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    • 4. 发明申请
    • ANNULAR SEISMIC SENSOR NODE
    • ANNULAR地震传感器节点
    • US20140033823A1
    • 2014-02-06
    • US13985323
    • 2012-02-08
    • Harry George Dennis Gosling
    • Harry George Dennis Gosling
    • G01H1/00
    • G01H1/00G01V1/20G01V1/3852
    • 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.
    • 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。
    • 9. 发明申请
    • ANNULAR AIRBORNE VEHICLE
    • US20100044496A1
    • 2010-02-25
    • US12594719
    • 2008-04-16
    • Harry George Dennis Gosling
    • Harry George Dennis Gosling
    • B64C15/12B64C9/00
    • B64C39/062B64C39/024B64C2201/028B64C2201/162
    • 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.
    • 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。