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1. 发明授权

US11014671B2 Tow cable system and method of use 有权
公开(公告)号：US11014671B2
公开(公告)日：2021-05-25
申请号：US15973346
申请日：2018-05-07
申请人： TGALTO Holding, LLC
发明人： Michael J. Gallo
IPC分类号： B64D3/00 , B64C31/02 , B64D1/10 , B64D1/12
摘要： A tow cable system and method of use wherein, in the context of towed flight of a glider behind an aircraft, positive load or tension of the cable therebetween is achieved through one or more of cable design and material selection, cable pre-tensioning, in-flight cable tensioning, and/or load dampening device(s), and the related interplay of such various components or sub-systems of the overall tow cable system.

2. 发明申请

US20200231269A1 FLIGHT ASSEMBLY AND METHOD FOR FLIGHT THEREOF 审中-公开
公开(公告)号：US20200231269A1
公开(公告)日：2020-07-23
申请号：US16251753
申请日：2019-01-18
申请人： Haile E. Woubou
发明人： Haile E. Woubou
IPC分类号： B64C3/56 , B64C31/02
摘要： A flight assembly and glider possessing bilateral, flexible, and collapsible wings and associated method of flight are provided. The flight assembly may include a central frame that may encapsulate a human operator. A wing frame may include at least a pair of wings that couple to the central frame, wherein each wing may include one or more pivotal connections. To control the extension and retraction of the pair of wings, a control lever network may be incorporated within the central frame and the wing frame. The control lever network may include wing sail deployment, flight deceleration and parachute wing conversion features.

3. 发明申请

US20200031469A1 UNMANNED GLIDER SYSTEM FOR PAYLOAD DISPERSION 审中-公开
公开(公告)号：US20200031469A1
公开(公告)日：2020-01-30
申请号：US16580263
申请日：2019-09-24
申请人： ALMOG RESCUE SYSTEMS LTD.
发明人： Ariel Zilbertstein
IPC分类号： B64C39/02 , B64C31/02 , B64D1/10 , B64D1/16
摘要： A disposable unmanned aerial glider (UAG) with pre-determined UAG flight capabilities. The UAG comprises a flight module comprising at least one aerodynamic arrangement; and a fuselage module comprising a container configured for storing therein a payload and having structural integrity. The container is pressurized so as to maintain structural integrity thereof at least during flight, so that the UAG flight capabilities are provided only when the container is pressurized.

4. 发明授权

US10416684B2 Airborne vehicle recovery 有权
公开(公告)号：US10416684B2
公开(公告)日：2019-09-17
申请号：US15492161
申请日：2017-04-20
申请人： Worcester Polytechnic Institute
发明人： Richard T. Eberheim , Nicholas F. Hassan , Joshua C. O'Connor
IPC分类号： G05D1/10 , B64B1/46 , B64C31/02 , B64C39/02 , B64D45/04 , G05D1/06 , B64C19/00
摘要： The airborne vehicle recovery method and apparatus enables radiosonde users to reliably recover launched radiosondes and provides new and unique opportunities for research and data acquisition with balloon launched radiosondes. Airborne vehicles such as radiosondes are disposed in a flight body adapted for propulsionless, gliding navigation for returning to one of several designated landing sites for recovery. Onboard electronics including a navigation computer, flight computer, and lightweight battery are employed for selecting a landing site, computing a heading and direction, and actuating flaps for pursuing a propulsionless, gliding path to the landing site. Gliding is directed only by right and left flaps responsive to respective actuators, such that the inclusion of only the actuators, navigation and flight electronics, and without active propulsion, enables sufficient gliding range from the lightweight construction and arrangement to reach one of several landing sites for effecting substantial recovery rates of the radiosondes.

5. 发明申请

US20180086434A1 An Aircraft for Aerial Delivery 审中-公开
公开(公告)号：US20180086434A1
公开(公告)日：2018-03-29
申请号：US15567585
申请日：2016-04-20
申请人： George Michael Cook
发明人： George Michael Cook , Jonathan Edward Cook , Michael Kevin Cook
IPC分类号： B64C13/28 , B64C3/56 , B64C1/06 , B64C31/02 , B64C39/02
CPC分类号： B64C13/30 , B64C1/061 , B64C3/56 , B64C13/28 , B64C31/02 , B64C39/024 , B64C2001/0054 , B64C2201/021 , B64C2201/102 , B64C2201/128 , B64C2201/141 , B64C2211/00
摘要： An aircraft for the autonomous aerial delivery of a load to a target location, the aircraft comprising an airframe having at least one adjustable control structure for controlling the flight of the aircraft and a main body adapted to receive a load a self-contained control module releaseably connected to the airframe, the control module containing an actuator for adjusting the control structure and a controller for producing an electrical drive signal for controlling the actuator; and at least one linkage extending from the control module to the at least one adjustable control structure so as to operably connect the control module to the at least one adjustable control structure, wherein the actuator of the control module is adapted to adjust the at least one adjustable control structure using the at least one linkage so as to control the flight of the aircraft and to steer the aircraft to the target location.

6. 发明申请

US20170259918A1 DUAL-AIRCRAFT SYSTEM 审中-公开
公开(公告)号：US20170259918A1
公开(公告)日：2017-09-14
申请号：US15066460
申请日：2016-03-10
申请人： NICHOLAS K. CHRISTENSEN
发明人： NICHOLAS K. CHRISTENSEN
IPC分类号： B64D1/02 , B64C31/02 , B64C11/00 , B64C39/02
CPC分类号： B64C31/02 , B64C37/02 , B64C39/024 , B64C2201/021 , B64C2201/027 , B64C2201/082 , B64C2201/086 , B64C2201/104 , B64C2201/108 , B64C2201/162 , B64C2201/206
摘要： One example includes a dual-aircraft system. The system includes a glider aircraft configured to perform at least one mission objective in a gliding-flight mode during a mission objective stage. The system also includes an unmanned singlecopter configured to couple to the glider aircraft via a mechanical linkage to provide propulsion for the glider aircraft during a takeoff and delivery stage. The unmanned singlecopter can be further configured to decouple from the glider aircraft during a detach stage in response to achieving at least one of a predetermined altitude and a predetermined geographic location to provide the gliding-flight mode associated with the glider aircraft, such that the glider aircraft subsequently enters the mission objective stage.

7. 发明授权

US09494937B2 Method and system for drone deliveries to vehicles in route 有权
公开(公告)号：US09494937B2
公开(公告)日：2016-11-15
申请号：US14310261
申请日：2014-06-20
申请人： HTI, IP, L.L.C.
发明人： Robert S. Siegel , Stephen Christopher Welch , James Ronald Barfield, Jr.
IPC分类号： G05D1/00 , B64C31/02 , B64D1/08 , B64D1/22 , G05D1/10 , G06Q10/08 , G01C21/20 , G01C21/34 , B64C39/02
CPC分类号： G05D1/0027 , B64C39/024 , B64C2201/128 , B64C2201/146 , B64D1/08 , B64D1/22 , G01C21/20 , G01C21/3438 , G05D1/00 , G05D1/0684 , G05D1/101 , G05D1/104 , G06Q10/083
摘要： A system comprise a server configured to communicate vehicle information with a vehicle transceiver of a vehicle moving along a vehicle route and communicate drone information with a drone transceiver of a drone moving along a drone route. A computing device with a memory and a processor may be configured to communicatively connect with the server, process the vehicle information and the drone information, identify a plurality of pickup locations based in part on the vehicle information and drone information, select at least one of the plurality of pickup locations based in part on a priority score associated with a travel time to or wait time for each of the plurality of pickup locations, and update the drone route based in part on the selected pickup location.

8. 发明申请

US20150266573A1 System for Airboarding Behind an Aircraft 审中-公开
标题翻译：飞机背后的飞机系统
公开(公告)号：US20150266573A1
公开(公告)日：2015-09-24
申请号：US14656648
申请日：2015-03-12
申请人： Aaron Wypyszynski
发明人： Aaron Wypyszynski
IPC分类号： B64C31/02 , B64C13/04 , B64C25/06 , B64C25/34 , B64D3/00 , B64D17/80
CPC分类号： B64D17/80 , B64C31/028 , B64C39/026 , B64D3/00
摘要： A system for airboarding and performing stunts behind an aircraft includes a lifting board, a handle, and a tow rope connected to the board and handle. The lifting board may include landing gear, a binding for securing an operator to the board, tail sections for stabilizing the board during flight, and ailerons for facilitating turns and rolls. The system may include a control system integrated into the handle and board that improves the operator's ability to control the board.
摘要翻译：飞机背后的飞行和执行特技的系统包括提升板，手柄和连接到板和手柄的拖绳。提升板可以包括起落架，用于将操作者固定到板的装订，用于在飞行期间稳定板的尾部部分和用于便于转动和滚动的副翼。该系统可以包括集成到手柄和板中的控制系统，其提高操作者控制电路板的能力。

9. 发明授权

US5566908A Air-launchable gliding sonobuoy 失效
标题翻译：空中发射滑翔伞
公开(公告)号：US5566908A
公开(公告)日：1996-10-22
申请号：US380178
申请日：1995-01-30
申请人： Samuel Greenhalgh
发明人： Samuel Greenhalgh
IPC分类号： B63B22/00 , F42B10/62 , F42B12/56 , B64D1/02 , B64C3/26 , B64C31/02
CPC分类号： B63B22/003 , F42B10/62 , F42B12/56
摘要： An air-launchable gliding sonobuoy store includes a canister enclosing an flatable membranous wing folded in a collapsed state with an electroacoustic system. After launching, the wing inflates and a steering mechanism controls the wing glide path by skewing the trailing edge thereof. Upon reaching the sea, the wing serves as a buoy with the electroacoustic system transducer depending therefrom.
摘要翻译：一个可发射的滑翔超声波存储器包括一个包围充气折叠状态的可膨胀的膜状翼的罐，其具有电声系统。发射后，机翼膨胀，转向机构通过使其后缘偏斜来控制机翼滑行路径。在到达大海时，机翼作为浮标，电声系统换能器从此浮起。

10. 发明授权

US4982917A Glider-canopy 失效
标题翻译：滑翔伞
公开(公告)号：US4982917A
公开(公告)日：1991-01-08
申请号：US302967
申请日：1989-01-30
申请人： Wilhelm Graske
发明人： Wilhelm Graske
IPC分类号： B64D17/10 , B64C31/02 , B64C31/036 , B64D17/02 , B64D17/34
CPC分类号： B64D17/025
摘要： A glider-canopy has a wing-shaped sail with a rear edge. Fins are mounted to the underside of the sail in an essentially parallel direction to the intended direction of flight. Shroud lines act on at least the fins and converge by their free ends into a personnel support. The fins are equipped with elastically bendable reinforcements tensioning the fins at least under traction from the shroud lines during flight. The fins are tensioned essentially in the horizontal direction so that in the loaded state the sail bulges downwardly at least at the rear edge, and in the event of a load decrease the reinforcements are stress relieved and the sail bulges upwardly at least at the rear edge.
摘要翻译：滑翔伞具有后翼的翼形帆。翅片沿着与预期飞行方向基本平行的方向安装在帆的下侧。护罩线至少作用于翅片，并通过其自由端收敛到人员支撑中。散热片装备有弹性可弯曲的增强件，其在飞行期间至少在护罩线的牵引下张紧翅片。翅片基本上在水平方向上张紧，使得在负载状态下，帆至少在后边缘处向下凸出，并且在负载减小的情况下，加强件应力消除，并且帆至少在后边缘处向上凸起。

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