Invention Grant
- Patent Title: Aircraft engine assembly, comprising an attachment device for the engine equipped with a structural cover attached on a central box
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Application No.: US15381821Application Date: 2016-12-16
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Publication No.: US10562639B2Publication Date: 2020-02-18
- Inventor: Olivier Pautis , Jean-Michel Rogero
- 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: FR1562540 20151216
- Main IPC: B64C27/26
- IPC: B64C27/26 ; B64D27/26 ; B64D27/18 ; B64D29/06 ; F02C7/20

Abstract:
In order to reduce congestion of attachments between an aircraft engine and its attachments, an engine assembly is provided, the primary structure of the device of which includes a structural cover surrounding the engine and connected on a central box, the cover including an outer skin interiorly delimiting a secondary flow. A group of main mounts is provided as a group of secondary mounts laid out at the rear of the group of main mounts, the group of main mounts including a plurality of bolts distributed around the longitudinal axis of the engine and ensuring the attachment of a front end of the cover to the hub of the intermediate case, and a group of secondary mounts including a plurality of secondary mounts distributed around the axis and ensuring attachment of a rear portion of the engine to a rear end of the cover.
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