Title:
前部領域において側方気流チャネルを形成しているエンジン取付パイロンを具備した航空機の翼配置
Document Type and Number:
Japanese Patent JP5129232
Kind Code:
B2
Abstract:
The arrangement (1) has a wing (2) including proximal and distal ends, and a hooking pylon (4) of an engine (6) e.g. turbojet engine, suspended under the wing. The wing has a front zone (8) e.g. aerodynamic zone, situated toward the front with respect to a wing`s leading edge (10). The zone has a lateral projection (12) delimiting an air flowing lateral channel (14) by projecting toward the proximal end of the wing, where air flow is accelerated through the channel and is evacuated in a direction privileged under the wing, between a lower surface of the wing and a nacelle of the engine.
Inventors:
Stephanie dantan
Thierry Fol
Ludovic Gerard
Philip Jimne
Thierry Fol
Ludovic Gerard
Philip Jimne
Application Number:
JP2009502076A
Publication Date:
January 30, 2013
Filing Date:
March 28, 2007
Export Citation:
Assignee:
Airbus Operations (SS)
International Classes:
B64C3/32; B64C23/00
Foreign References:
| GB2144688A | ||||
| WO1995017334A1 | ||||
| US4643376 |
Attorney, Agent or Firm:
Masatake Shiga
Takashi Watanabe
Yasuhiko Murayama
Shinya Mitsuhiro
Takashi Watanabe
Yasuhiko Murayama
Shinya Mitsuhiro