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ANTI-ICE DEVICE, WING, AIRCRAFT, AND ANTI-ICE METHOD

机译:抗冰装置,机翼,飞机和抗冰方法

摘要

The purpose of the present invention is to provide an anti-ice device, a wing, an aircraft, and an anti-ice method which prevent, with a simple structure, icing on the aircraft which flies in a flying environment under an icing condition. The anti-ice device according to the present invention outputs pressure waves to water drops that float in air in a supercooled state which exists in a traveling direction of the aircraft (10) to change the water drops into ice by the pressure waves. The pressure waves have 0.9 to 3.3 [Pa] on a predetermined position in consideration of attenuation in the case where an acceleration of, for example, 10 G is given to the water drops.
机译:本发明的目的是提供一种防冰装置,机翼,飞行器和防冰方法,它们以简单的结构防止在结冰条件下在飞行环境中飞行的飞机上结冰。根据本发明的防冰装置向在飞行器(10)的行进方向上存在的过冷状态下漂浮在空气中的水滴输出压力波,以通过压力波将水滴变成冰。考虑到在对水滴施加例如10G的加速度的情况下的衰减,压力波在预定位置上具有0.9至3.3 [Pa]。

著录项

  • 公开/公告号WO2012098809A1

    专利类型

  • 公开/公告日2012-07-26

    原文格式PDF

  • 申请/专利权人 MITSUBISHI HEAVY INDUSTRIES LTD.;INOUE NOBUO;

    申请/专利号WO2011JP80044

  • 发明设计人 INOUE NOBUO;

    申请日2011-12-26

  • 分类号B64D15;

  • 国家 WO

  • 入库时间 2022-08-21 17:14:38

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