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1. 发明申请

US20230028104A1 REFUELING TOOL AND SYSTEM INCORPORATING THE REFUELING 有权
公开(公告)号：US20230028104A1
公开(公告)日：2023-01-26
申请号：US17785571
申请日：2020-12-21
申请人： MACDONALD, DETTWILER AND ASSOCIATES INC.
发明人： ANDREW PAUL TURNER , TEJ SACHDEV , ANDREW SCOTT OGILVIE , NATALIE PANEK , STEVE FISHER , MICHAEL HONEYBROWN , DREW ALEXANDER GRANDY , VICTOR NIFO
IPC分类号： B64G1/64 , B64D39/04 , B64G1/10 , B64G1/40
摘要： The present disclosure relates to a robotically controlled satellite refueling tool and associated robotically controlled support and site preparation tools which facilitates on-orbit refueling by teleoperation of fill/drain valves of various designs and dimensions on satellites not originally prepared for on-orbit servicing, through the installation of quick connect safety valves, using vision-based feedback as well as feedback from sensors embedded in the refueling tool to operate a suite of adaptable and adjustable mechanisms. The refueling tool has an open architecture to allow a refueling tool vision system to see the fill/drain valve and the section of the refueling tool that is engaged with the fill/drain valve. The support tools include a blanket cutter tool, a blanket handler tool, a wire cutter tool, a gripper tool, and the site preparation tools include a B-nut removal tool and a crush seal removal tool. Each of these tools includes a common base structure which is interfaced to the end effector of the robotic arm for transmitting rotation and torque to the various tools.

2. 发明授权

US11167860B2 Devices, systems and methods for refueling air vehicles 有权
公开(公告)号：US11167860B2
公开(公告)日：2021-11-09
申请号：US16537074
申请日：2019-08-09
申请人： ISRAEL AEROSPACE INDUSTRIES LTD.
发明人： Ohad Rix , Joshua Gur , Michael Litvak , Elie Koskas
IPC分类号： B64D39/06 , B64D39/00 , B64D39/04 , B64D3/00 , G05D1/00 , G05D1/10
摘要： A variety of refueling devices, systems and methods are disclosed for use in in-flight refueling. In one example one such device is towed by a tanker aircraft via a fuel hose at least during in-flight refueling, and has a boom member with a boom axis. The boom member enables fuel to be transferred from the fuel hose to a receiver aircraft along the boom axis during in-flight refueling. The device maintains a desired non-zero angular disposition between the boom axis and a forward direction at least when the refueling device is towed by the tanker aircraft in the forward direction via the fuel hose.

3. 发明授权

US10654584B2 Refueling system and method 有权
公开(公告)号：US10654584B2
公开(公告)日：2020-05-19
申请号：US15681336
申请日：2017-08-18
申请人： Marinus Ben Bosma
发明人： Marinus Ben Bosma
IPC分类号： B64D39/06 , B64D39/04 , B64C39/02
摘要： An apparatus and method for refueling an aircraft comprising a hose guide. The hose guide includes a framework having wings and remotely-adjustable control surfaces interacting with air through which the hose guide moves. An attachment interface, attaching the hose guide to a fuel hose extended from a tanker aircraft, at a distal end away from the tanker aircraft, and a control system adjusting the adjustable control surfaces. Wherein the hose guide is towed as a glider by the tanker aircraft, and adjustment of the control surfaces adjusts three-dimensional position of the end of the fuel hose at the hose guide relative to position of the tanker aircraft.

4. 发明授权

US10577119B2 System and apparatus for refueling aircraft from a watercraft 有权
公开(公告)号：US10577119B2
公开(公告)日：2020-03-03
申请号：US16199589
申请日：2018-11-26
申请人： Konstantinos Margetis
发明人： Konstantinos Margetis
IPC分类号： B64D39/04 , B64D39/06 , B63B27/34 , B63G8/00 , B63B27/24 , B64D39/00 , B63B25/08 , B64C39/02
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.

5. 发明申请

US20190382126A1 DEVICES, SYSTEMS AND METHODS FOR REFUELING AIR VEHICLES 审中-公开
公开(公告)号：US20190382126A1
公开(公告)日：2019-12-19
申请号：US16537074
申请日：2019-08-09
申请人： ISRAEL AEROSPACE INDUSTRIES LTD.
发明人： Ohad RIX , Joshua GUR , Michael LITVAK , Elie KOSKAS
IPC分类号： B64D39/06 , G05D1/10 , G05D1/00 , B64D3/00 , B64D39/04 , B64D39/00
摘要： A variety of refueling devices, systems and methods are disclosed for use in in-flight refueling. In one example one such device is towed by a tanker aircraft via a fuel hose at least during in-flight refueling, and has a boom member with a boom axis. The boom member enables fuel to be transferred from the fuel hose to a receiver aircraft along the boom axis during in-flight refueling. The device maintains a desired non-zero angular disposition between the boom axis and a forward direction at least when the refueling device is towed by the tanker aircraft in the forward direction via the fuel hose.

6. 发明申请

US20190092487A1 SYSTEM AND APPARATUS FOR REFUELING AIRCRAFT FROM A WATERCRAFT 审中-公开
公开(公告)号：US20190092487A1
公开(公告)日：2019-03-28
申请号：US16199589
申请日：2018-11-26
申请人： Konstantinos Margetis
发明人： Konstantinos Margetis
IPC分类号： B64D39/04 , B64D39/06 , B63G8/00 , B64D39/00
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.

7. 发明申请

US20180346141A1 FLYING BOOM MAST FOR MULTI-PURPOSE AERIAL REFUELING AIRCRAFT 审中-公开
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
IPC分类号： B64D39/02 , B64D39/04 , B64D39/06
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.

8. 发明申请

US20160318621A1 DUAL MODE FRANGIBLE REFUELING NOZZLE 有权
标题翻译：双模式可燃回弹喷嘴
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
IPC分类号： B64D39/06 , B64D39/04
CPC分类号： B64D39/06 , B64D39/04
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。

9. 发明申请

US20160311554A1 CONTACT DETECTING SYSTEM AND METHOD FOR AIR REFUELING TANKER EQUIPPED WITH AIR REFUELING BOOM SYSTEM 审中-公开
标题翻译：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
申请人： Airbus Defence and Space S.A.
发明人： Jose Luis Marcos Montes , Francisco Jose Lagares Carrasco , Guillaume Angibaud
IPC分类号： B64D39/04
CPC分类号： B64D39/04 , B64D39/06
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。

10. 发明授权

US09315277B2 System and method for transferring fuel in flight from a tanker aircraft to multiple receiver aircraft 有权
标题翻译：将飞行中的燃料从油罐机转移到多台接收机上的系统和方法
公开(公告)号：US09315277B2
公开(公告)日：2016-04-19
申请号：US13972707
申请日：2013-08-21
申请人： Singapore Technologies Aerospace Ltd.
发明人： Chi Hui Frederic Foo , Siew Liong Tay , Kim Chiew Tay , Zheng Liang Lu
IPC分类号： B64D39/00 , B64D39/04 , B64D39/02
CPC分类号： B64D39/04 , B64D39/02
摘要： A trailing boom system for aerial refueling and a method for aerial refueling of multiple receiver aircraft. The trailing boom system for aerial refueling includes a parent pod capable of being connected to a wing of an aircraft, and a detachable pod releasable from the parent pod, the detachable pod including an extendible boom for refueling aircraft in flight.
摘要翻译：用于空中加油的牵引臂系统和用于多个接收机的空中加油的方法。用于空中加油的牵引臂系统包括能够连接到飞行器的翼的母体荚和可从主荚释放的可拆卸的荚，该可拆卸的荚包括用于在飞行中加油飞行器的可伸缩起重臂。

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