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1. 发明申请

US20180265212A1 DROGUE CONTROL SYSTEMS AND APPARATUS 审中-公开
公开(公告)号：US20180265212A1
公开(公告)日：2018-09-20
申请号：US15461685
申请日：2017-03-17
申请人： Analytical Mechanics Associates, Inc.
发明人： Daniel Allan Pruzan , Daniel Joseph Lesieutre
IPC分类号： B64D39/02 , B64D39/04
CPC分类号： B64D39/02 , B64D39/04 , B64D39/06
摘要： Systems, apparatus, and methods may control movement of an object through a fluid. The systems, apparatus, and methods may utilize a rotatable control unit including a pair of fins to generate a control force at least partially perpendicular to a direction of travel of the object through the fluid. One fin may be configured to generate a different amount of rolling moment than the other fin to provide rotational acceleration and energy production.

2. 发明申请

US20180044033A1 SYSTEM AND APPARATUS FOR REFUELING AIRCRAFT FROM A WATERCRAFT 审中-公开
公开(公告)号：US20180044033A1
公开(公告)日：2018-02-15
申请号：US15723571
申请日：2017-10-03
申请人： Konstantinos Margetis
发明人： Konstantinos Margetis
IPC分类号： B64D39/04 , B63B27/24 , B63B27/34 , B64D39/06
CPC分类号： B64D39/04 , B63B25/08 , B63B27/24 , B63B27/34 , B63G8/001 , B64D39/00 , B64D39/06
摘要： The invention is a watercraft to aircraft refueling system (“WARS”). A WARS is a refueling system based from a watercraft, such as a surface ship or submarine. A WARS would typically include an elevation apparatus to lift a refueling hose above the water. The elevation apparatus can compose a lifting or swiveling mechanism. In some embodiments both a lifting and swiveling mechanism is used. The WARS lifts the refueling hose above the water, allowing an aircraft to engage with the WARS. The refueling hose may also include a telescoping mechanism or a rotor apparatus or a pressurized water nozzle system to elevate the refueling hose and assist in engaging a WARS with an aircraft.

3. 发明授权

US09266620B2 Braking apparatus and method for an aerial refueling boom system 有权
公开(公告)号：US09266620B2
公开(公告)日：2016-02-23
申请号：US14678022
申请日：2015-04-03
申请人： The Boeing Company
发明人： Lance A. Cutler , Forrest Richardson
IPC分类号： B64D39/02 , B64D39/04
CPC分类号： B64D39/02 , B64D39/04
摘要： A braking apparatus of an aerial refueling boom system is provided to reduce the likelihood of or to prevent anomalous boom extension. The braking apparatus includes a pulley about which a cable wraps. The pulley is configured to be operably mounted to a first tube of the boom system and to rotate in response to movement of a second tube relative to the first tube as a result of the connection of the cable to the second tube. The braking apparatus also includes a lock, such as a brake or a pin lock, having open and actuated positions. In the actuated position, rotation of the pulley and movement of the second tube relative to the first tube are prevented. The lock is configured to be actuated by a reduction in performance of an actuation source that otherwise controls the relative positions of the first and second tubes.

4. 发明申请

US20150041591A1 MULTIPURPOSE FLYING BOOM 有权
标题翻译：多用途飞行器
公开(公告)号：US20150041591A1
公开(公告)日：2015-02-12
申请号：US13960614
申请日：2013-08-06
申请人： THE BOEING COMPANY
发明人： Aaron J. Kutzmann
IPC分类号： B64D39/00
CPC分类号： B64D39/00 , B64D39/04 , B64D39/06 , Y10T29/49826
摘要： Embodiments provide a flying boom that is capable of refueling both receptacle-equipped aircraft and probe-equipped aircraft. In one embodiment, a flying boom includes a refueling tube at an end of the flying boom that is adapted to extend from the end of the flying boom to refuel receptacle-equipped aircraft. The flying boom further includes a retractable hose and drogue assembly at the end of the flying boom that is adapted to extend from the end of the flying boom to refuel probe-equipped aircraft.
摘要翻译：实施例提供了一种飞行吊杆，其能够对装有插座的飞机和装有探针的飞机进行加油。在一个实施例中，飞行吊杆包括在飞行吊杆的端部处的加油管，其适于从飞行吊架的端部延伸至配备有加油装置的飞机。飞行吊架还包括在悬臂的末端处的可伸缩软管和锥形组件，其适于从飞行架的末端延伸到加油探针配备的飞机。

5. 发明授权

US08950708B2 Air-to-air refueling drogue assemblies 有权
标题翻译：空对空加油锥套
公开(公告)号：US08950708B2
公开(公告)日：2015-02-10
申请号：US13368431
申请日：2012-02-08
申请人： Christopher Mouskis , Georgios Filippos Papaioannou , Adrian Bedford , Richard John Foxwell , James Kemmitt
发明人： Christopher Mouskis , Georgios Filippos Papaioannou , Adrian Bedford , Richard John Foxwell , James Kemmitt
IPC分类号： B64D39/00 , B64D39/06 , B64D39/04 , B64F1/28
CPC分类号： B64D39/06 , B64D39/00 , B64D39/04 , B64F1/28
摘要： An air to air refuelling drogue assembly includes a reception coupling and a drogue canopy connected to the reception coupling by connection means which hold the canopy in an operative, drag producing, position relative to the reception coupling during refuelling. The drogue assembly is arranged to controllably fail so as to reduce the drag load produced by the drogue when a drag load on the canopy exceeds a predetermined threshold.
摘要翻译：空气对空气加油锥套组件包括接收联接器和通过连接装置连接到接收联接器的锥套罩，所述连接装置在加油期间相对于接收耦合器将冠盖保持在可操作的，阻力产生位置。锥形组件布置成可控制地失效，以便当在顶篷上的拖曳负载超过预定阈值时减小由锥套产生的牵引载荷。

6. 发明授权

US08596580B1 Advanced performance refueling boom 有权
标题翻译：高级性能加油繁荣
公开(公告)号：US08596580B1
公开(公告)日：2013-12-03
申请号：US12891394
申请日：2010-09-27
申请人： Sergey D. Barmichev , Harry Wilbert Slusher
发明人： Sergey D. Barmichev , Harry Wilbert Slusher
IPC分类号： B64D39/00
CPC分类号： B64D39/04
摘要： Apparatuses, systems, and methods described herein provide for a refueling boom having vertical control surfaces extending primarily downward below the horizontal control surfaces out of the auxiliary power unit (APU) exhaust and airframe-induced turbulent flow fields, while reducing the torque moments applied to the boom beam and increasing control authority. According to one aspect of the disclosure provided herein, a refueling boom includes a boom beam, at least one horizontal control surface, and a pair of vertical control surfaces. The vertical control surfaces are positioned on opposing ends of the horizontal control surfaces and each include an upper portion and a longer lower portion projecting downward below the horizontal control surface. Aspects further improve the aerodynamic characteristics of the boom beam, reducing the drag associated with the refueling boom.
摘要翻译：本文所述的装置，系统和方法提供了一种加油悬臂，其具有垂直控制表面，其垂直控制表面主要向下延伸到辅助动力单元（APU）排气和机体引起的湍流流场外的水平控制表面之下，同时减小施加到繁荣梁和增加的控制权。根据本文提供的本公开的一个方面，加油吊杆包括吊臂梁，至少一个水平控制表面和一对垂直控制表面。垂直控制表面位于水平控制表面的相对端上，并且每个包括在水平控制表面下方向下突出的上部和较长的下部。方面进一步改善了起重臂梁的空气动力特性，减少了与加油臂相关联的阻力。

7. 发明申请

US20130168498A1 SYSTEMS AND METHODS FOR AIR VEHICLES 有权
标题翻译：空中车辆的系统和方法
公开(公告)号：US20130168498A1
公开(公告)日：2013-07-04
申请号：US13467682
申请日：2012-05-09
申请人： Ohad RIX
发明人： Ohad RIX
IPC分类号： B64D39/00 , G06F19/00
CPC分类号： B64D39/06 , B64D3/00 , B64D39/00 , B64D39/04 , G05D1/0094 , G05D1/101
摘要： A method for controlling in-flight refueling of a receiver aircraft having a fuel receptacle, comprising: automatically steering a refueling device to an engagement enabling position, including: repeatedly determining a spatial disposition of the refueling device with respect to the receiver aircraft, the refueling device being capable of engaging and refueling the receiver aircraft via a boom member, when the device arrives to the engagement enabling position at which the boom member is in a predetermined spaced and spatial relationship with respect to the fuel receptacle of the receiver aircraft; repeatedly calculating steering commands based at least on the repeatedly determined spatial dispositions and characteristics of a spatial control system of the refueling device; sending the steering commands to the spatial control system; whereby at the engagement enabling position, the boom member of the refueling device is capable of engaging with the fuel receptacle to enable refueling of the receiver aircraft.
摘要翻译：一种用于控制具有燃料容器的接收器飞行器的飞行中加油的方法，包括：自动地将加油装置转向到接合使能位置，包括：重复地确定加油装置相对于接收器飞机的空间布置，加油装置能够通过悬臂构件接合和加油接收器飞机，当装置到达接合使能位置时，悬臂构件相对于接收器飞机的燃料容器处于预定的间隔和空间关系; 至少基于重新确定的加油装置的空间控制系统的空间配置和特性重复计算转向命令; 向空间控制系统发送转向命令; 由此在接合使能位置，加油装置的悬臂构件能够与燃料容器接合以使得接收器飞机能够加油。

8. 发明申请

US20130068889A1 WIRELESS REFUELING BOOM 有权
标题翻译：无线电话
公开(公告)号：US20130068889A1
公开(公告)日：2013-03-21
申请号：US13238800
申请日：2011-09-21
申请人： Forrest E. Richardson , Carl W. Beck , Lance A. Cutler , Mark A. Shelly
发明人： Forrest E. Richardson , Carl W. Beck , Lance A. Cutler , Mark A. Shelly
IPC分类号： B64D39/00
CPC分类号： B64D39/04 , B64D39/00
摘要： A refueling boom is described. The refueling boom includes a non-telescoping portion configured to be coupled to a fuel tanker vehicle and a telescoping portion that is extendable and retractable relative to the non-telescoping portion. The telescoping portion includes a fuel nozzle. The refueling boom also includes a wireless communication system operable to enable wireless communication between a first location of the telescoping portion to a second location of the non-telescoping portion. The refueling boom also includes a control unit coupled to the telescoping portion. The control unit is operable to send first information to the fuel tanker vehicle via the wireless communication system and to receive second information from the fuel tanker vehicle via the wireless communication system.
摘要翻译：描述了加油繁荣。加油吊杆包括非伸缩部分，该非伸缩部分构造成联接到燃料油罐车辆和可相对于非伸缩部分可伸缩的伸缩部分。伸缩部分包括燃料喷嘴。加油吊杆还包括无线通信系统，其可操作以实现伸缩部分的第一位置与非伸缩部分的第二位置之间的无线通信。加油斗还包括耦合到伸缩部分的控制单元。控制单元可操作以经由无线通信系统向燃料油罐车辆发送第一信息，并且经由无线通信系统从燃料油罐车辆接收第二信息。

9. 发明申请

US20120199696A1 AIR-TO-AIR REFUELING DROGUE ASSEMBLIES 有权
标题翻译：空对空清洁饮料组件
公开(公告)号：US20120199696A1
公开(公告)日：2012-08-09
申请号：US13368431
申请日：2012-02-08
申请人： Christopher MOUSKIS , Georgios Filippos PAPAIOANNOU , Adrian BEDFORD , Richard John FOXWELL , James KEMMITT
发明人： Christopher MOUSKIS , Georgios Filippos PAPAIOANNOU , Adrian BEDFORD , Richard John FOXWELL , James KEMMITT
IPC分类号： B64D39/00
CPC分类号： B64D39/06 , B64D39/00 , B64D39/04 , B64F1/28
摘要： An air to air refuelling drogue assembly includes a reception coupling and a drogue canopy connected to the reception coupling by connection means which hold the canopy in an operative, drag producing, position relative to the reception coupling during refuelling. The drogue assembly is arranged to controllably fail so as to reduce the drag load produced by the drogue when a drag load on the canopy exceeds a predetermined threshold.
摘要翻译：空气对空气加油锥套组件包括接收联接器和通过连接装置连接到接收联接器的锥套罩，所述连接装置在加油期间相对于接收耦合器将冠盖保持在可操作的，阻力产生位置。锥形组件布置成可控制地失效，以便当在顶篷上的拖曳负载超过预定阈值时减小由锥套产生的牵引载荷。

10. 发明授权

US07954764B2 Smart boom tip assembly 有权
标题翻译：智能动臂头组件
公开(公告)号：US07954764B2
公开(公告)日：2011-06-07
申请号：US11542631
申请日：2006-10-03
申请人： Mariano Ortega De Miguel , Antonio San Jose Orche
发明人： Mariano Ortega De Miguel , Antonio San Jose Orche
IPC分类号： B64D39/06
CPC分类号： B64D39/04 , B64D39/00
摘要： A refueling apparatus for interconnecting a tanker aircraft (11) with a receiver aircraft in flight comprising a boom (21) joined to said tanker aircraft (11) by means of a mechanical articulation (41) having control means including a central computer station, an inner fuel conduit, a refueling nozzle (27) at its distal end and, and a smart tip assembly comprising a first module (83) having load sensing means, a second module (85) having load alleviation means and a third module (87), joined to the nozzle (27), having a mechanical fuse (99) for allowing the safe separation of tanker and receiver aircraft in the event of overloads. The invention also comprises a method of load alleviation for minimizing the loads on the boom (21).
摘要翻译：一种用于将油船飞机（11）与飞行中的接收机飞行器相互连接的加油装置，包括通过具有控制装置的机械铰接（41）连接到所述油罐飞机（11）的起重臂（21），所述控制装置包括中央计算机站，内部燃料管道，其远端处的加油喷嘴（27）和智能尖端组件，其包括具有负载感测装置的第一模块（83），具有负载减轻装置的第二模块（85）和第三模块（87）连接到喷嘴（27），其具有用于在过载的情况下允许油罐和接收器飞机的安全分离的机械保险丝（99）。本发明还包括一种负载减轻的方法，以使起重臂（21）上的负载最小化。

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