Title:
進入段階での航空機の操縦方法
Document Type and Number:
Japanese Patent JP5112425
Kind Code:
B2
Abstract:
According to the invention, high lift leading-edge slats (13) and high lift flaps (14) are simultaneously deployed, when the speed of the aircraft is equal to and less than an AES threshold.
Inventors:
Do-Laplace, Frank
Richter, Martin
Lang, Dietel
Richter, Martin
Lang, Dietel
Application Number:
JP2009514835A
Publication Date:
January 09, 2013
Filing Date:
June 07, 2007
Export Citation:
Assignee:
Elbus Opera (S.A.S.)
International Classes:
B64C13/16; B64C9/28
Domestic Patent References:
| JP56112398A | ||||
| JP4500649A | ||||
| JP2225199A | ||||
| JP63108898U |
Foreign References:
| EP1498794A1 |
Other References:
内藤子生,2・6 高揚力装置(high lift device),飛行力学の実際,日本,(社) 日本航空技術協会,1980年 9月25日,P31-P33
Attorney, Agent or Firm:
Shoji Suzue