首页> 外国专利> Aerodynamic device for transporting e.g. front section of fuselage of aircraft on carrier aircraft, has aerodynamic support for positioning and maintaining front, rear and intermediate sections of fuselage of aircraft on carrier aircraft

Aerodynamic device for transporting e.g. front section of fuselage of aircraft on carrier aircraft, has aerodynamic support for positioning and maintaining front, rear and intermediate sections of fuselage of aircraft on carrier aircraft

机译:用于运输的气动装置航空母舰飞机机身的前部,具有气动支撑,用于定位和维护航空母舰飞机机身的前,后和中间部分

摘要

The device (10) has an aerodynamic support (14) for positioning and maintaining front and rear sections (Tav, Tar) and an intermediate section of a fuselage of an aircraft on a carrier aircraft (12) with longitudinal axes (Lav, Lar) and a longitudinal axis of the respective sections parallel to a plane axis (A) of the carrier aircraft. The support includes support elements (16, 18, 20, 22) fixed on an upper part (24) of the fuselage of the carrier aircraft. The support elements are aligned behind each other along the plane axis.
机译:装置(10)具有空气动力学支撑件(14),该空气动力学支撑件(14)用于在具有纵向轴线(Lav,Lar)的运载飞机(12)上定位和保持飞机的机身的前部和后部(Tav,Tar)和机身的中间部。各个部分的纵轴平行于运载飞机的平面轴(A)。支撑件包括固定在运输机机身的上部(24)上的支撑元件(16、18、20、22)。支撑元件沿着平面轴线彼此后方对齐。

著录项

  • 公开/公告号FR2987345A1

    专利类型

  • 公开/公告日2013-08-30

    原文格式PDF

  • 申请/专利权人 AIRBUS OPERATIONS;

    申请/专利号FR20120051823

  • 申请日2012-02-29

  • 分类号B64C7;B64D5;B64F5;

  • 国家 FR

  • 入库时间 2022-08-21 16:20:55

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