Flap/spoiler combination
US4720066A · kind A · utility
38Cited by
2References
4Claims
0Family size
Assignee
Inventors
Key dates
| Filing date | Aug 26, 1986 |
| Grant date | Jan 19, 1988 |
| Priority date | — |
| Expiry date | Aug 26, 2006 |
Classification
- Technology area (CPC B)Performing Operations; Transporting
- CPC primaryB64C13/26
- WIPO fieldTransport
- WIPO sectorMechanical engineering
Abstract
A flap arrangement for an aircraft wing having along its trailing edge independently actuated high lift flap and spoiler. During cruising the flap is used for camber line curvature control while the spoiler is controlled in a follow up configuration such that a gap between the spoiler and the high lift flap does not form.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.