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1. 发明授权

US3658101A Jet stream refueling system 失效
标题翻译：喷气式回流系统
公开(公告)号：US3658101A
公开(公告)日：1972-04-25
申请号：US3658101D
申请日：1968-05-29
申请人： US NAVY
发明人： WALDRON ALTON L
IPC分类号： B63B27/18 , B63B27/24 , B63B27/26 , B63B27/34
CPC分类号： B63B27/18 , B63B27/24 , B63B27/26 , Y10T137/5762
摘要： A system for refueling ships at sea or at dockside capable of delivering large quantities of oil at high speed by forcing the oil through a nozzle on a supply oiler in a coherent stream trajectory and receiving the oil in a receiver on a receiving ship at a distance of 60-200 feet. The nozzle on the sending ship may be trained and elevated to allow for the pitch and roll and relative position of the respective ships. An accordion bellows shroud is provided between the nozzle and the receiver to eliminate dileterious effects of wind and water on the trajectory stream.
摘要翻译：一种用于在海上或码头处加油的系统，其能够通过强制油通过供油机上的喷嘴以相干的流动轨迹高速输送大量油，并在接收船上的接收器中远距离接收油 60-200英尺发送船上的喷嘴可以被训练和升高以允许各个船舶的俯仰和滚动以及相对位置。在喷嘴和接收器之间提供了一个手风琴波纹管罩，以消除风和水对轨迹流的矛盾影响。

2. 发明授权

US07059564B2 Methods and apparatuses for capturing and recovering unmanned aircraft, including a cleat for capturing aircraft on a line 有权
标题翻译：用于捕获和恢复无人机的方法和装置，包括用于在线上捕获飞机的防滑板
公开(公告)号：US07059564B2
公开(公告)日：2006-06-13
申请号：US10758940
申请日：2004-01-16
申请人： Brian D. Dennis
发明人： Brian D. Dennis
IPC分类号： B64F1/02
CPC分类号： B64F1/06 , B63B27/26 , B64C39/024 , B64C2201/042 , B64C2201/044 , B64C2201/048 , B64C2201/084 , B64C2201/102 , B64C2201/146 , B64C2201/165 , B64C2201/182 , B64C2201/201 , B64F1/04
摘要： Methods and apparatuses for capturing and recovering unmanned aircraft and other flight devices or projectiles are described. In one embodiment, the aircraft can be captured by a recovery line in flight, a process that can be aided by a line capture device having a retainer with two portions spaced apart by a distance great enough to receive the recovery line, e.g., to capture the recovery line with increased security. The line capture device can be operatively mounted on a lifting surface of the aircraft.
摘要翻译：描述了用于捕获和恢复无人驾驶飞机和其他飞行装置或射弹的方法和装置。在一个实施例中，飞行器可以由飞行中的恢复线捕获，该过程可以由具有保持器的线捕获装置辅助，该保持器具有两个间隔开足够大的距离以接收恢复线，例如捕获恢复线增加了安全性。线捕获装置可以可操作地安装在飞行器的提升表面上。

3. 发明申请

US20040232282A1 Methods and apparatuses for capturing and recovering unmanned aircraft, including a cleat for capturing aircraft on a line 有权
标题翻译：用于捕获和恢复无人机的方法和装置，包括用于在线上捕获飞机的防滑板
公开(公告)号：US20040232282A1
公开(公告)日：2004-11-25
申请号：US10758940
申请日：2004-01-16
发明人： Brian D. Dennis
IPC分类号： B64C037/00
CPC分类号： B64F1/06 , B63B27/26 , B64C39/024 , B64C2201/042 , B64C2201/044 , B64C2201/048 , B64C2201/084 , B64C2201/102 , B64C2201/146 , B64C2201/165 , B64C2201/182 , B64C2201/201 , B64F1/04
摘要： Methods and apparatuses for capturing and recovering unmanned aircraft and other flight devices or projectiles are described. In one embodiment, the aircraft can be captured by a recovery line in flight, a process that can be aided by a line capture device having a retainer with two portions spaced apart by a distance great enough to receive the recovery line, e.g., to capture the recovery line with increased security. The line capture device can be operatively mounted on a lifting surface of the aircraft.
摘要翻译：描述了用于捕获和恢复无人驾驶飞机和其他飞行装置或射弹的方法和装置。在一个实施例中，飞行器可以由飞行中的恢复线捕获，该过程可以由具有保持器的线捕获装置辅助，该保持器具有两个间隔开足够大的距离以接收恢复线，例如捕获恢复线增加了安全性。线捕获装置可以可操作地安装在飞行器的提升表面上。

4. 发明授权

US3586065A Fluid transfer methods and systems 失效
标题翻译：流体传递方法和系统
公开(公告)号：US3586065A
公开(公告)日：1971-06-22
申请号：US3586065D
申请日：1967-12-26
申请人： BOWLES FLUIDICS CORP
发明人： BOWLES ROMALD E
IPC分类号： B63B27/24 , B63B27/26 , B63B27/34
CPC分类号： B63B27/26 , B63B27/24 , Y10T137/9682
摘要： Fluid is transferred from a supply station to one or more receiving stations separated from the supply station and in motion relative thereto, by directing a coherent, high-velocity, well-defined jet of the fluid from a discharge nozzle or nozzles, whose orientation may be varied according to the relative movement of the respective receiving station, toward and into a fluid catcher at the receiving station from which the received fluid may be distributed to appropriate storage tanks. The fluid jet is unconfined throughout its path from the supply station to the receiving station, passing directly through the open space between the stations, the maintenance of integrity of the jet over that path depending upon such factors as discharge nozzle design, supply pressure, and viscosity of the fluid.

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