Invention Grant
- Patent Title: Process for applying a protective layer to a turbine component
- Patent Title (中): 将保护层施加到涡轮部件的工艺
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Application No.: US14398462Application Date: 2013-04-10
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Publication No.: US09309597B2Publication Date: 2016-04-12
- Inventor: Susanne Gollerthan , Torsten-Ulf Kern
- Applicant: Siemens Aktiengesellschaft
- Applicant Address: DE Munich
- Assignee: Siemens Aktiengesellschaft
- Current Assignee: Siemens Aktiengesellschaft
- Current Assignee Address: DE Munich
- Agency: Beusse Wolter Sanks & Maire
- Priority: EP12166937 20120507
- International Application: PCT/EP2013/057418 WO 20130410
- International Announcement: WO2013/167334 WO 20131114
- Main IPC: B23K31/02
- IPC: B23K31/02 ; C23C30/00 ; B23K35/30 ; B23K35/32 ; C23C26/02 ; B23K35/02 ; B23K1/00 ; C23C26/00
Abstract:
A turbine component is provided, on which a protective layer is arranged, for example to avoid droplet impact erosion, wherein, in a first method step, a nanofilm is applied and a brazing metal is applied to the nanofilm, and the nanofilm chosen is one which, after initial ignition, leads to an exothermic reaction, whereby fusion of the brazing metal with the base material takes place to form a protective layer.
Public/Granted literature
- US20150110962A1 PROCESS FOR APPLYING A PROTECTIVE LAYER TO A TURBINE COMPONENT Public/Granted day:2015-04-23
Information query
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