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公开(公告)号：US4206892A
公开(公告)日：1980-06-10
申请号：US927020
申请日：1978-07-24
摘要： An efficient aircraft utilizes a stabilizer spaced from a fixed wing, and supported for controlled rolling about an axis extending generally in a forward direction, to control aircraft yaw. The stabilizer extends generally horizontally in straight forward flight. Pitch of the stabilizer is also controlled.
摘要翻译： 高效的飞行器利用与固定翼隔开的稳定器，并且被支撑用于围绕通常沿向前方向延伸的轴线的受控滚动以控制飞机偏航。 稳定器在直线向前飞行中大致水平地延伸。 稳定器的间距也受到控制。
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公开(公告)号：US3603537A
公开(公告)日：1971-09-07
申请号：US3603537D
申请日：1969-09-02
摘要： The invention concerns the provision of an apparatus that includes a light weight tethered object, such as a miniature kite, and a blower having a flow director located for directing blower displaced air toward the object to maintain the object in an elevated position.
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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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公开(公告)号：US5082079A
公开(公告)日：1992-01-21
申请号：US519015
申请日：1990-05-04
CPC分类号： B64C39/024 , B64C27/20 , B64C2201/027 , B64C2201/042 , B64C2201/044 , B64C2201/108 , B64C2201/141 , B64C2201/146 , B64C2201/162
摘要： A flight system capable of passively stable hover comprises an apparatus defining a vertical axis, and including multiple upright ducts spaced about the axis; fluid momentum generators in the ducts to effect flow of fluid downwardly in the ducts; and fluid flow deflector structure in the path of the downwardly flowing fluid, and angled to deflect the fluid flow away from the axis, in such manner as to provide stability in hover of the apparatus.
摘要翻译： 能够被动地稳定悬停的飞行系统包括限定垂直轴线的装置，并且包括围绕该轴线间隔开的多个直立导管; 管道中的流体动量发生器以使流体在管道中向下流动; 以及在向下流动的流体的路径中的流体流动偏转器结构，并且成角度以使流体流离开轴线，以便提供装置悬停的稳定性。
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公开(公告)号：USD243450S
公开(公告)日：1977-02-22
申请号：US596658
申请日：1975-07-17
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公开(公告)号：US5070955A
公开(公告)日：1991-12-10
申请号：US583477
申请日：1990-09-17
CPC分类号： B64C27/20 , B64C39/024 , B64C2201/027 , B64C2201/042 , B64C2201/044 , B64C2201/108 , B64C2201/141 , B64C2201/146 , B64C2201/162
摘要： A flight system capable of passively stable hover and horizontal translatory flight, comprises an apparatus defining a vertical axis, and including multiple ducts with substantially vertical axes in hover mode, spaced the axis; fluid momentum generators in the ducts to effect flow of fluid downwardly in the ducts in hover; and fluid flow deflector structure in the path of the flowing duct fluid, and angled to deflect the fluid flow away from the axis, in such manner as to provide stability in hover of the apparatus, as well as stability when the entire device is tilted through approximately 90.degree. to execute horizontal translatory flight.
摘要翻译： 能够被动地稳定悬停和水平平移的飞行系统包括限定垂直轴的装置，并且包括多个具有悬挂模式的基本垂直轴线的管道，该轴线间隔开; 管道中的流体动量发生器以在悬浮的管道中使流体向下流动; 以及在流动管道流体的路径中的流体流动偏转器结构，并且成角度以使流体流离开轴线，以便提供装置悬停的稳定性，以及当整个装置倾斜通过时的稳定性 大约90°执行水平平移飞行。
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公开(公告)号：US5035382A
公开(公告)日：1991-07-30
申请号：US339090
申请日：1989-04-17
CPC分类号： A63H27/00 , B64C39/024 , B64D47/08 , B64C2201/042 , B64C2201/104 , B64C2201/127 , B64C2201/141 , B64C2201/146 , B64C2201/148 , B64C2201/165 , B64C2201/187 , B64C2201/201 , B64C2201/203
摘要： A terrain surveillance, powered aircraft is disclosed to have an on-board video camera that is not gimballed relative to the aircraft, the aircraft typically comprising multiple components; the method of the invention including: assembling the components into aircraft configuration at or near a launch site; launching the aircraft at that site with no human pilot on board same; remotely controlling the flight path of the aircraft by radio or cable link, to fly to a location for terrain surveillance; operating the on-board video camera to survey the terrain while varying yaw of the aircraft to provide sweep viewing of the terrain; and recovering the aircraft by controlling its flight to steeply descend to a landing zone.
摘要翻译： 公开了一种地形监视，动力飞机，具有相对于飞机而不是游戏的车载摄像机，该飞机通常包括多个部件; 本发明的方法包括：将组件组装成发射场所处或附近的飞行器构型; 在该地点发射飞机，没有人造飞行员在船上; 通过无线电或有线链路远程控制飞机的飞行路径，飞到一个地形进行地形监视; 操作车载摄像机以在改变飞行器的偏航的同时对地形进行调查，以提供对地形的扫描观察; 并通过控制飞机陡降到着陆区来恢复飞机。
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公开(公告)号：US4057280A
公开(公告)日：1977-11-08
申请号：US629366
申请日：1975-11-06
IPC分类号： B62D35/00
CPC分类号： B62D35/001
摘要： An elongated protrusion extends adjacent and along a truck body corner in enveloping relation therewith, the corner located at the junction between the exterior side and top walls of a truck body, said protrusion having two rearwardly elongated edge portions respectively attached to the body exterior side wall and top wall, the protrusion having a rearwardly elongated mid-portion which is outwardly convex and which protrudes laterally throughout the major length of the protrusion.
摘要翻译： 一个细长的突出部，其与包围关系的卡车本体角相邻并且沿着卡车本体角延伸，角部位于卡车车体的外侧和顶壁之间的接合处，所述突起具有分别附接到车身外侧壁的两个向后延伸的边缘部分 和顶壁，所述突起具有向外凸出的向后伸长的中间部分，并且在所述突起的整个长度方向上横向突出。
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公开(公告)号：US3934923A
公开(公告)日：1976-01-27
申请号：US556210
申请日：1975-03-07
IPC分类号： B62D35/00
CPC分类号： B62D35/001
摘要： A drag reducing means for a truck includes a porous structure typically mounted on the cab roof to pass air into the gap between the cab and trailer body in rearward flowing streams that undergo deceleration. Eddies are formed in the gap and act as a barrier to airfow into the gap at its sides and top.
摘要翻译： 用于卡车的减阻装置包括通常安装在驾驶室车顶上的多孔结构，以便在经过减速的向后流动的气流中将空气传递到驾驶室和拖车车身之间的间隙中。 涡流形成在空隙中，作为空气障碍物进入其侧面和顶部的间隙。
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公开(公告)号：US3934922A
公开(公告)日：1976-01-27
申请号：US503290
申请日：1974-09-05
IPC分类号： B62D35/00
CPC分类号： B62D35/001
摘要： Apparatus combined with or combinable with a vehicle body having a longitudinally elongated corner from which body surfaces extend at an angle, one of the surfaces presented forwardly toward oncoming air flow, and the other surface extending generally rearwardly away from that corner, the apparatus comprisingA. means for preventing, reducing, or delaying separation of the flow boundary layer from said other surface rearwardly of said corner at normal operating speeds of the vehicle,B. said means comprising a longitudinally elongated protrusion having a substantially smooth, arcuate outer surface projecting smoothly outwardly of a first of said body surfaces said protrusion surface having a first longitudinally elongated terminal extent merging toward said first body surface in spaced relation to said corner, and second longitudinally elongated terminal extent merging toward a second of said body surfaces proximate said corner.
摘要翻译： 装置与具有纵向细长的角部的车身结合或可组合，车身表面从该角度以一定角度延伸，其中一个表面朝向迎面而来的气流向前展现，另一个表面大致向后延伸远离该角，该装置包括A 。防止，减少或延迟流动边界层从车辆的正常操作速度后面的其他表面分离的手段，B.表示包含具有实质性平滑的长时间延伸的突出部分，突出表面投射平滑的ARCE表面 第一个身体表面的第一个表面的表面表面具有第一个长期延长的终端终端合并，向上表示与表面角相关的第一个身体表面，以及第二个长期延长的终端接合，第二个身体表面的第二个身体表面接近角膜。
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