Systems and methods for determining strength of cylindrical structures by internal pressure loading

1. An apparatus, comprising:

a mandrel;

an expansion cylinder, comprising:

opposite first and second ends;

an inner circumferential surface extending between the ends and characterized by an inner diameter, the inner circumferential surface defining a hollow cavity;

an outer circumferential surface extending between the ends and characterized by an outer diameter that is greater than the inner diameter;

a plurality of slots extending from the inner circumferential surface to the outer circumferential surface and latitudinally oriented between the ends, wherein the slots are characterized by an arrangement selected from:

a plurality of curved lines;

a zigzag pattern; and

an expanding web; and

one or more base plates configured to engage one of the ends of the expansion cylinder; and

one or more sensors,

wherein the one or more sensors are configured to detect one or more indicia of a structural failure of a test cylinder,

wherein at least one of the one or more sensors is configured for positioning along the outer circumferential surface of the test cylinder, and

wherein the mandrel is physically configured to engage the expansion cylinder along the inner circumferential surface thereof for causing expansion thereof.

2. The apparatus as recited in claim 1 , further comprising a test cylinder, the test cylinder comprising:

an inner circumferential surface characterized by an inner diameter; and

an outer circumferential surface characterized by an outer diameter;

wherein the inner diameter of the test cylinder is greater than the outer diameter of the expansion cylinder, and

wherein the expansion cylinder is positioned inside the inner circumferential surface of the test cylinder.

3. The apparatus as recited in claim 1 , wherein each of the slots extends from the inner circumferential surface of the expansion cylinder to the outer circumferential surface of the expansion cylinder.

4. The apparatus as recited in claim 1 , wherein the expansion cylinder comprises one or more of titanium and a titanium alloy.

5. The apparatus as recited in claim 1 , wherein the mandrel has an outer periphery characterized by a substantially conical shape,

wherein the mandrel is characterized by a taper angle θ, and

wherein θ is a value in a range from about 15° to about 25°.

6. The apparatus as recited in claim 1 , wherein each of the slots is configured to expand along a longitudinal direction of the expansion cylinder.

7. The apparatus as recited in claim 1 , further comprising a mechanism coupled to the mandrel, the mechanism being configured to apply a force to the mandrel in a direction substantially parallel to a central axis of the expansion cylinder, and

wherein the force comprises one or more of a gravimetric force, a magnetic force, and an electrostatic force.

8. The apparatus as recited in claim 1 , wherein the mandrel comprises a material selected from a group consisting of: steel; titanium; aluminum; steel alloy; titanium alloy and aluminum alloy.

9. The apparatus as recited in claim 1 , wherein the one or more indicia of the structural failure comprise an increase in one or more of the inner diameter of the test cylinder and the outer diameter of the test cylinder.

10. The apparatus as recited in claim 9 , wherein the increase in one or more of the inner diameter of the test cylinder and the outer diameter of the test cylinder is in a range from about 1.5% to about 2%.

11. The apparatus as recited in claim 9 , the one or more indicia of the structural failure further comprising at least one of:

a rapid decrease in an amount of force required to push the mandrel through the hollow cavity;

an amount of strain exerted on the test cylinder; and

a displacement of the mandrel.

12. An apparatus, comprising:

a mandrel;

an expansion cylinder, comprising:

opposite first and second ends;

an inner circumferential surface extending between the ends and characterized by an inner diameter, the inner circumferential surface defining a hollow cavity;

an outer circumferential surface extending between the ends and characterized by an outer diameter that is greater than the inner diameter; and

a plurality of slots extending from the inner circumferential surface to the outer circumferential surface and latitudinally oriented between the ends; and

one or more base plates configured to engage one of the ends of the expansion cylinder; and

a liner configured for positioning on an outside of the outer circumferential surface of the expansion cylinder, and

wherein the mandrel is physically configured to engage the expansion cylinder along the inner circumferential surface thereof for causing expansion thereof.

13. The apparatus as recited in claim 12 , wherein the liner comprises a material selected from a group consisting of: steel; titanium; aluminum; steel alloy; titanium alloy and aluminum alloy.

14. A method, comprising:

arranging an expansion cylinder inside a test cylinder;

arranging a mandrel inside the expansion cylinder;

applying a force to the mandrel for exerting a radial force on the expansion cylinder; and

detecting one or more indicia of a structural failure of the test cylinder, wherein the one or more indicia of the structural failure comprise an increase in one or more of an inner diameter of the test cylinder and an outer diameter of the test cylinder.

15. The method as recited in claim 14 , wherein the detecting one or more indicia of a structural failure of the test cylinder further comprises one or more of:

detecting a rapid decrease in an amount of force required to push the mandrel through a hollow cavity of the expansion cylinder;

detecting an amount of strain exerted on the test cylinder; and

detecting a displacement of the mandrel.

16. The method as recited in claim 14 , wherein applying the force to the mandrel urges the mandrel through a hollow cavity in the expansion cylinder along a central axis of the expansion cylinder, and

wherein the force comprises one or more of a gravimetric force, a magnetic force, and an electrostatic force.

17. The method as recited in claim 14 , further comprising positioning a liner on an outside of an outer circumferential surface of the expansion cylinder, wherein the liner is configured to facilitate a substantially uniform increase in a circumference of the expansion cylinder as the mandrel moves through a hollow cavity thereof.

18. The method as recited in claim 14 , further comprising applying a lubricant to the mandrel.

19. The method as recited in claim 14 , further comprising: positioning one or more sensors configured to detect the one or more indicia of the structural failure along an outer circumferential surface of the test cylinder.