Unlike heat-resistant steel, high temperature alloys can be used at higher temperatures and are resistant to high temperature oxidation and thermal corrosion. In the long-term and high temperature environment, the crystal structure is stable and the solid solution does not change. The characteristics of Gina high temperature alloys relying on alloy element design optimization and precision control, and special vacuum refining technology are excellent stability low degeneration on mechanical performance during whole service life and material safety guarantee.
ASTM B 637, B 670 SAE AMS 5589, 5590, 5596, 5597, 5662 – 5664, 5832, 5914, 5950, 5962
C≤0.08；Mn≤0.35；Si≤0.015；P≤0.35；S≤0.015；Cr17-21；Ni50-55；Mo2.8-3.3；Cu≤0.3；Ti0.65-1.15；Al0.2-0.8；Fe余量 Nb4.75-5.5；B≤0.006
Aerospace, Gas turbine
Sheet and Plate, Forging, Wire, Rod and Bar, Machined parts
ESR Ingot, ESR slab, Forged billet
Precipitation hardening nickel iron chromium alloy containing niobium, molybdenum and a small amount of aluminum and titanium. It combines the comprehensive characteristics of corrosion resistance, high strength and excellent welding resistance after weld
SAE AMS 5660, 5661
Ni 43, Cr 13; Fe Bal.; Mo 6; Ti 2.35-3,1;
Aerospace, Gas turbine
Forging, Rod and Bar, Machined parts
ESR Ingot, ESR slab, Forged billet
Titanium containing aluminum precipitation strengthened and molybdenum solution strengthened nickel iron chromium alloy has high temperature, high yield strength and creep resistance. The temperature of the alloy is as high as 600 degrees C.
ASTM B 163, B 166 – B 168, B 366, B 516, B 517, B 564
Ni 73; Cr 16; Fe 9; C 0.02-0.07
Chemical Process Industry, Oil and Gas, Automotive , Aerospace, gas turbin, Energy , Industry
Sheet and Plate, Strip, pipe and tube, Forging, Wire, Rod and Bar, Machined parts
ESR Ingot, ESR slab, Forged billet
Nickel and chromium alloy with high temperature oxidation resistance, chloride ion stress corrosion resistance, high purity water cracking and corrosion resistance to sulfur and alkali corrosion.
ASTM B 366, B 443, B 444, B 446, B 564, B 704, B 705, B 751, B 775, B 829
Ni 61; Cr 21,5; Fe 4,5; Mo 9; Nb 3.5;C 0.07;Si 0.15
Chemical Process Industry, Oil and Gas, Automotive , Aerospace, gas turbin, Energy , Industry
Sheet and Plate, Strip, pipe and tube, Forging, Wire, Rod and Bar, Machined parts
ESR Ingot, ESR slab, Forged billet
Ni Cr Mo alloy with Nb and Mo strengthening to improve the alloy strength. This alloy is resistant to extensive corrosion and particularly resistant to pitting and crevice corrosion.
ASTM B 366, B 443, B 444, B 446, B 564, B 704, B 705, B 751, B 775, B 829
Ni 61; Cr 21,5; Fe 4,5; Mo 9; Nb 3.5;C 0.02;N 0.01max;Si 0.1
Chemical Process Industry, Oil and Gas, Automotive , Aerospace, gas turbin, Energy , Industry
Sheet and Plate, Strip, pipe and tube, Forging, Wire, Rod and Bar, Machined parts
ESR Ingot, ESR slab, Forged billet
On the basis of 625 alloy, low carbon, low silicon and low nitrogen are controlled to improve the high temperature fatigue strength of materials.
ASTM A 240, A 480, B 163,B 366, B 407 – 409,B 514, B 515, B 564, B 751, B 775, B 829
Ni 30,5; Cr 20,5; Fe Bal.; Al+Ti max. 0,7;
Aerospace, Chemical process industry, Energy and environmental engineering
Sheet and Plate, Strip, pipe and tube, Forging, Wire, Rod and Bar, Machined parts
ESR Ingot, ESR slab, Forged billet
Ni Co Cr Mo alloy has high temperature oxidation resistance, alloy structure stability and corrosion resistance.
ASTM B 166 – B 168, B 751, B 775, B 829
Ni 60; Cr 23; Fe 14; AL 1,4;
Automotive, Chemical Process Industry, Energy and environmental engineering
Sheet and Plate, Strip, pipe and tube, Forging, Wire, Rod and Bar, Machined parts
ESR Ingot, ESR slab, Forged billet
Al Ni Cr alloy has high temperature oxidation resistance and corrosion resistance.
ASTM A 453, A 638SAE AMS 5525, 5726, 5731, 5732, 5734, 5737, 5858, 5895, 7235
Ni 25,5; Cr 15; Fe 56; Ti 2,1;
Aerospace, Automotive
Strip, Rod and Bar, Wire, Machined parts
ESR Ingot, ESR slab, Forged billet
Precipitation strengthened high strength alloy. The alloy has high temperature oxidation resistance and alloy structure stability. The temperature is as high as 700 C.
ASTM A 240, A 480, B 163,B 366, B 407 – 409,B 514, B 515, B 564, B 751, B 775, B 829
Ni 30,5; Cr 20,5; Fe Bal.; Al+Ti max. 0,7;
Automotive, Chemical Process Industry, Energy and environmental engineering
Sheet and Plate Strip Forging Rod and Bar Machined parts
ESR Ingot, ESR slab, Forged billet
On the basis of the 800 alloy, the creep fracture resistance and mechanical strength can be improved by strictly controlling the carbon aluminum titanium ratio and heat treatment system.
N08811
Ni 30,5; Cr 20,5; Fe Bal.; AL + Ti 1;
Automotive, Chemical Process Industry, Energy and environmental engineering
Sheet and Plate, Strip, pipe and tube, Forging, Wire, Rod and Bar, Machined parts
ESR Ingot, ESR slab, Forged billet
On the basis of the 800 alloy, the creep fracture resistance and mechanical strength can be improved by strictly controlling the carbon aluminum titanium ratio and heat treatment system.
BS 3076 (NA20), HR1,HR201, HR401, HR601
Ni 75; Cr 20; Ti 2,3; Al 1,4; C 0.06；
Aerospace, Automotive
Forging, Rod and Bar, Machined parts
ESR Ingot, ESR slab, Forged billet
Adding titanium and aluminum age hardening nickel chromium alloy, the service temperature is as high as 815 degrees C.
BS HR2, HR202, HR402,HR501 – HR503
Ni 余量; Co 19；Cr 20; Ti 2.5; Al 1.8; C 0.08；Cu 0.05；Zr 0.06；B 0.004；
Gas turbine
Forging, Rod and Bar, Machined parts
ESR Ingot, ESR slab, Forged billet
Ni Cr co precipitation strengthened alloy, high stress fracture resistant and creep resistant alloy, high temperature corrosion resistance and oxidation. The service temperature is up to 920 C.
AMS 5608 AMS 5772
Ni 22; Co 余量；Cr 22; C 0.07；Cu 0.05；Zr 0.06；B 0.004；Mn0.8；Si 0.3；La 0.02；W 14；Fe2；
Aerospace, Gas turbine
Forging, Rod and Bar, Machined parts
ESR Ingot, ESR slab, Forged billet
Cobalt based alloys with excellent high temperature properties. The temperature is below 1093 C. Good oxidation resistance and good sulfuration resistance, good metallurgical stability at high temperature.
AMS 5391 GB/T 14992 GJB 5512.1 Pratt&Whitney (PWA)655 Rolls Royce Corp(EMS)73632/73648 Honeywell(EMS)55371 Snecma (DMD) 0421-32
C 0.1; Cr 13.5; Ni Bal.; Mo 4.5; Nb 2; Ti 0.8; Al 6; B 0.01; Zr 0.06
Aerospace, Gas turbine, Automotive
Master alloy(Condition: Polish / Polish + Turning/ Turning)bar Ø2.875in/73 mm,Ø3.500in/89 mm,L≤1067mm.
.
Equiaxed crystal nickel based precipitation hardening high temperature alloy.
AMS 5377 GB/T 14992 GJB 5512.1 General Electric B50T1239 Rolls Royce Corp(MSRR)7048 Honeywell(EMS)55079/55444
C 0.06; Cr 12; Ni Bal.; Mo 4.3; Nb 2; Ti 0.7; Al 5.8; B 0.007; Zr 0.06
Aerospace, Gas turbine, Automotive
Master alloy(Condition: Polish / Polish + Turning/ Turning)bar Ø2.875in/73 mm,Ø3.500in/89 mm,L≤1067mm.
.
Equiaxed crystal nickel based precipitation hardening high temperature alloy.
AMS 5383 GB/T 14992 GJB 5512.1 Pratt&Whitney (PWA)649 / 1469/1490 General Electric B50T68/B50TF16 Rolls Royce Corp(MSRR)7132 Rolls Royce Corp(EMS)73618 / 73665 Honeywell(EMS)55422 Snecma (DMD) 0423-32
C 0.05; Cr 19; Ni 52.5.; Mo 3; Nb 5; Ti 0.9; Al 0.55; B 0.005;
Aerospace, Gas turbine
Master alloy(Condition: Polish / Polish + Turning/ Turning)bar Ø2.875in/73 mm,Ø3.500in/89 mm,L≤1067mm.
.
Equiaxed crystal nickel based precipitation hardening high temperature alloy.
GB/T 14992 GJB 5512.1
C 0.16; Cr 9.5; Ni Bal.; Co 15；Mo 3.1; Ti 4.75; Al 5.5; B 0.015; Zr 0.05 V 0.7
Aerospace, Gas turbine
Master alloy(Condition: Polish / Polish + Turning/ Turning)bar Ø2.875in/73 mm,Ø3.500in/89 mm,L≤1067mm.
.
Equiaxed crystal nickel based precipitation hardening high temperature alloy.
GB/T 14992 GJB 5512.1 Rolls Royce Corp(MSRR)7173 Rolls Royce Corp(EMS)73618 / 73661
C 0.09; Cr 16; Ni Bal.; Co 8.5; Nb 0.8; Mo 1.7; W 2.5;Ta 1.7;Ti 3.5; Al 3.5; B 0.01; Zr 0.05
Gas turbine
Master alloy(Condition: Polish / Polish + Turning/ Turning)bar Ø2.875in/73 mm,Ø3.500in/89 mm,L≤1067mm.
.
Equiaxed crystal nickel based precipitation hardening high temperature alloy with low density.
GB/T 14992 GJB 5512.1
C 0.16; Cr 9; Ni Bal.; Co 10；Mo 3.1; Ti 4.2; Al 5.5; B 0.015; Zr 0.06 V 0.7
Aerospace, Gas turbine
Master alloy(Condition: Polish / Polish + Turning/ Turning)bar Ø2.875in/73 mm,Ø3.500in/89 mm,L≤1067mm.
.
Equiaxed crystal nickel based precipitation hardening high temperature alloy with low density.
GB/T 14992 GJB 5512.1 General ElectricB50A563 Rolls Royce Plc. (MSRR)7125 / 7133 / 7228 Rolls Royce Corp (EMS)73657 Honeywell (EMS)55445
C 0.17; Cr 16; Ni Bal.; Co 8.5;W 2.5;；Mo 1.7; Ti 3.5; Al 3.5;Nb 0.8; Ta 1.7;B 0.01; Zr 0.1
Gas turbine
Master alloy(Condition: Polish / Polish + Turning/ Turning)bar Ø2.875in/73 mm,Ø3.500in/89 mm,L≤1067mm.
.
Equiaxed crystal nickel based precipitation hardening high temperature alloy.
GB/T 14992 GJB 5512.1
C 0.07; Cr 16.2; Ni Bal.; Co 11；Nb 0.2; W 5.7; Mo 2.1; Ti 4.8; Al 3.1; B 0.015; Zr 0.01 Y0.02；Hf 0.3;
Gas turbine
Master alloy(Condition: Polish / Polish + Turning/ Turning)bar Ø2.875in/73 mm,Ø3.500in/89 mm,L≤1067mm.
.
Equiaxed crystal nickel based precipitation hardening high temperature alloy.
GB/T 14992 GJB 5512.1
C 0.09; Cr 16.5; Ni5.2.; W 3.5；Nb 15.5；Mo 1.8; Ti 1.1; Al 2.5; Fe Bal；B 0.008; Zr 0.005 Y 0.008；La 0.05；
Gas turbine
Master alloy(Condition: Polish / Polish + Turning/ Turning)bar Ø2.875in/73 mm,Ø3.500in/89 mm,L≤1067mm.
.
Equiaxed crystal nickel based precipitation hardening high temperature alloy.
GB/T 14992 GJB 5512.1
C 0.45; Cr 25.5; Ni 10.5;Co Bal；W 7.5; B 0.007; Zr 0.05 Mn 0.6；Si 0.6；
Gas turbine
Master alloy(Condition: Polish / Polish + Turning/ Turning)bar Ø2.875in/73 mm,Ø3.500in/89 mm,L≤1067mm.
.
Equiaxed crystal Cobalt based precipitation hardening high temperature alloy.
General ElectricC50TF94
C 0.12; Cr 6.8; Ni Bal ;Co 12；W 5; Mo 2;Ta 6;B 0.015; Zr 0.02;Al 6.2；Hf 1.5;Re3；
Aerospace
Master alloy(Condition: Polish / Polish + Turning/ Turning)bar Ø2.875in/73 mm,Ø3.500in/89 mm,L≤1067mm.
.
Directional solidification Columnar crystal nickel based precipitation hardening high temperature alloy.
GB/T 14992 GJB 5512.1
C 0.11; Cr 21.5; Ni Bal.;Co 11.5；W 3.5；Nb 0.3；Mo 1.8; Ti 3.8; Al 2.8; Fe Bal；B 0.015; Zr 0.05 Y 0.02；La 0.01；
Gas turbine
Master alloy(Condition: Polish / Polish + Turning/ Turning)bar Ø2.875in/73 mm,Ø3.500in/89 mm,L≤1067mm.
.
Equiaxed crystal nickel based precipitation hardening high temperature alloy.
Gina Advanced Materials Corp., Ltd. is a manufacture in high performance specialty alloys and process solutions. Adhere to traditional business ethics and focus on technological Innovation, we are creating high performance products engineered for Industry mission critical service.
