发明名称 WINGSAIL WITH ADAPTABLE FLEXIBLE FLAP
摘要 Wingsail. The wingsail includes a substantially rigid airfoil section having a leading and a trailing edge and a flap is attached to the trailing edge through a torsion fitting having a torsional stiffness along the span of the rigid airfoil section selected to control flap deflection with respect to the rigid airfoil section under aerodynamic loading to control rolling moment of the wingsail.
申请公布号 WO2016048606(A1) 申请公布日期 2016.03.31
申请号 WO2015US47912 申请日期 2015.09.01
申请人 MASSACHUSETTS INSTITUTE OF TECHNOLOGY 发明人 WIDNALL, SHEILA, E.;WILLIAMS, PETER, JOSEPH;CORNWELL, HAYDEN, K.
分类号 B63H9/06 主分类号 B63H9/06
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