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公开(公告)号：US20140226440A1
公开(公告)日：2014-08-14
申请号：US14345725
申请日：2012-09-11
CPC分类号： G01V1/38 , B63B1/04 , B63B2241/12 , B63G8/001 , B63G8/08 , B63G2008/002 , G01V1/3852
摘要： A method of deploying a device to the seabed with a submersible vehicle, the vehicle having a hull which defines a hull axis and appears substantially annular when viewed along the hull axis. The hull has an interior defining a duct which is open at both ends. The device is mounted to the hull on one or more struts so that it is positioned in line with the duct or at least partially within the duct. The device is transported to the seabed mounted to the hull on the strut(s), water flowing through the duct as it does so. The device is then deployed on the seabed after it has been transported to the seabed by the vehicle.
摘要翻译： 一种利用潜水车辆将设备部署到海床的方法，该车辆具有船身，其限定了船体轴线，并且当沿着船体轴线观察时其呈现大致环形。 船体有一个内部，限定两端敞开的管道。 该装置在一个或多个支柱上安装到船体上，使得其与导管成一直线或至少部分地位于管道内。 该装置被运送到安装在支柱上的船体上的海底，如同这样做时流过管道的水。 该装置然后在车辆被运送到海底后部署在海床上。
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公开(公告)号：US20120256043A1
公开(公告)日：2012-10-11
申请号：US13466343
申请日：2012-05-08
CPC分类号： B64C39/062 , B64C39/024 , B64C2201/028 , B64C2201/162
摘要： An airborne vehicle having a wing-body which defines a wing-body axis and appears substantially annular when viewed along the wing-body axis, the interior of the annulus defining a duct which is open at both ends. A propulsion system is provided comprising one or more pairs of propulsion devices, each pair comprising a first propulsion device mounted to the wing-body and positioned on a first side of a plane including the wing-body axis, and a second propulsion device mounted to the wing-body and positioned on a second side of the plane including the wing-body axis.
摘要翻译： 一种机载车辆，其具有限定翼体轴线的翼体，并且当沿翼体轴线观察时呈现大致环形，所述环形空间的内部限定在两端敞开的管道。 提供了包括一对或多对推进装置的推进系统，每对推进装置包括安装到翼体上并定位在包括翼体轴线的平面的第一侧上的第一推进装置，以及安装到 翼体并且定位在包括翼体轴线的平面的第二侧上。
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公开(公告)号：US20100044496A1
公开(公告)日：2010-02-25
申请号：US12594719
申请日：2008-04-16
CPC分类号： B64C39/062 , B64C39/024 , B64C2201/028 , B64C2201/162
摘要： An airborne vehicle having a wing-body which defines a wing-body axis and appears substantially annular when viewed along the wing-body axis, the interior of the annulus defining a duct which is open at both ends. A propulsion system is provided comprising one or more pairs of propulsion devices, each pair comprising a first propulsion device mounted to the wing-body and positioned on a first side of a plane including the wing-body axis, and a second propulsion device mounted to the wing-body and positioned on a second side of the plane including the wing-body axis. A direction of thrust of the first propulsion device can be adjusted independently of the direction of thrust of the second propulsion device and/or a magnitude of thrust of the first propulsion device can be adjusted independently of the magnitude of thrust of the second propulsion device. In certain embodiments the wing-body appears swept forward when viewed from a first viewing angle, and swept backward when viewed from a second viewing position at right angles to the first viewing angle.
摘要翻译： 一种机载车辆，其具有限定翼体轴线的翼体，并且当沿翼体轴线观察时呈现大致环形，所述环形空间的内部限定在两端敞开的管道。 提供了包括一对或多对推进装置的推进系统，每对推进装置包括安装到翼体上并定位在包括翼体轴线的平面的第一侧上的第一推进装置，以及安装到 翼体并且定位在包括翼体轴线的平面的第二侧上。 可以独立于第二推进装置的推力方向来调节第一推进装置的推力方向，和/或可以独立于第二推进装置的推力的大小来调节第一推进装置的推力的大小。 在某些实施例中，当从第一视角观察时，翼体呈向前扫掠，并且当从与第一视角成直角的第二观察位置观看时向后扫掠。
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公开(公告)号：US20140033823A1
公开(公告)日：2014-02-06
申请号：US13985323
申请日：2012-02-08
IPC分类号： G01H1/00
CPC分类号： G01H1/00 , G01V1/20 , G01V1/3852
摘要： A seismic sensor node comprising an annular body (2) with an annular cutting edge (3) at one end. One or more seismic sensors (8, 9) are coupled to the annular body (2). The annular body (2) surrounds a duct (5) which is open at either end to permit liquid to flow through the duct, and which increases in cross-sectional area as it extends towards the cutting edge (3). The compression of the seabed material squeezes out water from the material, making it more dense so that it transmit seismic vibrations more efficiently. The shape of the duct (5) also means that the centre of gravity of the node is lower than it would be for a cylindrical node—thus increasing the stability of the node compared with a cylindrical one.
摘要翻译： 地震传感器节点包括在一端具有环形切削刃（3）的环形体（2）。 一个或多个地震传感器（8,9）联接到环形体（2）。 环形体（2）围绕在任一端开口的管道（5），以允许液体流过管道，并且当其朝向切割边缘（3）延伸时，其横截面积增加。 海底材料的压缩从材料中挤出水分，使其更致密，从而更有效地传递地震振动。 管道（5）的形状也意味着节点的重心低于圆柱形节点的重心，从而提高节点与圆柱节点的稳定性。
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公开(公告)号：US20120305714A1
公开(公告)日：2012-12-06
申请号：US13466327
申请日：2012-05-08
IPC分类号： B64C39/06
CPC分类号： B64C39/062 , B64C39/024 , B64C2201/028 , B64C2201/162
摘要： An airborne vehicle having a wing-body which defines a wing-body axis and appears substantially annular when viewed along the wing-body axis, the interior of the annulus defining a duct which is open at both ends. A propulsion system is provided comprising one or more pairs of propulsion devices, each pair comprising a first propulsion device mounted to the wing-body and positioned on a first side of a plane including the wing-body axis, and a second propulsion device mounted to the wing-body and positioned on a second side of the plane including the wing-body axis.
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公开(公告)号：US08025021B2
公开(公告)日：2011-09-27
申请号：US12090547
申请日：2006-10-19
IPC分类号： B63G8/08
CPC分类号： B63G8/22 , B63B1/04 , B63B35/04 , B63B2241/12 , B63G8/001 , B63G8/08 , B63G8/24 , B63G8/26 , B63G2008/002 , B63H1/32 , B63H1/36 , B63H5/14 , B63H2001/005
摘要： A submersible vehicle having an outer hull which defines a hull axis and appears substantially annular when viewed along the hull axis, the interior of the annulus defining a duct which is open at both ends so that when the vehicle is submerged in a liquid, the liquid floods the duct. The vehicle further comprising means for rolling the vehicle about the hull axis. A buoyancy control system may be provided, and the outer hull may be swept with respect to the hull axis. Various methods of deploying and using the vehicle are described.
摘要翻译： 一种潜艇，其具有外壳，其限定船体轴线，并且当沿着船体轴线观察时呈现大致环形，所述环形空间的内部限定了在两端敞开的管道，使得当车辆浸没在液体中时，液体 洪水管道。 车辆还包括用于围绕船体轴线滚动车辆的装置。 可以提供浮力控制系统，并且外壳可以相对于船体轴线扫掠。 描述了部署和使用车辆的各种方法。
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公开(公告)号：US08677921B2
公开(公告)日：2014-03-25
申请号：US13096721
申请日：2011-04-28
IPC分类号： B63G8/00
CPC分类号： B63G8/22 , B63B1/04 , B63B35/04 , B63B2241/12 , B63G8/001 , B63G8/08 , B63G8/24 , B63G8/26 , B63G2008/002 , B63H1/32 , B63H1/36 , B63H5/14 , B63H2001/005
摘要： A submersible vehicle having an outer hull which defines a hull axis and appears substantially annular when viewed along the hull axis, the interior of the annulus defining a duct which is open at both ends so that when the vehicle is submerged in a liquid, the liquid floods the duct. At least part of the outer hull is swept with respect to the hull axis A buoyancy control system may be provided. Various methods of deploying and using the vehicle are described.
摘要翻译： 一种潜艇，其具有外壳，其限定船体轴线，并且当沿着船体轴线观察时呈现大致环形，所述环形空间的内部限定了在两端敞开的管道，使得当车辆浸没在液体中时，液体 洪水管道。 外壳的至少一部分相对于船体轴线扫掠。可以提供浮力控制系统。 描述了部署和使用车辆的各种方法。
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公开(公告)号：US20140036622A1
公开(公告)日：2014-02-06
申请号：US13985331
申请日：2012-02-08
IPC分类号： G01V1/18
摘要： A seismic sensor node 1 comprising one or more seismic sensors (8,9) and an annular skirt (3) defining an annular axis. The annular skirt (3) has a cutting edge (10) which appears serrated when viewed at a right angle to the annular axis. The skirt (3) also has a series of ribs (15) and channels (11) which terminate at the cutting edge so that the cutting edge has an undulating shape when viewed parallel with the annular axis. The ribbed shape of the skirt (3) makes it particularly resistant to ellipsoid or modal oscillation, so that it can transmit seismic vibrations to the seismic sensor (s) with minimal distortion, attenuation or damping.
摘要翻译： 地震传感器节点1包括一个或多个地震传感器（8,9）和限定环形轴线的环形裙部（3）。 环形裙部（3）具有当与环形轴成直角观察时出现锯齿状的切割边缘（10）。 裙部（3）还具有一系列肋（15）和通道（11），其终止于切割边缘处，使得当与环形轴线平行时切割边缘具有起伏的形状。 裙部（3）的肋状形状使其特别耐椭球或模态振动，使得其可以以最小的失真，衰减或阻尼将地震振动传递给地震传感器。
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公开(公告)号：US08328131B2
公开(公告)日：2012-12-11
申请号：US13466343
申请日：2012-05-08
IPC分类号： B64C39/06
CPC分类号： B64C39/062 , B64C39/024 , B64C2201/028 , B64C2201/162
摘要： An airborne vehicle having a wing-body which defines a wing-body axis and appears substantially annular when viewed along the wing-body axis, the interior of the annulus defining a duct which is open at both ends. A propulsion system is provided comprising one or more pairs of propulsion devices, each pair comprising a first propulsion device mounted to the wing-body and positioned on a first side of a plane including the wing-body axis, and a second propulsion device mounted to the wing-body and positioned on a second side of the plane including the wing-body axis.
摘要翻译： 一种机载车辆，其具有限定翼体轴线的翼体，并且当沿翼体轴线观察时呈现大致环形，所述环形空间的内部限定在两端敞开的管道。 提供了包括一对或多对推进装置的推进系统，每对推进装置包括安装到翼体上并定位在包括翼体轴线的平面的第一侧上的第一推进装置，以及安装到 翼体并且定位在包括翼体轴线的平面的第二侧上。
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公开(公告)号：US08262016B2
公开(公告)日：2012-09-11
申请号：US12594719
申请日：2008-04-16
IPC分类号： B64C15/00
CPC分类号： B64C39/062 , B64C39/024 , B64C2201/028 , B64C2201/162
摘要： An airborne vehicle having a wing-body which defines a wing-body axis and appears substantially annular when viewed along the wing-body axis, the interior of the annulus defining a duct which is open at both ends. A propulsion system is provided comprising one or more pairs of propulsion devices, each pair comprising a first propulsion device mounted to the wing-body and positioned on a first side of a plane including the wing-body axis, and a second propulsion device mounted to the wing-body and positioned on a second side of the plane including the wing-body axis. A direction of thrust of the first propulsion device can be adjusted independently of the direction of thrust of the second propulsion device and/or a magnitude of thrust of the first propulsion device can be adjusted independently of the magnitude of thrust of the second propulsion device. In certain embodiments the wing-body appears swept forward when viewed from a first viewing angle, and swept backward when viewed from a second viewing position at right angles to the first viewing angle.
摘要翻译： 一种机载车辆，其具有限定翼体轴线的翼体，并且当沿翼体轴线观察时呈现大致环形，所述环形空间的内部限定在两端敞开的管道。 提供了包括一对或多对推进装置的推进系统，每对推进装置包括安装到翼体上并定位在包括翼体轴线的平面的第一侧上的第一推进装置，以及安装到 翼体并且定位在包括翼体轴线的平面的第二侧上。 可以独立于第二推进装置的推力方向来调节第一推进装置的推力方向，和/或可以独立于第二推进装置的推力的大小来调节第一推进装置的推力的大小。 在某些实施例中，当从第一视角观察时，翼体呈向前扫掠，并且当从与第一视角成直角的第二观察位置观看时向后扫掠。
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