Self-Repairing, Reinforced Matrix Materials

a reinforced matrix and self-repairing technology, applied in the field of matrix materials, can solve the problems of low tensile strength, low impact resistance of concrete, frequent brittleness, etc., and achieve the effect of improving durability

Inactive Publication Date: 2008-02-28
DRY CAROLYN
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

One major drawback of concrete is that it is relatively low in tensile strength.
Concrete also has little impact resistance and is frequently brittle.
A third major drawback is that its durability is significantly reduced when it is used in applications which require it to be exposed to repeated freeze-thaw cycles in the presence of water.
Freezing and thawing with the accompanying expansion and contraction of the water, forms cracks in the concrete.
The addition of fibers to concrete has improved its tensile strength but has decreased its compression strength.
Providing exterior coatings on the outer surfaces of the concrete has reduced water permeation, but it is a time-consuming additional step and has little, if any, effect on the lasting strength of the concrete.
These efforts have met with generally unsatisfactory results.
Moreover, the melted, permeated agents leave behind voids in the concrete which weakens the overall structure under load.
In connection with the polymer and / or metal or ceramic matrix composite materials, as well as, in the settable building materials such as concrete materials, special problems cause structures made from these materials to become aged or damaged in use.
More particularly, special structural defects arise in use including microcracking, fiber debonding, matrix delamination, fiber breakage, and fiber corrosion, to name but a few.
Any one of these microscopic and macroscopic phenomena may lead to failures which alter the strength, stiffness, dimensional stability and life span of the materials.
Microcracks, for example, may lead to major structural damage and environmental degradation.
The microcracks may grow into larger cracks with time and cause overall material fatigue so that the material deteriorates in long-term use.
Advanced matrix composites used in structural applications are susceptible to damage on both the macro- and microscopic levels.
Typical macroscopic damage to composite laminates involves delaminations and destruction of the material due to impact.
On the micrographic scale, damage usually involves matrix microcracking and / or debonding at the fiber / matrix interface.
Internal damage such as matrix microcracking alters the mechanical properties of shaped articles made therefrom such as strength, stiffness and dimensional stability depending on the material type and the laminate structure.
Thus, microcracks can ultimately lead to overall material degradation and reduced performance.
Moreover, prior studies have shown that microcracks cause both fiber and matrix dominated properties of the overall composite to be effected.
Repair of damages is a major problem when these matrix composite materials are employed in large-scale construction or advanced structures.
Microscale damage occurring within the matrix is likely to go undetected and the damage which results from this type of breakdown may be difficult to detect and very difficult to repair.

Method used

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Embodiment Construction

[0061] In accordance with the present invention, new and improved shaped articles comprise curable, settable, cross-linkable and / or hardenable matrix materials. The matrix material comprises a continuous phase and is a material that may be shaped to form a three-dimensional shaped article adapted for a particular use. Matrix materials can include any curable, settable or hardenable materials used in construction, building, roofing, roadway, aircraft, automotive, marine, appliances, transportation and / or biomedical fields for making shaped articles. Typically these materials will be moldable or castable to form shaped objects or may be laminated or assembled into finished products. The matrix materials may be inorganic or organic in nature and may include by way of illustration: cement, concrete, sintered fly ash or bottom ash / phosphoric acid mixtures, ceramic including, for example, silicon oxide, titanium oxide, silicon nitride, and metals such as aluminum, steel or other metal all...

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Abstract

Self-repairing, fiber reinforced matrix materials include a matrix material including inorganic as well as organic matrices. Disposed within the matrix are hollow fibers having a selectively releasable modifying agent contained therein. The hollow fibers may be inorganic or organic and of any desired length, wall thickness or cross-sectional configuration. The modifying agent is selected from materials capable of beneficially modifying the matrix fiber composite after curing. The modifying agents are selectively released into the surrounding matrix in use in response to a predetermined stimulus be it internal or externally applied. The hollow fibers may be closed off or even coated to provide a way to keep the modifying agent in the fibers until the appropriate time for selective release occurs. Self-repair, smart fiber matrix composite materials capable of repairing microcracks, releasing corrosion inhibitors or permeability modifiers are described as preferred embodiments in concrete and polymer based shaped articles.

Description

CROSS-REFERENCE TO RELATED APPLICATIONS [0001] This is a continuation of application of Ser. No. 11 / 278,631, filed Apr. 4, 2006 which is a continuation of application Ser. No. 10 / 376,906, filed Feb. 28, 2003, U.S. Pat. No. 7,022,179, which is a continuation of application Ser. No. 09 / 447,894, filed Nov. 23, 1999, U.S. Pat. No. 6,261,360, which is in turn a continuation of Ser. No. 08 / 918,630, filed Aug. 22, 1997, now U.S. Pat. No. 5,989,334, which is in turn a continuation of application Ser. No. 08,537,228, filed Sep. 29, 1995, now U.S. Pat. No. 5,660,624, which is in turn a continuation of application Ser. No. 08 / 189,665, filed Feb. 1, 1994, abandoned, which is in turn a continuation-in-part of U.S. Ser. No. 08 / 174,751, filed Dec. 29, 1993, now U.S. Pat. No. 5,575,841, which is in turn a continuation of U.S. Ser. No. 07 / 540,191, filed Jun. 19, 1990 abandoned.BACKGROUND OF THE INVENTION [0002] The present invention generally relates to matrix materials for use in a wide variety of ...

Claims

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Application Information

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Patent Type & Authority Applications(United States)
IPC IPC(8): B32B9/00C04B20/00C04B28/00A61L27/48B23B3/20B28B17/00C04B22/00C04B38/00C04B40/00C04B40/02C04B40/06C08J3/24C08K7/00C08K7/02
CPCC04B22/006C04B20/1025C04B35/80C04B38/0003C04B40/0028C04B40/0092C04B40/0263C04B40/06C04B40/0633C04B40/0641C04B40/0675C04B2103/0067C04B2111/72C04B2235/5284C08J3/241C08K7/00C08K7/02C22C47/00C22C47/04C22C49/00C22C49/14C04B28/34C04B20/0056C04B20/0048B82Y30/00B32B2605/18B32B2603/00B32B2307/762B32B2307/554B32B2307/54B32B2250/40B32B2250/03B32B17/10963B32B17/10036B32B17/04B32B15/20B32B15/18B32B15/14B32B5/02A61L27/48B28B17/00B29C73/163B29C73/22C04B26/14C04B22/085C04B24/08C04B24/282C04B24/32C04B24/42C04B28/02C04B26/02C04B2103/0046C04B2103/00Y10T428/249971Y10T428/249997Y10T428/249995Y10T428/249994C04B35/52C04B2235/3217C04B2235/80C04B2235/524
Inventor DRY, CAROLYN
Owner DRY CAROLYN
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