High-lift device of flight vehicle
US9623956B2 · kind B2 · utility
1Cited by
22References
8Claims
0Family size
Assignees
Inventors
Key dates
| Filing date | Feb 24, 2016 |
| Grant date | Apr 18, 2017 |
| Priority date | — |
| Expiry date | Feb 24, 2036 |
Classification
- Technology area (CPC Y)Emerging Cross-Sectional Technologies
- CPC primaryY02T50/40
- WIPO fieldTransport
- WIPO sectorMechanical engineering
Abstract
A high-lift device of a flight vehicle includes: a flap main body provided at a trailing edge portion of a main wing of the flight vehicle so as to be extracted from and be retracted in the trailing edge portion and extending in a wing span direction of the main wing; and a vortex suppressing portion provided at a tip end portion of the flap main body in a wing span direction of the flap main body and configured to suppress a vortex rolling up from a lower surface of a tip end portion of the flap main body to an upper surface of the tip end portion.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.