Title:
スラット、航空機の翼、航空機の動翼、航空機
Document Type and Number:
Japanese Patent JP5710005
Kind Code:
B2
Abstract:
A flight control surface such as a slat capable of keeping and achieving a minimum basic functions even when it is damaged by collisions of birds or the like, and a wing using the same are provided. Both ends of one wire cable 15 or more are fixed to paired ribs 10A and 10B provided in a short direction of the slat. This wire cable 15 is placed so as to pass through a through-hole 13 formed in each of the ribs 10 positioned between the paired ribs 10A and 10B. Even if birds or the like collide with slat 3 at the time of a flight of the aircraft to damage and deform not only a skin 4 of the slat 3 but also any rib 10, the wire cable 15 between the paired ribs 10A and 10B prevents the slat 3 from being broken into pieces.
Inventors:
Hideaki Tanaka
Application Number:
JP2013529871A
Publication Date:
April 30, 2015
Filing Date:
August 21, 2012
Export Citation:
Assignee:
Mitsubishi Aircraft Corporation
International Classes:
B64C9/00
Domestic Patent References:
| JP2009006987A |
Foreign References:
| GB525400A |
Other References:
マイクル・C・Y・ニウ,航空機構造設計 - 機体設計のための実用書,日本,有限会社 名古屋航空技術,2000年 2月21日,343-344
Attorney, Agent or Firm:
Mitsuru Oba
Horikawa Miyuki
Yuko Otake
Horikawa Miyuki
Yuko Otake