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1. 发明申请

US20090302162A1 PASSIVE VARIABLE SPEED DROGUE 审中-公开
标题翻译：被动变速驱动
公开(公告)号：US20090302162A1
公开(公告)日：2009-12-10
申请号：US12477696
申请日：2009-06-03
申请人： Eric Reed , William L. Kirkland
发明人： Eric Reed , William L. Kirkland
IPC分类号： B64D39/00
CPC分类号： B64D39/04
摘要： The passive variable speed drogue includes an articulated center strut lever linkage assembly pivotally connected between adjacent pairs of center struts and trailing edge struts, biased by an extension spring mounted to the center strut to move the center strut to a required stop position to maintain substantially constant loads on the drogue within a range of refueling speeds, and to permit improved interfacing of the variable speed drogue assembly with a stowage tube. A center strut bumper on the center strut also provides improved interfacing of the variable speed drogue assembly with a stowage tube.
摘要翻译：被动可变速度锥套包括枢转地连接在相邻成对的中心支柱和后缘支柱之间的铰接中心支柱杆联动组件，其被安装到中心支柱上的延伸弹簧偏置，以将中心支柱移动到所需的停止位置以保持基本恒定在加油速度范围内的锥套上的负载，并且允许改变可变速度锥形组件与储存管的接口。中心支柱上的中心支柱保险杠还提供了可变速度锥形组件与存放管的改进的接口。

2. 发明申请

US20110226905A1 STABILIZED CONTROLLABLE DROGUE FOR AERIAL FLIGHT REFUELING 有权
标题翻译：稳定的可控制的航空器飞行员
公开(公告)号：US20110226905A1
公开(公告)日：2011-09-22
申请号：US12831185
申请日：2010-07-06
申请人： William L. Kirkland , Eric Reed
发明人： William L. Kirkland , Eric Reed
IPC分类号： B64D39/00 , B64D39/06
CPC分类号： B64D39/04
摘要： The stabilized controllable drogue for an inflight aerial refueling system includes a reception coupling, a paradrogue frame, a drogue canopy, and a plurality of actuators for moving the drogue canopy in a desired direction to control, steer and stabilize the stabilized controllable drogue during turbulent conditions.
摘要翻译：用于飞行空中加油系统的稳定的可控锥形包括接收联接器，平移架，锥形罩和多个致动器，用于在期望的方向上移动锥套盖，以在湍流条件下控制，转向和稳定稳定的可控制锥。

3. 发明授权

US08317136B2 Stabilized controllable drogue for aerial flight refueling 有权
标题翻译：用于空中加油的稳定的可控制冷冻
公开(公告)号：US08317136B2
公开(公告)日：2012-11-27
申请号：US12831185
申请日：2010-07-06
申请人： William L. Kirkland , Eric Reed
发明人： William L. Kirkland , Eric Reed
IPC分类号： B64D39/00
CPC分类号： B64D39/04
摘要： The stabilized controllable drogue for an inflight aerial refueling system includes a reception coupling, a paradrogue frame, a drogue canopy, and a plurality of actuators for moving the drogue canopy in a desired direction to control, steer and stabilize the stabilized controllable drogue during turbulent conditions.
摘要翻译：用于飞行空中加油系统的稳定的可控锥形包括接收联接器，平移架，锥形罩和多个致动器，用于在期望的方向上移动锥套盖，以在湍流条件下控制，转向和稳定稳定的可控制锥。

4. 发明申请

US20110108669A1 VARIABLE SPEED DROGUE 审中-公开
标题翻译：可变速度榨汁
公开(公告)号：US20110108669A1
公开(公告)日：2011-05-12
申请号：US12841949
申请日：2010-07-22
申请人： William L. Kirkland
发明人： William L. Kirkland
IPC分类号： B64D39/00
CPC分类号： B64D39/04
摘要： The variable speed drogue includes a plurality of leading edge struts and trailing edge struts pivotally mounted to a refueling coupling member, and a drogue canopy connected between the trailing ends of the leading edge and trailing edge struts. A spring and an articulated strut brace assembly are connected between each of the leading edge and trailing edge struts. A center strut is pivotally connected to the trailing end of each leading edge strut, and each center strut includes a free end connected to a center portion of the canopy drogue. The drogue canopy is connected to the trailing ends of the leading edge and trailing edge struts such that the drogue canopy is movable between a radially inward position and a radially outward position, to provide substantially constant loads on the drogue within the range of refueling speeds.
摘要翻译：可变速度锥套包括枢转地安装到加油联接构件的多个前缘支柱和后缘支柱，以及连接在前缘和后缘支柱的后端之间的锥套罩。弹簧和铰接支柱组件连接在每个前缘和后缘支柱之间。中心支柱枢转地连接到每个前缘支柱的尾端，并且每个中心支柱包括连接到顶盖的中心部分的自由端。锥形顶盖连接到前缘和后缘支柱的后端，使得锥套顶盖可以在径向向内的位置和径向向外的位置之间移动，以在加油速度范围内在锥套上提供基本上恒定的负载。

5. 发明授权

US5255877A Variable speed drogue 失效
标题翻译：变速锥
公开(公告)号：US5255877A
公开(公告)日：1993-10-26
申请号：US964378
申请日：1992-10-21
申请人： Matts Lindgren , William L. Kirkland
发明人： Matts Lindgren , William L. Kirkland
IPC分类号： B64D39/00 , B64D37/00
CPC分类号： B64D39/00
摘要： The variable speed drogue for use with an inflight aerial refueling system includes a refueling coupling for receiving a refueling probe. A plurality of trailing edge support arms are pivotally mounted to the trailing edge portion of the refueling coupling, projecting rearwardly, a plurality of pivot linkage members are pivotally connected to the trailing edge portion of the refueling coupling, and a plurality of leading edge support arms are pivotally connected to the pivot linkages. A mechanism is also provided for uniformly and symmetrically longitudinally changing the pivot points of the leading edge support arms to change the projected area of the drogue canopy.
摘要翻译：与飞行空中加油系统一起使用的变速泵包括用于接收加油探头的加油联轴器。多个后缘支撑臂枢转地安装到加油联轴器的后缘部分，向后突出，多个枢转连杆构件枢转地连接到加油联轴器的后缘部分，并且多个前缘支撑臂枢转地连接到枢转连杆。还提供了用于均匀和对称地纵向改变前缘支撑臂的枢转点以改变锥套顶部的投影面积的机构。

6. 发明授权

US06588465B1 Passive variable speed drogue 有权
标题翻译：被动变速锥头
公开(公告)号：US06588465B1
公开(公告)日：2003-07-08
申请号：US10050682
申请日：2002-01-15
申请人： William L. Kirkland , Matts Lindgren , Jerry Stultz
发明人： William L. Kirkland , Matts Lindgren , Jerry Stultz
IPC分类号： B64D3700
CPC分类号： B64D39/04 , Y10T137/6906 , Y10T137/8807
摘要： The aerial refueling drogue utilizes a bleeding drogue canopy providing substantially constant loads over a range of refueling speeds, by passive movement of the bleeding drogue between a retracted position and and extended position. The passive variable speed drogue comprises leading edge support arms, center support arms, and trailing edge support arms mounted to a refueling coupling member, with a forward drogue canopy attached between the leading edge support arms and the center support arms. An aft bleeding drogue canopy is connected between the center support arms and the trailing edge support arms. Springs in the trailing edge support arms bias the bleeding drogue canopy to a retracted position. In an alternate embodiment, cords are attached to the trailing edge of the aft bleeding drogue canopy, continue through the trailing edge support arms, up each center support arm, and through rings attached to the inside of the aft bleeding drogue canopy. The other ends of the cords are also attached to the trailing edge of the aft bleeding drogue canopy.
摘要翻译：空中加油锥套利用出血锥套顶盖，通过在缩回位置和延伸位置之间的出血锥的被动运动，在加油速度范围内提供基本上恒定的载荷。被动变速锥包括前缘支撑臂，中心支撑臂和安装在加油联接构件上的后缘支撑臂，其中前缘护盖连接在前缘支撑臂和中心支撑臂之间。尾部出血囊套冠连接在中心支撑臂和后缘支撑臂之间。后缘支撑臂中的弹簧将出血的顶盖顶盖偏压到缩回位置。在替代实施例中，绳索连接到后出血囊盖的后缘，继续穿过后缘支撑臂，向上每个中心支撑臂，以及穿过附接到后部出血椎囊冠内侧的环。电线的另一端也连接到后出血的顶盖的后缘。

7. 发明授权

US5427333A Variable speed drogue 失效
标题翻译：变速锥
公开(公告)号：US5427333A
公开(公告)日：1995-06-27
申请号：US280879
申请日：1994-07-26
申请人： William L. Kirkland
发明人： William L. Kirkland
IPC分类号： B64D39/00 , B64D37/00
CPC分类号： B64D39/00
摘要： The variable speed drogue for use with an inflight aerial refueling system includes a refueling coupling for receiving a refueling probe. A plurality of trailing edge support arms are pivotally mounted to the trailing edge portion of the refueling coupling, projecting rearwardly, and a plurality of leading edge support arms are pivotally connected to the refueling coupling forward and outward of the trailing edge support arms. A drogue canopy is connected between the trailing ends of the leading and trailing edge support arms, presenting a projected area, to provide drag. A plurality of cord linkages are secured at one end to the leading edge of the drogue canopy, and are connected at their other end to a rear cord ring mounted to the trailing edge portion of the refueling coupling member. A mechanism is provided for uniformly and symmetrically extending and retracting the cord linkages longitudinally with respect to the refueling coupling member to uniformly and symmetrically change the projected area of the drogue canopy.
摘要翻译：与飞行空中加油系统一起使用的变速泵包括用于接收加油探头的加油联轴器。多个后缘支撑臂枢转地安装到加油联轴器的后缘部分，向后突出，并且多个前缘支撑臂可枢转地连接到后缘支撑臂的向前和向外的加油联轴器。一个锥套冠连接在前缘和后缘支撑臂的后端之间，呈现一个投影区域，以提供阻力。多个绳索连接件在一端固定到锥套顶端，并且在其另一端连接到安装到加油联接构件的后缘部分的后帘线环。提供了一种用于相对于加油联接构件纵向均匀和对称地延伸和缩回绳索的机构，以均匀和对称地改变锥套顶部的投影面积。

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