Multirotor aircraft with enhanced yaw control
US9764829B1 · kind B1 · utility
51Cited by
7References
20Claims
0Family size
Assignee
Inventors
Key dates
| Filing date | Jun 9, 2015 |
| Grant date | Sep 19, 2017 |
| Priority date | — |
| Expiry date | Apr 3, 2036 |
Classification
- Technology area (CPC B)Performing Operations; Transporting
- CPC primaryB64U2201/10
- WIPO fieldTransport
- WIPO sectorMechanical engineering
Abstract
A configuration of a multirotor aircraft that will facilitate enhanced yaw control includes one or more adjustable members that will twist the frame of the multirotor aircraft, thereby adjusting the orientation of the motors and propellers and enhancing the yaw control of the multirotor aircraft. In some implementations, the adjustable member(s) are passive and twist in response to differential thrusts generated by the propellers. In other implementations, the adjustable members are active and twist in response to a yaw command from the multirotor aircraft control system.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.