Survey apparatus and method employing rate-of-turn and free gyroscopes

• US 4,297,790 A
• Filed: 06/25/1979
• Issued: 11/03/1981
• Est. Priority Date: 07/17/1978
• Status: Expired due to Term

• Current Assignee: Applied Technologies Associates, Inc.
• Original Assignee: Applied Technologies Associates, Inc.
• Inventors: Van Steenwyk, Donald H., Ott, Paul W., Cash, John R.
• Primary Examiner(s): Stephan, Steven L.
• Application Number:
  US06/051,893
• Time in Patent Office: 862 Days
• Field of Search: 33/304, 33/312, 33/313, 33/321, 33/323, 33/324
• US Class Current: 33/313
• CPC Class Codes: E21B 47/022 of the borehole, e.g. using geomagnetism
• CPC Class Codes: G01C 19/38 with north-seeking action by other than magnetic means, e.g. gyrocompasses using earth's rotation

Abstract

Survey apparatus and method employs a free gyroscope for fast determination of azimuth, free gyroscope alignment being periodically corrected by a rate gyroscope which is periodically rotated for accurate azimuth determination. An accelerometer is also usable in conjunction with the gyroscopes for tilt determination. More generally, method and means is provided for calibrating (initially or periodically) an angle or position reference device.

Claims

1. In apparatus for determining azimuth, the combination that comprises

(a) a rate-of-turn gyroscope including a first rotor having a spin axis,

(b) support means to support the gyroscope for lengthwise travel along another axis and to rotate about said other axis,

(c) said gyroscope having first means for producing an output which varies as a function of azimuth orientation of the gyroscope relative to the earth'"'"'s spin axis, and

(d) a free gyroscope operatively carried for movement along said other axis with said rate-of-turn gyroscope, said free gyroscope including a second rotor having a spin axis subject to re-orientation,

(e) said free gyroscope also having means for producing an output which varies as a function of azimuth orientation of the free gyroscope,

(f) other means responsive to the output of the rate-of-turn gyroscope to effect said re-orientation of the free gyroscope spin axis,

(g) control means connected with said other means to periodically cause said other means to effect said alignment, while said travel is effectively interrupted, and

(h) said support means supporting both gyroscopes for travel in a bore hole.

2. The combination of claim 1 wherein said free gyroscope has a frame carried by said support means to rotate about said other axis.

3. The combination of claim 2 wherein said support means comprises well tubing operable to rotate said rate-of-turn gyroscope about said other axis in response to well tubing rotation.

4. The combination of claim 2 wherein said support means includes a motor operatively connected with said gyroscopes to rotate them about said other axis.

5. The combination of claim 4 wherein said support means includes a housing supporting and containing said motor and said gyroscopes.

6. The combination of claim 4 wherein the rate-of-turn gyroscope includes a carrier frame rotatable by the motor, and a sub-frame, the first rotor carried by the sub-frame, the free gyroscope also carried by the carrier frame.

7. The combination of claim 1 including an inclinometer operatively carried for movement along said other axis with said gyroscopes.

8. The combination of claim 6 including an inclinometer carried by said carrier frame.

9. The combination of claim 1 wherein said support means includes a housing containing said gryoscopes.

10. The combination of claim 7 wherein said inclinometer comprises an accelerometer.

11. The combination of claim 8 wherein said inclinometer comprises an accelerometer.

12. The combination of claim 1 wherein the free gyroscope has two sets of gimbals, and caging means to cage and uncage one set of said gimbals, at times during which the spin axis of the free gyroscope is re-oriented.

13. The combination of claim 1 wherein said other means includes a drive operatively connected between the rate-of-turn gyroscope and the free gyroscope to be responsive to the output of the rate-of-turn gyroscope for periodically re-orienting the spin axis of the free gyroscope.

14. The combination of claim 1 including a housing independently supporting both the free gyroscope and the rate-of-turn gyroscope.

15. The combination of claim 1 wherein said support means includes a cable suspending a housing for said gyroscopes.

16. The combination of claim 5 including structure suspending said housing for running in a well.

17. In a survey method which employs instrumentation embodying both rate-of-turn and free gyroscopes, the steps that include

(a) traveling both said gyroscopes together along a travel direction,

(b) operating the free gyroscope to produce an output indicative of azimuth orientation of the instrumentation, and

(c) operating the rate-of-turn gyroscope to produce an output which is indicative of azimuth orientation of the instrumentation,

(d) periodically using the output of the rate-of-turn gyroscope to re-orient the free gyroscope, while said traveling of both gyroscopes along said direction is substantially interrupted.

(e) and employing a cable to suspend said gyroscopes for said travel in a bore hole.

18. The method of claim 17 wherein said free gyroscope has a spin axis, and wherein said (d) step includes re-orienting the spin axis of the free gyroscope relative to North.

19. The method of claim 17 including the step of caging the free gyroscope during said (d) step.

20. In apparatus for determining azimuth, the combination comprising

(a) an angle reference device carried for movement along a travel axis in a bore hole, said device having a calibratable component,

(b) first means for measuring angular rate and having output for effecting calibration of said component, and

(c) control means operatively connected with said first means to cause said first means to periodically effect said callibration of said component.

21. The apparatus of claim 20 wherein said first means comprises a rate-of-turn gyroscope.

22. The apparatus of claim 20 wherein said device comprises a free gyroscope.

23. The apparatus of claim 20 wherein said device comprises a rate gyroscope.

24. The apparatus of claim 20 wherein said device comprises a rate integrating gyroscope.

25. The apparatus of claim 20 wherein said device comprises an inertial reference system.

26. The apparatus of claim 20 wherein said device comprises an angular accelerometer.

27. The apparatus of claim 20 wherein said device comprises a linear accelerometer.

28. The apparatus of claim 20 wherein said device comprises an inclinometer.

29. The apparatus of claim 20 wherein said device comprises a magnetometer.

30. In a survey method which employs an angle reference device and first means for measuring angular rate and having an output for effecting calibration of said device, the steps that include

(a) traveling both said device and first means together along a travel direction in a bore hole;

(b) operating said device to produce an output indicative of azimuth orientation; and

(c) periodically using said output of said first means to calibrate said device, while said traveling is substantially interrupted.

31. In apparatus for determining azimuth, the combination that comprises

(a) a rate-of-turn sensor,

(b) support means to support the sensor for lengthwise travel along a travel axis,

(c) said sensor having first means for producing an output which varies as a function of azimuth orientation of the sensor relative to the earth'"'"'s spin axis, and

(d) a free gyroscope operatively carried for movement along said travel axis with said sensor, said free gyroscope including a calibratable component,

(e) said free gyroscope also having means for producing an output which varies as a function of azimuth orientation of the free gyroscope,

(f) other means responsive to the output of the sensor to effect said calibration of the free gyroscope,

(g) control means connected with said other means to periodically cause said other means to effect said calibration,

(h) said support means supporting said sensor and said free gyroscope for travel in a bore hole.

32. In apparatus for determining azimuth, the combination that comprises

(a) a rate-of-turn gyroscope including a first rotor having a spin axis,

(b) support means to support the gyroscope for lengthwise travel along another axis and to rotate about said other axis,

(c) said gyroscope having first means for producing an output which varies as a function of azimuth orientation of the gyroscope relative to the earth'"'"'s spin axis, and

(d) a free gyroscope operatively carried for movement along said other axis with said rate-of-turn gyroscope, said free gyroscope including a calibratable component,

(e) said free gyroscope also having means for producing an output which varies as a function of azimuth orientation of the free gyroscope,

(f) other means responsive to the output of the rate-of-turn gyroscope to effect said calibration of the free gyroscope,

(g) control means connected with said other means to periodically cause said other means to effect said calibration, and

(h) said support means supporting both gyroscopes for travel in a bore hole.

33. In a survey method which employs instrumentation including a rate-of-turn sensor and a calibratable free gyroscope, the steps that include

(a) traveling said sensor and said gyroscope together along a travel direction,

(b) operating the free gyroscope to produce an output indicative of azimuth orientation of the instrumentation, and

(c) operating the sensor to produce an output which is indicative of azimuth orientation of the instrumentation, and

(d) periodically using the output of the sensor to calibrate the free gyroscope, at different locations along said travel direction,

(e) and employing a cable to suspend said sensor and said gyroscope for said travel in a bore hole.