首页> 外国专利> Heating tarpaulin for airplanes, has double walled gas-tight tarpaulin element for support of ice surface, particularly on airplane, which is kept free

Heating tarpaulin for airplanes, has double walled gas-tight tarpaulin element for support of ice surface, particularly on airplane, which is kept free

机译:飞机的加热防水油布,具有双壁气密性防水油布元件,用于支撑冰面,尤其是在飞机上,该元件可以自由放置

摘要

The heating tarpaulin has a double walled gas-tight tarpaulin element for the support of ice surface, particularly on an airplane, which is kept free. The tarpaulin element with is filled gas, particularly with warm air, where a gas inlet and a gas outlet are provided. An independent claim is also included for a method for deicing a surface of an airplane.
机译:加热篷布具有双壁气密篷布元件,用于支撑冰面,尤其是在飞机上,该冰面保持自由。带有填充气体的篷布元件,特别是充满热空气的填充油元件,其中设置有进气口和出气口。还包括用于飞机表面除冰的方法的独立权利要求。

著录项

  • 公开/公告号DE102011009596A1

    专利类型

  • 公开/公告日2012-08-02

    原文格式PDF

  • 申请/专利权人 LIEBL HORST;

    申请/专利号DE20111009596

  • 发明设计人 LIEBL HORST;

    申请日2011-01-27

  • 分类号B64F5;B64D15/02;

  • 国家 DE

  • 入库时间 2022-08-21 17:05:00

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