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Electromagnetic exploration method

机译:电磁勘探法

摘要

848,428. Electric tests. CANADIAN AIRBORNE GEOPHYSICS Ltd. Nov. 12, 1957 [Dec. 4, 1956], No. 35239/57. Class 37 Apparatus for geophysical cryoloration comprises a pair of transmitting coils mounted at right angles to one another, a pair of receiving coils similarly mounted, means feeding the coils alternately with A.C. and means for indicating the difference between the signals in the receiving coils at corresponding intervals. The transmitting coils may be carried on one aircraft while the receiving coils are in a case towed behind or in a different aircraft or a case towed behind it. In the arrangement shown in Fig. 2 the A.C. source is connected by switch 4 alternately to transmitting coils 2, 3. Receiving coils 2SP1/SP 3SP1/SP detect the fields of the corresponding coils in the absence of disturbing bodies and their outputs are amplified by amplifiers 19, 18 respectively. Imperfect alignment of the receiving with the transmitting coils may mean that receiving coil 2 1 will receive a signal from transmiitter 3, and 3SP1/SP from 2. This is avoided by switches 17, 17SP1/SP coupled to switch 4 to disable the appropriate amplifier channel when the other coil is receiving a pick-up signal. In addition coils 2SP11/SP, 3SP11/SP, near the transmitting coils combine their signals with the outputs of the receiving coils so as to eliminate unwanted pick-ups. The outpots E 1, Ex may be rectified and fed with appropriate signs to a long time constant indicator which indicates their difference. Alternatively, as shown, the difference between the two signals is split in to in-phase and out-of-phase components at 7, 8 using the A.C. source 1 as a reference. In the arrangement of Fig. 1 (not shown) the outputs of the receiving coils are fed through non-linear amplifiers which eliminate the small signals produced by unwanted coupling when the other coil of the pair is energized.
机译:848,428。电气测试。加拿大航空地球物理有限公司1957年11月12日[十二月[1956年4月],第35239/57号。用于地球物理冰冻作用的37类设备包括一对相互成直角安装的发射线圈,一对类似安装的接收线圈,向线圈交替馈送交流电的装置以及用于在相应位置指示接收线圈中信号差的装置间隔。发射线圈可以被携带在一架飞机上,而接收线圈可以被拖曳在后面或在另一架飞机或被拖曳在后面的情况下。在图2所示的布置中,交流电源通过开关4交替连接到发送线圈2、3。接收线圈2 1 3 1 检测相应线圈的磁场。没有干扰体的线圈及其输出分别由放大器19、18放大。接收线圈与发射线圈的不完全对准可能意味着接收线圈2 1将接收来自发射器3的信号,而接收来自2的3 1 的信号。这可以通过开关17、17 1 < / SP>耦合到开关4,以在另一个线圈接收到拾取信号时禁用适当的放大器通道。此外,靠近发射线圈的线圈2 11 ,3 11 会将其信号与接收线圈的输出进行组合,以消除不必要的拾取。出口E 1,Ex可以被整流并以适当的符号馈入指示其差异的长时间常数指示器。或者,如图所示,以交流电源1为基准,将两个信号之间的差在7、8分为同相和异相分量。在图1的布置中(未示出),接​​收线圈的输出通过非线性放大器馈送,当该对线圈中的另一个线圈通电时,该非线性放大器消除了由不希望的耦合产生的小信号。

著录项

  • 公开/公告号GB848428A

    专利类型

  • 公开/公告日1960-09-14

    原文格式PDF

  • 申请/专利权人 CANADIAN AIRBORNE GEOPHYSICS LIMITED;

    申请/专利号GB19570035239

  • 发明设计人

    申请日1957-11-12

  • 分类号G01V3/165;

  • 国家 GB

  • 入库时间 2022-08-23 19:02:35

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