FIELD: flying vehicles provided with trim control systems. SUBSTANCE: wing has primary structure and two-sided flexible skin. Side beams of primary structure are bent in plane of wing. Bend is ensured by means of rope ties and tubular struts located inside wing profile forming preliminary bending system for outer wing panel. Each drag strut may move over side beam in transversal direction. EFFECT: improved flying characteristics. 5 cl, 4 dwg
Title | Year | Author | Number |
---|---|---|---|
SUPERLIGHT FLYING VEHICLE | 0 |
|
SU1759728A1 |
FLYING VEHICLE WITH BALANCING CONTROL | 1995 |
|
RU2110447C1 |
DELTA-PLANER | 0 |
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DELTAPLANE WING | 1993 |
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RU2064880C1 |
FLYING VEHICLE | 1997 |
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RU2148528C1 |
HANGING GLIDER | 0 |
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BALANCING FLYING VEHICLE | 1993 |
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PILOTLESS AIRCRAFT | 2008 |
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DELTAPLANE | 0 |
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SU1121181A1 |
AIRCRAFT AND METHOD OF CONTROL THEREOF | 2010 |
|
RU2461493C2 |
Authors
Dates
2003-07-20—Published
2001-12-27—Filed