- 专利标题: COMPONENT OF A MOLYBDENUM ALLOY AND METHOD FOR FORMING AN OXIDATION PROTECTION LAYER THEREFOR
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申请号: US15431925申请日: 2017-02-14
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公开(公告)号: US20170241271A1公开(公告)日: 2017-08-24
- 发明人: Markus FRIED , Wilfried SMARSLY , Andreas BROETZNER
- 申请人: MTU Aero Engines AG
- 优先权: DE102016202872.3 20160224
- 主分类号: F01D5/28
- IPC分类号: F01D5/28 ; C22C30/00 ; C23C14/16 ; F01D9/02 ; C23C14/58 ; C23C16/42 ; C23C16/38 ; C23C16/56 ; C22C27/04 ; C23C14/34
摘要:
Disclosed is a method for improving the high-temperature stability of a component, in particular a blade of a turbomachine, formed at least partially from a molybdenum alloy that, besides molybdenum, silicon, boron and titanium, comprises iron and/or yttrium. The method comprises depositing a diffusion barrier layer formed from technically pure molybdenum or tungsten or being an alloy based on molybdenum and/or tungsten at least on an outer surface, which comprises the molybdenum alloy, of the component, and depositing silicon on the diffusion barrier layer to form molybdenum silicides and/or tungsten silicides.
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