Patent · US Active

Air vehicle

US10287011B2 · kind B2 · utility

33Cited by
27References
19Claims
0Family size

Assignee

Inventors

Key dates

Filing dateMay 26, 2010
Grant dateMay 14, 2019
Priority date
Expiry dateApr 30, 2031

Classification

  • Technology area (CPC B)Performing Operations; Transporting
  • CPC primaryB64U2101/00
  • WIPO fieldTransport
  • WIPO sectorMechanical engineering

Abstract

In embodiments, a system and method for providing propulsion and control to an air vehicle, and for operating the vehicle, include at least three propulsion units that provide vertical thrust for vectored thrust flight, in which at least one or two of the propulsion units also provide thrust for vectored thrust cruising or aerodynamic flight by suitably tilting the respective propulsion units for changing the thrust vector. At the same time, the three or more propulsion units are operated to generate controlling moments to the air vehicle about three orthogonal axes, pitch, roll and yaw, during vectored thrust flight (hover, cruising, etc.) or during aerodynamic flight for controlling the vehicle.

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