首页> 外国专利> Vstol aircraft with improved forward speed - with streamline circular fuselage with forward thrusters and encircling rotor

Vstol aircraft with improved forward speed - with streamline circular fuselage with forward thrusters and encircling rotor

机译:Vstol飞机具有更高的前进速度-流线型圆形机身带有前推力器和环绕旋翼

摘要

The streamlined fuselage is provided with short wing surfaces on either side to form a circular shape from above. A ring shaped rotor is fitted around the craft powered by two thrusters mounted on opposite sides of the craft. The separate wing sections of the rotor can be tilted to control vertical lift, or can be feathered for forward flight. Another two thrusters are mounted on either side of the fuselage for forward thrust. The aircraft combines the vertical control of a helicopter with the forward speed of a conventional aircraft.
机译:流线型机身在两侧均设有短翼表面,从上方形成圆形。环形转子安装在船只周围,由安装在船只相对两侧的两个推进器驱动。旋翼的单独机翼部分可以倾斜以控制垂直升力,也可以用羽毛装饰以向前飞行。另外两个推进器安装在机身的任一侧,用于向前推进。该飞机将直升飞机的垂直控制与常规飞机的前进速度结合在一起。

著录项

  • 公开/公告号DE2336055A1

    专利类型

  • 公开/公告日1975-02-06

    原文格式PDF

  • 申请/专利权人 KOCHANNECKUWE;

    申请/专利号DE19732336055

  • 发明设计人 KOCHANNECKUWE;

    申请日1973-07-16

  • 分类号B64C29/00;B64C15/00;

  • 国家 DE

  • 入库时间 2022-08-23 03:58:57

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