Title:
航空機エンジンの吸気口のハウジング上に配置されるエンジン吸気フラップ、そのようなエンジン吸気フラップを有するエンジン、及び、航空機システム
Document Type and Number:
Japanese Patent JP2011514465
Kind Code:
A
Abstract:
An engine inlet flap for mounting on the housing of an air inlet or air inlet duct of an engine of an aircraft, having a first end and a second end arranged in opposition thereto at a distance therefrom in the longitudinal direction of the inlet flap, where the longitudinal direction in the given installation is aligned against the flow direction of the air flowing into the engine; and the inlet flap includes an inlet flap base body with a connector device for a jointed connector for jointed connection of the inlet flap base body to the housing of the air inlet or air inlet duct, with a rotational axis running along the second end, an inlet flap extension piece structurally integrated with the inlet flap base body, with a first and a second lateral piece, which extends from the inlet flap base body on the two opposed lateral edges of the inlet flap running in the longitudinal direction with a number of transverse struts or longitudinal struts, arranged in the leading region of the engine inlet flap.
Inventors:
Borender, Lars
Verknon, Sebastian
Verknon, Sebastian
Application Number:
JP2010544650A
Publication Date:
May 06, 2011
Filing Date:
February 04, 2009
Export Citation:
Assignee:
Airbus Opera Zion Gesellschaft Mitt Beschlenktel Haftung
International Classes:
B64D15/16; F02C7/042; B64D33/02; F02C7/00; F02C7/055; F02C9/00
Attorney, Agent or Firm:
Hironobu Onda
Makoto Onda
Atsushi Honda
Miho Ikegami
Makoto Onda
Atsushi Honda
Miho Ikegami