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 |