Invention Application
- Patent Title: ASSEMBLY OF A PRIMARY STRUCTURE OF AN AIRCRAFT PYLON AND A REAR ENGINE ATTACHMENT COMPRISING AT LEAST ONE LATERAL FASTENING ELEMENT AND AIRCRAFT COMPRISING AT LEAST ONE SUCH ASSEMBLY
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Application No.: US17733065Application Date: 2022-04-29
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Publication No.: US20220355945A1Publication Date: 2022-11-10
- Inventor: Paolo Messina , Olivier Pautis
- 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
- Priority: FR2104681 20210504
- Main IPC: B64D27/26
- IPC: B64D27/26
Abstract:
An assembly includes a rear engine attachment having a joining part, and also at least one support connected to the joining part by a connecting system. A lower spar of a primary structure of an aircraft pylon has a central part and also first and second lips disposed on either side of the central part and oriented in the direction of the rear engine attachment. The support has a base connected to the central part of the lower spar, at least one transverse flange supporting the connecting system and also at least one longitudinal flange connected to the base, pressed against the first or second lip of the lower spar and connected to the latter by at least one lateral connecting element.
Information query
