首页> 外国专利> Aircraft nacelle de-icing and de-icing system, aircraft engine nacelle, and, process of command of an ice-de-icing and anti-icing system

Aircraft nacelle de-icing and de-icing system, aircraft engine nacelle, and, process of command of an ice-de-icing and anti-icing system

机译:飞机机舱除冰和除冰系统,飞机发动机机舱以及除冰和防冰系统的命令过程

摘要

ICE REMOVAL AND ICE REMOVAL SYSTEM FROM AIRCRAFT ENGINE NICKEL, AIRCRAFT ENGINE NECKLACE, AND ICE REMOVAL AND ANTI-FORMATION SYSTEM CONTROL PROCESS. The object of the invention is an aircraft engine nacelle anti-icing and anti-icing system comprising an air inlet (2) provided with a lip (3) followed by an inlet tubular part (4) provided with a first acoustic attenuation panel (5) comprising ice removal means (6, 6a, 6b, 6c, 6d) consisting of at least one network of heating resistive elements contained in an insulating material , the ice removal means being in the form of a mat incorporating the resistive elements into the thickness of the air inlet lip.
机译:飞机发动机镍,飞机发动机项链的除冰和除冰系统,以及除冰和反形成系统的控制过程。发明内容本发明的目的是一种飞机发动机机舱的防冰和防冰系统,该系统包括:进气口(2),其具有唇缘(3);进气口管状部分(4),其具有第一声衰减板(5)。 )包括除冰装置(6、6a,6b,6c,6d),该除冰装置由包含在绝缘材料中的至少一个加热电阻元件网络组成,除冰装置为垫的形式,该垫将电阻元件并入厚度进气口唇的角度。

著录项

  • 公开/公告号BRPI0612110A2

    专利类型

  • 公开/公告日2010-10-19

    原文格式PDF

  • 申请/专利权人 AIRBUS FRANCE;

    申请/专利号BR2006PI12110

  • 发明设计人 GILLES CHENE;ALAIN PORTE;JACQUES LALANE;

    申请日2006-06-19

  • 分类号B64D15/12;F02C7/047;

  • 国家 BR

  • 入库时间 2022-08-21 18:47:22

相似文献

  • 专利
  • 外文文献
  • 中文文献
获取专利

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号