DEVICE AND METHOD OF ADAPTIVE CONTROL OVER AERODYNAMIC CHARACTERISTICS OF WING ELEMENT Russian patent published in 2011 - IPC B64C5/08 B64C3/38 B64C5/10

Abstract RU 2412863 C2

FIELD: transport.

SUBSTANCE: invention relates to aircraft engineering. Device for adaptive control over aerodynamic characteristics of wing element 1 whereto small wing is attached to turn thereabout. Small wing 2 or its sections can turn about element 1 so that angle between rotational axis 7 and main direction of wing element panel 6 is other than 90°. Method and device is characterised by the use of above described device. Said device is proposed to be incorporated with aircraft.

EFFECT: reduced fuel consumption.

21 cl, 10 dwg

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RU 2 412 863 C2

Authors

Vertman Vitalij

Kordt Mikhael'

Dates

2011-02-27—Published

2006-05-19—Filed