Title:
スラット展開機構
Document Type and Number:
Japanese Patent JP5336575
Kind Code:
B2
Abstract:
An aircraft slat deployment mechanism including a first drive member coupled to a slat at a first pivot point and a second drive member coupled to the slat at a second pivot point offset from the first pivot point. A first rack is provided on the first drive member, and a first pinion is carried by the drive shaft. The first pinion is arranged to transmit mechanical power from the drive shaft to the first drive member via the first rack. A second rack is provided on the second drive member, and a second pinion is carried by the drive shaft. The second pinion has a different radius to the first pinion. The second pinion is arranged to transmit mechanical power from the drive shaft to the second drive member via the second rack, such that the first and second drive members move at a different speed.
Inventors:
Man, Alan
Application Number:
JP2011501295A
Publication Date:
November 06, 2013
Filing Date:
March 12, 2009
Export Citation:
Assignee:
Airbus Operations Limited
International Classes:
B64C9/24
Foreign References:
| US4753402 | ||||
| US4880189 | ||||
| US6149105 | ||||
| US4650140 | ||||
| EP0291328A2 | ||||
| US20070102587 | ||||
| WO2009118547A2 |
Attorney, Agent or Firm:
Atsushi Aoki
Jun Tsuruta
Tetsuro Shimada
Shinji Mitsuhashi
Koichi Ito
Tatsuki Sone
Jun Tsuruta
Tetsuro Shimada
Shinji Mitsuhashi
Koichi Ito
Tatsuki Sone