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    • 21. 发明申请
    • APPARATUS FOR AIRBORNE AND GROUND ELECTROMAGNETIC PROSPECTING AND METHOD THEREOF
    • 空中飞行器和地面电磁波前置装置及其方法
    • US20170023694A1
    • 2017-01-26
    • US15218372
    • 2016-07-25
    • Advanced Electromagnetic Technologies
    • José Manuel MARTINEZ ORTEGA
    • G01V3/165G01V3/38G01V3/16
    • G01V3/165
    • There is described an improvement of the signal-to-noise ratio of an airborne/ground time-domain electromagnetic apparatus and a measuring/interpretation method for the voltage signal recorded. The system comprises: at least one embedded transmitter-receiver structure with at least one large receiver element allowing low system base frequency excitation and discrimination of targets at depths of at least 1 km; wherein the receiver element is positioned throughout the electromagnetic cavity created by transmitter elements whereas no bucking or suspension means are required; a computer network comprising: a microprocessor, a controller from the microprocessor and a host computer controls transmission of primary magnetic field intensities and reception of secondary magnetic field intensities with least 500 kS/s. A method of interpreting of the voltage recorded by receivers elements based on new sensitivity magnetic kernels is disclosed. The fabrication process the apparatus serving for airborne or ground electromagnetic surveying is disclosed.
    • 描述了机载/地面时域电磁装置的信噪比的改善以及记录的电压信号的测量/解释方法。 该系统包括:具有至少一个大的接收器元件的至少一个嵌入式发射器 - 接收器结构,允许低的系统基频激励和在至少1km的深度处的目标的辨别; 其中所述接收器元件被定位在由发射器元件产生的整个电磁腔内,而不需要弯曲或悬挂装置; 计算机网络包括:微处理器,来自微处理器的控制器和主计算机控制初级磁场强度的传输和接收具有至少500kS / s的次级磁场强度。 公开了一种基于新的灵敏度磁性内核来解释由接收机元件记录的电压的方法。 公开了用于机载或地面电磁测量的装置的制造过程。
    • 22. 发明申请
    • Airborne Geophysical Survey System
    • 机载地球物理测量系统
    • US20160131790A1
    • 2016-05-12
    • US14933740
    • 2015-11-05
    • Alan Vowles
    • Alan Vowles
    • G01V3/16G01V3/17
    • G01V3/165
    • An airborne ElectroMagnetic (EM) survey system wherein the system includes; first, a series of transmitter coils, which induce a primary (EM) field into the earth resulting in a secondary EM field being created in any sub-surface electrically conductive bodies; and second, a set of three orthogonal receiver coils which detect the secondary EM field. Multiple transmitter coils through which an electric current is pumped, form part of the structural, aluminum framework of a multi-rotor drone. The receiver sensor may be an EM induction sensor, comprised of multi-turn, copper windings, mounted inside an aerodynamic bird and separated by non-conductive sphalerite, which acts as an electrical insulator to limit self-induction and capacitance.Additionally a lighter-than-air balloon may be used to add vertical lift and increase a pendulum effect.
    • 一种机载电磁测量系统,其中系统包括: 首先,一系列发射器线圈,其将初级(EM)场引入地球,导致在任何子表面导电体中产生二次EM场; 第二,检测二次EM场的一组三个正交接收线圈。 多个发射器线圈通过电流泵送,形成多转子无人机的结构铝框架的一部分。 接收器传感器可以是EM感应传感器,包括多圈铜绕组,安装在空气动力学鸟类内部并由非导电闪锌矿隔开,其用作电绝缘体以限制自感和电容。 此外,可以使用轻便气球来增加垂直提升并增加摆锤效果。
    • 24. 发明申请
    • AIRBORNE ELECTROMAGNETIC SYSTEM WITH LARGE SUSPENSION COIL ASSEMBLY
    • 具有大型悬挂线圈组件的AIRBORNE电磁系统
    • US20150369944A1
    • 2015-12-24
    • US14421502
    • 2013-08-19
    • CGG DATA SERVICES AG
    • Philip John MILESWilliam Wallace MARR
    • G01V3/165G01V3/16
    • G01V3/16G01V3/081G01V3/165
    • The present invention provides an airborne electromagnetic receiver having a large dimension to allow low transmitter base frequency. A modular and configurable suspension assembly is provided for use within a receiver support structure and suspending the support structure. The suspension assembly has a rigid support having a suspension portion, and links connecting the suspension portion and the suspended structure. The links are adjustable in length and tension to radially suspend said equipment support structure. The natural frequency of the suspension assembly and the suspended receiver motion can be optimized by adjusting mass distribution, suspension link length and suspension link tension. The suspension assembly can be used to suspend a receiver having large receiver coils. The suspension assembly converts high frequency vibration forces imparted on the receiver to a low frequency oscillation. The suspension assembly may also be tuned to avoid coincidence with the excitation frequencies.
    • 本发明提供一种具有大尺寸以允许低发射机基频的机载电磁接收机。 提供模块化和可配置的悬挂组件,用于在接收器支撑结构内使用并悬挂支撑结构。 悬架组件具有刚性支撑件,其具有悬挂部分,以及连接悬架部分和悬挂结构的连杆。 连杆可以在长度和张力上调节以径向悬挂所述设备支撑结构。 可以通过调节质量分布,悬挂连杆长度和悬挂连杆张力来优化悬架组件的固有频率和悬架接收器运动。 悬挂组件可用于悬挂具有大的接收器线圈的接收器。 悬挂组件将接收器上施加的高频振动力转换为低频振荡。 还可以调节悬架组件以避免与激励频率的一致。
    • 27. 发明授权
    • Receiver coil assembly for airborne geophysical surveying with noise mitigation
    • 用于具有噪声减轻的机载地球物理测量的接收器线圈组件
    • US08878538B2
    • 2014-11-04
    • US12954797
    • 2010-11-26
    • Petr Valentinovich KuzminJack Dodds
    • Petr Valentinovich KuzminJack Dodds
    • G01V3/16G01V3/17
    • G01V3/17
    • An airborne geophysical surveying system comprising a receiver coil assembly for towing by an aircraft, the receiver assembly including a receiver coil for sensing changes in a magnetic field component of a magnetic field, and a receiver coil orientation sensing system for sensing orientation changes of the receiver coil. A controller receives signals representing the sensed changes in the magnetic field component from the receiver coil and the sensed orientation changes from the receiver coil orientation sensing system and corrects the sensed changes in the magnetic field component to provide a signal that is corrected for noise caused by changing orientation of the receiver coil in a static geomagnetic field.
    • 一种机载地球物理测量系统,包括用于由飞行器牵引的接收器线圈组件,所述接收器组件包括用于感测磁场的磁场分量的变化的接收器线圈和用于感测接收器的取向变化的接收器线圈定向感测系统 线圈 控制器接收表示来自接收器线圈的感测到的磁场分量变化的信号,并且感测到的方向从接收器线圈定向感测系统改变,并校正感测到的磁场分量变化,以提供对由 在静态地磁场中改变接收线圈的方位。
    • 28. 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。
    • 30. 发明申请
    • Airborne Electromagnetic (EM) Survey System
    • 机载电磁(EM)调查系统
    • US20080246484A1
    • 2008-10-09
    • US12098062
    • 2008-04-04
    • Philip J. MilesJason BerringerDavid G. HodgesPeter A. Wolfgram
    • Philip J. MilesJason BerringerDavid G. HodgesPeter A. Wolfgram
    • G01V3/16
    • G01V3/165
    • An airborne electromagnetic survey system for conducting geological mapping is disclosed. A transmitter closed loop structure is used in the system and is designed for connection to a towing airborne vehicle. The transmitter loop structure comprises a plurality of interconnected loop segments, and transmitting means are fitted to at least one of the loop segments for generating and transmitting an earthbound primary electromagnetic field effective for geological surveying. Sensing means are fitted to the loop segments for receiving and sensing a vertical component of a secondary resulting electromagnetic field which arises from an interaction of the primary electromagnetic field with ground bodies that are traversed by the sensing means, while simultaneously nulling the primary electromagnetic field. Helical sensing means are positioned in close proximity to the transmitting means to receive and sense a horizontal electromagnetic field contained in the secondary resulting field, while simultaneously nulling the primary electromagnetic field.
    • 公开了一种用于进行地质测绘的机载电磁勘测系统。 在系统中使用发射机闭环结构,并且设计用于连接到牵引机载车辆。 发射机环路结构包括多个互连的环路段,并且传输装置安装在至少一个环路段上,用于产生和传输有效地质测量的地球主要电磁场。 感测装置安装到环段上,用于接收和感测由主要电磁场与由感测装置穿过的地面主体的相互作用产生的次要产生的电磁场的垂直分量,同时使主电磁场归零。 螺旋检测装置位于靠近传送装置的位置,以接收和感测二次产生场中包含的水平电磁场,同时使主电磁场归零。