Patent · US Active

Vertical take-off and landing aerial vehicle

US9725170B2 · kind B2 · utility

5Cited by
9References
20Claims
0Family size

Assignee

Inventors

Key dates

Filing dateSep 11, 2015
Grant dateAug 8, 2017
Priority date
Expiry dateFeb 17, 2036

Classification

  • Technology area (CPC B)Performing Operations; Transporting
  • CPC primaryB64U10/13
  • WIPO fieldTransport
  • WIPO sectorMechanical engineering

Abstract

A VTOL (vertical take-off and landing) aerial flying vehicle comprising an inner frame, a gimbal system and an outer frame, the inner frame comprising a propulsion system and a control system. The propulsion system being able to generate a lift force. The VTOL may also include a decoupling mechanism having either a linear or non-linear beam coupled to a ring. The beam may optionally include sliders at ends thereof that provide an additional rotation freedom to the inner frame.

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