Superalloys
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GH1035(RUSSIA:XH38BT) |
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Physical Properties:
Density: 8.17g/cm3 Melting Point:℃
Modulus of Elasticity:142-199GPa Thermal Conductivity: 12.6λ/(W(m•℃)
Hardness: HBS230 Electrical Resistivity( 20 - 100°C):13.7x10-6K-1
Main Characteristics:Good anti-oxidation, plastic and impact properties.
Applications:900 ° C in the following long-term work of the turbine engine com-bustion chamber and turbine outer ring, exhaust.
Specification:Forgings,Rod, Plate, Strip,Ring, Wire, Bolts, Springs and other consultations supply, according to customer's production
Chemical Compositions:
|
Chemical Compositions(%) |
|
C |
Cr |
Ni |
Al |
Fe |
Ti |
W |
Nb |
Mn |
Si |
Ce |
P |
S |
|
0.06
-
0.12 |
20.0
-
23.0 |
35.0
-
40.0 |
≤
0.50
|
rem |
0.70
-
1.20 |
2.50
-
3.50 |
1.20
-
1.70 |
≤
0.70 |
≤
0.80 |
≤
0.05 |
≤
0.030 |
≤
0.020 |
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GH2132 (US: UNSS66286) (FRANCE: ZbNCT25) |
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Physical Properties:
Density:7.93g/cm3 Melting Point:1364~1424℃
Modulus of Elasticity:149.8~200GPa Thermal Conductivity: 14.2λ/(W(m•℃)
Hardness:HBS255 ~321 Electrical Resistivity( 20 - 100°C):16.09x10-6K-1
Main Characteristics:In the following 650 ° C with a high yield strength and lasting, creep has good strength and plastic processing and welding satisfied with the performance.
Applications:650 ° C in the following long-term work of the air force for high-temperature engine parts, such as the turbine disk, and so on.
Specification:Forgings,Rod, Plate, Strip,Ring, Wire, Bolts, Springs and other consultations supply, according to customer's production
Chemical Compositions:
|
Chemical Compositions(%) |
|
C |
Cr |
Ni |
V |
Fe |
Ti |
Mo |
Mn |
B |
Si |
Al |
P |
S |
|
≤
0.08 |
13.5
-
16.0 |
24.0
-
27.0 |
0.10
-
0.50 |
rem |
1.75
-
2.30 |
1.00
-
1.50 |
1.00
-
2.00 |
0.001
-
0.01 |
≤
1.00
|
≤
0.40 |
≤
0.030 |
≤
0.020 |
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GH3536 (US: UNS N06002 Hastelloy X) |
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Physical Properties:
Density:8.29g/cm3 Melting Point:1295~1381℃
Modulus of Elasticity:149~206GPa Thermal Conductivity: 13.39λ/(W(m•℃)
Hardness:HB90 Electrical Resistivity( 20 - 100°C):12.1x10-6K-1
Main Characteristics:At 900 ° C below middle of the lasting strength and creep, cold, heat-formed and welded good performance.
Applications:Aero-engine used in the manufacture of components and other high-temperature combustion chamber components.
Specification:Forgings,Rod, Plate, Strip,Ring, Wire, Bolts, Springs and other consultations supply, according to customer's production
Chemical Compositions:
Chemical Compositions(%) |
| C |
Cr |
Ni |
V |
Fe |
Ti |
Mo |
Mn |
B |
Si |
Al |
P |
S |
≤
0.08 |
13.5
-
16.0 |
24.0
-
27.0 |
0.10
-
0.50 |
rem |
1.75
-
2.30 |
1.00
-
1.50 |
1.00
-
2.00 |
0.001
-
0.01 |
≤
1.00 |
≤
0.40 |
≤
0.030 |
≤
0.020 |
|
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GH4145(US:Inconel X-750) |
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Physical Properties:
Density: 8.25g/cm3 Melting Point: 1395-1425℃
Modulus of Elasticity:160.8-213.7GPa Thermal Conductivity: 14.7 λ/(W(m•℃)
Hardness: -HBS100-350 Electrical Resistivity( 20 - 100°C):13.1 x10-6K-1
Main Characteristics:Below 980 ℃ has a good corrosion resistance and anti-oxidation performance, while forming a good performance and strong capability of welding.
Applications:Applicable to aviation engines, corrosion resistance of the plane wave springs and seals, etc.
Specification:Forgings,Rod, Plate, Strip,Ring, Wire, Bolts, Springs and other consultations supply, according to customer's production
Chemical Compositions:
|
Chemical Compositions(%) |
|
C |
Cr |
Ni |
Al |
Fe |
Ti |
Nb |
Co |
Mn |
Si |
Cu |
P |
S |
|
≤
0.08 |
14.0
-
17.0 |
rem |
0.40
-
1.00 |
5.00
-
9.00 |
2.25
-
2.75 |
0.70
-
1.20 |
≤
1.00 |
≤
1.00 |
≤
0.50 |
≤
0.05 |
≤
0.015 |
≤
0.010 |
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