Central wing panel for a flying vehicle and method of its control
US10611459B2 · kind B2 · utility
Assignee
Inventor
Key dates
| Filing date | Oct 8, 2015 |
| Grant date | Apr 7, 2020 |
| Priority date | — |
| Expiry date | Apr 4, 2036 |
Classification
- Technology area (CPC Y)Emerging Cross-Sectional Technologies
- CPC primaryY02T50/10
- WIPO fieldTransport
- WIPO sectorMechanical engineering
Abstract
A central wing panel for a hybrid transportation vehicle for ground and air transportation configured to enable transitioning between an air mode and a ground mode. The central wing panel has a front frame section and a rear frame section connected by one or more cross members. The central wing panel is configured to rotate enabling adjustment of an angle of attack of the vehicle. The rear frame section is configured to rotate enabling coupling and uncoupling of the rear frame section from a first wing and a second wing for transitioning between the air mode and the ground mode. The central wing panel is also configured to allow rotation of ailerons and flaps so that they fold over onto the top front portion of the wings.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.