Invention Grant
- Patent Title: Compressor blade flow form technique for repair
- Patent Title (中): 压缩机叶片流动形式修复技术
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Application No.: US11303579Application Date: 2005-12-15
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Publication No.: US08127442B2Publication Date: 2012-03-06
- Inventor: John F. Mullooly , William M. Rose , David R. Malley , Monika D. Kinstler
- Applicant: John F. Mullooly , William M. Rose , David R. Malley , Monika D. Kinstler
- 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: B23P6/00
- IPC: B23P6/00
Abstract:
A method for repairing a turbine engine component is provided. The method broadly comprises the steps of providing a turbine engine component having an airfoil portion, applying a coating to the airfoil portion, and restoring a tip portion, a chord, and surfaces of the airfoil portion to original dimensions in a single operation. A system for repairing the turbine engine component is also described.
Public/Granted literature
- US20090320287A1 Compressor blade flow form technique for repair Public/Granted day:2009-12-31
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