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11. 发明授权

US06892981B2 Stealthy duffel bag airplane 失效
标题翻译：隐形行李袋飞机
公开(公告)号：US06892981B2
公开(公告)日：2005-05-17
申请号：US10408981
申请日：2003-04-08
申请人： Jay Lipeles
发明人： Jay Lipeles
IPC分类号： B64C3/30 , B64C3/56 , B64C39/02 , B64C39/10 , B64D33/04 , B64C39/00
CPC分类号： B64C39/024 , B64C3/30 , B64C3/56 , B64C39/10 , B64C2201/028 , B64C2201/044 , B64C2201/046 , B64C2201/105 , B64C2201/127 , B64C2201/141 , B64C2201/146 , B64C2201/203 , B64C2201/22 , B64D33/04 , B64D2033/045
摘要： The Duffel Bag Airplane is an inflatable flying wing unmanned airborne vehicle (UAV). The fuselage will house everything but the wings. The wing can be rolled up around the fuselage into a small package when deflated for easy transportation, such as by being carried in a duffle bag. Fabric construction, a small internal combustion engine with cooled exhaust, and wing warping controls combine to make the airplane inexpensive and extremely stealthy. All the usual signatures have been suppressed, which allow it to be used to make observations from close range under combat conditions. Control of this airplane is accomplished by warping the wings and is supplemented with stability augmentation.
摘要翻译： Duffel Bag飞机是一种充气飞翼无人机载机（UAV）。机身将会容纳除翅膀之外的所有东西。机翼可以卷绕在机身周围，当放气以便于运输时，例如通过携带在行李箱中，成为小包装。织物结构，具有冷却排气的小型内燃机和机翼翘曲控制相结合，使飞机廉价而且非常隐蔽。所有通常的签名已经被压制，这允许它用于在战斗条件下从近距离观察。这架飞机的控制是通过扭转机翼来实现的，并补充了稳定性增强。

12. 发明申请

US20040211862A1 Unmanned aerial vehicle with integrated wing battery 审中-公开
标题翻译：无人机配有集成翼电池
公开(公告)号：US20040211862A1
公开(公告)日：2004-10-28
申请号：US10423187
申请日：2003-04-25
发明人： Daryl B. Elam
IPC分类号： B64D041/00
CPC分类号： A63H27/02 , B64C39/024 , B64C2201/046 , B64C2201/048 , B64C2201/104 , B64C2201/126 , B64C2201/127 , B64C2201/146 , B64C2201/167 , B64D27/24 , Y02T50/44 , Y02T50/62
摘要： An unmanned aerial vehicle, such as a remotely-piloted airplane, includes lift-producing wings that have batteries embedded or otherwise located within them. Locating the batteries within the wings allows more efficient use of the interior space of the unmanned vehicle. Space within a fuselage of the vehicle, which would otherwise be used for batteries, may be used for other components. Alternatively, fuselage, weight and/or size of the unmanned aerial vehicle may be reduced. In addition, locating the batteries within the wings may provide better structural performance of the wings, and/or may allow characteristics of the wings, such as inertia and moments, to be optimized.
摘要翻译：诸如遥控飞机的无人驾驶飞行器包括具有嵌入或以其他方式位于其中的电池的升降机翼。将电池放置在机翼内可以更有效地利用无人驾驶车辆的内部空间。车辆的机身中的空间，否则将用于电池，可用于其他部件。或者，可以减少无人驾驶飞行器的机身，重量和/或尺寸。此外，将电池定位在机翼内可以提供更好的机翼的结构性能，和/或可以允许优化机翼的特性，例如惯性和力矩。

13. 发明授权

US06749153B1 Survivable and reusable launch vehicle 有权
标题翻译：生存和可重复使用的运载火箭
公开(公告)号：US06749153B1
公开(公告)日：2004-06-15
申请号：US10309828
申请日：2002-12-04
申请人： Henry August
发明人： Henry August
IPC分类号： B04B120
CPC分类号： B64C39/024 , B64C2201/021 , B64C2201/046 , B64C2201/104 , B64C2201/121 , F42B10/16 , F42B10/62 , F42B12/58 , F42B12/62 , F42B15/00
摘要： A reusable, mach-velocity mobile platform delivers a weapons payload via vertical launch, powerless glide, weapons release, and landing operation phases. The platform includes a generally tubular shaped body having an aft and forward end, and a payload section. An arch wing is supported by the body aft end. The arch wing has an upper and a lower wing joined at distal ends by two curved end plates. A nose assembly is connected at the forward end having an upward directed fixed angle-of-attack to generate forward end lift. Thermal tiles attached under the body and the lower wing under-side radiate/dissipate heat generated during a high angle-of-attack platform reentry. Radar absorptive or radar translucent material is used. The platform preferably discharges payload from the aft end for safe separation. A landing gear is extended for the landing phase of operation.
摘要翻译：可重复使用的马赫速度移动平台通过垂直发射，无力滑翔，武器释放和着陆操作阶段提供武器有效载荷。平台包括具有尾部和前端的大致管状的主体和有效载荷部分。一个弓翼由身体后端支撑。拱翼具有通过两个弯曲端板在远端连接的上翼和下翼。前端组件在前端连接，具有向上定向的固定迎角，以产生前端提升。安装在车体下方的散热瓦片和下部翼片下侧辐射/消散在高角度攻角平台折返期间产生的热量。使用雷达吸收或雷达半透明材料。该平台优选地从尾端排出有效载荷以进行安全分离。起落架延伸到着陆阶段。

14. 发明授权

US06698685B2 Circular vertical take off and landing aircraft 失效
标题翻译：圆形垂直起降飞机
公开(公告)号：US06698685B2
公开(公告)日：2004-03-02
申请号：US10084749
申请日：2002-02-26
申请人： Eric Ronald Walmsley
发明人： Eric Ronald Walmsley
IPC分类号： B64C3906
CPC分类号： B64C27/20 , B64C29/0066 , B64C39/001 , B64C39/024 , B64C39/06 , B64C39/062 , B64C2201/027 , B64C2201/046 , B64C2201/048 , B64C2201/108 , B64C2201/121 , B64C2201/127
摘要： A circular VTOL aircraft with a central vertically mounted jet or rocket engine 7, (or engines) having below vertical thrust vents 14 at cardinal points, together with a jet/rocket engine 20 (or engines) horizontally mounted on turntable pod 16 which is steerable through 360 degrees and centrally situated below the vertical engine (s). Alternatively the horizontal engine can be replaced by central thrust vent 36 delivering thrust from the vertical engine to vectored thrust nozzle 37 attached to the turntable. Thrust from the four vertical thrust vents is controlled by valves 21 giving VTOL thrust control as well as pitch and bank control. The horizontal engine provides acceleration and retro-thrust for horizontal flight and directional control through 360 degrees. The passenger cabin is situated in the main body of the aircraft. Fuel tanks are installed around the central engines. The flight-deck is situated at the top-centre of the craft above the engines, which are detachable for maintenance.
摘要翻译：具有中心垂直安装的喷气式或火箭发动机7（或发动机）的圆形垂直起降飞机与在水平安装在可转向的转盘舱16上的喷气/火箭发动机20（或发动机）一起在主要点处具有下垂直推力通风口14 通过360度并位于垂直发动机下方的中心位置。或者，水平发动机可以由中心推力孔36代替，其将来自垂直发动机的推力传递到附接到转盘的向量推力喷嘴37。来自四个垂直推力通风口的推力由阀门21控制，提供垂直起动器推力控制以及俯仰和组合控制。水平发动机提供加速度和逆向推力，用于水平飞行和360度方向控制。客舱位于飞机的主体。燃油箱安装在中央发动机周围。飞行甲板位于发动机上方的工艺的顶部中心，可拆卸以进行维护。

15. 发明授权

US4666105A Unmanned aircraft 失效
标题翻译：无人机
公开(公告)号：US4666105A
公开(公告)日：1987-05-19
申请号：US784484
申请日：1985-10-04
申请人： Juergen Dellinger , Hans-Jochen Hoeppner , Ulrich Kraemer
发明人： Juergen Dellinger , Hans-Jochen Hoeppner , Ulrich Kraemer
IPC分类号： B64C39/02 , F42B15/36 , B64F1/04
CPC分类号： F42B15/36 , B64C39/024 , B64C2201/046 , B64C2201/127 , B64C2201/128 , B64C2201/165 , B64C2201/185
摘要： An unmanned craft having a fuselage, a propeller drive with a propeller being arranged in the tail portion of the fuselage for purposes of cruising, and a rocket assist propulsion system for the takeoff phase is releasably mounted to the fuselage, the improvement includes three spring biased thrust rods being secured to the frame and releasably engaging peripheral points of the craft. The thrust rods are radially pivotal in outer direction. Support points on the wings and the rudder engage front ends of the rods in contourmatching relationship but are disengageable therefrom.
摘要翻译：具有机身的无人飞行器，具有推进器的螺旋桨驱动器布置在机身的尾部以用于巡航，并且用于起飞阶段的火箭辅助推进系统可释放地安装到机身，改进包括三个弹簧偏置推杆被固定到框架并且可释放地接合工艺的外围点。推力杆在外部方向上是径向枢转的。机翼和方向舵上的支撑点以轮廓匹配关系与杆的前端接合，但是与其脱离接合。

16. 发明授权

US4530476A Ordnance delivery system and method including remotely piloted or programmable aircraft with yaw-to-turn guidance system 失效
标题翻译：兵器交付系统和方法包括遥控或可编程飞机与偏航转弯导向系统
公开(公告)号：US4530476A
公开(公告)日：1985-07-23
申请号：US292260
申请日：1981-08-12
申请人： Charles H. Thurber, Jr. , Frederick A. Behrens , John H. Hunton
发明人： Charles H. Thurber, Jr. , Frederick A. Behrens , John H. Hunton
IPC分类号： B64C39/02 , B64F1/10 , F41G7/00 , F41G7/22 , F41F3/00 , F42B15/16
CPC分类号： F41G7/22 , B64C39/024 , B64F1/06 , F41G7/007 , B64C2201/021 , B64C2201/046 , B64C2201/084 , B64C2201/102 , B64C2201/127 , B64C2201/141 , B64C2201/146 , B64C2201/165 , B64C2201/201 , B64C2201/208
摘要： A method and system for delivering ordnance to a target via a remotely piloted or programmable aircraft including a yaw-to-turn guidance system, a deployment and launching system and packaging for the aircraft are disclosed.
摘要翻译：公开了一种用于通过远程驾驶或可编程飞行器向目标提供弹药的方法和系统，包括偏航转弯引导系统，用于飞行器的展开和发射系统和包装。

17. 发明授权

US09969490B2 Motor vehicle with captive aircraft 有权
公开(公告)号：US09969490B2
公开(公告)日：2018-05-15
申请号：US14645194
申请日：2015-03-11
申请人： Elwha LLC
发明人： William D. Duncan , Roderick A. Hyde , Jordin T. Kare , Stephen L. Malaska , Nathan P. Myhrvold , Robert C. Petroski , Thomas Allan Weaver , Lowell L. Wood, Jr.
IPC分类号： B64C39/02 , B64F1/00
CPC分类号： B64C39/024 , B64C39/022 , B64C2201/021 , B64C2201/042 , B64C2201/046 , B64C2201/063 , B64C2201/066 , B64C2201/12 , B64C2201/127 , B64C2201/145 , B64C2201/146 , B64C2201/208 , B64F1/00 , G05D1/0094
摘要： A motor vehicle system includes a motor vehicle including an aircraft landing portion, and an actively propelled unmanned aircraft configured to be supported on the aircraft landing portion. The vehicle and aircraft are configured such that the vehicle can provide at least one of fuel and electrical energy to the aircraft while the aircraft is supported on the aircraft landing portion.

18. 发明申请

US20150102154A1 MOTOR VEHICLE WITH CAPTIVE AIRCRAFT 审中-公开
标题翻译：具有主动飞机的电动车
公开(公告)号：US20150102154A1
公开(公告)日：2015-04-16
申请号：US14054613
申请日：2013-10-15
申请人： Elwha LLC
发明人： William D. Duncan , Roderick A. Hyde , Jordin T. Kare , Stephen L. Malaska , Nathan P. Myhrvold , Robert C. Petroski , Thomas Allan Weaver , Lowell L. Wood, JR.
IPC分类号： B64F1/00 , B64D47/08 , B64D9/00 , B64C39/00 , B64D37/00
CPC分类号： B64C39/024 , B64C39/022 , B64C2201/021 , B64C2201/042 , B64C2201/046 , B64C2201/063 , B64C2201/066 , B64C2201/12 , B64C2201/127 , B64C2201/145 , B64C2201/146 , B64C2201/208 , B64F1/00 , G05D1/0094
摘要： A motor vehicle system includes a motor vehicle including an aircraft landing portion, and an actively propelled unmanned aircraft configured to be supported on the aircraft landing portion. The vehicle and aircraft are configured such that the vehicle can provide at least one of fuel and electrical energy to the aircraft while the aircraft is supported on the aircraft landing portion.
摘要翻译：机动车辆系统包括包括飞行器着陆部分的机动车辆和被配置为被支撑在飞行器着陆部分上的主动推进无人飞行器。车辆和飞行器构造成使得当飞行器被支撑在飞行器着陆部分上时，车辆能够向飞机提供燃料和电能中的至少一种。

19. 发明申请

US20140231594A1 ROTOCRAFT 审中-公开
公开(公告)号：US20140231594A1
公开(公告)日：2014-08-21
申请号：US14061723
申请日：2013-10-23
申请人： Robert Marcus
发明人： Robert Marcus
IPC分类号： B64C19/00 , B64D45/00
CPC分类号： B64C19/00 , B64C29/0058 , B64C39/024 , B64C2201/027 , B64C2201/046 , B64C2201/088 , B64D45/00
摘要： An aerial vehicle includes independently controlled horizontal thrusters and vertical lifters to provide design and operational simplicity while allowing precision flying with six degrees of freedom and use of mounted devices such as tools, sensors, and instruments. Each horizontal thruster and vertical lifter can be mounted as constant-pitch, fixed-axis rotors while still allowing for precise control of yaw, pitch, roll, horizontal movement, and vertical elevation. Gyroscopes and inclinometers can be used to further enhance flying precision. A controller manages thrust applied the horizontal thrusters and vertical lifters to compensate for forces and torques generated by the use of tools and other devices mounted to the aerial vehicle.
摘要翻译：飞行器包括独立控制的水平推进器和垂直升降器，以提供设计和操作简单性，同时允许六度自由度的精确飞行和使用诸如工具，传感器和仪器的安装设备。每个水平推进器和垂直升降器可以安装为恒定间距的固定轴转子，同时仍然允许精确控制偏航，俯仰，滚动，水平运动和垂直高程。陀螺仪和倾斜仪可用于进一步提高飞行精度。控制器管理施加水平推进器和垂直升降器的推力，以补偿由使用安装在飞行器上的工具和其他装置产生的力和扭矩。

20. 发明授权

US08669504B2 Hand launchable unmanned aerial vehicle 有权
公开(公告)号：US08669504B2
公开(公告)日：2014-03-11
申请号：US13790655
申请日：2013-03-08
申请人： Gerald Miller , James Stewart
发明人： Gerald Miller , James Stewart
IPC分类号： F41F7/00
CPC分类号： B64C19/00 , B64C39/028 , B64C2201/046 , B64C2201/084 , B64C2201/104 , B64C2201/127 , B64C2201/141 , B64C2201/201 , B64C2201/203 , F41F3/042 , F41G7/008 , F41G7/2206 , F41G7/2253 , F41G7/2293 , F42B12/20 , F42B12/365 , F42B15/01 , F42B15/10 , G05D1/12
摘要： An unmanned aerial vehicle including a controller operating in a search mode of operation where a receiver of an acquisition sensor searches for a target and causes flight control surfaces to guide the vehicle in a downward spiral path, a terminal mode of operation where the acquisition sensor detects a target and causes flight control surfaces to direct the vehicle toward the target, and an activation mode of operation where a trigger sensor detects a target within a predetermined distance to the vehicle and the controller activates a responder.

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