首页> 外国专利> Braking flap for deceleration of aircraft against air-flow which surrounds aircraft, comprises many vortex edges, which resolve individual edge section into number of vortex part, are arranged at free edge

Braking flap for deceleration of aircraft against air-flow which surrounds aircraft, comprises many vortex edges, which resolve individual edge section into number of vortex part, are arranged at free edge

机译：用于使飞机减速以抵抗围绕飞机的气流的制动襟翼包括许多涡流边缘，该涡流边缘将各个边缘部分分解为多个涡流部分，并被布置在自由边缘处

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摘要

Braking flap (20) comprises many vortex edges formed on the free edge (21), in many partial vortexes loosing individual edge sections (22). The vortex edges are arranged at free edge and are formed by a wavelike structure of the free edge.

机译：制动翼片（20）包括形成在自由边缘（21）上的许多涡流边缘，在许多局部涡流中，这些涡流边缘失去了单个边缘部分（22）。涡流边缘布置在自由边缘处并且由自由边缘的波浪状结构形成。

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公开/公告号DE102005054248A1

专利类型
公开/公告日2007-05-24

原文格式PDF
申请/专利权人 AIRBUS DEUTSCHLAND GMBH;
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申请/专利号DE20051054248
发明设计人 BENDER KLAUS;
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申请日2005-11-15
分类号B64C9/32;B64C3/58;
国家 DE
入库时间 2022-08-21 20:29:39

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