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公开(公告)号：US09120555B2
公开(公告)日：2015-09-01
申请号：US12804988
申请日：2010-08-02
IPC分类号： B64C3/38 , B64C17/00 , B64C3/42 , B64C3/52 , B64C15/02 , B64C39/02 , B64C39/10 , B64D27/24 , B64D31/06 , H04B7/185
CPC分类号： B64C3/38 , B64C3/42 , B64C3/52 , B64C15/02 , B64C17/00 , B64C39/024 , B64C39/10 , B64C2201/028 , B64C2201/042 , B64C2201/102 , B64C2201/122 , B64C2201/126 , B64C2201/127 , B64C2201/146 , B64C2201/165 , B64D27/24 , B64D31/06 , B64D2211/00 , H04B7/18504 , Y02T50/12 , Y02T50/14 , Y02T50/44 , Y02T50/55
摘要： A span-loaded, highly flexible flying wing, having horizontal control surfaces mounted aft of the wing on extended beams to form local pitch-control devices. Each of five spanwise wing segments of the wing has one or more motors and photovoltaic arrays, and produces its own lift independent of the other wing segments, to minimize inter-segment loads. Wing dihedral is controlled by separately controlling the local pitch-control devices consisting of a control surface on a boom, such that inboard and outboard wing segment pitch changes relative to each other, and thus relative inboard and outboard lift is varied.
摘要翻译： 跨度加载，高度灵活的飞翼，具有安装在延伸梁上的机翼后部的水平控制表面，以形成局部俯仰控制装置。 机翼的五个翼展翼段中的每一个具有一个或多个电动机和光伏阵列，并且独立于其它翼段产生其自己的电梯，以最小化段间负载。 翼形二面体通过单独控制由悬臂上的控制表面组成的局部俯仰控制装置来控制，使得内侧和外侧翼段节距相对于彼此变化，因此相对的内侧和外侧升力变化。
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公开(公告)号：US20100308161A1
公开(公告)日：2010-12-09
申请号：US12804988
申请日：2010-08-02
IPC分类号： B64C3/38
CPC分类号： B64C3/38 , B64C3/42 , B64C3/52 , B64C15/02 , B64C17/00 , B64C39/024 , B64C39/10 , B64C2201/028 , B64C2201/042 , B64C2201/102 , B64C2201/122 , B64C2201/126 , B64C2201/127 , B64C2201/146 , B64C2201/165 , B64D27/24 , B64D31/06 , B64D2211/00 , H04B7/18504 , Y02T50/12 , Y02T50/14 , Y02T50/44 , Y02T50/55
摘要： A span-loaded, highly flexible flying wing, having horizontal control surfaces mounted aft of the wing on extended beams to form local pitch-control devices. Each of five spanwise wing segments of the wing has one or more motors and photovoltaic arrays, and produces its own lift independent of the other wing segments, to minimize inter-segment loads. Wing dihedral is controlled by separately controlling the local pitch-control devices consisting of a control surface on a boom, such that inboard and outboard wing segment pitch changes relative to each other, and thus relative inboard and outboard lift is varied.
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公开(公告)号：US07198225B2
公开(公告)日：2007-04-03
申请号：US10310415
申请日：2002-12-05
申请人： Derek L. Lisoski , Greg T. Kendall
发明人： Derek L. Lisoski , Greg T. Kendall
IPC分类号： B64D27/00
CPC分类号： B64C3/42 , B64C3/52 , B64C15/02 , B64C39/024 , B64C39/10 , B64C2201/028 , B64C2201/042 , B64C2201/102 , B64C2201/122 , B64C2201/126 , B64C2201/127 , B64C2201/146 , B64C2201/165 , B64D27/24 , B64D31/06 , B64D2211/00 , G05D1/0022 , G05D1/0077 , H04B7/18504 , Y02T50/12 , Y02T50/14 , Y02T50/44 , Y02T50/55 , Y02T50/62
摘要： A solar rechargeable, long-duration, span-loaded flying wing, having no fuselage or rudder. Having a two-hundred foot wingspan that mounts photovoltaic cells on most all of the wing's top surface, the aircraft uses only differential thrust of its eight propellers to turn, pitch and yaw. The wing is configured to deform under flight loads to position the propellers such that the control can be achieved. Each of five segments of the wing has one or more motors and photovoltaic arrays, and produces its own lift independent of the other segments, to avoid loading them. Five two-sided photovoltaic arrays, in all, are mounted on the wing, and receive photovoltaic energy both incident on top of the wing, and which is incident also from below, through a bottom, transparent surface.
摘要翻译： 太阳能可再充电，长时间，跨度的飞翼，没有机身或方向舵。 拥有两百英尺的翼展，将光伏电池安装在大部分机翼的顶部表面上，飞机只使用其八个螺旋桨的差速推力来转弯，俯仰和偏航。 机翼构造成在飞行载荷下变形以定位螺旋桨，使得可以实现控制。 翼的五个部分中的每一个具有一个或多个电动机和光伏阵列，并且独立于其它部分产生其自身的升降机，以避免加载它们。 五个双面光伏阵列总体上安装在机翼上，并且接收能量入射到机翼的顶部并且从下方入射的光能通过底部的透明表面。
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