Invention Application
- Patent Title: AIRCRAFT PROPULSION ASSEMBLY COMPRISING A THRUST FORCE UPTAKE DEVICE
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Application No.: US17947273Application Date: 2022-09-19
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Publication No.: US20230113400A1Publication Date: 2023-04-13
- Inventor: Michael Berjot , Thomas Robiglio , Karla Mariana Arellanes Mendoza
- 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: FR2109869 20210920
- Main IPC: B64D27/26
- IPC: B64D27/26

Abstract:
A propulsion assembly includes an engine below a pylon by engine attachments, including a thrust force uptake device, the engine having a longitudinal axis and a vertical median plane parallel to the longitudinal axis, the thrust force uptake device having a main fitting fixed below the pylon and two links disposed on either side of the vertical median plane and which each have a rear end articulated to the main fitting by a spreader mounted to pivot on the main fitting about an axis of rotation which, on the one hand, is orthogonal to a mean plane for transmitting thrust forces parallel to the longitudinal axis of each of the links, and which is disposed in the vertical median plane, each link being articulated to the spreader by a connecting pin extending parallel to the mean plane for transmitting thrust forces and perpendicular to the longitudinal axis of the link.
Public/Granted literature
- US11807374B2 Aircraft propulsion assembly comprising a thrust force uptake device Public/Granted day:2023-11-07
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