Title:
スラットアセンブリ
Document Type and Number:
Japanese Patent JP5587872
Kind Code:
B2
Abstract:
A method of operating an aircraft wing assembly, the assembly comprising a main wing element with a leading edge; a slat on the leading edge of the main wing element; and a seal member. The assembly is placed in a first configuration during take off in which the slat is in a deployed position with a slot between the slat and the main wing element, and the seal member is in a deployed position in which it seals the slot. During cruise both the slat and the seal member are retracted. During landing the slat is deployed fully with a slot between the slat and the main wing element, but the seal member is kept in its retracted position so that the slot remains open.
Inventors:
Timothy Davit James Wollaston
James Michael Ribeiro
James Michael Ribeiro
Application Number:
JP2011513052A
Publication Date:
September 10, 2014
Filing Date:
June 02, 2009
Export Citation:
Assignee:
Airbus Operations Limited AIRBUS OPERATIONS LIMITED
International Classes:
B64C9/24
Attorney, Agent or Firm:
Kenji Sugimura
Tatsuya Sawada
Takahiro Yamazaki
Tatsuya Sawada
Takahiro Yamazaki