Patent · US Active

Vertical take-off and landing aircraft

US9567088B2 · kind B2 · utility

20Cited by
19References
18Claims
0Family size

Assignee

Inventors

Key dates

Filing dateAug 14, 2014
Grant dateFeb 14, 2017
Priority date
Expiry dateDec 24, 2034

Classification

  • Technology area (CPC B)Performing Operations; Transporting
  • CPC primaryB64U2101/30
  • WIPO fieldTransport
  • WIPO sectorMechanical engineering

Abstract

A VTOL aircraft includes at least one puller rotor and at least one pusher rotor. The VTOL aircraft, for example, may include three puller rotors and one pusher rotor. The combination of static puller and pusher rotors allows the rotors to remain in a fixed orientation (i.e., no moving mechanical axes are required) relative to the wings and fuselage of the VTOL aircraft, while being able to transition the aircraft from a substantially vertical flight path to a substantially horizontal flight path.

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