Title:
翼端装置
Document Type and Number:
Japanese Patent JP5126609
Kind Code:
B2
Abstract:
An aircraft includes a wing having a positive dihedral, the wing having a tip and a wing tip device mounted in the region of the tip. The wing tip device is generally downwardly extending and has a region inclined at a cant of more than 180 degrees. The region is arranged to generate lift during flight. The region inclined at a cant of more than 180 degrees may be located at the distal end of the wing tip device. The wing tip may be swept and may aeroelastically deform during flight.
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Inventors:
Alan man
Application Number:
JP2008530604A
Publication Date:
January 23, 2013
Filing Date:
September 12, 2006
Export Citation:
Assignee:
AIRBUS OPERATIONS LIMITED
International Classes:
B64C3/10; B64C23/06
Domestic Patent References:
| JP2002173093A | ||||
| JP4325395A |
Foreign References:
| EP1493660A1 | ||||
| US20040262451 | ||||
| US4382569 | ||||
| US3411738 | ||||
| US5961068 | ||||
| EP0122790A1 | ||||
| US5072894 | ||||
| DE202004014384U1 | ||||
| WO2007031732A1 |
Attorney, Agent or Firm:
Calyx
Miyazaki Yoshio
Kaoru Onozuka
Akio Tagami
High Masahiro
Tsutomu Kato
Kyoko Oyama
Norio Mori
Seiji Yamada
Miyazaki Yoshio
Kaoru Onozuka
Akio Tagami
High Masahiro
Tsutomu Kato
Kyoko Oyama
Norio Mori
Seiji Yamada