首页> 外国专利> ADAPTIVE PNEUMATIC WINGS FOR FLYING DEVICES WITH FIXED WINGS

ADAPTIVE PNEUMATIC WINGS FOR FLYING DEVICES WITH FIXED WINGS

机译:带固定翼的飞行装置的自适应气动翼

摘要

Modules that can be impinged upon bycompressed air are arranged in front of and behind abox-shaped spar (1), whereby said modules have anairtight top skin and an airtight bottom skin andplates (7) which can transmit thrust are disposedtherebetween. Each plate (7) has a console on eachside. Said console extends along the entire lengthof the wing profile. One to two flexible tubes (9)that are airtight and only slightly extensible areinserted between two such consoles. When the tubesare subjected to pressure, they cause the plates (9)to move substantially parallel to each other andprovide the wing with the desired camber. Theaerodynamic profile is defined by rigid sheeting (10)whereby said sheeting (10) is secured to the topskin, bottom skin (5) and the sheet in an articulatedmanner by the plates (11) that are provided with.hinges (14). The on-flow edge (3) of the wing hastwo airtight and only slightly extensible flexibletubes (15,16) which, when inflated in an appropriatemanner, provide the on-flow edge (3) with therequired shape. The off-flow edge (4) is open.
机译:可能受到影响的模块压缩空气布置在箱形梁(1),其中所述模块具有气密的顶部皮肤和气密的底部皮肤设置了可以传递推力的板(7)之间。每个板(7)的每个板上都有一个控制台侧。所述控制台沿整个长度延伸机翼轮廓1-2个挠性管(9)密封的,只有一点可扩展的插入两个这样的控制台之间。当管承受压力会导致板(9)彼此基本平行移动为机翼提供所需的外倾角。的空气动力学轮廓由硬质片材(10)定义从而将所述薄板(10)固定到顶部皮,底皮(5)和铰接的床单通过设置的板(11)的方式。铰链(14)。机翼的进气边缘(3)具有两个气密,只有一点可伸展的弹性适当充气时的管子(15,16)方式,为流动边缘(3)提供所需的形状。排气边缘(4)打开。

著录项

  • 公开/公告号CA2298005C

    专利类型

  • 公开/公告日2004-02-03

    原文格式PDF

  • 申请/专利权人 PROSPECTIVE CONCEPTS AG;

    申请/专利号CA19992298005

  • 发明设计人 KAMMER RES;TO FREDERICK E.;

    申请日1999-05-06

  • 分类号B64C3/46;B63B1/24;B64C3/30;

  • 国家 CA

  • 入库时间 2022-08-21 23:05:03

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