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    • 63. 发明授权
    • Aerodynamically stabilized tow assembly for aircraft for geophysical surveying
    • 用于地球物理测量的飞机的空气动力学稳定的牵引组件
    • US08847599B2
    • 2014-09-30
    • US13948017
    • 2013-07-22
    • GEO Equipment Manufacturing Ltd.
    • Edward Beverly MorrisonElton Townsend
    • G01V3/16G01V3/165G01V3/17B64D3/00
    • G01V3/16B64D3/00G01V3/165G01V3/17
    • A airborne geophysical electromagnetic (EM) survey tow assembly system for use with an aircraft, including a substantially rigid receiver coil frame that defines a central open area, the receiver coil frame forming a continuous internal passageway that extends around the central open area; a receiver coil housed within the internal passageway isolated from the central open area, the receiver coil being configured to measure the response of surveyed terrain to naturally occurring EM events; and a tow cable for suspending the receiver coil frame from the aircraft, the receiver coil frame being formed from rigid members configured to provide aerodynamic stabilization to maintain the receiver coil frame in a desired pitch and yaw orientation relative to a direction of travel and the horizontal when the receiver coil frame is suspended during flight.
    • 一种与飞机一起使用的机载地球物理电磁(EM)测量拖车组件系统,包括限定中心开放区域的基本上刚性的接收器线圈框架,接收器线圈框架形成围绕中央开放区域延伸的连续内部通道; 接收器线圈,其容纳在与所述中央开放区域隔离的所述内部通路内,所述接收器线圈被配置为测量被测地形对自然发生的EM事件的响应; 以及用于将接收器线圈框架悬挂在飞机上的牵引电缆,接收器线圈框架由刚性构件形成,该刚性构件构造成提供空气动力学稳定性,以将接收器线圈框架相对于行进方向和横向维持在期望的俯仰和偏航方向 当接收器线圈架在飞行期间暂停。
    • 68. 发明申请
    • Airborne geophysical measurements
    • 机载地球物理测量
    • US20050017721A1
    • 2005-01-27
    • US10492391
    • 2002-10-11
    • Ken McCrackenJames Lee
    • Ken McCrackenJames Lee
    • G01V20060101G01V3/16
    • G01V3/16
    • This invention concerns a method of making airborne geophysical measurements. Such measurements may be made from fixed or moving wing airplanes or dirlgibles. The method comprises the following steps: taking first real time measurements from one, or more, geophysical instruments mounted in an aircraft to produce geophysical data related to the ground below that instrument. Taking second real time measurements from navigation and mapping instruments associated with or carried by the aircraft. Computing a background response of each geophysical instrument using the second real time measurements to take account of its time varying altitude, and the time varying topography of the ground below it. Adjusting an operating or data processing condition of each geophysical instrument using the respective background response and the intrument's altitude to enhance the performance of that instrument. And, adjusting the geophysical data output for that instrument having reduced effects resulting from variations in altitude, attitude and topography.
    • 本发明涉及一种进行空中地球物理测量的方法。 这样的测量可以由固定或移动的翼型飞机或旋转轮进行。 该方法包括以下步骤:从安装在飞机上的一个或多个地球物理仪器获取第一次实时测量,以产生与该仪器下面的地面相关的地球物理数据。 从与飞机相关或携带的导航和制图仪器进行第二次实时测量。 使用第二次实时测量计算每个地球物理仪器的背景响应,以考虑其时变高度,以及其下方地面的时变变化。 使用各自的背景响应和文件的高度调整每个地球物理仪器的操作或数据处理状况,以提高该仪器的性能。 并且,调整该仪器的地球物理数据输出,由于高度,姿态和地形的变化而导致的效果降低。
    • 69. 发明申请
    • Method and apparatus for a rigidly joined together and floating bucking and receiver coil assembly for use in airborne electromagnetic survey systems
    • 用于机载电磁测量系统中的刚性接合在一起的浮动屈曲和接收线圈组件的方法和装置
    • US20030169045A1
    • 2003-09-11
    • US10378850
    • 2003-03-05
    • Raymond Macklin Whitton
    • G01V003/16
    • G01V3/105G01V3/16
    • A housing and bucking coil and receiving coil system for a helicopter towed concentric coil electromagnetic survey system that reduces micro phonic and primary field noise. The device includes an isolation housing, a bucking coil and receiving coil assembly with structural members to rigidly join the two coils together and a suspension system to suspend the joined bucking and receiving coils, in a floating manner, by bungee cords or similar non-metallic vibration dampening devices. A housing with dimensions large enough to enclose the suspended bucking and receiving coil assembly that is lined with acoustic and other vibration dampening material A method for suspending the joined bucking and receiving coil assembly that isolates the assembly from vibration and at the same time keeps the coil assembly from twisting and turning in angular planes from the plane of the transmitter, wherein the acceptable minor motions the coil assembly will be allowed to make by the suspension system are up-down, back-forward and left-right motions.
    • 用于直升机牵引的同心线圈电磁测量系统的壳体和弯曲线圈和接收线圈系统,其减少微电声和主场噪声。 该装置包括隔离壳体,抗弯线圈和接收线圈组件,其具有用于将两个线圈刚性地连接在一起的结构构件和悬挂系统,以浮动方式悬挂连接的弯曲和接收线圈,由蹦极绳或类似的非金属 减震装置。 具有尺寸足够大以包围衬有声学和其它减振材料的悬挂的屈曲和接收线圈组件的壳体用于悬挂连接的弯曲和接收线圈组件的方法,其将组件与振动隔离并同时保持线圈 组装从角度平面从发射机的平面扭转和转动,其中由悬挂系统允许线圈组件可允许的可接受的小运动是上下,后向和左右运动。