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Infrared decoy and a method for deployment thereof

机译:红外诱饵及其部署方法

摘要

The decoy (1) has a launcher provided with a dragline (3). The dragline is attached to an airplane. The dragline suspends infrared (IR) radiation in a spectral band relevant for IR homing heads. An air brake (10) comprises a delivering region that is adapted for IR radiation seen from the airplane behind the air brake. A front body portion (7) is provided with a radiation-producing material. A dragging eyelet (5) is provided in a region of the front body portion for recording a drag line. Independent claims are also included for the following: (1) a control unit for controlling of deployment velocity of dragline (2) a method for exposure of an IR decoy for a guard of an airplane.
机译:诱饵(1)的发射器配有拉索(3)。拉铲索连接到飞机上。牵引铲将红外(IR)辐射悬挂在与IR归位头相关的光谱带中。空气制动器(10)包括适于从空气制动器后面的飞机看到的IR辐射的输送区域。前主体部分(7)设置有产生辐射的材料。在前主体部分的区域中设置有拖眼(5),用于记录拖线。还包括以下方面的独立权利要求:(1)用于控制拉铲铲的展开速度的控制单元(2)一种用于暴露于飞机后卫的IR诱饵的方法。

著录项

  • 公开/公告号GB199919616D0

    专利类型

  • 公开/公告日2015-02-11

    原文格式PDF

  • 申请/专利权人 DAIMLERCHRYSLER AEROSPACE AG;

    申请/专利号GB19990019616

  • 发明设计人

    申请日1999-08-17

  • 分类号F41J9/10;F23R3/34;F41J2/02;

  • 国家 GB

  • 入库时间 2022-08-21 14:54:07

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