Invention Grant
- Patent Title: Structural guide vane circumferential load bearing shear pin
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Application No.: US14433861Application Date: 2013-03-12
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Publication No.: US10167737B2Publication Date: 2019-01-01
- Inventor: Gregory E. Reinhardt , Paul Thomas Rembish , Steven L. Conner , Thomas B. Hyatt , Steven J. Feigleson , Carl Brian Klinetob
- 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: Carlson, Gaskey & Olds, P.C.
- International Application: PCT/US2013/030318 WO 20130312
- International Announcement: WO2014/062220 WO 20140424
- Main IPC: F01D25/26
- IPC: F01D25/26 ; F01D9/02 ; F01D25/16
Abstract:
A turbofan engine structural guide vane is mounted to a forward bulkhead of a core engine case structure at an inner end and to a fan case at an outer end. A plurality of shear pins extend from the aft portion of the structural guide vane into a corresponding plurality of openings defined in the bulkhead for bearing circumferential loads.
Public/Granted literature
- US20150275694A1 STRUCTURAL GUIDE VANE CIRCUMFERENTIAL LOAD BEARING SHEAR PIN Public/Granted day:2015-10-01
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