F - Mech Eng,Light,Heat,Weapons – 01 – D
Patent
F - Mech Eng,Light,Heat,Weapons
01
D
F01D 11/12 (2006.01) C23C 4/18 (2006.01)
Patent
CA 2631362
The invention relates to a method for manufacturing a run-in coating, wherein a metallic run-in coating is provided on a stator-side component of a turbomachine, in particular a gas turbine. According to the invention, the provided run-in coating is subjected to a thermal treatment in order to improve its run-in capability.
L'invention concerne un procédé de fabrication d'une garniture d'admission dans lequel une garniture métallique d'admission est réalisée sur un composant du côté du stator d'un turbomoteur et en particulier d'une turbine à gaz. Selon l'invention, la garniture d'admission proposée subit un traitement thermique pour améliorer sa capacité d'admission.
Marks & Clerk
Mtu Aero Engines Gmbh
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