发明申请
US20160200436A1 Tri-Rotor Aircraft Capable of Vertical Takeoff and Landing and Transitioning to Forward Flight
审中-公开
![Tri-Rotor Aircraft Capable of Vertical Takeoff and Landing and Transitioning to Forward Flight](/abs-image/US/2016/07/14/US20160200436A1/abs.jpg.150x150.jpg)
基本信息:
- 专利标题: Tri-Rotor Aircraft Capable of Vertical Takeoff and Landing and Transitioning to Forward Flight
- 专利标题(中):三转子飞机能够垂直起飞和着陆并向前飞行
- 申请号:US15080167 申请日:2016-03-24
- 公开(公告)号:US20160200436A1 公开(公告)日:2016-07-14
- 发明人: David D. North , Mark J. Aull , William J. Fredericks , Mark D. Moore , Paul M. Rothhaar , WILLIAM T. Hodges , Zachary R. Johns
- 申请人: U.S.A. as represented by the Administrator of the National Aeronautics and Space Administration
- 专利权人: U.S.A. as represented by the Administrator of the National Aeronautics and Space Administration
- 当前专利权人: U.S.A. as represented by the Administrator of the National Aeronautics and Space Administration
- 主分类号: B64C29/00
- IPC分类号: B64C29/00 ; B64C39/02 ; B64C5/02 ; B64C25/52 ; B64D27/24 ; B64C3/40
摘要:
Systems, methods, and devices provide a vehicle, such as an aircraft, with rotors configured to function as a tri-copter for vertical takeoff and landing (“VTOL”) and a fixed-wing vehicle for forward flight. One rotor may be mounted at a front of the vehicle fuselage on a hinged structure controlled by an actuator to tilt from horizontal to vertical positions. Two additional rotors may be mounted on the horizontal surface of the vehicle tail structure with rotor axes oriented vertically to the fuselage. For forward flight of the vehicle, the front rotor may be rotated down such that the front rotor axis may be oriented horizontally along the fuselage and the front rotor may act as a propeller. For vertical flight, the front rotor may be rotated up such that the front rotor axis may be oriented vertically to the fuselage, while the tail rotors may be activated.
摘要(中):
系统,方法和设备提供诸如飞行器的车辆,其具有被配置为用作用于垂直起飞和着陆(“垂直起落架”)和用于向前飞行的固定翼车辆的三重起重机的转子。 一个转子可以安装在车身机身的前部,并由致动器控制的铰链结构从水平位置倾斜到垂直位置。 两个附加的转子可以安装在车辆尾部结构的水平表面上,其转子轴线垂直于机身。 对于车辆的前进飞行,前转子可以向下旋转,使得前转子轴线可以沿着机身水平定向,并且前转子可以用作螺旋桨。 对于垂直飞行,前转子可以向上旋转,使得前转子轴线可以垂直定向到机身,而尾转子可以被启动。
公开/授权文献:
IPC结构图谱:
B | 作业;运输 |
--B64 | 飞行器;航空;宇宙航行 |
----B64C | 飞机;直升飞机 |
------B64C29/00 | 能垂直起飞或着陆的飞机 |