Invention Application
- Patent Title: CERAMIC COATING COMPOSITIONS FOR COMPRESSOR BLADE AND METHODS FOR FORMING THE SAME
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Application No.: US15278860Application Date: 2016-09-28
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Publication No.: US20180087515A1Publication Date: 2018-03-29
- Inventor: Neelesh Nandkumar Sarawate , Larry Steven Rosenzweig , Sathyanarayanan Raghavan , Changjie Sun , Ananda Barua , Jinjie Shi
- Applicant: General Electric Company
- Main IPC: F04D29/02
- IPC: F04D29/02 ; F04D29/32 ; C23C30/00

Abstract:
Coating systems for components of a gas turbine engine, such as a compressor blade tip, are provided. The coating system can include a ceramic material disposed along the compressor blade tip and may be used with a bare compressor casing. The ceramic coating is harder than the bare compressor casing and can reduce the rub ratio thereby increasing the lifetime of the compressor blades. Methods are also provided for applying the coating system onto a compressor blade.
Public/Granted literature
- US10415579B2 Ceramic coating compositions for compressor blade and methods for forming the same Public/Granted day:2019-09-17
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