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1. 发明申请

US20050258306A1 Delta-winged hybrid airship 有权
标题翻译：三角翼混合飞艇
公开(公告)号：US20050258306A1
公开(公告)日：2005-11-24
申请号：US10853299
申请日：2004-05-24
申请人： Edward Barocela , Patrick Cassidy
发明人： Edward Barocela , Patrick Cassidy
IPC分类号： B64B1/20 , B64C39/10 , B64D27/24
CPC分类号： B64C39/10 , B64B2201/00 , B64D27/24 , B64D2211/00 , Y02T50/55 , Y02T50/64 , Y10S244/901
摘要： In one aspect, a hybrid airship including an outer shell, a plurality of helium filled gas envelopes, and an all-electric propulsion system may have the shape of a delta-wing. In some embodiments, the hybrid airship may be launched using buoyancy lift alone and aerodynamic lift may be provided by the all-electric propulsion system. In one aspect, a photovoltaic array and a high energy density power storage system may be combined to power the propulsion system making the propulsion system regenerative. The delta-wing shape can provide a surface area large enough to accommodate very large circular or elliptical transmission devices. By continuously recharging the power storage system, the hybrid airship in accordance with some embodiments can stay aloft at an operational altitude of at least about 85,000 ft for months or even years. The hybrid airship may function as an airborne military communications relay platform.
摘要翻译：一方面，包括外壳，多个氦气填充的气体包络和全电动推进系统的混合式飞艇可以具有三角翼的形状。在一些实施例中，混合式飞艇可以单独使用浮力提升机来启动，而空气动力提升可由全电动推进系统提供。在一个方面，光伏阵列和高能量密度功率存储系统可以组合起来，为推进系统提供动力，使推进系统再生。三角翼形状可以提供足够大的表面积以适应非常大的圆形或椭圆形传输装置。通过不断地对蓄电系统充电，根据一些实施例的混合式飞艇可以在至少约85,000英尺的操作高度上保持高度数月甚至数年。混合型飞艇可以作为空中军事通信中继平台。

2. 发明申请

US20030001045A1 Autonomous flying wing 失效
公开(公告)号：US20030001045A1
公开(公告)日：2003-01-02
申请号：US09895332
申请日：2001-07-02
申请人： ELSE Ltd.
发明人： Aharon Yifrach
IPC分类号： B64C003/00
CPC分类号： B64C39/024 , B64C3/56 , B64C39/10 , B64C2201/028 , B64C2201/042 , B64C2201/044 , B64C2201/048 , B64C2201/102 , B64C2201/123 , B64C2201/127 , B64C2201/141 , B64C2201/146 , B64C2201/167 , B64C2201/201 , B64D5/00 , Y10S244/90 , Y10S244/901
摘要： An unmanned flying vehicle comprises an autonomous flying wing having at least two wing portions arranged substantially symmetrically about a center portion. Each wing portion is pivotally attached to each adjoining portion such that the wing portions are foldable for storage and openable for deployment. A preferred form is the so-called seagull wing having four wing portions. The vehicles may be programmable from a mother aircraft whilst being borne to a deployment zone using a data link which may be wireless.

3. 发明授权

US4186680A Sail assembly 失效
标题翻译：帆组件
公开(公告)号：US4186680A
公开(公告)日：1980-02-05
申请号：US871805
申请日：1978-01-24
申请人： George B. Harpole
发明人： George B. Harpole
IPC分类号： B63B35/79 , B63H9/06
CPC分类号： B63H9/06 , B63B35/7973 , Y10S244/901 , Y10T24/44222 , Y10T24/44368
摘要： A skate sail is rigged with leading edge spars set by manipulation of a cruciform frame. The sail and frame assembly is suitable for mounting on a boat or vehicle as well as for being hand held, and is collapsible for compact stowing. When provided with a cinch line the sail assembly can be used for hang gliding. Rigging is set by joining separable lengths of a mast and advancing a transverse brace along the mast toward the mast head to deploy by toggle-like action head spars to which the sail is lashed thereby spreading and drawing taut a trapezium configuration of sail foil which is anchored to the foot of the mast. Laterally extendable wings may be provided and deployed separately to provide troughs which catch air spilling from the main sail foil and ease handling of the sail and enhance the ability of a user to trim the sail readily.
摘要翻译：溜冰帆是通过操纵十字架而设置的前缘翼梁。帆和框架组件适用于安装在船上或车辆上以及用于手持，并且可折叠以用于紧凑的收起。当提供一个系带线时，帆组件可用于悬挂滑行。通过连接桅杆的可分离长度来设置索具，并且沿着桅杆朝向桅杆头前进横向支架，以通过跷跷板状的动作头部翼梁来展开，桅杆被鞭打，从而展开并拉伸帆板的梯形构造锚固在桅杆的脚下。可以分开地设置和展开可伸缩翼，以提供捕获从主帆箔溢出的空气的槽，并且易于操纵帆，并且增强使用者容易地修剪帆的能力。

4. 发明授权

US4133500A Toy kites 失效
标题翻译：玩具风筝
公开(公告)号：US4133500A
公开(公告)日：1979-01-09
申请号：US834512
申请日：1977-09-19
申请人： Thomas M. Chapman
发明人： Thomas M. Chapman
IPC分类号： A63H27/01 , A63H27/08 , A63H33/20 , B64C31/02 , B64C31/06
CPC分类号： A63H33/20 , A63H27/08 , Y10S244/901
摘要： A toy kite has the general form of a hang glider and has a tow line which is releasable from the kite when in flight by slackening the tension in the tow line. Spars of the kite frame are hinged together by unitary plastic hinges and the frame can be folded and erected by moving a slider along a main spar. A pilot figure suspended in a harness below the kite is adjustable to alter the trim.
摘要翻译：一种玩具风筝具有悬挂式滑翔机的一般形式，并且具有拖曳线，该拖曳线在飞行中通过松弛拖曳线中的张力而从风筝中释放出来。风筝框架的花边通过单一塑料铰链铰接在一起，并且框架可以通过沿着主翼梁移动滑块而被折叠和竖立。悬挂在风筝下方的吊带的飞行员可以调整以改变装饰。

5. 发明授权

US3356316A Hinged spar flexible wing glider 失效
标题翻译：铰链翼梁柔性翼滑翔机
公开(公告)号：US3356316A
公开(公告)日：1967-12-05
申请号：US49672665
申请日：1965-10-15
申请人： FOREHAND JOSEPH E
发明人： FOREHAND JOSEPH E
IPC分类号： B64C31/02 , B64C31/032
CPC分类号： B64C31/032 , B64C31/02 , Y10S244/901

6. 发明授权

US3250500A Kite construction 失效
公开(公告)号：US3250500A
公开(公告)日：1966-05-10
申请号：US35383364
申请日：1964-03-23
申请人： HALL RUSSELL S
发明人： HALL RUSSELL S
IPC分类号： B64C31/06
CPC分类号： A63H27/08 , Y10S244/901

7. 发明授权

US3197158A Flexible wing vehicle configurations 失效
标题翻译：灵活的机动车配置
公开(公告)号：US3197158A
公开(公告)日：1965-07-27
申请号：US42969564
申请日：1964-12-11
申请人： ROGALLO FRANCIS M
发明人： ROGALLO FRANCIS M
IPC分类号： B64C31/032
CPC分类号： B64C31/032 , Y10S244/901

8. 发明授权

US06626397B2 Autonomous flying wing 失效
标题翻译：自主飞翼
公开(公告)号：US06626397B2
公开(公告)日：2003-09-30
申请号：US09895332
申请日：2001-07-02
申请人： Aharon Yifrach
发明人： Aharon Yifrach
IPC分类号： B65C300
CPC分类号： B64C39/024 , B64C3/56 , B64C39/10 , B64C2201/028 , B64C2201/042 , B64C2201/044 , B64C2201/048 , B64C2201/102 , B64C2201/123 , B64C2201/127 , B64C2201/141 , B64C2201/146 , B64C2201/167 , B64C2201/201 , B64D5/00 , Y10S244/90 , Y10S244/901
摘要： An unmanned flying vehicle comprises an autonomous flying wing having at least two wing portions arranged substantially symmetrically about a center portion. Each wing portion is pivotally attached to each adjoining portion such that the wing portions are foldable for storage and openable for deployment. A preferred form is the so-called seagull wing having four wing portions. The vehicles may be programmable from a mother aircraft whilst being borne to a deployment zone using a data link which may be wireless.
摘要翻译：无人驾驶飞行器包括具有至少两个围绕中心部分大致对称布置的翼部的自主飞行翼。每个翼部可枢转地附接到每个相邻部分，使得翼部可折叠以用于存储并且可展开。优选的形式是所谓的具有四个翼部的海鸥翼。车辆可以从母机飞行器编程，同时使用可能是无线的数据链路承载到部署区域。

9. 发明授权

US5816537A Inflatable kite arrangement and launcher 失效
标题翻译：充气风筝安排和发射器
公开(公告)号：US5816537A
公开(公告)日：1998-10-06
申请号：US481317
申请日：1996-03-13
申请人： Vernon G. Pascoe , Bernard W. Hanning
发明人： Vernon G. Pascoe , Bernard W. Hanning
IPC分类号： A63H27/08 , B64C31/06 , F41J9/10
CPC分类号： A63H27/085 , B64C31/06 , Y10S244/901
摘要： An inflatable kite (150) that includes a plurality of longitudinal inflatable tubes (54). The kite includes transverse inflatable tube (53) at the rear end of the kite. When the kite is inflated, the front end has a larger cross-sectional area than the rear end. When inflated the rear edge and the side edges are coplanar. Air vents (57, 157) are provided. The kite may be inflated and launched manually or by an automatic launcher.
摘要翻译： PCT No.PCT / GB94 / 00672 Sec。 371日期：1996年3月13日 102（e）日期1996年3月13日PCT 1994年3月30日PCT公布。第WO94 / 23812号公报日期1994年10月27日包括多个纵向可充气管（54）的充气风筝（150）。风筝包括风筝后端的横向充气管（53）。当风筝膨胀时，前端具有比后端更大的横截面积。当充气时，后边缘和侧边缘是共面的。提供通风口（57，157）。风筝可以手动或通过自动发射器进行充气和放风。

10. 发明授权

US4047679A Triangular-wing glider 失效
标题翻译：三角翼滑翔机
公开(公告)号：US4047679A
公开(公告)日：1977-09-13
申请号：US647160
申请日：1976-01-07
申请人： Paul Marcel Edmond Decroix
发明人： Paul Marcel Edmond Decroix
IPC分类号： B64C31/032 , B64C31/02
CPC分类号： B64C31/032 , Y10S244/901
摘要： A light triangular-wing glider, comprises an auxiliary wing or stabilizer, arranged in an average plane approximately parallel to that of the principal wing, in front and above the latter. This auxiliary wing is flexible, principally constituted from a material such as cloth and capable of taking a curvilinear shape under the influence of the relative airstream. The pilot can thereby modify the angle of attack of the whole of the glider and notably pull the craft out of a dive.
摘要翻译：轻型三角翼滑翔机包括辅助机翼或稳定器，其布置在大致平行于主翼翼平面的平面上，在前后方向上。这种辅助翼是柔性的，主要由诸如布料的材料构成，并且能够在相对气流的影响下呈现曲线形状。飞行员可以改变整个滑翔机的攻角，特别是把飞艇从潜水中拉出来。

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