Hot gas-guided component of a turbomachine

Details Hot gas-guided component of a turbomachine Hot gas-guided component of a turbomachine

C - Chemistry, Metallurgy

23

C

C23C 30/00 (2006.01) F01D 5/28 (2006.01) C22C 38/06 (2006.01) C22C 38/18 (2006.01)

Patent

CA 2700755

The disclosure relates to a hot-gas conducting component for a flow machine having a nickel-base wrought alloy as structural material and a hot gas-side lining made from the group of iron-chromium-aluminum-yttrium alloys, and to a flow machine having a component of this type.

L'invention concerne un composant traversé par du gaz chaud pour une turbomachine, avec un alliage corroyé de base au nickel comme matériau structurel et avec un revêtement côté gaz chaud du groupe des alliages fer-chrome-aluminium-yttrium. L'invention concerne également une turbomachine dotée d'un tel composant.

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