专利快速检索-快速检索全球专利，免费商用专利数据库-IPRDB

1. 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。

2. 发明申请

US20060108475A1 Apparatus and method for controlling aerial refueling hose 审中-公开
标题翻译：用于控制空中加油软管的装置和方法
公开(公告)号：US20060108475A1
公开(公告)日：2006-05-25
申请号：US10521687
申请日：2002-08-03
申请人： Asher Bartov
发明人： Asher Bartov
IPC分类号： B64D39/00
CPC分类号： B64D39/02
摘要： The invention is a variable displacement hydraulic motor-controlled hose reel drive system (10) for aerial refueling of a receiver aircraft from a tanker aircraft. The system includes a variable displacement hydraulic motor (26), a tachometer (34), position sensor (34), a reaction torque sensor (36) and a microprocessor (29) which, depending upon data received from the system's position and reaction torque sensors, sends appropriate signals to the motor. The invention is also a method for deploying a hose and drogue so as to reduce the likelihood that the hose (22) would go into oscillation after initial engagement of a receiver aircraft's probe with the drogue (24). In an embodiment of the invention, the hose (22) is retracted prior to hook up of the probe and drogue (24), and the force required to retract the hose (22) is recorded. After initial engagement of the probe with the drogue (24), the hose (22) is retracted until the force required to retract the hose rises to about the same force previously recorded.
摘要翻译：本发明是用于从油船飞行器对接收机飞行器进行空中加油的可变排量液压马达控制软管卷盘驱动系统（10）。该系统包括可变排量液压马达（26），转速计（34），位置传感器（34），反作用转矩传感器（36）和微处理器（29），其根据从系统的位置接收的数据和反作用力矩传感器向电机发送适当的信号。本发明还是一种用于部署软管和锥套的方法，以便降低在接收器飞机的探头与锥套（24）初始接合之后软管（22）将进入振荡的可能性。在本发明的一个实施例中，软管（22）在钩接探头和锥套（24）之前缩回，并且记录缩回软管（22）所需的力。在探头与锥套（24）初始接合之后，软管（22）缩回直到使软管缩回所需的力上升到与之前记录的大致相同的力。

3. 发明授权

US06454212B1 Aerial refueling hose reel drive controlled by a variable displacement hydraulic motor and method for controlling aerial refueling hose reel 有权
标题翻译：由可变排量液压马达控制的空中加油软管卷盘驱动器和用于控制空中加油软管卷盘的方法
公开(公告)号：US06454212B1
公开(公告)日：2002-09-24
申请号：US09643804
申请日：2000-08-22
申请人： Asher Bartov
发明人： Asher Bartov
IPC分类号： B64D3700
CPC分类号： B64D39/02
摘要： The invention is a variable displacement hydraulic motor-controlled hose reel drive system. The system includes a variable displacement hydraulic motor, having an electro-hydraulic control valve; a tachometer/position sensor; a reaction torque sensor; and a microprocessor which, depending upon data received from the system's position and reaction torque sensors, sends appropriate signals to the electro-hydraulic control valve.
摘要翻译：本发明是一种可变排量液压马达控制软管卷盘驱动系统。该系统包括具有电动液压控制阀的可变排量液压马达，转速计/位置传感器; 一个反作用转矩传感器; 以及根据从系统的位置和反作用转矩传感器接收的数据，将适当的信号发送到电动液压控制阀的微处理器。

4. 发明授权

US06786455B1 Method for engaging a probe and drogue for aerial refueling 有权
标题翻译：用于接合探头和冷气用于空中加油的方法
公开(公告)号：US06786455B1
公开(公告)日：2004-09-07
申请号：US10236830
申请日：2002-09-05
申请人： Asher Bartov
发明人： Asher Bartov
IPC分类号： B64D3700
CPC分类号： B64D39/00
摘要： The invention is a method for engaging the drogue of a hose and drogue refueling system with the probe of a receiver aircraft for aerial refueling from a tanker aircraft. The tanker aircraft and receiver aircraft approximately match speed and direction, with the probe of the receiver aircraft maintained at approximately a first predetermined distance behind the tanker aircraft. The hose and drogue are extended rearward from the tanker aircraft so that the drogue is positioned at a second predetermined distance (shorter than the first predetermined distance) behind the tanker aircraft. The drogue and probe are orthogonally aligned with each other, and the hose is extended back beyond the second predetermined distance so that the drogue moves away from the tanker aircraft to and into engagement with the probe. The force of the air stream on the drogue is sufficient to provide for secure engagement of the drogue with the probe.
摘要翻译：本发明是一种用于将软管和锥形加油系统的锥套与用于从油船飞行器进行空中加油的接收器飞机的探头接合的方法。油轮飞机和接收机大致匹配速度和方向，接收机的探头保持在油轮飞机后面约第一预定距离。软管和锥套从油罐飞机向后延伸，使得锥套位于油罐飞机后面的第二预定距离（比第一预定距离短）。锥套和探头彼此正交对准，并且软管延伸回超过第二预定距离，使得锥套从油罐飞机移开并与探头接合。气流在锥套上的力足以提供锥套与探头的牢固接合。

5. 发明申请

US20100072320A1 PROGRAMMABLE AERIAL REFUELING RANGE 审中-公开
标题翻译：可编程的空气净化范围
公开(公告)号：US20100072320A1
公开(公告)日：2010-03-25
申请号：US12237305
申请日：2008-09-24
申请人： ASHER BARTOV
发明人： ASHER BARTOV
IPC分类号： B64D39/00
CPC分类号： B64D39/02
摘要： In an aerial refueling system for refueling a receiver aircraft in flight from a tanker aircraft, wherein the refueling system includes a hose reel rotatably coupled to the tanker aircraft's fuselage, a hose wound around the reel, said hose having an outlet end, and a drogue affixed to said outlet end, a hose reel drive system including a microprocessor electrically coupled to the reel; and a machine-readable program embodied in the microprocessor for directing operation of the system, the machine-readable program including instructions for establishing a refueling range. A method including receiving information of a receiver aircraft for aerial refueling; and establishing, in flight, a refueling range for an aerial refueling system coupled to a tanker aircraft based on the received information.
摘要翻译：在空中加油系统中，用于对来自油轮飞机的飞行中的接收机进行加油，其中加油系统包括可旋转地联接到油罐飞机的机身的软管卷筒，围绕卷轴缠绕的软管，所述软管具有出口端和锥形固定到所述出口端，软管卷轴驱动系统，包括电耦合到所述卷轴的微处理器; 以及体现在微处理器中以引导系统操作的机器可读程序，该机器可读程序包括用于建立加油范围的指令。一种方法，包括接收用于空中加油的接收机飞机的信息; 并根据接收到的信息在飞行中建立与油轮飞机相连的空中加油系统的加油范围。

6. 发明授权

US06866228B2 Aerial refueling hose reel drive controlled by a variable displacement hydraulic motor and method for controlling aerial refueling hose reel 有权
标题翻译：由可变排量液压马达控制的空中加油软管卷盘驱动器和用于控制空中加油软管卷盘的方法
公开(公告)号：US06866228B2
公开(公告)日：2005-03-15
申请号：US10199134
申请日：2002-07-22
申请人： Asher Bartov
发明人： Asher Bartov
IPC分类号： B64D39/02 , B64D37/00
CPC分类号： B64D39/02
摘要： The invention is a variable displacement hydraulic motor-controlled hose reel drive system for aerial refueling of a receiver aircraft from a tanker aircraft. The system includes a variable displacement hydraulic motor, a tachometer/position sensor, a reaction torque sensor and a microprocessor which, depending upon data received from the system's position and reaction torque sensors, sends appropriate signals to the motor. The invention is also a method for deploying a hose and drogue so as to reduce the likelihood that the hose would go into oscillation after initial engagement of a receiver aircraft's probe with the drogue. In an embodiment of the invention, the hose is retracted prior to hook up of the probe and drogue, and the force required to retract the hose is recorded. After initial engagement of the probe with the drogue, the hose is retracted until the force required to retract the hose rises to about the same force previously recorded.
摘要翻译：本发明是用于从油船飞机对接收机飞行器进行空中加油的可变排量液压马达控制软管卷盘驱动系统。该系统包括可变排量液压马达，转速计/位置传感器，反作用转矩传感器和微处理器，根据从系统位置接收的数据和反作用转矩传感器，向马达发送合适的信号。本发明还是一种用于部署软管和锥套的方法，以便降低在接收器飞机的探头与锥套最初接合之后软管将进入振荡的可能性。在本发明的一个实施例中，软管在钩住探头和脱水之前缩回，并且记录缩回软管所需的力。在探头与锥套初始接合后，软管将缩回，直到缩回软管所需的力上升至与之前记录的大致相同的力。

7. 发明申请

US20140060017A1 MULTI-ORIFICE BYPASS FOR A HYDRAULIC MOTOR ASSEMBLY 有权
标题翻译：液压马达组件的多级旁路
公开(公告)号：US20140060017A1
公开(公告)日：2014-03-06
申请号：US13597006
申请日：2012-08-28
申请人： Asher Bartov
发明人： Asher Bartov
IPC分类号： F15B13/042
CPC分类号： B64D39/02 , F15B11/08 , F15B2211/40507 , F15B2211/40515 , F15B2211/415 , F15B2211/426 , F15B2211/7058 , F15B2211/763 , F16H61/4052
摘要： Apparatuses and systems that use a variable displacement motor-pump (VDMP) to control the position of a hose of an aerial refueling system are disclosed. At VDMP displacements greater than required to hold a position of the hose, the VDMP operates in a motor mode to retract the hose. For lesser VDMP displacements, the VDMP operates in a pump mode to control extension of the hose. In accordance with some embodiments, a dual orifice conveys hydraulic fluid at varying rates depending upon the VDMP operational mode.
摘要翻译：公开了使用可变排量电动泵（VDMP）来控制空中加油系统的软管的位置的装置和系统。在大于保持软管位置所需的VDMP位移时，VDMP以电机模式运行，以缩回软管。对于较小的VDMP位移，VDMP以泵模式运行，以控制软管的延伸。根据一些实施例，双孔口根据VDMP操作模式以不同的速率输送液压流体。

8. 发明授权

US09102415B2 Multi-orifice bypass for a hydraulic motor assembly 有权
标题翻译：用于液压马达组件的多孔旁路
公开(公告)号：US09102415B2
公开(公告)日：2015-08-11
申请号：US13597006
申请日：2012-08-28
申请人： Asher Bartov
发明人： Asher Bartov
IPC分类号： F16D31/02 , B64D39/02 , F16H61/4052 , F15B11/08
CPC分类号： B64D39/02 , F15B11/08 , F15B2211/40507 , F15B2211/40515 , F15B2211/415 , F15B2211/426 , F15B2211/7058 , F15B2211/763 , F16H61/4052
摘要： Apparatuses and systems that use a variable displacement motor-pump (VDMP) to control the position of a hose of an aerial refueling system are disclosed. At VDMP displacements greater than required to hold a position of the hose, the VDMP operates in a motor mode to retract the hose. For lesser VDMP displacements, the VDMP operates in a pump mode to control extension of the hose. In accordance with some embodiments, a dual orifice conveys hydraulic fluid at varying rates depending upon the VDMP operational mode.
摘要翻译：公开了使用可变排量电动泵（VDMP）来控制空中加油系统的软管的位置的装置和系统。在大于保持软管位置所需的VDMP位移时，VDMP以电机模式运行，以缩回软管。对于较小的VDMP位移，VDMP以泵模式运行，以控制软管的延伸。根据一些实施例，双孔口根据VDMP操作模式以不同的速率输送液压流体。

9. 发明申请

US20140064998A1 Hydraulic Motor Assembly For An Aerial Refueling System 有权
标题翻译：液压马达组件用于空中加油系统
公开(公告)号：US20140064998A1
公开(公告)日：2014-03-06
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： B64D39/02
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。

你已经成功收藏专利！

检索式保存成功!

IPRDB

热门服务

关于我们

友情链接

联系方式