Jan 24, 2025 Leave a message

GH5188 High Temperature Alloy

GH5188 nickel based superalloys has excellent creep and fatigue resistance and can maintain stable mechanical properties for a long time in high temperature environments.
GH5188 ni based superalloy is particularly suitable for manufacturing key components such as aircraft engine turbine blades, combustion chambers and turbine disks. Its high temperature corrosion resistance and good welding performance further enhance its reliability and durability under harsh working conditions.

GH5188's standard product forms include tubes, pipes, plates, strips, sheets, round bars, flat bars, forgings, hexagonal bars and wires. These products are available in a wide variety of sizes. Please contact us at ss@gneesteel.com for details.

GH5188 High Temperature Alloy Chemical Composition

C Cr Ni Co W Fe B La
0.05~0.15 20.0~24.0 20.0~24.0 Remain 13.0~16.0 ≤3.0 ≤0.015 0.03~0.12
Mn Si P S Ag Bi Pb Cu
No more than
≤1.25 0.20~0.50 0.02 0.015 0.001 0.0001 0.001 0.07

GH5188 High Temperature Alloy Physical Properties

Particle size range Particle size range Hall flow rate Bulk density Tap density
D10 D50 D90
15-53μm 17-22μm 32-38μm 52-58μm ≤18s/50g ≥4.80g/cm3 ≥5.40g/cm3

GH5188 High Temperature Alloy Mechanical Properties

variety Tensile properties Long-lasting performance Hardness HV Other features
θ/℃ σP0.2/MPa σb/MPa δ5/% θ/℃ σ/MPa t/h δ5/%
Not less than Not less than
Middle plate 20 380 860 45 815① 165 23 10 282 Grain size ≥ 4
927① 76 23 15
sheet 20 380 860 45 927 76 23 15 - Bending, oxidation resistance, grain size
650 250 620 50
Strip 20 380 860 40 927 62 23 8 - Bending 180°, anti-oxidation, grain size ≥ 4
δ≤0.51mm 650 250 620 40
Strip 20 380 860 45 927 76 23 15 -
δ>0.51mm 650 250 620 50
Rods 20 380 860 45 927 90 23 15 HBS≤302 Antioxidant
Forgings 20 380 860 45 927 83 23 15 HBS≤293 Antioxidant
Precision castings 20② 300 600 10 815 165 15 - - -

 

Available products and standard specifications
Specifications for GH5188 include the following:
GH5188GJB 3317-1998 Specifications for hot-rolled plates of high-temperature alloys for aviation use
GH5188Z9 0103-1990 Technical conditions for GH188 alloy plates
GH5188Z9 132-1999 Technical conditions for cold-drawn wires of GH188 alloy for welding
GH5188Q/5B 4002-1992 Cold-rolled strips of GH188 alloy
GH5188Q/5B 4003-1992 Cold-rolled plates of GH188 alloy
GH5188Q/5B 4014-1992 Technical conditions for GH188 alloy forgings
GH5188Q/5B 4020-1992 K188 alloy investment castings
GH5188Q/5B 4022-1992 GH188 alloy bar
GH5188Q/5B 4057-1992 GH188 high temperature alloy cold drawn welding wire

GH5188 nickel based superalloys GH5188 nickel based superalloys

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