Invention Grant
- Patent Title: CMC turbine components and methods of forming CMC turbine components
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Application No.: US14612806Application Date: 2015-02-03
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Publication No.: US09718735B2Publication Date: 2017-08-01
- Inventor: John McConnell Delvaux , Andres Jose Garcia-Crespo , Victor John Morgan , Jacob John Kittleson
- Applicant: GENERAL ELECTRIC COMPANY
- Applicant Address: US NY Schenectady
- Assignee: General Electric Company
- Current Assignee: General Electric Company
- Current Assignee Address: US NY Schenectady
- Agency: McNees Wallace & Nurick LLC
- Main IPC: B32B3/24
- IPC: B32B3/24 ; F01D25/12 ; F01D25/24 ; C04B35/00 ; C04B35/44 ; C04B35/52 ; C04B35/565 ; B29C70/54 ; F01D5/18 ; B29C71/04 ; F01D25/14 ; F01D5/28 ; F01D11/08 ; F02C6/06 ; F02C6/08 ; B29L31/00 ; B32B3/26 ; F01D11/24

Abstract:
Components are disclosed which include a CMC substrate having a first surface and a second surface. The first surface is in fluid communication with a compressed, dry fluid, and the second surface is in fluid communication with a wet fluid stream and includes a hermetic coating. The components further include at least one opening extending from the first surface through a portion of the CMC substrate, wherein, upon removal of a fragment of one or both of the hermetic coating and the CMC substrate, the at least one opening selectively permits a flow of the compressed, dry fluid to the second surface. In one embodiment, the component is a gas turbine component, the wet fluid stream is a hot combustion stream, the hermetic coating is an environmental barrier coating, and the flow reduces or eliminates volatilization of the CMC substrate. Methods for forming the components are also disclosed.
Public/Granted literature
- US20160221881A1 CMC TURBINE COMPONENTS AND METHODS OF FORMING CMC TURBINE COMPONENTS Public/Granted day:2016-08-04
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