.k)℃	/(10-6/k)
			20~900℃	100~900℃	20~900℃
8.28	None	13.38-33.44	1.18-1.29	0.3726-0.561	16.1
temperature 0/℃	20	100	200	400	600
Elastic modulus E/GPa	206	230	199	187	174