Patent Number: 
Section: claims

1. A compression sleeve useable in a nuclear reactor, comprising:a single-piece tubular body,the tubular body having a first end and a second end,the first end shaped to surround an end of a jet pump sensing line,the second end shaped to surround a replacement line portion for the jet pump sensing line,at least one of the first and second ends being a tapered, malleable end configured to deform to provide a seal between the compression sleeve and the respective jet pump sensing line or replacement line portion,the tapered, malleable end having a first, second, and third section, the second section having an outer surface with a concave, longitudinal cross-sectional profile, the second section being between the first and third sections, the longitudinal cross-sectional profile existing along a longitudinal length of the compression sleeve. 2. The sleeve of claim 1, wherein the jet pump sensing line and the replacement line portion are in a Boiling Water Reactor (BWR). 3. The sleeve of claim 1, wherein the tapered, malleable end includes grooves on an inner surface forming a crenulated pattern configured to form a labyrinth seal with the respective jet pump sensing line or the replacement line portion. 4. The sleeve of claim 1, wherein,thicknesses of each of the first, second, and third section are not equal and are configured to permit deformation of the first, second, and third sections while substantially preventing deformation to portions of the tubular body other than the first, second, and third sections. 5. The sleeve of claim 4, whereinthe first section is closest to the tubular body and tapers continuously from the tubular body at an angle,the third section is farthest from the tubular body and tapers at about the same angle, andthe concave cross-sectional profile of the second section is continuous between the first section and third section. 6. The sleeve of claim 1, wherein the tubular body has an inner diameter of about 0.01 inches larger than an outer diameter of a connected component. 7. The sleeve of claim 1, wherein the tubular body is made of about 99% nickel, and is heat annealed at about two-thousand (2000) degrees Fahrenheit for about 15 minutes. 8. A mechanical coupling assembly for repairing a sensing line of a jet pump in a nuclear reactor, comprising:a compression sleeve including,a single-piece tubular body,the tubular body having a first end and a second end,the tubular body being malleable, heat-annealed, and about 99% nickel,the first end shaped to surround an end of a jet pump sensing line;a replacement tube, the second end shaped to surround the replacement tube,the first and second ends being tapered, malleable ends configured to deform to provide a seal between the compression sleeve and the respective jet pump sensing line and replacement tube,the tapered, malleable ends each having a first, second, and third section, the second section having an outer surface with a concave, longitudinal cross-sectional profile, the second section being between the first and third sections, the longitudinal cross-sectional profile existing along a longitudinal length of the compression sleeve;a collar configured to join the compression sleeve and at least one of the replacement tube and the end of the jet pump sensing line; andat least one compression nut configured to mate with the collar to compress and collapse the concave second section of the compression sleeve against an outer surface of at least one of the replacement tube and the end of the jet pump sensing line. 9. The mechanical coupling assembly of claim 8, wherein the replacement tube replaces a segment of the sensing line. 10. A compression sleeve used in a pipe repair within a nuclear reactor, comprising:a single-piece tubular body having a first end and a second end,wherein the tubular body is made of about 99% pure Nickel,the first end shaped to surround an end of a jet pump sensing line,the second end shaped to surround a replacement line portion for the jet pump sensing line; anda reduced-thickness, circumferential segment having an outer surface with a concave, longitudinal cross-sectional profile at each of the first and second ends to facilitate deformation of the ends when connected to one of the jet pump sensing line and the replacement line portion so as to provide a seal between the connected component and sleeve, the longitudinal cross-sectional profile existing along a longitudinal length of the compression sleeve. 11. The sleeve of claim 10, wherein one or both of the ends includes a plurality of spaced circumferential grooves on an inner surface forming a crenulated pattern configured to form a labyrinth seal with a component that is to be received therein. 12. The sleeve of claim 10, wherein each of the ends is a tapered section that forms a conical, angled seating surface at each end. 13. The sleeve of claim 12, wherein the conical, angled seating surface is at an approximately 10 degree angle with a horizontal axis of rotation of the sleeve. 14. The sleeve of claim 1, wherein the concave cross-sectional profile of the second section is configured to allow a fastening device to fit over and collapse the second section. 15. The sleeve of claim 1, wherein the second section is configured to compress and collapse against an outer surface of at least one of the replacement line portion and the end of the jet pump sensing line when a compression force is applied to the outer surface of the second section, the compression force being in a direction that is about perpendicular to the outer surface of the second section. 16. The sleeve of claim 10, wherein the reduced-thickness, circumferential segment is configured to compress and collapse against an outer surface of at least one of the replacement line portion and the jet pump sensing line.