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公开(公告)号：US20230202670A1
公开(公告)日：2023-06-29
申请号：US18175472
申请日：2023-02-27
CPC分类号： B64D39/06 , B67D7/04 , B67D7/40 , B64C39/024 , B64D5/00 , B64D1/06 , B64D1/22 , B64D1/16 , B64U30/10
摘要： A refueling system has a vehicle having a fuel tank connected to a deployable fuel hose, an end effector having controlled flight, the fuel hose connected at an end away from the first vehicle, through the end effector to a fuel connector under the end effector, a second vehicle having a fuel tank coupled through a pumping apparatus to a fueling port on an acquisition apparatus adapted to acquire the end effector and connect the fueling port and the fuel connector of the end effector, and control circuitry enabling controlled flight of the end effector, wherein the end effector is controlled to be acquired by the acquisition apparatus to couple the fuel connector with the fueling port and fuel is provided from the fuel tank of one of the vehicles to the fuel tank of the other of the vehicles through the pumping apparatus.
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公开(公告)号：US20190210738A1
公开(公告)日：2019-07-11
申请号：US15864883
申请日：2018-01-08
申请人： THE BOEING COMPANY
CPC分类号： B64D39/06 , B64C1/1407
摘要： A device includes a drive link coupled to an actuator and a first link coupled to the drive link, the first link and the drive link forming a first pivot point. The device also includes a second link coupled to the first link and a support shaft coupled to second link. The second link and the first link form a second pivot point and the second link is configured to rotate about the support shaft. The device further includes a third link coupled to the second link and includes a fourth link coupled to third link and coupled to a door assembly. The third link and the second link form a third pivot point, and the fourth link and the third link form a fourth pivot point. When the door assembly is in an open position, the support shaft, the third pivot point, and the fourth pivot point are aligned.
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公开(公告)号：US20190092487A1
公开(公告)日：2019-03-28
申请号：US16199589
申请日：2018-11-26
CPC分类号： B64D39/04 , B63B25/08 , B63B27/24 , B63B27/34 , B63G8/001 , B64C39/022 , 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.
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公开(公告)号：US20180346141A1
公开(公告)日：2018-12-06
申请号：US15994032
申请日：2018-05-31
申请人： EMBRAER S.A.
发明人： Paulo Henrique HASMANN , Marcos VINICIUS , Gabriel Kendjy KOIKE , Cristian Escobar SANTIAGO , Rodrigo Pinto Moreira PIEDRAS , Reinaldo Pinto Dias JUNIOR
CPC分类号： B64D39/00 , B64C1/1415 , B64D39/06
摘要： Cargo aircraft having a cargo ramp and cargo door oppositely hinged relative to one another to allow access to the aircraft's cargo space may be provided with a flying boom mast that is physically mounted at the aft portion of the fuselage so as to configure such cargo aircraft for aerial refueling operations. The flying boom mast may therefore be operably associated with the aft portion of the fuselage and moveable between a stowed and deployed conditions relative to the aft portion of the fuselage, while a fuel supply line fluid-interconnects the flying boom mast with an on-board fuel supply of the aircraft so as to allow aerial refueling of a receiver aircraft when the flying boom mast is in the deployed condition thereof.
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公开(公告)号：US09969502B2
公开(公告)日：2018-05-15
申请号：US14640652
申请日：2015-03-06
摘要： A method for in-flight refueling of a receiver aircraft from a tanker aircraft including: measuring continuously a tension at an end of a hose extending from the tanker aircraft towards the receiver aircraft, and using the measured tension to control a torque applied to a drum device deploying the hose from the tanker aircraft such that the tension at the end of the hose conforms to target tensions during each phase of the refueling operation.
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公开(公告)号：US20170341769A1
公开(公告)日：2017-11-30
申请号：US15606201
申请日：2017-05-26
申请人： Neoex Systems, Inc.
CPC分类号： B64D39/06 , B64C39/024 , B64C2201/063 , B64C2201/16 , B64C2201/18 , B64D37/14 , B64D2041/005 , B64F1/28 , F17C5/007 , F17C5/02 , F17C2205/0355 , F17C2205/037 , F17C2221/012 , F17C2223/0161 , F17C2223/033 , F17C2225/0161 , F17C2225/033 , F17C2227/0107 , F17C2227/0135 , F17C2227/044 , F17C2260/032 , F17C2265/065 , F17C2270/0189
摘要： A system and method for the transfer of cryogenic fluid fuel includes a nozzle positionable with respect to fuel tank inlet, e.g., of an unmanned aerial vehicle (UAV), a seal to seal the area where the nozzle and inlet are connected, a collapsible and expandable bellows providing an isolation volume where the fluid is transferred from the nozzle into the inlet; a vacuum is provided in the volume to avoid accumulation of fuel or other species in the volume.
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公开(公告)号：US20170073080A1
公开(公告)日：2017-03-16
申请号：US14855148
申请日：2015-09-15
申请人： THE BOEING COMPANY
发明人： TRUMAN HUGHES , GLENN E. STINSON
CPC分类号： B64D39/06 , B65H75/425 , B65H75/486 , B65H2701/34 , H01B11/1033 , H01R13/60 , H01R24/28
摘要： A boom nozzle assembly for use with an aerial refueling boom on an aerial refueling aircraft where a shielded wiring cable from the aerial refueling boom is connected to an articulated boom nozzle through an electrical connection on the wear ring of the articulated boom nozzle and then routed to a solenoid and other devices of the articulated boom nozzle without passing through the universal joint area of the articulated boom nozzle. The boom nozzle assembly may include a torsion cable reel that keeps the shielded wiring cable in tension as the articulated boom nozzle changes its position relative to the boom nozzle assembly. The torsion cable reel may be positioned within a cable reel housing attached at the aft end of the aerial refueling boom.
摘要翻译： 一种用于空中加油飞机上的空中加油吊杆的吊杆喷嘴组件，其中来自空中加油臂的屏蔽布线电缆通过铰接式喷杆喷嘴的耐磨环上的电连接连接到铰接式喷嘴喷嘴，然后被路由到 铰链式喷嘴喷嘴的螺线管和其他装置，而不穿过铰接式喷杆喷嘴的万向接头区域。 动臂喷嘴组件可以包括扭转电缆卷轴，当扭转臂喷嘴改变其相对于悬臂喷嘴组件的位置时，扭转电缆卷轴保持屏蔽布线电缆的张力。 扭转电缆卷轴可以位于附接在空中加油站的后端的电缆卷轴壳体内。
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公开(公告)号：US20160318621A1
公开(公告)日：2016-11-03
申请号：US14698515
申请日：2015-04-28
申请人： JON F. GARRUBA
发明人： JON F. GARRUBA
摘要： An in-flight refueling probe includes a first tubular member secured to an aircraft and a second tubular member having a releasable connection with the first tubular member such that the second tubular member detaches from the first tubular member in response to a predetermined force applied to the connection. A nozzle secured to the second tubular member can be coupled to a receptacle of a fuel dispensing aircraft. A tethering member is connected to the first tubular member and one of the second tubular member and the nozzle. The tethering member remains intact to connect the detached second tubular member to the first tubular member when a first tensile force is applied to the tethering member. The tethering member ruptures to disconnect the detached second tubular member from the first tubular member when a second tensile force greater than the first tensile force is applied to the tethering member.
摘要翻译： 飞行中加油探头包括固定到飞行器的第一管状构件和具有与第一管状构件可释放连接的第二管状构件，使得第二管状构件响应于施加到第一管状构件的预定力而与第一管状构件分离 连接。 固定到第二管状构件的喷嘴可以联接到燃料分配飞行器的容器。 连接构件连接到第一管状构件和第二管状构件和喷嘴中的一个。 当第一张力施加到束缚构件时，束缚构件保持完整以将分离的第二管状构件连接到第一管状构件。 当大于第一张力的第二拉力施加到栓系构件时，系链构件破裂以将分离的第二管状构件与第一管状构件断开。
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9.发明申请CONTACT DETECTING SYSTEM AND METHOD FOR AIR REFUELING TANKER EQUIPPED WITH AIR REFUELING BOOM SYSTEM 审中-公开空气补给装置系统和空气净化装置的检测系统及方法公开(公告)号：US20160311554A1
公开(公告)日：2016-10-27
申请号：US15138724
申请日：2016-04-26
IPC分类号： B64D39/04
摘要： A contact detecting system for an air refueling tanker equipped with an air refueling boom, the system comprising a boom refueling nozzle comprising a valve to allow the exit of fuel, a latch to engage the refueling nozzle, a first contact detecting mechanism configured to transmit a signal when the refueling nozzle is in a contact position, a second contact detecting mechanism configured to detect the position of the latch and to transmit a signal when the latch is latched, and a third contact detecting mechanism configured to detect the position of the valve and to transmit a signal when the valve is open. The system further comprises a computing device configured to receive the signals from the first, second and third contact detecting mechanisms and to provide an output signal of the contact status of the refueling nozzle.
摘要翻译： 一种用于装备有空气加油斗的空中加油车的接触检测系统，该系统包括一个起重臂加油喷嘴，该起重臂加油喷嘴包括一个允许燃料排出的阀，一个与加油喷嘴接合的闩锁;一个第一接触检测机构， 信号，当加油喷嘴处于接触位置时，第二接触检测机构构造成检测闩锁的位置并且当闩锁被锁定时传递信号;以及第三接触检测机构，其构造成检测阀的位置，以及 当阀门打开时传送信号。 该系统还包括被配置为从第一，第二和第三接触检测机构接收信号并且提供加油喷嘴的接触状态的输出信号的计算装置。
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公开(公告)号：US09469410B2
公开(公告)日：2016-10-18
申请号：US13188716
申请日：2011-07-22
申请人： Steven C. Peake
发明人： Steven C. Peake
CPC分类号： B64D45/00 , B64D39/02 , B64D39/06 , B64D47/02 , B64D2203/00
摘要： An aerial refueling system utilizes the full drogue-probe coupling event as a control parameter for hose control. A variety of different types of signal sending and signal receiving devices may be used to indicate a coupling event between the drogue and probe. A positive coupling signal may serve to trigger a hose reel actuator to take up slack in the hose 16.
摘要翻译： 空中加油系统利用完全锥形探头耦合事件作为软管控制的控制参数。 可以使用各种不同类型的信号发送和信号接收装置来指示锥形和探针之间的耦合事件。 正耦合信号可以用于触发软管卷筒致动器以吸收软管16中的松弛。
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