Invention Grant
US08822874B2 Method and apparatus for microplasma spray coating a portion of a compressor blade in a gas turbine engine
有权
微型喷雾涂覆燃气涡轮发动机中压缩机叶片的一部分的方法和装置
- Patent Title: Method and apparatus for microplasma spray coating a portion of a compressor blade in a gas turbine engine
- Patent Title (中): 微型喷雾涂覆燃气涡轮发动机中压缩机叶片的一部分的方法和装置
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Application No.: US13664562Application Date: 2012-10-31
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Publication No.: US08822874B2Publication Date: 2014-09-02
- Inventor: Paul Zajchowski , Donn Blankenship , Gary C. Shubert
- Applicant: United Technologies Corporation
- Applicant Address: US CT Hartford
- Assignee: United Technologies Corporation
- Current Assignee: United Technologies Corporation
- Current Assignee Address: US CT Hartford
- Agency: Bachman & LaPointe, P.C.
- Main IPC: B23K10/00
- IPC: B23K10/00

Abstract:
A method and apparatus for microplasma spray coating a portion of a substrate, such as a gas turbine compressor blade, without masking any portions thereof. The apparatus includes a microplasma gun with an anode, cathode, and an arc generator for generating an electric arc between the anode and cathode. An arc gas emitter injects inert gas through the electric arc. The electric arc is operable for ionizing the gas to create a plasma gas stream. A powder injector injects powdered material into a plasma stream. A localized area of the compressor blade is coated with the powdered material without having to mask the compressor blade.
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