Title:
航空機翼のフラップ用補助支持システム
Document Type and Number:
Japanese Patent JP7269032
Kind Code:
B2
Abstract:
Described herein is an auxiliary support system for a flap coupled to a wing of an aircraft. The auxiliary support system comprises a base fixable relative to the wing. The auxiliary support system also comprises a first track engagement assembly fixed to the base. The auxiliary support system further comprises a second track engagement assembly fixed to the base. The auxiliary support system additionally comprises a track arm attachable to the flap and comprising a first rail, movably engaged with the first track engagement assembly, and a second rail, movably engaged with the second track engagement assembly. The first rail is spaced apart from and non-parallel to the second rail.
Inventors:
Brett A. Bowers
Mirella Icek
Mirella Icek
Application Number:
JP2019037611A
Publication Date:
May 08, 2023
Filing Date:
March 01, 2019
Export Citation:
Assignee:
The Boeing Company
International Classes:
B64C3/50; B64C9/18
Domestic Patent References:
| JP2011515277A |
Foreign References:
| US20150090843 | ||||
| US3940093 | ||||
| US20070102587 | ||||
| WO2018005534A1 |
Attorney, Agent or Firm:
Minoru Yoshida
Tatsuya Tanaka
Suzuki Yasumitsu
Usui Nao
Shintaro Suzuki
Keita Kobuchi
Tomokazu Saito
Tatsuya Tanaka
Suzuki Yasumitsu
Usui Nao
Shintaro Suzuki
Keita Kobuchi
Tomokazu Saito