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1. 发明申请

US20220348346A1 SYSTEM AND METHOD FOR RECONNECTABLY COUPLING AN AFT VEHICLE TO A FORWARD VEHICLE IN FLIGHT 有权
公开(公告)号：US20220348346A1
公开(公告)日：2022-11-03
申请号：US17725889
申请日：2022-04-21
申请人： Sky Launch Corporation
发明人： Gerald D. Budd , Thomas Milton McNicholas , Angela Monheim
IPC分类号： B64D39/06 , B64D39/02 , B64D3/00
摘要： Disclosed are systems and methods for reconnectably coupling an aft vehicle to a forward vehicle in flight. A docking structure is affixed to the forward vehicle. A coupler has a line connection portion, a probe receiver port, and a plurality of aerodynamic controls. The probe receiving port receives and releasably retains a probe portion of the aft vehicle. A tow line has a proximal end, a distal end, and a line extension length. The proximal end may be attached to the tow actuation element. The distal end is connectable to the coupler. The tow actuation element is configured to adjust the line extension length. The aerodynamic control elements are configured to adjust lateral and vertical positioning of the coupler with respect to the probe portion when the system is in flight. Movement of the coupler is restrained with respect to the docking structure when docked thereto.

2. 发明申请

US20220212810A1 AIR TO AIR ACTIVE REFUELLING SYSTEM AND METHOD FOR GENERATING AERODYNAMIC RADIAL LOADS AT A HOSE-END 有权
公开(公告)号：US20220212810A1
公开(公告)日：2022-07-07
申请号：US17512250
申请日：2021-10-27
申请人： AIRBUS DEFENCE AND SPACE, S.A.U.
发明人： Gonzalo MARTÍN GÓMEZ , Samuel DE LA FUENTE LÓPEZ
IPC分类号： B64D39/02 , B64D39/06
摘要： An air to air refueling system that monitors and adapts the movement at an end of an air to air refueling hose of a tanker aircraft to counteract undesirable movements at the end of the hose though generating aerodynamic loads in the end of the hose. The system includes grid fins at the end of the hose that are automatically rotated to counteract the undesirable movements.

3. 发明授权

US11027838B2 In flight charging system 有权
公开(公告)号：US11027838B2
公开(公告)日：2021-06-08
申请号：US15972129
申请日：2018-05-05
申请人： Karman, Inc.
发明人： Joshua Clemente , George O'Neal , Chiranjeev Kalra
IPC分类号： B64C37/02 , B64D39/02 , B64D27/24 , B64C39/02
摘要： An in-flight charging system includes a first electric air vehicle, a second electric air vehicle, an elevated power supply system (EPSS) and a flexible tension member coupled to the first electric air vehicle and coupled to the second electric air vehicle. The flexible tension member provides power from the second electric vehicle to the first electric vehicle. The EPSS further includes one or more current carrying conductors, wherein the second electric air vehicle travels along the one or more current carrying conductors and receives power transferred from the one or more current carrying conductors.

4. 发明申请

US20210139161A1 SYSTEMS AND METHODS FOR AERIAL AIRCRAFT RESUPPLY 有权
公开(公告)号：US20210139161A1
公开(公告)日：2021-05-13
申请号：US17095634
申请日：2020-11-11
申请人： Bell Textron Inc.
发明人： Jeffrey Paul Nissen , Troy Cyril Schank , Brent Chadwick Ross , Steven Ray Ivans
IPC分类号： B64D39/04 , B64D39/02 , B64D7/00
摘要： An aerial resupply system (ARS) including a supply aircraft. The supply aircraft includes at least one of supply fuel, an ordinance, and data. The supply aircraft also includes a retractable boom system (RBS) configured for selective stowage within a fuselage of the supply aircraft and configured to supply at least one of supply fuel, the ordinance, and data to a location external to the fuselage.

5. 发明授权

US10784761B2 Coil actuator 有权
公开(公告)号：US10784761B2
公开(公告)日：2020-09-22
申请号：US16439646
申请日：2019-06-12
申请人： Skydio, Inc.
发明人： Daniel Thomas Adams , Patrick Allen Lowe , Benjamin Scott Thompson , Abraham Galton Bachrach , Adam Parker Bry
IPC分类号： H02K41/03 , G03B15/00 , B64D47/08 , B64D39/02 , G03B17/56 , H02K41/035 , B64C39/02
摘要： An actuator is introduced that utilizes the forces that result from placing a current carrying coil in a magnetic field to rotate a connected object about at least one axis. In some embodiments, the introduced coil actuator includes a coil of conductor coupled to an arm or other type of structural element that extends radially from an axis of rotation. The introduced coil actuator can be utilized to provide motion control in a variety of different applications such as gimbal mechanisms. In some embodiments, the introduced coil actuator can be implemented in a gimbal mechanism for adjusting an orientation of a device such as a camera relative to a connected platform such as the body of an aerial vehicle.

6. 发明申请

US20200239154A1 EN ROUTE FLUID TRANSMITTING APPARATUS 审中-公开
公开(公告)号：US20200239154A1
公开(公告)日：2020-07-30
申请号：US16686615
申请日：2019-11-18
申请人： AIRBUS HELICOPTERS DEUTSCHLAND GMBH
发明人： Yann LE CADET , Samuel PELLERIN
IPC分类号： B64D39/02 , B64D39/04 , B64C39/02 , B64D47/00
摘要： An en route fluid transmitting apparatus for transmitting a fluid from a transmitting entity to a probe of a receiving vehicle includes a funnel, a hose and a thrust producing device. Thrust producing device includes a main body that is rigidly attached to the funnel, and at least two rotors that are connected to the main body for producing thrust. The thrust producing device is adapted to move the funnel freely in any direction to a predetermined position relative to the probe where the funnel engages with the probe.

7. 发明授权

US10343788B2 Telescoping refueling boom control systems and methods 有权
公开(公告)号：US10343788B2
公开(公告)日：2019-07-09
申请号：US15716151
申请日：2017-09-26
申请人： The Boeing Company
发明人： Christopher M. Jacobus , Blain A. Lawson , Ian A. Halley , Jung Soon Jang , Kimberly A. Hinson
IPC分类号： G05D3/12 , B64D39/02 , B64D39/04 , G05B11/01 , G05D13/02
摘要： Systems and methods according to one or more embodiments are provided for rate and position control modes used in the operations of a telescoping refueling boom system. In one example, a system includes a telescoping tube and an actuator coupled to the telescoping tube and configured to extend and/or retract the telescoping tube. A processor is coupled to the actuator and configured to select a telescoping tube rate control mode and/or a telescoping tube position control mode based on a telescoping tube current position error, a telescoping tube current rate of movement, and a value of a telescoping tube rate command.

8. 发明授权

US09102414B2 Hydraulic motor assembly for an aerial refueling system 有权
标题翻译：用于空中加油系统的液压马达组件
公开(公告)号：US09102414B2
公开(公告)日：2015-08-11
申请号：US13597002
申请日：2012-08-28
申请人： Asher Bartov , Charles Kubilos
发明人： Asher Bartov , Charles Kubilos
IPC分类号： F16D31/02 , B64D39/02 , F16H61/4043 , F15B21/04 , F15B13/02
CPC分类号： B64D39/02 , F15B13/024 , F15B21/042 , F15B2211/20553 , F15B2211/20569 , F15B2211/40546 , F15B2211/50518 , F15B2211/528 , F15B2211/61 , F15B2211/62 , F15B2211/6303 , F15B2211/6652 , F15B2211/6656 , F16H61/4043 , Y10T137/86493
摘要： Apparatuses and systems that use a variable displacement motor-pump (VDMP) to control the position and speed of a hose for an aerial refueling system are disclosed. At displacements greater than required to hold a position of the hose, the VDMP operates in a motor mode to retract the hose. For lesser displacements, the VDMP operates in a pump mode to control extension of the hose. In accordance with some embodiments, a pump-motor relief valve operates to throttle hydraulic fluid flow from the VDMP and to control mixing of hydraulic fluid flowing from the VDMP with system hydraulic fluid.
摘要翻译：公开了使用可变排量马达泵（VDMP）来控制空中加油系统的软管的位置和速度的装置和系统。在大于保持软管位置所需位移的情况下，VDMP以马达模式运行以缩回软管。对于较小的位移，VDMP以泵模式运行，以控制软管的延伸。根据一些实施例，泵电动机安全阀操作以节流来自VDMP的液压流体流动并且控制从VDMP流动的液压流体与系统液压流体的混合。

9. 发明申请

US20120298805A1 Aerial Refueling Drogue Deployment System 有权
标题翻译：空中加油Drogue部署系统
公开(公告)号：US20120298805A1
公开(公告)日：2012-11-29
申请号：US13117586
申请日：2011-05-27
申请人： Forrest Eugene Richardson
发明人： Forrest Eugene Richardson
IPC分类号： B64D39/00 , B64D39/02
CPC分类号： B64D39/02 , Y10T74/20468 , Y10T74/20474 , Y10T74/2048 , Y10T74/20486
摘要： Systems and methods provide for a drogue deployment system that may be removably attached to a non-tanker aircraft to modify the aircraft for providing aerial refueling operations. Aspects of the disclosure provide a drum unit that may be secured in a cargo area of the non-tanker aircraft and connected to the fuel system of the aircraft. A drogue deployment unit may be removably attached to an external surface of the aircraft fuselage and includes a drogue extension tube that may be selectively deployed outward from the fuselage to provide separation between a refueling drogue and the aircraft. The drogue and corresponding refueling hose may be deployed from a drogue container attached to the drogue extension tube and extended rearward for providing fuel to a receiving aircraft.
摘要翻译：系统和方法提供了一种锥形部署系统，其可以可移除地附接到非油轮飞行器以修改飞行器以提供空中加油操作。本公开的方面提供了可以固定在非油罐飞机的货物区域中并连接到飞行器的燃料系统的滚筒单元。锥形展开单元可以可移除地附接到飞行器机身的外表面，并且包括可从机身向外选择性地展开以提供加油锥套与飞行器之间的分离的锥形延伸管。锥套和相应的加油软管可以从附接到锥形延伸管的锥形容器展开并向后延伸以向接收飞机提供燃料。

10. 发明授权

US07185854B2 In-flight refueling system and method for extending and retracting an in-flight refueling device 失效
标题翻译：飞行中加油系统和用于扩展和缩回飞行加油装置的方法
公开(公告)号：US07185854B2
公开(公告)日：2007-03-06
申请号：US10872225
申请日：2004-06-18
申请人： German Von Thal , Harry W. Slusher , Stephen M. Stecko
发明人： German Von Thal , Harry W. Slusher , Stephen M. Stecko
IPC分类号： B64D39/02
CPC分类号： B64D39/00 , B64D39/02
摘要： An in-flight refueling system and method are provided to extend and retract an in-flight refueling device between a stowed position and an extended position relative to a tanker aircraft. The system and method of the present invention provide an induction device configured to extend and retract the in-flight refueling device such that the in-flight refueling system requires less maintenance and may be packaged in a compact, low-profile arrangement so that the in-flight refueling system may be carried by a variety of tanker aircraft in a variety of different configurations.
摘要翻译：提供了一种飞行中加油系统和方法，以在收起位置和相对于油罐飞行器的延伸位置之间延伸和缩回飞行中加油装置。本发明的系统和方法提供了一种引导装置，其被配置为延伸和缩回飞行中加油装置，使得飞行中加油系统需要较少的维护，并且可以以紧凑，低调的布置包装，使得在 - 多种不同配置的各种油轮飞机可以装载轻型加油系统。

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