- Patent Title: Output assembly for an accessory gearbox of a gas turbine engine
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Application No.: US15906278Application Date: 2018-02-27
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Publication No.: US11002318B2Publication Date: 2021-05-11
- Inventor: Paolo Altamura
- Applicant: GE Avio Srl
- Applicant Address: IT Rivalta di Torino
- Assignee: GE Avio Srl
- Current Assignee: GE Avio Srl
- Current Assignee Address: IT Rivalta di Torino
- Agency: Dority & Manning, P.A.
- Priority: EP17425038 20170328
- Main IPC: F02C7/32
- IPC: F02C7/32 ; F16D9/08 ; F02C7/36 ; F01D25/36 ; F16D41/18 ; F16H35/10 ; F02C3/04 ; F16D41/069 ; F16H1/22

Abstract:
An output assembly for an accessory system of a gas turbine engine includes a first rotating member extending along an axis and including a mechanical connector for coupling the output assembly to an accessory system. The output assembly also including a second rotating member extending along the axis, the second rotating member coupled to the first rotating member at a first axial position and at a second axial position, the second rotating member coupled to the first rotating member at the second axial position through a one-way clutch. Additionally, the first rotating member of the output assembly further includes an extension member extending at least partially between the first axial position and the second axial position, the extension member including a designed fail point.
Public/Granted literature
- US20180283464A1 OUTPUT ASSEMBLY FOR AN ACCESSORY GEARBOX OF A GAS TURBINE ENGINE Public/Granted day:2018-10-04
Information query
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