Vertical take-off and landing aerial vehicle
US9725170B2 · kind B2 · utility
Assignee
Inventors
Key dates
| Filing date | Sep 11, 2015 |
| Grant date | Aug 8, 2017 |
| Priority date | — |
| Expiry date | Feb 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.