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    • 2. 发明授权
    • Aerial refueling boom nozzle with integral pressure regulation
    • 具有整体压力调节的空中加油臂喷嘴
    • US08485474B2
    • 2013-07-16
    • US12872696
    • 2010-08-31
    • Lance A. CutlerMark A. Shelly
    • Lance A. CutlerMark A. Shelly
    • B64D39/00
    • B64D39/04B64D39/06
    • Apparatus and methods described herein provide for a boom/receiver-type aerial refueling system having a pressure regulator integrated into the system at the tanker boom nozzle. During refueling operations, pressure of the fuel at the interface between the nozzle at the distal end of the boom assembly and the fuel receptacle of the receiving aircraft is maintained by an integrated pressure regulator integrated into the nozzle or located inline of the fuel flow between the boom assembly and the nozzle. The integrated pressure regulator maintains the pressure of the fuel at the nozzle within a defined range regardless of the elevation azimuth of the boom assembly, the extended length of the telescoping extension, the temperature of the outside air or surfaces of the boom, and other factors that may affect the flow of fuel through the boom.
    • 本文所述的装置和方法提供了一种具有在油罐吊杆喷嘴处集成到系统中的压力调节器的起重臂/接收器型空中加油系统。 在加油操作期间,在悬臂组件的远端处的喷嘴与接收飞机的燃料接收器之间的界面处的燃料的压力由集成在喷嘴中的集成的压力调节器维持,或者位于燃料流的位置之间 起重臂总成和喷嘴。 集成式压力调节器将喷嘴处的燃料压力保持在规定范围内,而不管吊臂组件的仰角方向,伸缩长度,伸缩长度,外部空气或悬臂表面的温度等因素 这可能会影响通过吊臂的燃料流。
    • 3. 发明申请
    • Aerial Refueling Boom Nozzle With Integral Pressure Regulation
    • 具有整体压力调节的空中加油臂喷嘴
    • US20120049004A1
    • 2012-03-01
    • US12872696
    • 2010-08-31
    • Lance A. CutlerMark A. Shelly
    • Lance A. CutlerMark A. Shelly
    • B64D39/00
    • B64D39/04B64D39/06
    • Apparatus and methods described herein provide for a boom/receiver-type aerial refueling system having a pressure regulator integrated into the system at the tanker boom nozzle. During refueling operations, pressure of the fuel at the interface between the nozzle at the distal end of the boom assembly and the fuel receptacle of the receiving aircraft is maintained by an integrated pressure regulator integrated into the nozzle or located inline of the fuel flow between the boom assembly and the nozzle. The integrated pressure regulator maintains the pressure of the fuel at the nozzle within a defined range regardless of the elevation azimuth of the boom assembly, the extended length of the telescoping extension, the temperature of the outside air or surfaces of the boom, and other factors that may affect the flow of fuel through the boom.
    • 本文所述的装置和方法提供了一种具有在油罐吊杆喷嘴处集成到系统中的压力调节器的起重臂/接收器型空中加油系统。 在加油操作期间,在悬臂组件的远端处的喷嘴与接收飞机的燃料接收器之间的界面处的燃料的压力由集成在喷嘴中的集成的压力调节器维持,或者位于燃料流的位置之间 起重臂总成和喷嘴。 集成的压力调节器将喷嘴处的燃料压力保持在规定的范围内,而不管吊臂组件的仰角方向,伸缩长度,伸缩长度,外部空气或悬臂表面的温度等因素 这可能会影响通过吊臂的燃料流。
    • 4. 发明授权
    • Braking apparatus and method for an aerial refueling boom system
    • 空中加油臂系统的制动装置和方法
    • US09102412B2
    • 2015-08-11
    • US12855284
    • 2010-08-12
    • Lance A. CutlerForrest Richardson
    • Lance A. CutlerForrest Richardson
    • B64D39/02B64D39/04
    • B64D39/02B64D39/04
    • 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.
    • 提供了一种空中加油臂系统的制动装置,以减少可能性或防止异常起重臂伸展的可能性。 制动装置包括滑轮,电缆缠绕在该滑轮上。 滑轮构造成可操作地安装到动臂系统的第一管并且由于电缆连接到第二管而响应于第二管相对于第一管的移动而旋转。 制动装置还包括具有打开和致动位置的锁,例如制动器或销锁。 在致动位置,防止滑轮的旋转和第二管相对于第一管的运动。 锁被配置为通过另外控制第一和第二管的相对位置的致动源的性能的降低来致动。
    • 5. 发明授权
    • Wireless refueling boom
    • 无线加油繁荣
    • US08905355B2
    • 2014-12-09
    • US13238800
    • 2011-09-21
    • Forrest E. RichardsonCarl W. BeckLance A. CutlerMark A. Shelly
    • Forrest E. RichardsonCarl W. BeckLance A. CutlerMark A. Shelly
    • B64D39/00B64D39/04
    • B64D39/04B64D39/00
    • 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.
    • 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。
    • 6. 发明申请
    • BRAKING APPARATUS AND METHOD FOR AN AERIAL REFUELING BOOM SYSTEM
    • 制动装置和方法
    • US20120037757A1
    • 2012-02-16
    • US12855284
    • 2010-08-12
    • Lance A. CutlerForrest Richardson
    • Lance A. CutlerForrest Richardson
    • B64D39/00
    • B64D39/02B64D39/04
    • 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.
    • 提供了一种空中加油臂系统的制动装置,以减少可能性或防止异常起重臂伸展的可能性。 制动装置包括滑轮,电缆缠绕在该滑轮上。 滑轮构造成可操作地安装到动臂系统的第一管,并且由于电缆与第二管的连接而响应于第二管相对于第一管的移动而旋转。 制动装置还包括具有打开和致动位置的锁,例如制动器或销锁。 在致动位置,防止滑轮的旋转和第二管相对于第一管的运动。 锁被配置为通过另外控制第一和第二管的相对位置的致动源的性能的降低来致动。
    • 7. 发明申请
    • WIRELESS REFUELING BOOM
    • 无线电话
    • US20130068889A1
    • 2013-03-21
    • US13238800
    • 2011-09-21
    • Forrest E. RichardsonCarl W. BeckLance A. CutlerMark A. Shelly
    • Forrest E. RichardsonCarl W. BeckLance A. CutlerMark A. Shelly
    • B64D39/00
    • B64D39/04B64D39/00
    • 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.
    • 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。