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Air intake, in particular for an aircraft chaff dispenser

机译:进气口,特别是用于飞机谷壳分配器的进气口

摘要

An aircraft chaff dispenser includes an elongated hollow housing intended to be fixed to the structure of the aircraft so as to be oriented in the longitudinal direction of the aircraft. The housing has a pair of side walls and the front of each side wall is provided with a pair of lateral air intakes each having a circular through-hole with a diameter d and a fence located behind the hole in the longitudinal direction, or in the direction of travel, of the aircraft at a distance 1 from the center of the hole and having a shape in the form of a horizontally lying V with its vertex directed away from the hole. The diameter d of the hole is between 8 and 12 mm. The ratio h/1 between the height h of the fence at the vertex of the V and the distance 1 is between 0.8 and 1, while the ratio h/d between the height h and the diameter d is between 1.5 and 2.
机译:飞机糠壳分配器包括细长的中空壳体,该壳体旨在固定在飞机的结构上,以便沿飞机的纵向方向定向。壳体具有一对侧壁,并且每个侧壁的前部具有一对侧向进气口,每个侧向进气口具有直径为d的圆形通孔,并且在纵向上或在通气孔内位于该孔的后面的围栏。距孔中心1的飞机的飞行方向,其形状为水平V形,其顶点指向远离孔的方向。孔的直径d在8至12mm之间。栅栏在V顶点处的高度h与距离1之间的比率h / 1在0.8和1之间,而高度h与直径d之间的比率h / d在1.5和2之间。

著录项

  • 公开/公告号US8485467B2

    专利类型

  • 公开/公告日2013-07-16

    原文格式PDF

  • 申请/专利权人 RICCARDO GEMMA;

    申请/专利号US20090919690

  • 发明设计人 RICCARDO GEMMA;

    申请日2009-02-24

  • 分类号B64D1/00;B64D33/02;

  • 国家 US

  • 入库时间 2022-08-21 16:47:11

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