Testing cement shear bond strength at reservoir conditions

1. A method for testing shear bond strength of cement with a sample under downhole conditions, the method comprising:

forming a bonding surface of the sample oriented at an angle between 50 and 70 degrees from a plane perpendicular to a longitudinal axis of the sample;

forming a composite sample by bonding the cement to the sample with the cement in contact with the bonding surface of the sample;

installing the composite sample in a cell casing,

installing the cell casing in a tri-axial testing machine;

applying a first pressure to the composite sample, wherein the first pressure is greater than an environmental pressure;

applying an axial pressure to the cell casing and sample that is greater than the first pressure;

measuring a wave velocity of the composite sample using a first acoustic transducer and a second acoustic transducer;

measuring an acoustic emission emitted by the composite sample using a third acoustic transducer; and

identifying a failure of the composite sample based on the measured acoustic emission and the measured velocity.

2. The method of claim 1 , further comprising coating the sample with a drilling fluid before forming the composite sample.

3. The method of claim 1 , wherein measuring the wave velocity of the composite sample comprises measuring a p wave velocity or an s wave velocity of the composite sample using the first acoustic transducer and the second acoustic transducer.

4. The method of claim 3 , wherein measuring the acoustic emission emitted by the composite sample comprises measuring an intensity, frequency, or dispersion of acoustic waves emitted by the composite sample using the third acoustic transducer.

5. The method of claim 4 , wherein identifying the failure of the composite sample based on the measured acoustic emission and the measured velocity comprises identifying an initial compaction phase of axial compression by detecting an increase in the measured acoustic emissions relative to an ambient condition and an increase in the measured p wave velocity, the measured s wave velocity, or both.

6. The method of claim 4 , wherein identifying the failure of the composite sample based on the measured acoustic emission and the measured velocity comprises identifying a quasi-linear elastic phase of axial compression by detecting a decrease in the measured acoustic emissions and a decrease in the measured wave velocity.

7. The method of claim 4 , wherein identifying the failure of the composite sample based on the measured acoustic emission and the measured velocity comprises identifying a micro-crack initiation and extension phase of axial compression by detecting an increase in the measured acoustic emissions.

8. The method of claim 4 , wherein identifying the failure of the composite sample based on the measured acoustic emission and the measured velocity comprises identifying a crack coalescence and dynamic failure phase of axial compression by detecting an increase in the measured acoustic emissions and a decrease in the measured p wave velocity and the measured s wave velocity.

9. The method of claim 4 , wherein identifying the failure of the composite sample based on the measured acoustic emission and the measured velocity comprises identifying a frictional sliding phase by detecting a decrease in a load bearing capacity of the composite sample, an increase in the measured acoustic emissions, or both.

10. The method of claim 4 , further comprising measuring a strain of the composite sample using a strain gauge located on the composite sample.

11. The method of claim 4 , further comprising determining the shear bond strength of the cement.

12. The method of claim 3 , wherein forming the composite sample comprises:

trimming the lower end surface to be flat and perpendicular to the longitudinal axis;

trimming the composite sample to achieve a length of the composite sample to a diameter of the composite sample ratio greater than or equal to 2; and

trimming the composite sample to be 40-60% cement and 40-60% sample.

13. The method of claim 1 , wherein identifying the failure of the composite sample based on the measured acoustic emission and the measured velocity comprises identifying the failure based on a magnitude or a rate of change of the measured velocity as a function of an axial stress of the composite sample.

14. The method of claim 1 , wherein identifying the failure of the composite sample based on the measured acoustic emission and the measured velocity comprises identifying the failure based on an intensity of the measured acoustic emissions and a rate of change of measured velocity.

15. The method of claim 1 , further comprising switching between measuring the wave velocity of the composite sample and measuring the acoustic emission emitted by the composite sample.

16. The method of claim 1 , further comprising determining a curve fit of the measured wave velocity as a function of axial stress, wherein identifying the failure of the composite sample based on the measured acoustic emission and the measured velocity comprises identifying the failure of the composite sample based on the determined curve fit of the wave velocity.

17. A system for testing a composite sample formed of a cement bonded with a primary sample to identify a shear bond strength of the cement with the primary sample, the system comprising:

a first acoustic transducer;

a second acoustic transducer;

a third acoustic transducer;

a strain gauge; and

a computer electrically connected to the first, second, and third acoustic transducers and the strain gauge;

wherein the first acoustic transducer and the second acoustic transducer are configured to measure a p wave velocity or an s wave velocity;

wherein the third acoustic transducer is passive and configured to measure an acoustic emission emitted by the composite sample using a third acoustic transducer; and

wherein the computer is operable to identify a failure of the composite sample based on the measured acoustic emission and the measured p or s wave velocity.

18. The system of claim 17 , further comprising:

a first end cap attachable to the composite sample with the first acoustic transducer mounted on the first end cap; and

a second end cap attachable to the composite sample with the second acoustic transducer mounted on the second end cap.

19. The system of claim 17 , wherein the first acoustic transducer is configured to transmit a signal and the second acoustic transducer is configured to receive the signal.

20. The system of claim 19 , further comprising a cylindrical casing, wherein the strain gauge is located on an outer surface of the cylindrical casing, and wherein the third acoustic transducer is mounted on the first end cap.

21. The system of claim 17 , wherein the computer is operable to identify the failure based on a magnitude or a rate of change of at least one of the measured p wave velocity and the measured s wave velocity as a function of an axial stress of the composite sample.

22. The system of claim 17 , wherein the computer is operable to identify the failure based on an intensity of the measured acoustic emissions and a rate of change of at least one of the measured p wave velocity and the measured s wave velocity.

23. The system of claim 17 , wherein the computer is further operable to switch between measuring the wave velocities of the composite sample and measuring the acoustic emission emitted by the composite sample.

24. The system of claim 17 , wherein the computer is further operable to determine a curve fit of at least one of the measured p wave velocity and the measured s wave velocity as a function of axial stress, wherein the computer is operable to identify the failure of the composite sample based on the determined curve fit of the at least one of the measured p wave velocity and the measured s wave velocity.

25. The system of claim 17 , wherein the computer is operable to identify the failure of the composite sample as an initial compaction phase of axial compression by detecting an increase in the measured acoustic emissions relative to an ambient condition and an increase in the measured p wave velocity, the measured s wave velocity, or both.

26. The system of claim 17 , wherein the computer is operable to identify the failure of the composite sample as a quasi-linear elastic phase of axial compression by detecting a decrease in the measured acoustic emissions and a decrease in at least one of the measured p wave velocity and the measured s wave velocity.