The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Aug. 04, 2015

Filed:

Sep. 21, 2011
Applicants:

Christopher J. Lazzara, Palm Beach Shores, FL (US);

Jozef Bicerano, Midland, MI (US);

Inventors:

Christopher J. Lazzara, Palm Beach Shores, FL (US);

Jozef Bicerano, Midland, MI (US);

Assignee:

Neptune Research, Inc., Riviera Beach, FL (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B29C 73/04 (2006.01); B29C 70/30 (2006.01); F16L 55/16 (2006.01); F16L 1/00 (2006.01); B29C 73/10 (2006.01); F16L 55/168 (2006.01); B29C 35/08 (2006.01);
U.S. Cl.
CPC ...
B29C 70/30 (2013.01); B29C 73/04 (2013.01); B29C 73/10 (2013.01); F16L 1/00 (2013.01); F16L 55/16 (2013.01); F16L 55/1683 (2013.01); B29C 2035/085 (2013.01); B29C 2035/0827 (2013.01); B29C 2035/0844 (2013.01); B29C 2035/0855 (2013.01); B29C 2035/0877 (2013.01);
Abstract

Methods are provided for strengthening (e.g., repairing, structurally reinforcing, etc.) a fluid-system component by installing, as a circumferential wrap or a patch, a radiation-curable composite laminate. Kits including composite repair materials and equipment for implementing the methods are also provided. Examples of fluid-system components that may be strengthened include pipework, pipelines, transmission pipelines, distribution pipelines, gathering lines, oil risers, gas risers, process piping, girth welds on pipelines or vessels, tanks, vessels, elbows, tees, flanges, and high-pressure injection lines. An approach where, prior to curing, the precursor to the composite laminate comprises a glass fabric, a carbon fabric, or any combination(s) thereof, pre-impregnated with an uncured epoxy resin, an uncured epoxy acrylate resin, or a mixture thereof, is used; curing is performed via electron beam irradiation; and the installation and curing procedures can be automated to the maximum extent possible, in exemplary embodiments of the present disclosure.


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