首页> 外国专利> Helmet for pilot of aircraft e.g. weapon airplane or helicopter, has conduit permitting transmission of air flow from ventilation unit towards evacuation unit, where air flow cools evacuation unit by natural or forced thermal convection

Helmet for pilot of aircraft e.g. weapon airplane or helicopter, has conduit permitting transmission of air flow from ventilation unit towards evacuation unit, where air flow cools evacuation unit by natural or forced thermal convection

机译:飞机驾驶员头盔武器飞机或直升机,具有允许空气流从通风装置流向疏散装置的管道,在此气流通过自然或强制热对流冷却疏散装置

摘要

The helmet has a dissipative equipment formed by an optical part (3), an LCD screen (4), and a light box (5), associated to a heat evacuation unit i.e. radiator (6). A conduit (11) permits transmission of air flow from a ventilation unit i.e. mechanical ventilator (7), towards the heat evacuation unit. Air flow is intended to cool the evacuation unit by natural or forced thermal convection. The ventilation unit is fixed on a protection shell formed by an external rigid layer (9) and a protection layer (10) at a level of an opening of the conduit.
机译:该头盔具有耗散设备,该耗散设备由与散热单元即散热器(6)关联的光学部件(3),LCD屏幕(4)和灯箱(5)组成。导管(11)允许气流从通风单元即机械通风器(7)流向热量排出单元。气流旨在通过自然或强制热对流来冷却疏散装置。通风单元固定在由外部刚性层(9)和保护层(10)形成的保护壳上,该保护壳在导管的开口的高度处。

著录项

  • 公开/公告号FR2944416A1

    专利类型

  • 公开/公告日2010-10-22

    原文格式PDF

  • 申请/专利权人 THALES;

    申请/专利号FR20090001871

  • 发明设计人 COUPEAUD CHRISTOPHE;

    申请日2009-04-17

  • 分类号A42B3/04;G02B27/01;

  • 国家 FR

  • 入库时间 2022-08-21 18:26:36

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