High speed multi-rotor vertical takeoff and landing aircraft
High speed multi-rotor vertical takeoff and landing aircraft
- New search for: CLARIDGE JERRY DANIEL
- New search for: MANNING CHARLES FISCHER
- New search for: CLARIDGE JERRY DANIEL
- New search for: MANNING CHARLES FISCHER
This disclosure is generally directed to a High Speed vertical takeoff and landing (VTOL) aircraft that includes fixed wing flight capabilities. The High Speed VTOL aircraft may include at least two thrust producing rotors located equidistant from a longitudinal axis of the aircraft on a main wing, and at least two thrust producing rotors located equidistant from a longitudinal axis of the aircraft on a vertical wing. The rotors may be driven by electric motors. However, other power sources may be used such as combustion or hybrid engines. By adjusting the speed and/or the pitch of the rotors, the aircraft can transition from a vertical flight configuration to a horizontal flight configuration and back. WO 2016/085610 PCT/US2015/057722 - 108J
Document information
High speed multi-rotor vertical takeoff and landing aircraft
2019-08-08
Patent
Electronic Resource
English
| IPC: | B64C AEROPLANES , Flugzeuge |
Similar titles
HIGH SPEED MULTI-ROTOR VERTICAL TAKEOFF AND LANDING AIRCRAFT
| European Patent Office | 2019
HIGH SPEED MULTI-ROTOR VERTICAL TAKEOFF AND LANDING AIRCRAFT
| European Patent Office | 2016
HIGH SPEED MULTI-ROTOR VERTICAL TAKEOFF AND LANDING AIRCRAFT
| European Patent Office | 2016
High speed multi-rotor vertical takeoff and landing aircraft
| European Patent Office | 2021
HIGH SPEED MULTI-ROTOR VERTICAL TAKEOFF AND LANDING AIRCRAFT
| European Patent Office | 2018