Title:
前縁の高揚力装置のための作動システム
Document Type and Number:
Japanese Patent JP5427786
Kind Code:
B2
Abstract:
An actuation system configured to deploy a high-lift device on a leading edge of an aircraft wing. The system comprises: a link pivotally connected to the wing at a first pivot point and to the high-lift device at a second pivot point; a first actuation mechanism configured to rotate the high-lift device about the first pivot point; and a second actuation mechanism configured to rotate the high-lift device about the second pivot point. The second actuation mechanism is operable independently of the first actuation mechanism, and can be operated in order to generate a sealing force between the high-lift device and the leading edge of the aircraft wing.
Inventors:
Francois Catherine
Edmond Kay
Edmond Kay
Application Number:
JP2010531587A
Publication Date:
February 26, 2014
Filing Date:
October 27, 2008
Export Citation:
Assignee:
AIRBUS OPERATIONS LIMITED
International Classes:
B64C9/24
Domestic Patent References:
| JP62157896A |
Foreign References:
| US4040579 | ||||
| US20020195527 | ||||
| US4915327 | ||||
| US4470569 | ||||
| US5474265 | ||||
| US4753402 | ||||
| US4399970 | ||||
| WO2005108205A1 | ||||
| WO2009056873A1 | ||||
| EP1972547A1 | ||||
| EP1607324A1 | ||||
| GB998895A |
Attorney, Agent or Firm:
Kenji Sugimura
Tatsuya Sawada
Harima Satoko
Tatsuya Sawada
Harima Satoko