首页> 外国专利> Annular wing aircraft capable of hovering - has gas turbines discharging over aerodynamically profiled lift surface with annular deflector around rim

Annular wing aircraft capable of hovering - has gas turbines discharging over aerodynamically profiled lift surface with annular deflector around rim

机译:能够悬停的环形翼飞机-燃气轮机在空气动力学轮廓的升力表面上排放,并在轮辋周围设有环形导流板

摘要

The annular-wing aircraft is capable of hovering and has a solid-of-revolution lift zone (5) with horizontal 'chord' and aerodynamically profiled upper surface. Over this is blown a gas stream from the peripheral outlet orifice (4) of an annular header (3) into which discharge several gas turbines (2). An annular baffle (6) above the wing outer rim deflects the gas stream, plus outer air it entrains, downwards around the craft. The craft can have several concentric lift zones, with profiles varying to reflect varying gas speeds. In this case the baffle (6) is fitted over the outermost zone.
机译:环形翼飞机能够悬停,并具有带有水平“弦”和空气动力学轮廓的上表面的旋转固体升力区(5)。在其上方吹出来自环形集管(3)的外围出口孔(4)的气流,几个燃气轮机(2)排放到其中。机翼外缘上方的环形挡板(6)使气流及其所带入的外部空气绕着飞行器向下偏转。该飞行器可以具有多个同心的提升区域,其轮廓变化以反映变化的气体速度。在这种情况下,挡板(6)安装在最外面的区域上。

著录项

  • 公开/公告号DE2819421A1

    专利类型

  • 公开/公告日1979-11-08

    原文格式PDF

  • 申请/专利权人 WILLIMCZIKWOLFHARTDIPL.-PHYS.;

    申请/专利号DE19782819421

  • 发明设计人 WILLIMCZIKWOLFHARTDIPL.-PHYS.;

    申请日1978-05-03

  • 分类号B64C3/12;

  • 国家 DE

  • 入库时间 2022-08-22 19:45:32

相似文献

  • 专利
  • 外文文献
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