Invention Grant
- Patent Title: Trunnion retention for a turbine engine
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Application No.: US16108133Application Date: 2018-08-22
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Publication No.: US11053812B2Publication Date: 2021-07-06
- Inventor: Brandon Wayne Miller , Ian Francis Prentice , Daniel Alan Niergarth
- 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: Dority & Manning, P.A.
- Main IPC: F01D21/04
- IPC: F01D21/04 ; F01D5/30 ; F01D7/00 ; F04D29/32 ; B64C11/06 ; F01D25/16 ; F02C3/04 ; F04D27/02

Abstract:
A fan for a gas turbine engine is provided. The fan includes a plurality of fan blades, a disk, and a trunnion mechanism for attaching the fan blades to the disk. The disk can be formed of a plurality of individual disk segments, with the trunnion mechanism attaching one of the plurality of fan blades to a respective disk segment. A retention member is also provided. The retention member includes a means for catching a portion of the trunnion mechanism should a primary attachment system of the trunnion mechanism fail.
Public/Granted literature
- US20190093503A1 TRUNNION RETENTION FOR A TURBINE ENGINE Public/Granted day:2019-03-28
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