Invention Application
- Patent Title: CMC Component with Flowpath Surface Ribs
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Application No.: US15841627Application Date: 2017-12-14
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Publication No.: US20190186271A1Publication Date: 2019-06-20
- Inventor: JinQuan Xu , Tracy A. Propheter-Hinckley
- Applicant: United Technologies Corporation
- Applicant Address: US CT Farmington
- Assignee: United Technologies Corporation
- Current Assignee: United Technologies Corporation
- Current Assignee Address: US CT Farmington
- Main IPC: F01D5/14
- IPC: F01D5/14 ; F01D5/28 ; F01D11/08 ; F01D25/00
Abstract:
A turbomachine airfoil element has a substrate. The substrate defines an airfoil having a pressure side and a suction side. A plurality of fiber composite ribs are along the pressure side.
Public/Granted literature
- US10605087B2 CMC component with flowpath surface ribs Public/Granted day:2020-03-31
Information query
