This invention provides an array of induction magnetometers for use in airborne transient electromagnetic geophysical exploration. These induction magnetometers have a similar weight and external dimensions to prior art induction magnetometers but are improved by using several smaller diameter cores instead of a single larger diameter core. Each smaller diameter core has an increased length-to-diameter ratio which increases the apparent permeability of the cores.
The reduction in core cross-sectional area is compensated for by having multiple cores. Spreading the coil windings over several cores, instead of just one, allows for smaller circumference windings over the small diameter cores, resulting in less total wire length being required which reduces noise and weight. Multiple smaller coils with fewer windings each also reduces inductance and allows for increased bandwidth.
The configuration of the individual elemental induction magnetometers in a cube arrangement allows for a very compact package, whose symmetry and hollow aspect permits the incorporation of a calibration field source in the center of the package, thus taking up no additional space and allowing for a permanent calibration system which is easy to use and can be used in flight.
Other embodiments of the present invention provide:
The novel features of the induction magnetometer are:
A prototype is developed and beta tests have been successful on a small scale.
US Patent 7,375,529 – Induction Magnetometer
This technology is available for licensing.
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