US 7,002,349 B2 · Remote sensing electric field exploration system

Abstract

An airborne exploration system used with an aircraft for shallow and deep exploration for oil and gas, mineral deposits and aquifers. The survey system uses natural electromagnetic EM fields as an energy source. The exploration system includes a pair of aerodynamic housing pods adapted for mounting on wing tips of the aircraft. The housing pods include electric field sensors with three orthogonal electric dipoles oriented along an X, Y and Z axis. An optional third set of orthogonal electric dipoles can be mounted in the tail of the aircraft. The field sensors are electrically attached to angular motion detectors mounted inside housing pods. The motion detectors are used for compensating for errors caused by angular motion of the aircraft when in the presence of strong electric field gradients. The system also includes a total field magnetometer mounted in the aircraft. The various filtered outputs of the magnetometer are used to provide phase and amplitude references for the similarly filtered and angular motion corrected outputs of the electric field sensors. The electric field data when normalized and phase referenced against the magnetic field data provides valuable geological and geophysical information related to the subsurface flow of telluric currents.

Claims15

Dependent claims

An airborne exploration survey system for exploration of oil and gas, mineral deposits and aquifers, the survey system using natural electromagnetic fields as an energy source, the survey system mounted on an aircraft, the system comprising:

a pair of aerodynamic housing pods adapted for mounting on wing tips of the aircraft;
a pair of electric field sensors mounted on said housing pods, said field sensors including electric dipoles mounted thereon, said electric dipoles measuring electric fields in a frequency range from 0.1 Hz. to 3 Hz.;
an angular motion detector mounted inside the aircraft and connected to said electric dipoles for compensating for errors caused by angular motion of the aircraft when in the presence of strong static electric field gradients above the earth's surface;
and
a total field magnetometer mounted inside the aircraft, said magnetometer output filtered at selective frequencies in the range of 0.1 Hz to 3.0 Hz in order to receive amplitude and phase references for electric field measurements made of the same frequencies.

2 more elements

a pair of aerodynamic housing pods adapted for mounting on wing tips of the aircraft;
a pair of electric field sensors mounted on said housing pods, said field sensors including electric dipoles mounted thereon, said electric dipoles measuring electric fields in a frequency range from 0.1 Hz. to 3 Hz., said electric dipoles include a first dipole for taking data measurements in a horizontal X axis perpendicular to a length of the aircraft, a second dipole for taking data measurements in a horizontal Y axis parallel to the length of the aircraft and a third dipole for taking data measurements in a vertical Z axis perpendicular to the length of the aircraft;
a pair of angular motion detectors mounted inside said housing pods and connected to said electric dipoles for compensating for errors caused by angular motion of the aircraft when in the presence of static electric field gradients;
a magnetometer mounted inside the aircraft for measuring low frequency magnetic components of electromagnetic gradients;
and
an airborne data acquisition unit mounted in the aircraft and connected to said electric dipoles for receiving and storing electric field data measurements from said electric dipoles, said data acquisition unit also connected to said angular motion detectors for receiving and storing angular motion measurements and connected to said magnetometer for storing low frequency magnetic field data measurements.

3 more elements

at least one aerodynamic housing pod adapted for mounting on a wing tip of the aircraft;
at least one electric field sensor mounted on said housing pod, said field sensor including electric dipoles mounted thereon, said electric dipoles measuring electric fields in a frequency range from 0.1 Hz. to 3 Hz., said electric dipoles include a first dipole for taking data measurements in a horizontal X axis perpendicular to a length of the aircraft, a second dipole for taking data measurements in a horizontal Y axis parallel to the length of the aircraft and a third dipole for taking data measurements in a vertical Z axis perpendicular to the length of the aircraft;
an angular motion detector mounted inside the aircraft and connected to said electric dipoles for compensating for errors caused by angular motion of the aircraft when in the presence of strong static electric field gradients;
a magnetometer mounted inside the aircraft for measuring the magnetic components of low frequency electromagnetic fields;
an airborne data acquisition unit mounted in the aircraft and connected to said electric dipoles for receiving and storing electric field data measurements from said electric dipoles, said data acquisition unit also connected to said angular motion detector for receiving and storing angular motion measurements and connected to said magnetometer for storing low frequency magnetic field data measurements;
and
an optional ground base station synchronized with said airborne data acquisition unit, said ground base station including a magnetometer, associated recording equipment and a GPS time reference for synchronization of EM magnetic field data measurements recorded from said airborne data acquisition unit with base station data.

4 more elements

Dependencies are inferred from the claim text.

Remote sensing electric field exploration system

Life of this patent

Remote sensing electric field exploration system

Life of this patent

Abstract

Claims15