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1. 发明申请

US20190047724A1 Pin Array Chamber Systems and Methods for Releasing and Capturing a Moving Object - Space 审中-公开
公开(公告)号：US20190047724A1
公开(公告)日：2019-02-14
申请号：US15672032
申请日：2017-08-08
申请人： Jeffrey Alan McChesney
发明人： Jeffrey Alan McChesney
IPC分类号： B64F1/02 , B64F5/50 , B64F1/04
CPC分类号： B64F1/02 , B64C2201/141 , B64C2201/146 , B64C2201/182 , B64F1/04 , B64F5/50
摘要： A pin array release and capture chamber system includes a chamber assembly having two parallel plates of pin arrays from which a plurality of pins extends and retract vertically opposite each other so as to release and capture a space vehicle. The pin arrays are separated from each other by a space having two vertical and two horizontal sides, and the space is sized so as to receive the space vehicle. Each pin arrays may be housed in a pin array chamber enclosure. The chamber assembly may be attached to a moving object, such as a host space vessel.

2. 发明授权

US09969504B1 Automated multi-plane propulsion system 有权
公开(公告)号：US09969504B1
公开(公告)日：2018-05-15
申请号：US15082255
申请日：2016-03-28
申请人： The United States of America, as represented by the Secretary of the Navy
发明人： Raymond Lawson Davis , Patrick Alan Livesay
IPC分类号： B64F1/04 , B64C39/02
CPC分类号： B64F1/04 , B64C39/024 , B64C2201/021 , B64C2201/08
摘要： Provided here is a UAV launcher generally comprising a launcher frame, first rail guide, second rail guide, and a conveyor system comprising a conveyor, where the first rail guide, second rail guide, and some portion of the conveyor are typically substantially parallel, and where the first and second rail guide typically extend beyond the driver wheel of the conveyor system in a launching direction. The driver wheel and driven wheel of the conveyor system rotate on axes generally perpendicular to the first and second rail guide. A DC motor is coupled to the driver wheel and generates rotation of the driver wheel, and correspondingly governs the linear velocity of the conveyor. A motor controller is configured to control the RPM of the DC motor using a motor speed profile and a wedge interface coupled to the transmission drive motivates a loaded UAV to a launching velocity such that the UAV achieves airborne operation.

3. 发明申请

US20180050823A1 CAPTURE AND LAUNCH APPARATUS AND METHOD OF USING SAME FOR AUTOMATED LAUNCH, RETRIEVAL, AND SERVICING OF A HOVERING AIRCRAFT 审中-公开
公开(公告)号：US20180050823A1
公开(公告)日：2018-02-22
申请号：US15421732
申请日：2017-02-01
申请人： Aerovel Corporation
发明人： Brian T. McGeer
IPC分类号： B64F1/04
CPC分类号： B64F1/04 , B64C29/02 , B64C39/024 , B64C2201/08 , B64C2201/182
摘要： Automated launch and retrieval of a “tail-sitting” VTOL aircraft is accomplished by exploiting the natural stability of hover when restrained in tension by an upwind wing tip. For retrieval, a flexible rod is lifted into contact with the trailing edge of the upwind wing as the aircraft translates downwind overhead. Sliding between the rod and wing leads to interlocking of hooks at the rod end and wing tip, while the aircraft swings into a stable tethered hover downwind of the rod. The rod is then used to pull the aircraft upwind into a fixture for secure parking and servicing. After servicing, the aircraft lifts-off into tethered hover, and power margin for climb is assessed. If the aircraft is judged to have sufficient power safely to proceed, then the interlocking hooks are disengaged, leaving the aircraft to climb away in free flight.

4. 发明申请

US20170334581A1 Aerial Vehicle Refueling System incorporating a Universal Refueling Interface 审中-公开
公开(公告)号：US20170334581A1
公开(公告)日：2017-11-23
申请号：US15160071
申请日：2016-05-20
申请人： Michael White , Miles Austin
发明人： Michael White , Miles Austin
IPC分类号： B64F1/36 , B60L11/18 , H01M2/10 , B64F1/04 , B64F1/28 , B64C39/02
CPC分类号： B64F1/36 , B60L53/80 , B60L2200/10 , B64C39/024 , B64C2201/024 , B64C2201/027 , B64C2201/04 , B64C2201/042 , B64D37/30 , B64D47/00 , B64D2221/00 , B64F1/007 , B64F1/04 , B64F1/22 , B64F1/28 , H01M2/1083 , H01M2220/20 , H01M2250/20 , Y02T10/7005 , Y02T10/7072 , Y02T90/124 , Y02T90/14 , Y02T90/32
摘要： A system for autonomously replacing batteries or fuel cells on small aerial vehicles such as Unmanned Aerial Vehicles (UAVs) or radio-controlled aircraft (RC) is described. At the core of this system is a “universal battery receptacle” that can be added to a variety of unmanned aircraft platforms and provides a uniform interface for battery or fuel cell replacement in the form of a commensurately designed “universal fuel cell”.Additionally, a system is described through which an aerial vehicle can be accepted, manipulated, the batteries replaced, and the vehicle re-launched, all without direct user intervention. Such systems can be deployed across a geographic area to increase the range of aerial vehicles without extensive ground support personnel.

5. 发明授权

US09811796B2 Method for delivering a shipment by an unmanned transport device 有权
公开(公告)号：US09811796B2
公开(公告)日：2017-11-07
申请号：US15303352
申请日：2015-04-01
申请人： Deutsche Post AG
发明人： Thomas Ogilvie , Matthäus Pruski , Ramin Benz
IPC分类号： B64C39/02 , G06Q10/08 , A47G29/14 , G07F17/12 , G06Q50/28 , B64F1/04 , B65G67/00 , B60L11/18 , B64D1/22 , B64D45/08
CPC分类号： G06Q10/083 , A47G29/14 , A47G29/141 , A47G2029/145 , A47G2029/149 , B60L11/1809 , B64C39/024 , B64C2201/042 , B64C2201/128 , B64D1/22 , B64D45/08 , B64F1/04 , B65G67/00 , G06Q10/0832 , G06Q50/28 , G07F17/12
摘要： The invention relates to a method for delivering a shipment by an unmanned transport device to a receiving container for said shipment, the method comprising the following and additional steps: moving the unmanned transport device into a destination area associated with the receiving container, on the basis of geographical co-ordinates; once the unmanned transport device has reached the destination area, pairing of the transport device with the receiving container and exchanging electronic authorization information between the receiving container and the unmanned transport device.

6. 发明授权

US09776713B2 Off-board gyrocopter take-off systems and associated methods 有权
公开(公告)号：US09776713B2
公开(公告)日：2017-10-03
申请号：US14602190
申请日：2015-01-21
申请人： Jaime G. Sada-Salinas
发明人： Jaime G. Sada-Salinas
IPC分类号： B64C27/02 , B64F1/04
CPC分类号： B64C27/025 , B64C27/02 , B64F1/04 , B64F1/16
摘要： Off-board gyrocopter take-off systems and associated methods are disclosed. A representative method includes restraining a gyrocopter from vertical and lateral movement, pre-rotating a fixed-pitch lift rotor of the gyrocopter via a power source located off the gyrocopter, and releasing the gyrocopter for vertical movement to allow the gyrocopter to lift under a force provided by the lift rotor. Optionally, the method can further include interrupting or reducing power from the power source to the gyrocopter as a way to release the gyrocopter for vertical movement.

7. 发明授权

US09771866B2 High temperature composite inlet 有权
公开(公告)号：US09771866B2
公开(公告)日：2017-09-26
申请号：US14609254
申请日：2015-01-29
申请人： ROHR, Inc.
发明人： Vijay V. Pujar , Teresa Kruckenberg
IPC分类号： B64D29/00 , F02C7/047 , B64D15/12 , B64B1/40 , B64F1/04 , B64D33/02
CPC分类号： F02C7/047 , B64B1/40 , B64D15/12 , B64D29/00 , B64D2033/0233 , B64F1/04 , F05D2300/434 , F05D2300/5024 , F05D2300/603 , F05D2300/6033 , F05D2300/611 , Y02T50/672
摘要： An inlet for an aircraft nacelle may comprise a nanoreinforced polyimide composite lip skin. The nanomaterials may increase thermal conductivity and decrease microcracking in the lip skin. A lip skin for an inlet with an electric heater may comprise a surface layer, an outer composite skin, an electric heater, an inner composite skin, and a thermal barrier coating. A lip skin for an inlet with a pneumatic deicing system may comprise a surface layer, a composite skin, and a thermal barrier coating.

8. 发明授权

US09580188B2 Airport capacity from takeoff assist 有权
标题翻译：机场容量起飞辅助
公开(公告)号：US09580188B2
公开(公告)日：2017-02-28
申请号：US14855712
申请日：2015-09-16
申请人： Exhaustless, Inc.
发明人： Steven P. Endres
IPC分类号： B64C25/50 , B64F1/04 , B64F1/00 , B64F1/06 , B64F1/10
CPC分类号： B64F1/06 , B64F1/002 , B64F1/04 , B64F1/10
摘要： Systems and methods for ground-based aircraft thrust systems are provided. A sled can be adapted to support at least wings and a fuselage of an aircraft. A guideway can be configured to receive the sled and move the sled along the guideway for assisted takeoff of the aircraft. A magnetic propulsion system can be configured to levitate the sled and propel the sled along the guideway independent of thrust provided by the aircraft.
摘要翻译：提供了基于地面的飞机推力系统的系统和方法。雪橇可以适应于至少支撑飞机的机翼和机身。导轨可以被配置成接收滑雪板并沿着导轨移动滑板以辅助起飞飞机。磁力推进系统可以被配置成悬挂滑雪板并且沿着导轨推动雪橇，而与飞行器提供的推力无关。

9. 发明申请

US20170039510A1 METHOD FOR DELIVERING A SHIPMENT BY AN UNMANNED TRANSPORT DEVICE 有权
标题翻译：通过不必要的运输设备运送装运的方法
公开(公告)号：US20170039510A1
公开(公告)日：2017-02-09
申请号：US15303352
申请日：2015-04-01
申请人： Deutsche Post AG
发明人： Thomas Ogilvie , Matthäus Pruski , Ramin Benz
IPC分类号： G06Q10/08 , A47G29/14 , B64D45/08 , B60L11/18 , B64C39/02 , B64D1/22
CPC分类号： G06Q10/083 , A47G29/14 , A47G29/141 , A47G2029/145 , A47G2029/149 , B60L11/1809 , B64C39/024 , B64C2201/042 , B64C2201/128 , B64D1/22 , B64D45/08 , B64F1/04 , B65G67/00 , G06Q10/0832 , G06Q50/28 , G07F17/12
摘要： The invention relates to a method for delivering a shipment by an unmanned transport device to a receiving container for said shipment, the method comprising the following and additional steps: moving the unmanned transport device into a destination area associated with the receiving container, on the basis of geographical co-ordinates; once the unmanned transport device has reached the destination area, pairing of the transport device with the receiving container and exchanging electronic authorisation information between the receiving container and the unmanned transport device.
摘要翻译：本发明涉及一种用于将无人运输装置的货物运送到用于所述装运的接收容器的方法，该方法包括以下步骤：将无人运输装置移动到与接收容器相关联的目的地区域中的地理坐标; 一旦无人运输装置到达目的地区域，将运输装置与接收容器配对，并在接收容器和无人运输装置之间交换电子授权信息。

10. 发明申请

US20160221689A1 Line Intersect Vehicle Launch and Recovery 审中-公开
标题翻译：线相交车辆启动和恢复
公开(公告)号：US20160221689A1
公开(公告)日：2016-08-04
申请号：US14952949
申请日：2015-11-26
申请人： Christopher Ralph Tridico
发明人： Christopher Ralph Tridico
IPC分类号： B64F1/04 , B64D3/00 , B64D47/02 , B64F1/08
CPC分类号： B64F1/04 , B64C39/024 , B64C2201/082 , B64C2201/182 , B64C2201/206 , B64D5/00
摘要： The present invention is a system which facilitates the launch and recovery of an aircraft or other vehicle by another vehicle or site. This system includes cables, wires or other “lines” that are connected to both the subject vehicle and the launch and recovery platform and facilities to extend, retract and position these lines. When the relative motion of the subject vehicle and launch and recovery platform causes the lines to intersect, the lines are connected to each other by means of a hook, carabiner or similar attachment device resulting in the effective capture of the subject vehicle. One or both of the lines may then be retracted resulting in the recovery of the subject vehicle. Launch is accomplished by extending one or both of the lines and subsequently releasing the attachment device.
摘要翻译：本发明是一种便于由其他车辆或场所发射和回收飞机或其他车辆的系统。该系统包括连接到主车辆和发射和恢复平台的电缆，电线或其他“线路”以及用于延伸，缩回和定位这些线路的设备。当主体车辆和发射和恢复平台的相对运动导致线路相交时，线路通过钩，卡扣或相似的附接装置彼此连接，从而有效地捕获本车辆。然后可以将一条或两条线缩回，导致本车辆的恢复。发射通过延伸一条或两条线并随后释放附着装置来实现。

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