Method and spoiler system for ensuring the aerodynamic continuity of the upper surface of an aircraft
US6981676B2 · kind B2 · utility
36Cited by
9References
9Claims
0Family size
Assignee
Inventor
Key dates
| Filing date | Sep 21, 2004 |
| Grant date | Jan 3, 2006 |
| Priority date | — |
| Expiry date | Sep 21, 2024 |
Classification
- Technology area (CPC B)Performing Operations; Transporting
- CPC primaryB64C2009/143
- WIPO fieldTransport
- WIPO sectorMechanical engineering
Abstract
Method and spoiler system for ensuring the aerodynamic continuity of the upper surface of an aircraft wing.According to the invention, the spoiler 7 has a chord (C) of adjustable length and means (16, 19, 20) are provided for acting on the length of said chord when said spoiler (7) is in the retracted position.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.