ES2425317B1 - Repair set to repair defects in element surfaces - Google Patents

Repair set to repair defects in element surfaces Download PDF

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Publication number
ES2425317B1
ES2425317B1 ES201331067A ES201331067A ES2425317B1 ES 2425317 B1 ES2425317 B1 ES 2425317B1 ES 201331067 A ES201331067 A ES 201331067A ES 201331067 A ES201331067 A ES 201331067A ES 2425317 B1 ES2425317 B1 ES 2425317B1
Authority
ES
Spain
Prior art keywords
repair
substrate
compartments
compartment
repaired
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Active
Application number
ES201331067A
Other languages
Spanish (es)
Other versions
ES2425317A1 (en
Inventor
Álvaro Pipó Benito
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
COMPOSITE PATCH S L
COMPOSITE PATCH SL
Original Assignee
COMPOSITE PATCH S L
COMPOSITE PATCH SL
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by COMPOSITE PATCH S L, COMPOSITE PATCH SL filed Critical COMPOSITE PATCH S L
Priority to ES201331067A priority Critical patent/ES2425317B1/en
Publication of ES2425317A1 publication Critical patent/ES2425317A1/en
Application granted granted Critical
Publication of ES2425317B1 publication Critical patent/ES2425317B1/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B65—CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
    • B65B—MACHINES, APPARATUS OR DEVICES FOR, OR METHODS OF, PACKAGING ARTICLES OR MATERIALS; UNPACKING
    • B65B29/00—Packaging of materials presenting special problems
    • B65B29/10—Packaging two or more different substances isolated from one another in the package but capable of being mixed without opening the package, e.g. forming packages containing a resin and hardener isolated by a frangible partition
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B65—CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
    • B65D—CONTAINERS FOR STORAGE OR TRANSPORT OF ARTICLES OR MATERIALS, e.g. BAGS, BARRELS, BOTTLES, BOXES, CANS, CARTONS, CRATES, DRUMS, JARS, TANKS, HOPPERS, FORWARDING CONTAINERS; ACCESSORIES, CLOSURES, OR FITTINGS THEREFOR; PACKAGING ELEMENTS; PACKAGES
    • B65D81/00—Containers, packaging elements, or packages, for contents presenting particular transport or storage problems, or adapted to be used for non-packaging purposes after removal of contents
    • B65D81/32—Containers, packaging elements, or packages, for contents presenting particular transport or storage problems, or adapted to be used for non-packaging purposes after removal of contents for packaging two or more different materials which must be maintained separate prior to use in admixture
    • B65D81/3261—Flexible containers having several compartments
    • B65D81/3266—Flexible containers having several compartments separated by a common rupturable seal, a clip or other removable fastening device
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01B—MEASURING LENGTH, THICKNESS OR SIMILAR LINEAR DIMENSIONS; MEASURING ANGLES; MEASURING AREAS; MEASURING IRREGULARITIES OF SURFACES OR CONTOURS
    • G01B11/00—Measuring arrangements characterised by the use of optical techniques
    • G01B11/16—Measuring arrangements characterised by the use of optical techniques for measuring the deformation in a solid, e.g. optical strain gauge
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01B—MEASURING LENGTH, THICKNESS OR SIMILAR LINEAR DIMENSIONS; MEASURING ANGLES; MEASURING AREAS; MEASURING IRREGULARITIES OF SURFACES OR CONTOURS
    • G01B5/00—Measuring arrangements characterised by the use of mechanical techniques
    • G01B5/30—Measuring arrangements characterised by the use of mechanical techniques for measuring the deformation in a solid, e.g. mechanical strain gauge

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Management, Administration, Business Operations System, And Electronic Commerce (AREA)
  • Solid State Image Pick-Up Elements (AREA)

Abstract

Conjunto de reparación para reparar defectos en superficies de elementos.#Permite conocer instantáneamente el estado de tensiones en el elemento reparado. El conjunto consta de unos primeros compartimentos (2), para alojar sustancias que mezcladas constituyen un adhesivo endurecible; unos primeros medios de separación que mantienen los primeros compartimentos (2) aislados entre sí, y que pueden facilitar que las sustancias se mezclen; un segundo compartimento (3) que aloja un sustrato (5) destinado a ser impregnado con el adhesivo para ser adherido al elemento a reparar; unos segundos medios de separación que mantienen el segundo compartimento (3) aislado de los primeros compartimentos (2), y que pueden permitir que el adhesivo acceda al segundo compartimento (3) impregnando el sustrato (5); y medios sensores (8) fijados al sustrato (5), que captan el estado tensional del sustrato (5), una vez reparado el elemento.Repair set to repair defects in element surfaces. # Allows you to instantly know the state of stress in the repaired element. The set consists of first compartments (2), to accommodate substances which, when mixed, constitute a hardenable adhesive; first separation means that keep the first compartments (2) isolated from each other, and that can facilitate the mixing of substances; a second compartment (3) housing a substrate (5) intended to be impregnated with the adhesive to be adhered to the element to be repaired; second separation means that keep the second compartment (3) isolated from the first compartments (2), and that may allow the adhesive to access the second compartment (3) by impregnating the substrate (5); and sensor means (8) fixed to the substrate (5), which capture the tension state of the substrate (5), once the element has been repaired.

Description



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Claims (1)



 imagen1image 1 imagen2image2
ES201331067A 2013-07-12 2013-07-12 Repair set to repair defects in element surfaces Active ES2425317B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
ES201331067A ES2425317B1 (en) 2013-07-12 2013-07-12 Repair set to repair defects in element surfaces

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
ES201331067A ES2425317B1 (en) 2013-07-12 2013-07-12 Repair set to repair defects in element surfaces

Publications (2)

Publication Number Publication Date
ES2425317A1 ES2425317A1 (en) 2013-10-14
ES2425317B1 true ES2425317B1 (en) 2014-08-11

Family

ID=49231800

Family Applications (1)

Application Number Title Priority Date Filing Date
ES201331067A Active ES2425317B1 (en) 2013-07-12 2013-07-12 Repair set to repair defects in element surfaces

Country Status (1)

Country Link
ES (1) ES2425317B1 (en)

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0730732A1 (en) * 1993-11-23 1996-09-11 Grumman Aerospace Corporation Instrumented patch for repair of fatigue damaged or sensitive structure
US7398698B2 (en) * 2005-11-03 2008-07-15 The Boeing Company Smart repair patch and associated method
ES2368541B1 (en) * 2008-10-16 2012-09-25 Rodriser Industria Aeronáutica Española, S.L. PATCH IMPLEMENTATION PROCEDURE FOR REPAIR OF AIRCRAFT STRUCTURES AND PATCH USED IN THIS PROCEDURE.
US8056726B2 (en) * 2009-03-20 2011-11-15 CDO Technologies, Inc. Method and apparatus for repairing a surface defect
DE102010032093B4 (en) * 2010-07-23 2018-12-27 Aed Engineering Gmbh Repairing device for repair patches, repair kit and method for monitoring a repair patch
DE102011122059A1 (en) * 2011-12-22 2013-06-27 Airbus Operations Gmbh System and method for repairing a structural component

Also Published As

Publication number Publication date
ES2425317A1 (en) 2013-10-14

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