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公开(公告)号：US10179648B2
公开(公告)日：2019-01-15
申请号：US15176250
申请日：2016-06-08
摘要： An airborne drone launch and recovery apparatus for selectively launching drones located on the underside of a carrier aircraft or recovering drones following flight of the drones, the airborne launch and recovery apparatus has an extensible stinger slidable along the length of a stinger sheath between a retracted position proximal the rear portion of the carrier aircraft and an extended position in front of the carrier aircraft, and a catcher shuttle carried on the forward part of the stinger for extending into the non-turbulent air in front of the carrier aircraft when the stinger is in the extended position. The carrier shuttle includes a launch/recovery assembly for selectively either having a locked condition for the recovery guide of a drone prior to the positioning of the catcher shuttle in a selected for the launch of the drone, and having an open condition for receiving the recovery guide of a drone at the termination of the flight of the drone to terminate the flight.
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公开(公告)号：US20160355261A1
公开(公告)日：2016-12-08
申请号：US15176250
申请日：2016-06-08
CPC分类号： B64D5/00 , B64C39/024 , B64C2201/082 , B64C2201/084 , B64C2201/206
摘要： An airborne drone launch and recovery apparatus for selectively launching drones located on the underside of a carrier aircraft or recovering drones following flight of the drones, the airborne launch and recovery apparatus has an extensible stinger slidable along the length of a stinger sheath between a retracted position proximal the rear portion of the carrier aircraft and an extended position in front of the carrier aircraft, and a catcher shuttle carried on the forward part of the stinger for extending into the non-turbulent air in front of the carrier aircraft when the stinger is in the extended position. The carrier shuttle includes a launch/recovery assembly for selectively either having a locked condition for the recovery guide of a drone prior to the positioning of the catcher shuttle in a selected for the launch of the drone, and having an open condition for receiving the recovery guide of a drone at the termination of the flight of the drone to terminate the flight.
摘要翻译： 一种空中无人机发射和恢复装置，用于选择性地发射位于载体飞行器的下侧上的无人机或在无人机的飞行之后恢复无人机，机载发射和恢复装置具有可伸长的刺针，沿着刺血刺鞘的长度在缩回位置 靠近载体飞行器的后部，并且在载体飞行器的前面延伸的位置，以及在托管架前部延伸到载体飞行器前方的非湍流空气中的捕手穿梭器，当托管架处于 延长的位置。 运输班车包括发射/恢复组件，用于选择性地具有用于无人机的恢复引导件的锁定状态，在捕集器穿梭机定位在被选择用于发射无人机之前，并且具有用于接收恢复的打开状态 在无人驾驶飞机终止时终止飞行的无人机指导。
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3.发明授权公开(公告)号：US10435274B2
公开(公告)日：2019-10-08
申请号：US15722105
申请日：2017-10-02
IPC分类号： B63C9/06 , B66B9/187 , B63B23/28 , B63B27/10 , B63B27/32 , B66C23/20 , F03D13/20 , B63C9/03 , E02B17/00
摘要： A container for maintenance capsule as a component of a maintenance system for an offshore wind turbine maintenance program. The container transports tools, parts and maintenance personnel to and from respective wind turbine towers. The container is seaworthy, watertight and floatable, and can be loaded on a maintenance vessel which carries the container to and from a wind turbine tower.
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公开(公告)号：US10443976B2
公开(公告)日：2019-10-15
申请号：US15627558
申请日：2017-06-20
摘要： A carriage for use in a rocket launch system for cooperating with an electromotive cableway traction drives conveyed beneath a two axis pivot anchored to the earth, elevated into a co-axial transfer tube leading to three primary tether cables whose weight is offset by balloons. The carriage has traction drives which grip cables from which they derive power and rotate to drive the carriage from the low altitude to the high altitude. The traction drives rotate in the opposite direction as the carriage descends the cable following the launch of a rocket under gravitational force. The kinetic energy of the traction drive is converted to electrical energy which is fed back to the cables during descent of the carriage.
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公开(公告)号：US20130007935A1
公开(公告)日：2013-01-10
申请号：US13577813
申请日：2011-02-10
CPC分类号： F41F3/06 , B64G1/005 , B64G6/00 , B64G2001/643 , F41F3/04
摘要： A rocket launch system (1) includes a tubular rocket launcher carriage (2) with electromotive cableway traction drives (26) conveyed beneath a two axis pivot (63) anchored to the earth, elevated into a co-axial transfer tube (124, 143) leading to three primary tether cables (27) whose weight is offset by balloons (164). The carriage is conveyed to a docking station (166) supported into the stratosphere by a pair of secondary cables (184) suspended under an attachment frame (162) for tensioning balloons. The carriage is engaged by a carriage end gripper (196) guided by two secondary and two tertiary cables (186) and lifted by a lower hoist (198) guided by the secondary cables. This lower hoist is supported by an upper hoist (168) suspended from the tensioning balloons attachment frame. The carriage, which engages a lift ring (183) guided by two secondary cables, is elevated further, rotated as desired, with rocket release and nearly recoilless ejection during freefall of the carriage, with engine ignition occurring at a safe distance.
摘要翻译： 火箭发射系统（1）包括管状火箭发射器托架（2），其具有在锚定到地球的两轴枢轴（63）下传送的电动索道牵引驱动器（26），升高到同轴传送管（124,143 ），其通过气球（164）偏移重量的三个主系绳电缆（27）。 托架通过悬挂在用于张紧气球的附接框架（162）下方的一对辅助电缆（184）被传送到支撑到平流层的坞站（166）。 滑架由两个辅助和两个第三电缆（186）引导的托架端部夹持器（196）接合，并由辅助电缆引导的下部起重机（198）提升。 该下部起重机由悬挂在张紧气球附件架上的上部起重机（168）支撑。 与两个辅助电缆引导的提升环（183）相接合的滑架进一步升高，随着火箭的释放而进行旋转，并在滑架自由下降期间几乎无后坐弹射，发动机点火发生在安全的距离。
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公开(公告)号：US20170284768A1
公开(公告)日：2017-10-05
申请号：US15627558
申请日：2017-06-20
CPC分类号： F41F3/06 , B64G1/005 , B64G6/00 , B64G2001/643 , F41F3/04
摘要： A carriage for use in a rocket launch system for cooperating with an electromotive cableway traction drives conveyed beneath a two axis pivot anchored to the earth, elevated into a co-axial transfer tube leading to three primary tether cables whose weight is offset by balloons. The carriage has traction drives which grip cables from which they derive power and rotate to drive the carriage from the low altitude to the high altitude. The traction drives rotate in the opposite direction as the carriage descends the cable following the launch of a rocket under gravitational force. The kinetic energy of the traction drive is converted to electrical energy which is fed back to the cables during descent of the carriage.
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7.发明申请公开(公告)号：US20180057321A1
公开(公告)日：2018-03-01
申请号：US15722105
申请日：2017-10-02
CPC分类号： B66B9/187 , B63B23/28 , B63B27/10 , B63B27/32 , B63C9/06 , B63C2009/035 , B66C23/207 , E02B17/0034 , E02B2017/0091 , F03D13/20
摘要： A container for maintenance capsule as a component of a maintenance system for an offshore wind turbine maintenance program. The container transports tools, parts and maintenance personnel to and from respective wind turbine towers. The container is seaworthy, watertight and floatable, and can be loaded on a maintenance vessel which carries the container to and from a wind turbine tower.
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公开(公告)号：US09821984B2
公开(公告)日：2017-11-21
申请号：US14775456
申请日：2014-03-12
IPC分类号： B66C23/18 , B63B35/44 , B66C11/12 , B66C9/08 , B63B27/10 , B63B27/32 , B66C23/20 , F03D13/20 , B63C9/03 , E02B17/00
CPC分类号： B66C23/18 , B63B27/10 , B63B27/32 , B63C2009/035 , B66C11/12 , B66C23/207 , E02B17/0034 , E02B2017/0091 , F03D13/20 , F03D80/50
摘要： An all-weather maintenance system for an offshore wind turbine maintenance program includes a maintenance capsule for transporting tools, parts and maintenance personnel to and from respective wind turbine towers, a maintenance vessel with a capsule support apparatus for transporting capsules supported on board by the capsule support apparatus to and from respective wind turbine towers, and a crane assembly with a trolley for transporting capsules between the respective wind turbine towers and the maintenance vessel.
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公开(公告)号：US09739567B2
公开(公告)日：2017-08-22
申请号：US13577813
申请日：2011-02-10
CPC分类号： F41F3/06 , B64G1/005 , B64G6/00 , B64G2001/643 , F41F3/04
摘要： A rocket launch system includes a tubular rocket launcher carriage with electromotive cableway traction drives conveyed beneath a two axis pivot anchored to the earth, elevated into a co-axial transfer tube leading to three primary tether cables whose weight is offset by balloons. The carriage is conveyed to a docking station supported into the stratosphere by a pair of secondary cables suspended under an attachment frame for tensioning balloons. The carriage is engaged by a carriage end gripper guided by two sets of secondary cables and two sets of tertiary cables and lifted by a lower hoist guided by the secondary cables to a lift ring assembly. This lower hoist is supported by an upper hoist suspended from the tensioning balloons attachment frame. The carriage, which engages a lift ring guided by two secondary cables, is elevated further, rotated in azimuth and elevation, and rocket ejection occurs from a launch tube during freefall of the carriage, with engine ignition occurring at a safe distance. The carriages have traction drives which grip cables from which they derive power and rotate to drive the carriage from the low altitude to the high altitude. The traction drives rotate in the opposite direction as the carriage descends the cable following the launch of a rocket under gravitational force. The kinetic energy of the traction drive is converted to electrical energy which is fed back to the cables during descent of the carriage.
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