Invention Grant
- Patent Title: Aircraft engine assembly comprising at least two rear engine attachments axially shifted from each other
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Application No.: US15285211Application Date: 2016-10-04
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Publication No.: US10246196B2Publication Date: 2019-04-02
- Inventor: Olivier Pautis , Wolfgang Brochard
- Applicant: AIRBUS OPERATIONS (S.A.S.)
- Applicant Address: FR Toulouse
- Assignee: Airbus Operations (S.A.S.)
- Current Assignee: Airbus Operations (S.A.S.)
- Current Assignee Address: FR Toulouse
- Agency: Jenkins, Wilson, Taylor & Hunt, P.A.
- Priority: FR1559474 20151005
- Main IPC: B64D27/18
- IPC: B64D27/18 ; B64D27/26 ; F02C7/20 ; F02K1/08

Abstract:
In order to reduce the width of the attachment between the rear portion of an aircraft engine and its attachment pylon, an engine assembly attachment include an assembly of rear engine attachments comprising a first connecting rod laid out in a longitudinal and median vertical plane, a second connecting rod substantially laid out tangentially to the inter-turbine case, and a rear engine attachment for transversely spreading the loads, axially shifted rearwards relatively to the first and second connecting rods, and comprising a shear pin oriented along a vertical direction of the engine assembly.
Public/Granted literature
- US20170096229A1 AIRCRAFT ENGINE ASSEMBLY COMPRISING AT LEAST TWO REAR ENGINE ATTACHMENTS AXIALLY SHIFTED FROM EACH OTHER Public/Granted day:2017-04-06
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