首页> 外国专利> Aircraft, has circular wings arranged in air channels, where air is reduced over upper surfaces of upper sphere for forming additional buoyancy when ventilator system or turbo-blower system or other drive systems is operated

Aircraft, has circular wings arranged in air channels, where air is reduced over upper surfaces of upper sphere for forming additional buoyancy when ventilator system or turbo-blower system or other drive systems is operated

机译:飞机具有布置在空气通道中的圆形机翼,在通风系统或涡轮鼓风机系统或其他驱动系统运行时,空气会在上方球体的上表面减少以形成额外的浮力

摘要

The aircraft (20) has circular wings (2, 3, 6) arranged in air channels (17), where the wings are attached at an incident angle. An upper sphere (7) and a lower sphere (9) cut the air channels to each other at a preset angle or at null such that elevons expand area of potentials of the aircraft, and a thrust vector is rapidly changed in an opposite position for emergency braking during maneuvers. Air is reduced over upper surfaces of the upper sphere for forming additional buoyancy when a ventilator system or turbo-blower system or other drive systems is operated.
机译:飞机(20)具有布置在空气通道(17)中的圆形机翼(2、3、6),其中机翼以入射角被附接。上球体(7)和下球体(9)以预设角度或零位彼此切开空气通道,从而使电子扩大了飞机的电势区域,推力矢量在相反的位置快速变化,从而演习中紧急制动。当通风系统或涡轮鼓风机系统或其他驱动系统运行时,空气会在上部球体的上表面上方减少,从而形成额外的浮力。

著录项

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