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Title:
ADJUSTMENT OF WING FOR VARIABLE CAMBER FOR OPTIMUM TAKE-OFF AND LANDING
Document Type and Number:
Japanese Patent JP2012126389
Kind Code:
A
Abstract:

To provide methods and systems for providing differential control of flap surface movement utilizing a single drive link to provide improved efficiency over the prior systems during take-off and landing.

This invention is directed to systems and methods for moving trailing edge high lift devices on an aircraft wing, and more particularly to moving inboard, outboard and midspan flaps 312, 313 and 316 differentially in order to produce better lift/drag characteristics during takeoff and landing of the aircraft.


Inventors:
GOOD MARK
JOHNSON PAUL
Application Number:
JP2011268801A
Publication Date:
July 05, 2012
Filing Date:
December 08, 2011
Export Citation:
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Assignee:
BOEING CO
International Classes:
B64C13/00; B64C3/50
Domestic Patent References:
JP2000264291A2000-09-26
Foreign References:
US7726610B22010-06-01
US20090206197A12009-08-20
US20120032030A12012-02-09
US20050151028A12005-07-14
US4892274A1990-01-09
US7556224B22009-07-07
US20060049308A12006-03-09
US20080255713A12008-10-16
US20050151028A12005-07-14
US20100282899A12010-11-11
Attorney, Agent or Firm:
Sonoda Yoshitaka
Kobayashi Yoshinori



 
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