Airborne locator of an underground object

Patent metadata

Field	Value
Publication number	US-11480704-B2
Application number	US-202017133220-A
Country	US
Kind code	B2
Filing date	Dec 23, 2020
Priority date	Jul 17, 2014
Publication date	Oct 25, 2022
Grant date	Oct 25, 2022

Abstract

A system for tracking a below-ground transmitter from an aerial receiver. The receiver has an antenna assembly, a processor, and a propulsion system. The antenna assembly detects the magnetic field from an underground transmitter and generates an antenna signal. The processor is programmed to receive the antenna signal and generate a command signal, which moves the receiver to a position above the transmitter. Once in the desired position, which may be a reference plane at a fixed elevation, the antenna assembly measures the magnetic field to determine the location of the drill bit along borepath.

First claim

The invention claimed is:

1. A device comprising:
a frame having a top and a bottom;
an antenna assembly attached to the frame; and
a propulsion system supported by the frame;
a positional sensor configured to determine an absolute position of the frame;
a processor configured to determine a distance between the antenna assembly and an underground dipole field transmitter based on the signal strength and magnetic field orientation emanating from the underground dipole field transmitter; and
wherein the processor is configured to determine an absolute position of the underground dipole field transmitter using the determined absolute position of the frame and the distance between the antenna assembly and the underground dipole field transmitter; and
wherein the propulsion system moves the frame to a position at a null location in the field in response to signal strength and magnetic field orientation measurements taken by the antenna assembly.

2. A system comprising:
dipole magnetic field transmitter, in which a dipole magnetic field is emitted from a downhole tool at an underground location; and
the device of claim 1 .

3. The device of claim 1 in which the processor is configured to direct the self-propelled autonomous receiver to move along a reference plane to the null in a dipole magnetic field, wherein the reference plane is at a constant elevation over mean sea level.

4. The device of claim 1 further comprising an altimeter to determine an altitude of the frame above ground level, wherein the processor is configured to determine a depth of the dipole field transmitter below ground using the altitude of the frame and the distance between the antenna assembly and the dipole field transmitter.

5. The device of claim 1 wherein the processor is configured to maintain the frame at the null location in the field within a reference plane as the underground dipole magnetic field transmitter moves.

6. The device of claim 5 in which the reference plane is at a constant elevation above mean sea level.

7. The device of claim 1 wherein the propulsion system comprises a helicopter rotor.

8. The device of claim 1 wherein the antenna assembly is attached to the bottom of the frame.

9. A method comprising:
providing an antenna assembly and a propulsion system capable of lifting the antenna assembly off the ground;
transmitting a magnetic field from an underground field transmitter;
engaging the propulsion system to lift the antenna assembly into the air;
detecting the magnetic field using the antenna assembly;
determining an absolute position of the antenna assembly;
moving the antenna assembly with the propulsion system to a position within the magnetic field indicative of a null in the field;
measuring the signal strength of the magnetic field and the orientation of the magnetic field using the antenna assembly to determine a position of the underground field transmitter relative to the antenna assembly; and
with the position of the underground field transmitter relative to the antenna assembly and the absolute position of the antenna assembly, determining the absolute position of the underground field transmitter.

10. The method of claim 9 further comprising:
maintaining the antenna assembly at a predetermined reference elevation relative to mean sea level;
wherein the step of moving the antenna assembly to the position in the magnetic field indicative of the null in the field occurs substantially at the predetermined reference elevation.

11. The method of claim 9 further comprising:
detecting an altitude of the antenna assembly above a ground surface; and
using the altitude of the antenna assembly and the relative position of the underground field transmitter relative to the antenna assembly, determining an actual depth of the underground transmitter.

12. The method of claim 9 further comprising:
moving the underground field transmitter through an underground environment; and
as the underground field transmitter moves, maintaining the antenna assembly within the null in the field.

13. The method of claim 12 further comprising:
as the underground field transmitter moves through the underground environment, mapping a path of the transmitter.

14. The method of claim 13 further comprising:
determining a planned path for the underground field transmitter; and
comparing the planned path to the path of the transmitter mapped as the underground field transmitter moves through the underground environment.

15. The method of claim 9 in which the null is characterized as a front null, the antenna assembly is characterized as a first antenna assembly and the propulsion system is characterized as a first propulsion system, further comprising:
providing a second antenna assembly and a second propulsion system capable of lifting the second antenna assembly off the ground;
engaging the second propulsion system to lift the second antenna assembly into the air;
detecting the magnetic field using the second antenna assembly;
moving the second antenna assembly with the second propulsion system to a position within the magnetic field indicative of a rear null in the field; and
measuring the signal strength of the magnetic field and the orientation of the magnetic field using the second antenna assembly to determine a position of the underground field transmitter relative to the antenna assembly.

16. The method of claim 9 in which the antenna assembly is characterized as a first antenna assembly, the propulsion system is characterized as a first propulsion system, and the null is characterized as a first null and further comprising:
providing a second antenna assembly and a second propulsion system capable of lifting the antenna assembly off the ground;
engaging the second propulsion system to lift the second antenna assembly into the air;
detecting the magnetic field using the second antenna assembly;
determining an absolute position of the second antenna assembly; and
moving the second antenna assembly with the second propulsion system to a position within the magnetic field indicative of a second null in the field.

17. The method of claim 16 further comprising:
determining a distance between the first antenna assembly and the second antenna assembly when the first antenna assembly is at the first null and the second antenna assembly is at the second null; and
from the determined distance, determining a position of the underground field transmitter.

18. The method of claim 16 further comprising:
moving the underground field transmitter; and
while the underground field transmitter is moving, maintaining the first antenna assembly at the first null and maintaining the second antenna assembly at the second null.

Assignees

• Charles Machine Works

Inventors

• Cole Scott B
• Bailey Brian K
• Morse Larry G

Classifications

• E21B47/002

  by visual inspection · CPC title

• E21B47/092

  by detecting magnetic anomalies · CPC title

• G01V3/165

  operating with magnetic or electric fields produced or modified by the object or by the detecting device (with electromagnetic waves G01V3/17) · CPC title

• E21B47/024

  of devices in the borehole (determining slope or direction of the borehole E21B47/022) · CPC title

• G01V3/16 Primary

  specially adapted for use from aircraft (G01V3/165 - G01V3/175 take precedence) · CPC title