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公开(公告)号：US20120207609A1
公开(公告)日：2012-08-16
申请号：US13499970
申请日：2010-10-07
申请人： Yukihide Kimura , Tomoaki Morimoto
发明人： Yukihide Kimura , Tomoaki Morimoto
摘要： A wing structure includes: a main wing that extends in a second direction intersecting a first direction as a fluid flow direction; and an auxiliary wing that is disposed so as to be separated from the main wing and faces the main wing at the front part side of the main wing, wherein a wing chord length of the auxiliary wing is shorter than a wing chord length of the main wing. A fluid contacts the auxiliary wing which is formed at the front part side of the main wing, the fluid is guided between the auxiliary wing and the main wing, and the fluid is compressed when passing between the auxiliary wing and the main wing, thereby appropriately forming a fluid compression process region on the surface of the main wing and increasing an acting force.
摘要翻译： 翼结构包括：主翼，沿与第一方向相交的第二方向作为流体流动方向延伸; 以及辅助翼，其设置成与主翼分离并且在主翼的前部侧面对主翼，其中辅助翼的翼弦长度短于主翼的翼弦长度 翅膀。 流体接触形成在主翼的前部侧的辅助翼，流体在辅助翼和主翼之间被引导，并且当在辅助翼与主翼之间通过时，流体被压缩，从而恰当地 在主翼的表面上形成流体压缩过程区域并增加作用力。
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公开(公告)号：US09090346B2
公开(公告)日：2015-07-28
申请号：US13499970
申请日：2010-10-07
申请人： Yukihide Kimura , Tomoaki Morimoto
发明人： Yukihide Kimura , Tomoaki Morimoto
摘要： A wing structure includes: a main wing that extends in a second direction intersecting a first direction as a fluid flow direction; and an auxiliary wing that is disposed so as to be separated from the main wing and faces the main wing at the front part side of the main wing, wherein a wing chord length of the auxiliary wing is shorter than a wing chord length of the main wing. A fluid contacts the auxiliary wing which is formed at the front part side of the main wing, the fluid is guided between the auxiliary wing and the main wing, and the fluid is compressed when passing between the auxiliary wing and the main wing, thereby appropriately forming a fluid compression process region on the surface of the main wing and increasing an acting force.
摘要翻译： 翼结构包括：主翼，沿与第一方向相交的第二方向作为流体流动方向延伸; 以及辅助翼，其设置成与主翼分离并且在主翼的前部侧面对主翼，其中辅助翼的翼弦长度短于主翼的翼弦长度 翅膀。 流体接触形成在主翼的前部侧的辅助翼，流体在辅助翼和主翼之间被引导，并且当在辅助翼与主翼之间通过时，流体被压缩，从而恰当地 在主翼的表面上形成流体压缩过程区域并增加作用力。
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