Invention Grant
- Patent Title: Gas turbine engine component with upstream-directed cooling film holes
-
Application No.: US14765222Application Date: 2014-02-04
-
Publication No.: US09958160B2Publication Date: 2018-05-01
- Inventor: James A. Dierberger
- Applicant: United Technologies Corporation
- Applicant Address: US CT Farmington
- Assignee: United Technologies Corporation
- Current Assignee: United Technologies Corporation
- Current Assignee Address: US CT Farmington
- Agency: O'Shea Getz P.C.
- International Application: PCT/US2014/014582 WO 20140204
- International Announcement: WO2014/123850 WO 20140814
- Main IPC: F23R3/06
- IPC: F23R3/06 ; F01D25/12 ; F01D25/30 ; F23R3/00
Abstract:
A component within a gas turbine engine includes a surface with one or more upstream-directed cooling film holes therethrough.
Public/Granted literature
- US20150369487A1 GAS TURBINE ENGINE COMPONENT WITH UPSTREAM-DIRECTED COOLING FILM HOLES Public/Granted day:2015-12-24
Information query
