Patent · US Active

Vertical takeoff and landing (VTOL) unmanned aerial vehicle (UAV)

US10287013B2 · kind B2 · utility

5Cited by
7References
17Claims
0Family size

Assignee

Inventors

Key dates

Filing dateSep 2, 2016
Grant dateMay 14, 2019
Priority date
Expiry dateFeb 5, 2037

Classification

  • Technology area (CPC B)Performing Operations; Transporting
  • CPC primaryB64U2201/20
  • WIPO fieldTransport
  • WIPO sectorMechanical engineering

Abstract

One example embodiment includes a vertical takeoff and landing (VTOL) unmanned aerial vehicle (UAV). The VTOL UAV includes a flight control system configured to provide avionic control of the VTOL UAV in a hover mode and in a level-flight mode. The VTOL UAV also includes a body encapsulating an engine and the flight control system. The VTOL UAV further includes a rotor disk coupled to the engine and configured to provide vertical thrust and cyclic pitch control in the hover mode and to provide horizontal thrust for flight during the level-flight mode.

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