公开(公告)号：US08950708B2

公开(公告)日：2015-02-10

申请号：US13368431

申请日：2012-02-08

申请人： Christopher Mouskis ,  Georgios Filippos Papaioannou ,  Adrian Bedford ,  Richard John Foxwell ,  James Kemmitt

发明人： Christopher Mouskis ,  Georgios Filippos Papaioannou ,  Adrian Bedford ,  Richard John Foxwell ,  James Kemmitt

IPC分类号： B64D39/00 ,  B64D39/06 ,  B64D39/04 ,  B64F1/28

CPC分类号： B64D39/06 ,  B64D39/00 ,  B64D39/04 ,  B64F1/28

摘要： An air to air refuelling drogue assembly includes a reception coupling and a drogue canopy connected to the reception coupling by connection means which hold the canopy in an operative, drag producing, position relative to the reception coupling during refuelling. The drogue assembly is arranged to controllably fail so as to reduce the drag load produced by the drogue when a drag load on the canopy exceeds a predetermined threshold.

摘要翻译： 空气对空气加油锥套组件包括接收联接器和通过连接装置连接到接收联接器的锥套罩，所述连接装置在加油期间相对于接收耦合器将冠盖保持在可操作的，阻力产生位置。 锥形组件布置成可控制地失效，以便当在顶篷上的拖曳负载超过预定阈值时减小由锥套产生的牵引载荷。

公开(公告)号：US08205837B2

公开(公告)日：2012-06-26

申请号：US12307183

申请日：2007-06-27

申请人： Christopher Mouskis ,  Ismet Gursul ,  James Kemmitt

发明人： Christopher Mouskis ,  Ismet Gursul ,  James Kemmitt

IPC分类号： B64D39/00

CPC分类号： B64D39/04

摘要： A drogue assembly includes a probe guide such as a standard small high speed drogue with a first canopy (14), and a foldable second canopy (20) mounted around the first canopy which is biased outwardly, and is foldable inwardly under air pressure loading to overlie the small drogue at low speeds. Thus the drag produced by the drogue varies automatically with airspeed allowing the assembly to be used over a wide range of airspeeds.

摘要翻译： 锥形组件包括探针引导件，例如具有第一冠层（14）的标准小型高速锥套，以及安装在第一冠层周围的可折叠的第二冠层（20），所述第一冠盖向外偏压，并且在空气压力加载下可向内折叠 在低速下覆盖小水龙头。 因此，锥形产生的阻力随空速自动变化，允许组件在宽范围的空速下使用。

公开(公告)号：US20100019090A1

公开(公告)日：2010-01-28

申请号：US12307183

申请日：2007-06-27

申请人： Christopher Mouskis ,  Ismet Gursul ,  James Kemmitt

发明人： Christopher Mouskis ,  Ismet Gursul ,  James Kemmitt

IPC分类号： B64D39/00

CPC分类号： B64D39/04

摘要： A drogue assembly includes a probe guide such as a standard small high speed drogue with a first canopy (14), and a foldable second canopy (20) mounted around the first canopy which is biased outwardly, and is foldable inwardly under air pressure loading to overlie the small drogue at low speeds. Thus the drag produced by the drogue varies automatically with airspeed allowing the assembly to be used over a wide range of airspeeds.

摘要翻译： 锥形组件包括探针引导件，例如具有第一冠层（14）的标准小型高速锥套，以及安装在第一冠层周围的可折叠的第二冠层（20），所述第一冠盖向外偏压，并且在空气压力加载下可向内折叠 在低速下覆盖小水龙头。 因此，锥形产生的阻力随空速自动变化，允许组件在宽范围的空速下使用。

公开(公告)号：US20100243061A1

公开(公告)日：2010-09-30

申请号：US12601719

申请日：2008-05-22

申请人： Christopher Mouskis

发明人： Christopher Mouskis

IPC分类号： F15D1/00 ,  F16K15/00

CPC分类号： B64D39/06 ,  B67D7/04 ,  B67D7/36 ,  G05D16/106 ,  G05D16/166 ,  Y10T137/0318 ,  Y10T137/7762 ,  Y10T137/7837 ,  Y10T137/7838 ,  Y10T137/87981

摘要： A pressure regulator valve arrangement comprises first (14) and second (24) regulator valves for closing a fluid passage (4) in the event of over-pressure. The valve members each have pressure ports for sensing the pressure, the ports being located downstream of the valve members to minimise interaction between the valves.

摘要翻译： 压力调节阀装置包括用于在过压情况下关闭流体通道（4）的第一（14）和第二（24）调节阀。 阀构件各自具有用于感测压力的压力端口，端口位于阀构件的下游，以最小化阀之间的相互作用。

公开(公告)号：US08152104B2

公开(公告)日：2012-04-10

申请号：US12282723

申请日：2007-03-08

申请人： Christopher Mouskis

发明人： Christopher Mouskis

IPC分类号： B64D37/02 ,  B64D39/00

CPC分类号： B64D39/04 ,  B64D47/02 ,  B64D2203/00

摘要： In a reception coupling and drogue assembly (2), light sources (32) are arranged around the wall (26) of the probe passage adjacent the opening (24). The light sources (32) each serve to illuminate the opposing part of the drogue, giving good visibility to the pilot of the following aircraft.

摘要翻译： 在接收联接和锥形组件（2）中，光源（32）围绕探头通道的靠近开口（24）的壁（26）布置。 光源（32）各自用于照亮锥形物的相对部分，使得对下列飞机的飞行员具有良好的可见性。

公开(公告)号：US20100282913A1

公开(公告)日：2010-11-11

申请号：US12742049

申请日：2008-11-10

申请人： Christopher Mouskis

发明人： Christopher Mouskis

IPC分类号： B64D39/00 ,  G06F19/00

CPC分类号： B64D39/00

摘要： A steerable drogue (2) comprises a steering mechanism (22, 34, 36) for twisting the canopy support arms (6) to produce an aerodynamic force in flight which can be used to produce movement of the drogue in a required direction.

摘要翻译： 可操纵的锥套（2）包括用于扭转天篷支撑臂（6）以在飞行中产生空气动力的转向机构（22,34,36），其可用于在所需方向上产生锥套的运动。

公开(公告)号：US08720502B2

公开(公告)日：2014-05-13

申请号：US13145466

申请日：2010-01-21

申请人： Christopher Mouskis

发明人： Christopher Mouskis

IPC分类号： B65B1/04 ,  F16L37/34 ,  F16L29/00 ,  F16L37/413

CPC分类号： F16L37/413 ,  B64D39/06 ,  F16L29/00 ,  Y10T137/87949

摘要： A nozzle includes a nozzle body having a nozzle tip for engaging a fuel hose coupling, the tip extending from the body, and a valve sleeve for opening and closing a fuel path between the tip and the body. The tip is mounted within the body on a flexible shaft, so as to accommodate misalignment between the nozzle and the fuel hose coupling. This eliminates the need for a bearing at the end of the shaft, which causes a pressure drop in the nozzle. The shaft is axially slidable in the mounting in a first portion of the nozzle body. The first and second portions of the body are joined with a weak link, which is frangible in the event of excessive load, to release the abutment and allow the nozzle tip to travel towards the body and close the fuel path. Thus a separate shut-off valve is not required. Also a pressure regulator sleeve moves out of the nozzle body towards the nozzle tip in the event of excessive fuel pressure.

摘要翻译： 喷嘴包括具有用于接合燃料软管接头的喷嘴头的喷嘴主体，从主体延伸的末端以及用于打开和关闭尖端与主体之间的燃料路径的阀套。 尖端安装在主体内的柔性轴上，以便适应喷嘴和燃料软管接头之间的未对准。 这消除了在轴端部处的轴承的需要，这导致喷嘴中的压降。 轴在喷嘴体的第一部分中在安装件中可轴向滑动。 主体的第一和第二部分与弱连接件连接，该薄弱环节在过载的情况下是易碎的，以释放邻接部分，并允许喷嘴尖端朝向主体行进并关闭燃料路径。 因此不需要单独的截止阀。 在燃料压力过大的情况下，压力调节器套筒也可以从喷嘴体向喷嘴尖端移动。

公开(公告)号：US08366048B2

公开(公告)日：2013-02-05

申请号：US12662475

申请日：2010-04-19

申请人： Christopher Mouskis

发明人： Christopher Mouskis

IPC分类号： B64D39/00

CPC分类号： B64D39/04

摘要： An adaptor for mounting a refuelling hose and drogue arrangement to a refuelling boom of an aircraft is arranged to provide fluid communication between the boom and a hose of the hose and drogue arrangement. The adaptor is also arranged such that the hose is movable with respect to the boom. The adaptor includes an actuator arranged to produce a biasing force on the hose, and arranged for affecting movement to adjust the position of the hose in relation to the boom.

摘要翻译： 将用于将加油软管和冷冻装置安装到飞机的加油臂上的适配器被布置成提供悬臂与软管的软管和冷却装置之间的流体连通。 适配器也布置成使得软管相对于起重臂可移动。 适配器包括致动器，其被布置成在软管上产生偏置力，并被布置成影响运动以调节软管相对于起重臂的位置。

公开(公告)号：US20100270431A1

公开(公告)日：2010-10-28

申请号：US12662475

申请日：2010-04-19

申请人： Christopher Mouskis

发明人： Christopher Mouskis

IPC分类号： B64D39/00

CPC分类号： B64D39/04

摘要： A boom drogue adapter for a refuelling boom of an aerial refuelling apparatus comprises a linkage arm between the boom and a hose and drogue arrangement, which arm can be pivotally moved about the boom to adjust the position of the hose and drogue and take up hose slack.

摘要翻译： 用于空中加油装置的加油臂的吊杆转接适配器包括在起重臂和软管之间的联动臂和棘爪装置，该臂可以围绕起重臂枢转运动，以调节软管的位置并使软管松动 。

公开(公告)号：US20120018039A1

公开(公告)日：2012-01-26

申请号：US13145466

申请日：2010-01-21

申请人： Christopher Mouskis

发明人： Christopher Mouskis

IPC分类号： B64D39/06 ,  F16K21/00

CPC分类号： F16L37/413 ,  B64D39/06 ,  F16L29/00 ,  Y10T137/87949

摘要： A nozzle includes a nozzle body having a nozzle tip for engaging a fuel hose coupling, the tip extending from the body, and a valve sleeve for opening and closing a fuel path between the tip and the body. The tip is mounted within the body on a flexible shaft, so as to accommodate misalignment between the nozzle and the fuel hose coupling. This eliminates the need for a bearing at the end of the shaft, which causes a pressure drop in the nozzle. The shaft is axially slidable in the mounting in a first portion of the nozzle body. The first and second portions of the body are joined a weak link, which is frangible in the event of excessive load, to release the abutment and allow the nozzle tip to travel towards the body and close the fuel path. Thus a separate shut-off valve is not required. Also a pressure regulator sleeve moves out of the nozzle body towards the nozzle tip in the event of excessive fuel pressure.

摘要翻译： 喷嘴包括具有用于接合燃料软管接头的喷嘴头的喷嘴主体，从主体延伸的末端以及用于打开和关闭尖端与主体之间的燃料路径的阀套。 尖端安装在主体内的柔性轴上，以便适应喷嘴和燃料软管接头之间的未对准。 这消除了在轴端部处的轴承的需要，这导致喷嘴中的压降。 轴在喷嘴体的第一部分中在安装件中可轴向滑动。 主体的第一部分和第二部分连接在一个弱连接部分上，该连杆在过载的情况下是易碎的，以便释放邻接部分，并允许喷嘴头朝向主体行进并关闭燃料通道。 因此不需要单独的截止阀。 在燃料压力过大的情况下，压力调节器套筒也可以从喷嘴体向喷嘴尖端移动。