Spherical Metal Powders GH5188 Cobalt based high-temperature alloy powder

Product Character：

GH5188 is a solid solution strengthened cobalt based high-temperature alloy, which is strengthened by adding 14% tungsten to give the alloy excellent high-temperature thermal strength. At the same time, adding a high content of chromium and trace amounts of lanthanum gives the alloy good high-temperature oxidation resistance. Compared to nickel based high-temperature alloys, GH5188 has more good creep resistance, thermal corrosion resistance, fatigue resistance, and high temperature strength. GH5188 has excellent formability, welding and other process properties, making it suitable for manufacturing parts for aircraft engines that require high strength below 980 ℃ and anti-oxidation below 1000 ℃. In the 1980s, GH5188 alloy was applied to components such as vortex plates and flame deflectors in turboshaft eight aircraft engines. Currently, some aircraft engines use GH5188 alloy sheets to prepare high-temperature components such as combustion chamber walls, outer walls, and sealing plates.

Brand Name	Jinchun
Origin	China
Product name	GH5188 powder
Application	Aircraft engines, etc.
Shape	Powder
Color	Metal gray
Size	15~53μm
Standard	GB/T 19001-2016/ISO9001: 2015
Purity	Ni: 20-24%, Cr:20-24%, W:13-16%, Co: Bal.
Material	Ni, Cr, W, Co
Packing	Vacuum packing

PRODUCT DETAIL

Product Character GH5188 is a solid solution strengthened cobalt based high-temperature alloy, which is strengthened by adding 14% tungsten to give the alloy excellent high-temperature thermal strength. At the same time, adding a high content of chromium and trace amounts of lanthanum gives the alloy good high-temperature oxidation resistance. Compared to nickel based high-temperature alloys, GH5188 has more good creep resistance, thermal corrosion resistance, fatigue resistance, and high temperature strength. GH5188 has excellent formability, welding and other process properties, making it suitable for manufacturing parts for aircraft engines that require high strength below 980 ℃ and anti-oxidation below 1000 ℃. In the 1980s, GH5188 alloy was applied to components such as vortex plates and flame deflectors in turboshaft eight aircraft engines. Currently, some aircraft engines use GH5188 alloy sheets to prepare high-temperature components such as combustion chamber walls, outer walls, and sealing plates. 2.Specification GH5188 powder

Chemical Composition (wt.%)
Element	C	Cr	Ni	Co	La	W	Si	Fe
Standard	0.05~0.15	20.0~24.0	20.0~24.0	Bal.	0.03~0.12	13.0~16.0	0.2~0.5	≤3.0
typical	0.11	22.33	22.17	Bal.	0.06	14.91	0.44	0.49
Element	Mn	P	S	Cu	B	O	N
Standard	≤1.25	≤0.02	≤0.015	≤0.070	≤0.015	≤0.030	≤0.030
typical	0.26	0.006	0.006	0.021	0.0092	0.017	0.01

GH5188	15~53μm Particle Size Distribution			Flow Rate (sec. for 50 g)	Apparent density (g/cm3)	Tap density (g/cm3)
	D10	D50	D90
Standard	15~25	30~40	50~60	≤25	≥4.55	≥5.30
typical	22.2μm	35.6μm	55.0μm	17	4.57	5.33

3.Pictures of Powder SEM morphology

Pictures of Production and Test:

4.Application

GH5188 has excellent formability, welding and other process properties, making it suitable for manufacturing parts for aircraft engines that require high strength below 980 ℃ and anti-oxidation below 1000 ℃. In the 1980s, GH5188 alloy was applied to components such as vortex plates and flame deflectors in turboshaft eight aircraft engines. Currently, some aircraft engines use GH5188 alloy sheets to prepare high-temperature components such as combustion chamber walls, outer walls, and sealing plates.