IP Library Granted Patent US 6,957,576
Granted Patent B2
US 6,957,576 · App. 10/618,328 · Granted Oct 25, 2005

Subterranean well pressure and temperature measurement

Assignee: Halliburton Energy Services, Inc.
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Quick Facts
Patent No.
US 6,957,576
App. No.
10/618,328
Granted
Oct 25, 2005
Kind
B2
Abstract

A well pressure and temperature measurement system and method are provided. In a described embodiment, a sensor system includes multiple strain sensors attached to a structure which changes dimensionally in response to well pressure and temperature changes. The strain sensors may be fiber optic sensors. The structure may be tubular and the strain sensors may detect axial and hoop strains in the structure.

Claims (91)

1. A subterranean well sensor system, comprising:

a structure in which strain is induced in response to a pressure differential in the well; approximately atmospheric pressure being applied to the structure in the well; and

first and second strain sensors attached to the structure and detecting strain in the structure when the pressure differential exists in the well, the first strain sensor detecting a first strain in a first direction in the structure, and the second strain sensor detecting a second strain in a second direction in the structure.

2. The sensor system according to claim 1 , wherein a predetermined mathematical relationship exists between the pressure differential, the first strain and the second strain.

3. The sensor system according to claim 1 , wherein strain is induced in the structure in response to a change in temperature in the well, and wherein at least one of the first and second strains includes strain induced in the structure due to the temperature change.

4. The sensor system according to claim 3 , wherein each of the first and second strains includes strain induced in the structure due to the temperature change.

5. The sensor system according to claim 1 , wherein each of the first and second strains includes strain induced in the structure due to the pressure differential.

6. The sensor system according to claim 1 , wherein only one of the first and second strains includes strain induced in the structure due to the pressure differential.

7. The sensor system according to claim 1 , wherein the structure includes a hollow cylinder, and wherein the first strain sensor detects axial strain in the cylinder and the second strain sensor detects hoop strain in the cylinder induced by the pressure differential.

8. The sensor system according to claim 7 , wherein the first and second strain sensors are each centered at approximately a same longitudinal position on the cylinder, and the first and second sensors are radially offset with respect to each other by approximately 180°.

9. The sensor system according to claim 7 , wherein each of the first and second strain sensors detects strain in the cylinder induced by a temperature change in the well.

10. The sensor system according to claim 9 , wherein each of the first and second strains includes strain induced in the cylinder by the pressure differential and by the temperature change.

11. The sensor system according to claim 10 , wherein a predetermined mathematical relationship exists between the pressure differential and the first and second strains, so that the pressure differential may be calculated when the first and second strains are known.

12. The sensor system according to claim 7 , wherein the pressure differential exists between an interior and an exterior of the cylinder.

13. A subterranean well sensor system, comprising:

a structure in which strain is induced in response to a pressure differential in the well; and

first and second strain sensors attached to the structure and detecting strain in the structure when the pressure differential exists in the well, the first strain sensor detecting a first strain in a first direction in the structure, and the second strain sensor detecting a second strain in a second direction in the structure,

wherein the structure includes a hollow cylinder, wherein the first strain sensor detects axial strain in the cylinder and the second strain sensor detects hoop strain in the cylinder induced by the pressure differential, wherein the pressure differential exists between an interior and exterior of the cylinder, and wherein well pressure is applied to the interior of the cylinder and approximately atmospheric pressure is applied to the exterior of the cylinder.

14. The sensor system according to claim 1 , wherein the structure includes a pressure responsive membrane, and wherein each of the first and second strain sensors detects strain in the membrane induced by the pressure differential.

15. The sensor system according to claim 14 , wherein each of the first and second strain sensors detects strain in the membrane induced by a temperature change in the well.

16. The sensor system according to claim 15 , wherein each of the first and second strains includes strain induced in the cylinder by the pressure differential and by the temperature change.

17. The sensor system according to claim 16 , wherein a predetermined mathematical relationship exists between the pressure differential and the first and second strains, so that the pressure differential may be calculated when the first and second strains are known.

18. The sensor system according to claim 14 , wherein the pressure differential exists between opposite sides of the membrane.

19. The sensor system according to claim 18 , wherein well pressure is applied to one side of the membrane and approximately atmospheric pressure is applied to the other side of the membrane.

20. The sensor system according to claim 1 , wherein the structure includes first and second portions, and wherein the first strain sensor detects strain in the first portion and the second strain sensor detects strain in the second portion.

21. The sensor system according to claim 20 , wherein the pressure differential induces strain in the first portion, but the pressure differential does not induce strain in the second portion.

22. The sensor system according to claim 20 , wherein each of the first and second strain sensors detects strain in the structure induced by a temperature change in the well.

23. The sensor system according to claim 22 , wherein the first strain includes strain induced in the structure by the pressure differential and by the temperature change, but the second strain does not include strain induced in the structure by the pressure differential.

24. The sensor system according to claim 23 , wherein a predetermined mathematical relationship exists between the pressure differential and the first and second strains, so that the pressure differential may be calculated when the first and second strains are known.

25. The sensor system according to claim 20 , wherein the pressure differential exists between an interior and an exterior of the structure.

26. The sensor system according to claim 25 , wherein well pressure is applied to the interior of the structure and approximately atmospheric pressure is applied to the exterior of the structure.

27. The sensor system according to claim 1 , wherein at least one of the first and second strain sensors is a fiber optic sensor.

28. The sensor system according to claim 27 , wherein the fiber optic sensor is an interferometric fiber optic sensor.

29. The sensor system according to claim 27 , wherein the fiber optic sensor comprises a fiber Bragg grating.

30. The sensor system according to claim 27 , wherein the fiber optic sensor comprises a pi-shifted fiber Bragg grating.

31. The sensor system according to claim 27 , wherein the fiber optic sensor comprises a long period grating.

32. The sensor system according to claim 27 , wherein the fiber optic sensor comprises a fiber Bragg laser.

33. The sensor system according to claim 27 , wherein the fiber optic sensor comprises a selected one of an intrinsic and extrinsic Fabry-Perot interferometer.

34. The sensor system according to claim 27 , wherein the fiber optic sensor comprises a Michelson interferometer.

35. The sensor system according to claim 27 , wherein the fiber optic sensor comprises a Mach-Zehnder interferometer.

36. The sensor system according to claim 27 , wherein the fiber optic sensor comprises a co-located fiber Bragg grating and pi-shifted fiber Bragg grating.

37. The sensor system according to claim 27 , wherein the fiber optic sensor comprises a fiber ring resonator.

38. A subterranean well sensor system, comprising:

a generally tubular structure having a pressure differential applied across its inner and outer surfaces, the pressure differential existing between well pressure applied to one of the inner and outer surfaces and a second predetermined pressure applied to the other of the inner and outer surfaces; and

first and second strain sensors, each of the first and second strain sensors detecting strain in the structure induced by the pressure differential and strain induced in the structure by a temperature change in the well, the first strain sensor detecting strain in the structure in a first direction, and the second strain sensor detecting strain in the structure in a second direction different from the first direction,

wherein the structure includes a hollow cylinder, wherein the first strain sensor detects axial strain in the cylinder, and wherein the second strain sensor detects hoop strain in the cylinder.

39. The sensor system according to claim 38 , wherein the first and second strain sensors are each centered at approximately a same longitudinal position on the cylinder, and the first and second sensors are radially offset with respect to each other by approximately 180°.

40. A subterranean well sensor system, comprising:

a hollow cylindrical structure having a pressure differential applied across its inner and outer surfaces, the pressure differential existing between well pressure applied to one of the inner and outer surfaces and a second predetermined pressure applied to the other of the inner and outer surfaces; and

first and second strain sensors, each of the first and second strain sensors detecting strain in the structure induced by the pressure differential and strain induced in the structure by a temperature change in the well, the first strain sensor detecting strain in the structure in a first direction, and the second strain sensor detecting strain in the structure in a second direction different from the first direction,

wherein the second predetermined pressure is contained within an annular space between the structure and an outer housing.

41. The sensor system according to claim 40 , wherein the first and second strain sensors are positioned in the annular space and are attached to the outer surface of the structure.

42. A subterranean well sensor system, comprising:

a generally tubular structure having a pressure differential applied across its inner and outer surfaces, the pressure differential existing between well pressure applied to one of the inner and outer surfaces and a second predetermined pressure applied to the other of the inner and outer surfaces; and

first and second strain sensors, each of the first and second strain sensors detecting strain in the structure induced by the pressure differential and strain induced in the structure by a temperature change in the well, the first strain sensor detecting strain in the structure in a first direction, and the second strain sensor detecting strain in the structure in a second direction different from the first direction,

wherein the second predetermined pressure is approximately atmospheric pressure.

43. The sensor system according to claim 38 , wherein at least one of the first and second strain sensors is a fiber optic sensor.

44. The sensor system according to claim 43 , wherein the fiber optic sensor is an interferometric fiber optic sensor.

45. The sensor system according to claim 43 , wherein the fiber optic sensor comprises a fiber Bragg grating.

46. The sensor system according to claim 43 , wherein the fiber optic sensor comprises a pi-shifted fiber Bragg grating.

47. The sensor system according to claim 43 , wherein the fiber optic sensor comprises a long period grating.

48. The sensor system according to claim 43 , wherein the fiber optic sensor comprises a fiber Bragg laser.

49. The sensor system according to claim 43 , wherein the fiber optic sensor comprises a selected one of an intrinsic and extrinsic Fabry-Perot interferometer.

50. The sensor system according to claim 43 , wherein the fiber optic sensor comprises a Michelson interferometer.

51. The sensor system according to claim 43 , wherein the fiber optic sensor comprises a Mach-Zehnder interferometer.

52. The sensor system according to claim 43 , wherein the fiber optic sensor comprises a co-located fiber Bragg grating and pi-shifted fiber Bragg grating.

53. The sensor system according to claim 43 , wherein the fiber optic sensor comprises a fiber ring resonator.

54. A method of measuring pressure in a subterranean well, the method comprising the steps of:

applying a pressure differential across a structure positioned in the well, approximately atmospheric pressure being applied to the structure within the well;

detecting a first strain in the structure in a first direction using a first strain sensor;

detecting a second strain different from the first strain in the structure in a second direction using a second strain sensor; and

calculating the pressure differential using a predetermined mathematical relationship between the pressure differential and the first and second strains.

55. The method according to claim 54 , further comprising the step of applying a change in temperature to the structure in the well, and

wherein each of the first and second strains includes strain induced by the temperature change.

56. The method according to claim 55 , wherein each of the first and second strains includes the same strain induced by the temperature change.

57. The method according to claim 55 , wherein the calculating step further comprises subtracting strain induced by the temperature change from the first and second strains.

58. The method according to claim 54 , wherein in the first and second strain detecting steps, the first and second directions are orthogonal to each other.

59. The method according to claim 54 , wherein in the pressure differential applying step, the structure includes a generally tubular portion and the pressure differential is applied between inner and outer surfaces of the tubular portion.

60. The method according to claim 59 , wherein in the first strain detecting step, the first strain is an axial strain in the tubular portion, and

wherein in the second strain detecting step, the second strain is a hoop strain in the tubular portion.

61. The method according to claim 54 , wherein in the first and second strain detecting steps, at least one of the first and second strain sensors is a fiber optic sensor.

62. A method of measuring pressure in a subterranean well, the method comprising the steps of:

applying a pressure differential across a structure positioned in the well, approximately atmospheric pressure being applied to the structure within the well;

applying a temperature change to the structure in the well;

detecting a first strain in the structure induced by the pressure differential and the temperature change using a first strain sensor; and

detecting a second strain different from the first strain in the structure induced by the pressure differential and the temperature change using a second strain sensor, a predetermined mathematical relationship existing between the pressure differential and the first and second strains.

63. The method according to claim 62 , wherein each of the first and second strains includes the same strain induced by the temperature change.

64. The method according to claim 62 , wherein in the first strain detecting step, the first strain sensor is attached to a generally tubular portion of the structure.

65. The method according to claim 64 , wherein in the second strain detecting step, the second strain sensor is attached to the tubular portion of the structure.

66. The method according to claim 65 , wherein the first and second strain sensors are each centered at approximately a same longitudinal position on the tubular portion, and the first and second sensors are radially offset with respect to each other by approximately 180°.

67. The method according to claim 65 , wherein in the first and second strain detecting steps, the first strain sensor senses hoop strain in the tubular portion and the second strain sensor senses axial strain in the tubular portion.

Assignments (7)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jun 4, 2012
From: LEBLANC, MICHEL J
To: THE GOVERNMENT OF THE UNITED STATES OF AMERICA, AS REPRESENTED BY THE SECRETARY OF THE NAVY
Reel/Frame 028310/0323 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded May 16, 2012
From: TODD, MICHAEL D
To: THE GOVERNMENT OF THE UNITED STATES OF AMERICA, AS REPRESENTED BY THE SECRETARY OF THE NAVY
Reel/Frame 028215/0230 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Sep 5, 2007
From: HALLIBURTON ENERGY SERVICES, INC.
To: WELLDYNAMICS, B.V.
Reel/Frame 019781/0406 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jan 18, 2007
From: HALLIBURTON ENERGY SERVICES, INC.
To: WELLDYNAMICS, B.V.
Reel/Frame 018767/0859 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jul 11, 2003
From: DENNIS, JOHN R.
To: HALLIBURTON ENERGY SERVICES, INC.
Reel/Frame 014284/0372 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jul 11, 2003
From: SKINNER, NEAL G.
To: HALLIBURTON ENERGY SERVICES INC.
Reel/Frame 014284/0375 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jul 11, 2003
From: JOHNSON, GREGG
To: HALLIBURTON ENERGY SERVICES, INC.
Reel/Frame 014284/0383 →
Priority Claims (1)
WO PCT/US02/23272 · Jul 23, 2002 · international
Continuity (1)
Related Publication 20040016295A1 · Jan 29, 2004