| 摘要 |
1,261,671. Geophysical surveying. INTERNATIONAL NICKEL CO. OF CANADA Ltd. Feb.20, 1970 [March 7, 1969], No.8249/70. Heading G1N. In order to reduce the effects of variation in the orientation of a search coil 21 of a geophysical surveying apparatus a second search coil 22 is arranged at 90 degrees to coil 21 in minimum mutual coupling relationship therewith, a phase difference of 90 degrees is introduced between the outputs of the two coils and the outputs of the two coils are vectorially added to form a resultant signal. A transmitter coil radiating a primary field is carried in an aircraft towing a bird in which the two search coils 21, 22 are mounted with their coils in mutually perpendicular planes which intersect at a line perpendicular to a plane through the longitudinal axis of the bird and substantially horizontal. The 90 degree phase difference may be introduced by means of a phase shifter 25, Fig.2, connected to one of the coils 21, 22 or by tuning by capacitors 23, 24 one of the coils to the upper half power point and the other to the lower half power point. The two outputs are vectorially added at amplifier 26 and the resultant signal including any disturbance of the primary field due to radiated secondary fields caused by eddy currents in ores in the ground is passed to a voltage meter and recorder carried in the aircraft. The arrangement reduces the effect of lateral axis noise. A dual frequency transmitter may be used having two transmitting coils Figs. 5, 6 (not shown) emitting frequencies F1, F2 respectively, in which case a third receiver coil is added to the circuit of Fig.2, Fig.3 (not shown) and having its coils coplanar with the F2 transmitter coil. In this case the third coil is tuned to the F2 frequency and the coils 21, 22 to frequency F1 The resultant of coils 21 and 22 and the signal from the third coil are fed through a broad band amplifier to a signal analysis circuit Fig.4 (not shown) including two frequency channels, the detected outputs of the two channels being fed to respective inputs of a differential amplifier to give a resultant difference signal. A fourth receiver coil may be provided, Fig. 10 (not shown) which together with the third coil and associated capacitors is tuned to the half power points at the F2 frequency to provide a 90 degree phase shift. The vectorially combined third and fourth coil output signals is applied together with the resultant signal from coils 21, 22 to a signal analysis circuit to give a resultant difference signal. This arrangement reduces roll maneuver noise and/or yaw maneuver noise dependent upon the orientation of the plane of the fourth coil. |
