发明名称 Assembly for attaching the hangers from which an aircraft propulsion unit is suspended
摘要 An assembly is designed to attach hangers from which an aircraft propulsion unit is suspended. The propulsion unit is intended to be suspended from a structural element of the aircraft. The propulsion unit includes a turbojet engine having a longitudinal axis and the attachment assembly having a clevis mount for attaching the hangers to a casing of the propulsion unit. The clevis mount is fixed to the casing by means designed to form a connection between the clevis mount and the casing at the external periphery of the casing.
申请公布号 US8839629(B2) 申请公布日期 2014.09.23
申请号 US201313862724 申请日期 2013.04.15
申请人 Aircelle;SNECMA 发明人 Hurlin Herve;Dezeustre Nicolas;Balk Wouter;Charier Gilles
分类号 B64D27/26 主分类号 B64D27/26
代理机构 Brinks Gilson & Lione 代理人 Brinks Gilson & Lione
主权项 1. An assembly for attaching hangers from which an aircraft propulsion unit is suspended, said propulsion unit being suspended from a structural element of the aircraft, said propulsion unit comprising a turbojet engine having a longitudinal axis, said attachment assembly comprising at least one clevis mount and a casing for attaching said hangers to said propulsion unit, characterized in that the casing comprises at least two connecting flanges, a first flange of the at least two connecting flanges placed upstream of the clevis and a second flange of the at least two connecting flanges placed downstream of the clevis, said at least two connecting flanges forming a rigid connection between the clevis mount and the casing at an outer periphery of said casing and along an axis parallel to the longitudinal axis of the turbojet engine.
地址 Gonfreville l'Orcher FR