Sphärische Metallpulver GH3536 Superlegierung Hochtemperaturlegierungspulver

Produkt Charakter GH3536 high-temperature alloy is a nickel based alloy with high iron content that has been solid solution strengthened with Cr and Mo elements high temperature alloy, which has good corrosion resistance and oxidation resistance, can be used for a long time at 900 ℃, suitable for manufacturing combustion chamber components of aircraft engines with a short-term working temperature of 1080 ℃ other high-temperature components.   2.Spezifikation GH3536powder

Chemische Zusammensetzung (wt.%)
Element	C	Cr	Ni	Co	Mo	Al	Ti	Fe	B
Standard	0.05~0.15	20.5~23.0	Bal.	0.5~2.5	8.0~10.0	≤0.50	≤0.15	17.0~20.0	≤0.010
typisch	0.08	21.94	Bal.	1.42	8.97	0.14	0.012	18.98	0.002
Element	Mn	P	S	Cu	W	Si	O	N
Standard	≤1.0	≤0.025	≤0.015	≤0.50	0.2-1.0	≤1.0	≤0.030	≤0.030
typisch	0.26	0.005	0.005	0.007	0.55	0.34	0.017	0.024

 

GH3536	15~53μm Partikelgrößenverteilung			Durchflussrate (sec. für 50 g)	Scheinbare Dichte (g/cm3)	Klopfdichte (g/cm3)
	D10	D50	D90
Standard	15~25	30~40	50~60	≤25	≥4.2	≥4.9
typisch	23.4μm	36.2μm	55.2μm	20	4.24	5.03

  3 Bilder der SEM-Morphologie des Pulvers Bilder von Produktion und Test:   4.Anwendung

• GH3536  powder  is applied in combustion chamber components of aircraft engines and other high-temperature components.