首页> 外国专利> Missile e.g. guided missile, for use with aircraft or combat aircraft, has aero-spike that extends from front face surface, where aero-spike has front body i.e. aero-disk, formed with porous material, whose open pores form flow channels

Missile e.g. guided missile, for use with aircraft or combat aircraft, has aero-spike that extends from front face surface, where aero-spike has front body i.e. aero-disk, formed with porous material, whose open pores form flow channels

机译:导弹用于飞机或作战飞机的制导导弹具有从前表面延伸的气钉,该气钉具有前主体,即由多孔材料形成的气碟,其开孔形成流动通道

摘要

The missile (1) has an aero-spike (4) that extends from a front face surface (3), where the aero-spike has a front body i.e. aero-disk (10), formed with a porous material, whose open pores form flow channels. The front body has a front surface that is oriented transverse to a longitudinal axis (11-11) of the missile. A deflecting unit is provided downstream of the channels for outwardly deflecting air flowing through the channels. The aero-spike is formed with a bar, which bears the front body and is supported by a carrier body and a retaining element.
机译:导弹(1)具有从前表面(3)伸出的气钉(4),其中气钉具有前体,即由多孔材料形成的气孔盘(10),其开孔形成流道。前主体的前表面横向于导弹的纵轴(11-11)定向。偏转单元设置在通道的下游,用于使流过通道的空气向外偏转。气钉形成有一根杆,该杆支撑着前车身并由承载体和保持元件支撑。

著录项

  • 公开/公告号DE102006061709B3

    专利类型

  • 公开/公告日2008-05-29

    原文格式PDF

  • 申请/专利权人 DEUTSCHES ZENTRUM FUER LUFT- UND RAUMFAHRT E.V.;

    申请/专利号DE20061061709

  • 发明设计人 SCHUELEIN ERICH;

    申请日2006-12-28

  • 分类号F42B10/46;F42B10;B64C23/04;

  • 国家 DE

  • 入库时间 2022-08-21 19:49:33

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