首页> 外国专利> Engine intake flap for being arranged on the housing of an air intake of an aircraft engine, as well as engine with such an engine intake flap and aircraft system

Engine intake flap for being arranged on the housing of an air intake of an aircraft engine, as well as engine with such an engine intake flap and aircraft system

机译:用于布置在飞机发动机的进气口的壳体上的发动机进气门以及具有这种发动机进气门的飞机和飞机系统

摘要

An engine inlet flap for mounting on the housing of an air inlet or air inlet duct of an engine of an aircraft, having a first end and a second end arranged in opposition thereto at a distance therefrom in the longitudinal direction of the inlet flap, where the longitudinal direction in the given installation is aligned against the flow direction of the air flowing into the engine; and the inlet flap includes an inlet flap base body with a connector device for a jointed connector for jointed connection of the inlet flap base body to the housing of the air inlet or air inlet duct, with a rotational axis running along the second end, an inlet flap extension piece structurally integrated with the inlet flap base body, with a first and a second lateral piece, which extends from the inlet flap base body on the two opposed lateral edges of the inlet flap running in the longitudinal direction with a number of transverse struts or longitudinal struts, arranged in the leading region of the engine inlet flap.
机译:一种用于安装在飞机发动机进气口或进气管的壳体上的发动机进气盖板,其第一端和第二端在进气盖板的纵向上与之相对设置有一定距离。给定设备的纵向与流入发动机的空气的流向对齐;进气口风门包括进气口风门基体,该进气口风门基体具有用于接头的连接器装置,该连接器用于将进气口风门基体与进气口或进气口的壳体连接连接,并且旋转轴线沿第二端延伸。进口风门延伸件与进口风门基体在结构上集成在一起,具有第一和第二侧向件,该第一和第二侧向件从进口风门基体在进口风门的两个相对的侧向边缘上沿纵向延伸,并沿多个横向方向延伸。支柱或纵向支柱,布置在发动机进气阀瓣的前部区域。

著录项

  • 公开/公告号US8590832B2

    专利类型

  • 公开/公告日2013-11-26

    原文格式PDF

  • 申请/专利权人 LARS BOLENDER;SÉBASTIEN WAGNON;

    申请/专利号US20090865931

  • 发明设计人 LARS BOLENDER;SÉBASTIEN WAGNON;

    申请日2009-02-04

  • 分类号B64D33/02;F02G3;

  • 国家 US

  • 入库时间 2022-08-21 16:00:16

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