Wing for short take-off and landing aircraft
US4498646A · kind A · utility
44Cited by
3References
2Claims
0Family size
Assignee
Inventors
Key dates
| Filing date | Mar 9, 1982 |
| Grant date | Feb 12, 1985 |
| Priority date | — |
| Expiry date | Mar 9, 2002 |
Classification
- Technology area (CPC Y)Emerging Cross-Sectional Technologies
- CPC primaryY02T50/10
- WIPO fieldTransport
- WIPO sectorMechanical engineering
Abstract
Profile design for aircraft lift-wings in general aviation up to flight speeds of about 700 km/h, the profile design being determined by the path of the center line with a forward (first) and rear (second) camber maximum and with a profile droplet superposed on the center line and of a specific thickness distribution, and by the design of the profile nose to have a relatively small nose radius and relatively strong camber.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.