Patent · US Active

Systems and methods for flight control of EVTOL aircraft

US12006035B1 · kind B1 · utility

3Cited by
1References
56Claims
0Family size

Assignee

Inventors

Key dates

Filing dateSep 15, 2023
Grant dateJun 11, 2024
Priority date
Expiry dateSep 15, 2043

Classification

  • Technology area (CPC B)Performing Operations; Transporting
  • CPC primaryB64D2221/00
  • WIPO fieldTransport
  • WIPO sectorMechanical engineering

Abstract

Aspects of this present disclosure relate to flight control of electric aircrafts and other vehicles. In one embodiment, an aircraft is disclosed comprising: a fuselage; two wings; a plurality of lift propellers, the lift propellers disposed aft of the wings during forward flight; plurality of tilt propellers that are tiltable between vertical lift and forward propulsion configurations, the tilt propellers disposed forward of the wings during forward flight; a plurality of tilt propellor actuators that tilt propellers between vertical lift and forward propulsion configurations, the tilt propellor actuators on opposite sides of the fuselage; and a plurality of electrical buses coupled to a flight control computer; wherein the flight control computer is configured to provide control signals for at least one of the lift propellers mounted to one of the wings and one of the tilt propellers mounted to the other wing via the same electrical bus.

Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.