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公开(公告)号:US20250010999A1
公开(公告)日:2025-01-09
申请号:US18761946
申请日:2024-07-02
Applicant: Airbus Operations SAS
Inventor: Michael BERJOT , Rémi LANSIAUX , Jean-Baptiste VIGNES , Veronica PARASCHIV
IPC: B64D27/40
Abstract: A propulsion unit comprising an engine, a pylon, an engine mount system which connects a front part of the engine and the pylon, in addition to a suspension system which connects the pylon and a rear part of the engine which is offset toward the rear end of the engine relative to the engine mount system.