Customization: | Available |
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Material: | Ni-Cr-Co-W Alloy |
Refractoriness (℃): | Refractoriness> 2000 |
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Grade
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Thickness(mm)
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Allowable Thickness Deviation(mm)
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Test temperature
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HVHV(Hardness) |
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General precision
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High Precision
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GH5188 GH5605 GH738 |
0.25<T≤0.6 |
+/-0.015 |
+/-0.01 |
23ºC |
GH5188 239/234/239 |
GH5605 262/260/267 |
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0.6<T≤1.0 |
+/-0.020 |
+/-0.015 |
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+/-0.030 |
+/-0.020 |
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1.0<T≤2.0 |
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Solid solution strengthened cobalt base superalloy with 14% - 15% tungsten solid solution strengthening makes the alloy have excellent high temperature thermal strength. Adding high content of chromium and trace lanthanum, the alloy has good high temperature oxidation resistance, satisfactory molding and welding process performance. It is suitable for manufacturing combustion chamber and guide vane of aeroengine, and high temperature parts with high oxidation resistance Application scope: aero engine combustion chamber, guide vane, high temperature parts, etc., can also be made into thin plate, strip, etc |