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公开(公告)号：US4406433A
公开(公告)日：1983-09-27
申请号：US217794
申请日：1980-12-18
申请人： Robert L. Radkey , Bart D. Hibbs
发明人： Robert L. Radkey , Bart D. Hibbs
IPC分类号： B64D17/02
CPC分类号： B64D17/025 , Y10S244/902
摘要： The air scoop opening at the leading edge of a flexible, ram-air inflated airfoil canopy, is framed between curved lip sections extending tangentially from the upper and lower surface members of the canopy to prevent airflow separation adjacent the leading edge and the drag producing effect thereof. A baffling curtain extends across the air scoop opening.
摘要翻译： 在柔性的冲压空气充气翼型罩的前缘处的空气勺开口被框架在从顶盖的上表面和下表面构件切向延伸的弯曲的唇部之间，以防止邻近前缘的气流分离和阻力产生效应 其中。 一个令人不安的窗帘延伸穿过空气勺开口。
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公开(公告)号：US5810284A
公开(公告)日：1998-09-22
申请号：US404540
申请日：1995-03-15
CPC分类号： B64D27/24 , B64C39/10 , H04B7/18504 , B64D2211/00 , Y02T50/12 , Y02T50/44 , Y02T50/62 , Y02T50/69
摘要： This disclosure provides a solar rechargeable aircraft that is inexpensive to produce, is steerable, and can remain airborne almost indefinitely. The preferred aircraft is a span-loaded flying wing, having no fuselage or rudder. Travelling at relatively slow speeds, and 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. Each of five sections of the wing has one or more engines and photovoltaic arrays, and produces its own lift independent of the other sections, 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. The aircraft is capable of a top speed of about ninety miles per hour, which enables the aircraft to attain and can continuously maintain altitudes of up to sixty-five thousand feet. Regenerative fuel cells in the wing store excess electricity for use at night, such that the aircraft can sustain its elevation indefinitely. A main spar of the wing doubles as a pressure vessel that houses hydrogen and oxygen gasses for use in the regenerative fuel cell. The aircraft has a wide variety of applications, which include weather monitoring and atmospheric testing, communications, surveillance, and other applications as well.
摘要翻译： 本公开提供了一种太阳能可再充电飞机，其生产便宜，是可操纵的，并且几乎可以无限期地保持空中飞行。 首选飞机是一个装有跨距的飞翼，没有机身或方向舵。 以相对较慢的速度行驶，并且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动推力来转动。 翼的五个部分中的每一个具有一个或多个发动机和光伏阵列，并且独立于其他部分产生其自己的升降机，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。 该飞机的最高时速约为每小时九十英里，这使飞机能够获得并可以持续维持高达六万五千英尺的高度。 机翼中的再生燃料电池储存了夜间使用的过量电力，使飞机能够无限期地维持其高度。 翼的主要翼梁加倍，作为容纳用于再生燃料电池的氢气和氧气的压力容器。 该飞机有各种各样的应用，包括天气监测和大气测试，通信，监视和其他应用程序。
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