GH4141 Nickel-based superalloy GH141

GH4141 Nickel-based superalloy GH141

 

GH4141 (GH141) nickel-based superalloy overview

GH141 is a precipitation-hardening nickel-based deformed superalloy. It has high tensile and long-term creep strength and good oxidation resistance in the range of 650-950 ℃. Due to the high content of aluminum, titanium, and molybdenum in the alloy, it is difficult to open the ingot, but the deformed material has good plasticity. It can be cold-formed or welded in the annealed state. The welded parts are prone to strain during heat treatment Aging crack. The varieties of alloys include thin plates, belts, wires, discs, rings, forgings, bars, and precision castings. They are suitable for the manufacture of high-temperature aerospace and aerospace engines that require high strength below 870 ℃ and resistance to oxidation below 980 ℃. Parts.

 

GH4141 (GH141) nickel-based superalloy chemical composition

C	Cr	Ni	Ti	Mo	Al	Zr	Fe
0.06 0.12	18.00 20.00	margin	3.00 3.50	9.00  10.50	1.40 1.80	≤ 0.07	≤ 5.00
B	Cu	Co	Mn	Si	P	S
0.003 0.010	≤ 0.50	10.00 12.00	≤ 0.50	≤ 0.50	≤ 0.015	≤ 0.015

 

GH4141 (GH141) similar grades of nickel-based superalloys

GH141 GH4141, UNS N07041, Rene'41, R41, Carpenter41, PYROMET41, UNITEMP41, HynessalloyR41, J1610 (United States).

 

GH4141 (GH141) nickel-based superalloy variety specifications and supply status

Can provide various specifications of round cakes, ring blanks, ring parts, thin plates, strips, bars, forgings and precision castings. The plates are delivered in solid solution, and the bars and forgings are delivered without heat treatment.

 

GH4141 (GH141) nickel-based superalloy applications

GH4141 nickel-based deformed superalloy is suitable for manufacturing high temperature parts of aerospace engines that require high strength below 870 ℃ and oxidation resistance below 980 ℃.