Invention Application
- Patent Title: CMC COMPONENT INCLUDING DIRECTIONALLY CONTROLLABLE CMC INSERT AND METHOD OF FABRICATION
-
Application No.: US16119142Application Date: 2018-08-31
-
Publication No.: US20200072078A1Publication Date: 2020-03-05
- Inventor: Douglas Glenn Decesare , Daniel Gene Dunn
- Applicant: General Electric Company
- Main IPC: F01D25/00
- IPC: F01D25/00 ; F01D5/28

Abstract:
A ceramic matrix composite (CMC) component including a plurality of layers of a CMC and a directionally controllable CMC insert. The directionally controllable CMC insert is disposed in the plurality of layers of a ceramic matrix composite. The directionally controllable CMC insert includes an optimized architecture to strengthen a high stress region of the CMC component. The directionally controllable CMC insert is geometrically configured and disposed within the plurality of layers of the CMC to redirect a crack in the CMC component toward a region of low crack growth driving force. A turbomachine and method of forming a turbomachine member including a plurality of layers of a CMC and having the directionally controllable CMC insert disposed in a shaped void are additionally disclosed.
Public/Granted literature
- US11459908B2 CMC component including directionally controllable CMC insert and method of fabrication Public/Granted day:2022-10-04
Information query