发明名称 Aerodynamic aft fairing of an aircraft engine suspension pylon
摘要 An aerodynamic aft fairing of an engine pylon ensuring the mounting of an engine underneath a wing of an aircraft is provided. The aerodynamic aft fairing includes an outer lateral panel and an inner lateral panel assembled together at least by a bottom panel, the bottom panel comprising, on either side of the lateral panels, an extension forming an aerothermic barrier capable of channeling hot air flows leaving the engine. The inner lateral panel and the outer lateral panel are attached to the bottom panel by a first angle bar and a second angle bar, respectively.
申请公布号 US8814080(B2) 申请公布日期 2014.08.26
申请号 US201213534967 申请日期 2012.06.27
申请人 Airbus Operations (S.A.S.) 发明人 Dumont Jean-François;Lefort Marc
分类号 B64D27/00 主分类号 B64D27/00
代理机构 Jenkins, Wilson, Taylor & Hunt, P.A. 代理人 Jenkins, Wilson, Taylor & Hunt, P.A.
主权项 1. An aft aerodynamic fairing of a suspension pylon for securing an engine mount under an aircraft wing, and comprising an inner lateral panel and an outer lateral panel, assembled together by at least one bottom panel, wherein: the bottom panel comprises, on either side of the lateral panels, an extension forming an aerothermic barrier for channeling hot air flows leaving an engine; the inner lateral panel is attached to the bottom panel by a first angle bar secured in an angle formed by the bottom panel and the inner lateral panel; and the outer lateral panel is attached to the bottom panel by a second angle bar secured in an angle formed by the bottom panel and the outer lateral panel.
地址 Toulouse FR