发明名称 CONCEPT OF A VARIABLE WINGLET FOR LATERAL LOAD REDUCTION FOR COMBINED LATERAL AND VERTICAL LOAD REDUCTION, AND FOR IMPROVING THE PERFORMANCE OF MEANS OF LOCOMOTION
摘要 <p>The device has a winglet movably attachable to a wing unit (1), and rotatable in relation to the wing unit, such that an angle between an associated rotary axis (7) and a main direction of extension (6) of the wing unit differs from 90 degree. An aerodynamic fairing unit is arranged between the wing unit and the winglet and/or winglet parts. A suspension unit is provided for attaching the winglet to the wing unit and movable by using a driven spindle. Independent claims are also included for the following: (1) a method for adapting aerodynamic characteristics of a wing unit (2) a locomotion device comprising an adaption device.</p>
申请公布号 WO2006122826(A1) 申请公布日期 2006.11.23
申请号 WO2006EP04774 申请日期 2006.05.19
申请人 AIRBUS DEUTSCHLAND GMBH;WEHRTMANN, VITALIJ;KORDT, MICHAEL 发明人 WEHRTMANN, VITALIJ;KORDT, MICHAEL
分类号 B64C23/06 主分类号 B64C23/06
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