Nothing Special   »   [go: up one dir, main page]

RU2011133776A - Способ по меньшей мере частичного восстановления или замены усиливающего элемента конструкции из волокнистого композита и соответствующее соединительное устройство - Google Patents

Способ по меньшей мере частичного восстановления или замены усиливающего элемента конструкции из волокнистого композита и соответствующее соединительное устройство Download PDF

Info

Publication number
RU2011133776A
RU2011133776A RU2011133776/05A RU2011133776A RU2011133776A RU 2011133776 A RU2011133776 A RU 2011133776A RU 2011133776/05 A RU2011133776/05 A RU 2011133776/05A RU 2011133776 A RU2011133776 A RU 2011133776A RU 2011133776 A RU2011133776 A RU 2011133776A
Authority
RU
Russia
Prior art keywords
reinforcing element
pressure
replacement part
mat
fibrous layer
Prior art date
Application number
RU2011133776/05A
Other languages
English (en)
Other versions
RU2487799C2 (ru
Inventor
Ханс МАРКУАРДТ
Original Assignee
Эйрбас Оператионс Гмбх
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 Эйрбас Оператионс Гмбх filed Critical Эйрбас Оператионс Гмбх
Publication of RU2011133776A publication Critical patent/RU2011133776A/ru
Application granted granted Critical
Publication of RU2487799C2 publication Critical patent/RU2487799C2/ru

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00—General aspects of processes or apparatus for joining preformed parts
    • B29C66/80—General aspects of machine operations or constructions and parts thereof
    • B29C66/82—Pressure application arrangements, e.g. transmission or actuating mechanisms for joining tools or clamps
    • B29C66/824—Actuating mechanisms
    • B29C66/8242—Pneumatic or hydraulic drives
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
    • B29C65/02—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure
    • B29C65/18—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using heated tools
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00—General aspects of processes or apparatus for joining preformed parts
    • B29C66/01—General aspects dealing with the joint area or with the area to be joined
    • B29C66/05—Particular design of joint configurations
    • B29C66/10—Particular design of joint configurations particular design of the joint cross-sections
    • B29C66/11—Joint cross-sections comprising a single joint-segment, i.e. one of the parts to be joined comprising a single joint-segment in the joint cross-section
    • B29C66/112—Single lapped joints
    • B29C66/1122—Single lap to lap joints, i.e. overlap joints
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00—General aspects of processes or apparatus for joining preformed parts
    • B29C66/40—General aspects of joining substantially flat articles, e.g. plates, sheets or web-like materials; Making flat seams in tubular or hollow articles; Joining single elements to substantially flat surfaces
    • B29C66/41—Joining substantially flat articles ; Making flat seams in tubular or hollow articles
    • B29C66/43—Joining a relatively small portion of the surface of said articles
    • B29C66/434—Joining substantially flat articles for forming corner connections, fork connections or cross connections
    • B29C66/4344—Joining substantially flat articles for forming fork connections, e.g. for making Y-shaped pieces
    • B29C66/43441—Joining substantially flat articles for forming fork connections, e.g. for making Y-shaped pieces with two right angles, e.g. for making T-shaped pieces, H-shaped pieces
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00—General aspects of processes or apparatus for joining preformed parts
    • B29C66/40—General aspects of joining substantially flat articles, e.g. plates, sheets or web-like materials; Making flat seams in tubular or hollow articles; Joining single elements to substantially flat surfaces
    • B29C66/47—Joining single elements to sheets, plates or other substantially flat surfaces
    • B29C66/474—Joining single elements to sheets, plates or other substantially flat surfaces said single elements being substantially non-flat
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00—General aspects of processes or apparatus for joining preformed parts
    • B29C66/50—General aspects of joining tubular articles; General aspects of joining long products, i.e. bars or profiled elements; General aspects of joining single elements to tubular articles, hollow articles or bars; General aspects of joining several hollow-preforms to form hollow or tubular articles
    • B29C66/51—Joining tubular articles, profiled elements or bars; Joining single elements to tubular articles, hollow articles or bars; Joining several hollow-preforms to form hollow or tubular articles
    • B29C66/53—Joining single elements to tubular articles, hollow articles or bars
    • B29C66/532—Joining single elements to the wall of tubular articles, hollow articles or bars
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00—General aspects of processes or apparatus for joining preformed parts
    • B29C66/50—General aspects of joining tubular articles; General aspects of joining long products, i.e. bars or profiled elements; General aspects of joining single elements to tubular articles, hollow articles or bars; General aspects of joining several hollow-preforms to form hollow or tubular articles
    • B29C66/61—Joining from or joining on the inside
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00—General aspects of processes or apparatus for joining preformed parts
    • B29C66/70—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
    • B29C66/72—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the structure of the material of the parts to be joined
    • B29C66/721—Fibre-reinforced materials
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00—General aspects of processes or apparatus for joining preformed parts
    • B29C66/70—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
    • B29C66/73—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset
    • B29C66/737—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the state of the material of the parts to be joined
    • B29C66/7375—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the state of the material of the parts to be joined uncured, partially cured or fully cured
    • B29C66/73751—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the state of the material of the parts to be joined uncured, partially cured or fully cured the to-be-joined area of at least one of the parts to be joined being uncured, i.e. non cross-linked, non vulcanized
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00—General aspects of processes or apparatus for joining preformed parts
    • B29C66/80—General aspects of machine operations or constructions and parts thereof
    • B29C66/81—General aspects of the pressing elements, i.e. the elements applying pressure on the parts to be joined in the area to be joined, e.g. the welding jaws or clamps
    • B29C66/814—General aspects of the pressing elements, i.e. the elements applying pressure on the parts to be joined in the area to be joined, e.g. the welding jaws or clamps characterised by the design of the pressing elements, e.g. of the welding jaws or clamps
    • B29C66/8145—General aspects of the pressing elements, i.e. the elements applying pressure on the parts to be joined in the area to be joined, e.g. the welding jaws or clamps characterised by the design of the pressing elements, e.g. of the welding jaws or clamps characterised by the constructional aspects of the pressing elements, e.g. of the welding jaws or clamps
    • B29C66/81455—General aspects of the pressing elements, i.e. the elements applying pressure on the parts to be joined in the area to be joined, e.g. the welding jaws or clamps characterised by the design of the pressing elements, e.g. of the welding jaws or clamps characterised by the constructional aspects of the pressing elements, e.g. of the welding jaws or clamps being a fluid inflatable bag or bladder, a diaphragm or a vacuum bag for applying isostatic pressure
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00—General aspects of processes or apparatus for joining preformed parts
    • B29C66/80—General aspects of machine operations or constructions and parts thereof
    • B29C66/81—General aspects of the pressing elements, i.e. the elements applying pressure on the parts to be joined in the area to be joined, e.g. the welding jaws or clamps
    • B29C66/816—General aspects of the pressing elements, i.e. the elements applying pressure on the parts to be joined in the area to be joined, e.g. the welding jaws or clamps characterised by the mounting of the pressing elements, e.g. of the welding jaws or clamps
    • B29C66/8161—General aspects of the pressing elements, i.e. the elements applying pressure on the parts to be joined in the area to be joined, e.g. the welding jaws or clamps characterised by the mounting of the pressing elements, e.g. of the welding jaws or clamps said pressing elements being supported or backed-up by springs or by resilient material
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00—General aspects of processes or apparatus for joining preformed parts
    • B29C66/80—General aspects of machine operations or constructions and parts thereof
    • B29C66/83—General aspects of machine operations or constructions and parts thereof characterised by the movement of the joining or pressing tools
    • B29C66/832—Reciprocating joining or pressing tools
    • B29C66/8322—Joining or pressing tools reciprocating along one axis
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00—General aspects of processes or apparatus for joining preformed parts
    • B29C66/90—Measuring or controlling the joining process
    • B29C66/91—Measuring or controlling the joining process by measuring or controlling the temperature, the heat or the thermal flux
    • B29C66/912—Measuring or controlling the joining process by measuring or controlling the temperature, the heat or the thermal flux by measuring the temperature, the heat or the thermal flux
    • B29C66/9121—Measuring or controlling the joining process by measuring or controlling the temperature, the heat or the thermal flux by measuring the temperature, the heat or the thermal flux by measuring the temperature
    • B29C66/91211—Measuring or controlling the joining process by measuring or controlling the temperature, the heat or the thermal flux by measuring the temperature, the heat or the thermal flux by measuring the temperature with special temperature measurement means or methods
    • B29C66/91212—Measuring or controlling the joining process by measuring or controlling the temperature, the heat or the thermal flux by measuring the temperature, the heat or the thermal flux by measuring the temperature with special temperature measurement means or methods involving measurement means being part of the welding jaws, e.g. integrated in the welding jaws
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00—General aspects of processes or apparatus for joining preformed parts
    • B29C66/90—Measuring or controlling the joining process
    • B29C66/91—Measuring or controlling the joining process by measuring or controlling the temperature, the heat or the thermal flux
    • B29C66/912—Measuring or controlling the joining process by measuring or controlling the temperature, the heat or the thermal flux by measuring the temperature, the heat or the thermal flux
    • B29C66/9121—Measuring or controlling the joining process by measuring or controlling the temperature, the heat or the thermal flux by measuring the temperature, the heat or the thermal flux by measuring the temperature
    • B29C66/91231—Measuring or controlling the joining process by measuring or controlling the temperature, the heat or the thermal flux by measuring the temperature, the heat or the thermal flux by measuring the temperature of the joining tool
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/28—Shaping operations therefor
    • B29C70/40—Shaping or impregnating by compression not applied
    • B29C70/42—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles
    • B29C70/44—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using isostatic pressure, e.g. pressure difference-moulding, vacuum bag-moulding, autoclave-moulding or expanding rubber-moulding
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29D—PRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCES IN A PLASTIC STATE
    • B29D99/00—Subject matter not provided for in other groups of this subclass
    • B29D99/001—Producing wall or panel-like structures, e.g. for hulls, fuselages, or buildings
    • B29D99/0014—Producing wall or panel-like structures, e.g. for hulls, fuselages, or buildings provided with ridges or ribs, e.g. joined ribs
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
    • B29C65/02—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure
    • B29C65/18—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using heated tools
    • B29C65/24—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using heated tools characterised by the means for heating the tool
    • B29C65/30—Electrical means
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00—General aspects of processes or apparatus for joining preformed parts
    • B29C66/80—General aspects of machine operations or constructions and parts thereof
    • B29C66/82—Pressure application arrangements, e.g. transmission or actuating mechanisms for joining tools or clamps
    • B29C66/826—Pressure application arrangements, e.g. transmission or actuating mechanisms for joining tools or clamps without using a separate pressure application tool, e.g. the own weight of the parts to be joined
    • B29C66/8266—Pressure application arrangements, e.g. transmission or actuating mechanisms for joining tools or clamps without using a separate pressure application tool, e.g. the own weight of the parts to be joined using fluid pressure directly acting on the parts to be joined
    • B29C66/82661—Pressure application arrangements, e.g. transmission or actuating mechanisms for joining tools or clamps without using a separate pressure application tool, e.g. the own weight of the parts to be joined using fluid pressure directly acting on the parts to be joined by means of vacuum
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00—General aspects of processes or apparatus for joining preformed parts
    • B29C66/90—Measuring or controlling the joining process
    • B29C66/91—Measuring or controlling the joining process by measuring or controlling the temperature, the heat or the thermal flux
    • B29C66/914—Measuring or controlling the joining process by measuring or controlling the temperature, the heat or the thermal flux by controlling or regulating the temperature, the heat or the thermal flux
    • B29C66/9141—Measuring or controlling the joining process by measuring or controlling the temperature, the heat or the thermal flux by controlling or regulating the temperature, the heat or the thermal flux by controlling or regulating the temperature
    • B29C66/91421—Measuring or controlling the joining process by measuring or controlling the temperature, the heat or the thermal flux by controlling or regulating the temperature, the heat or the thermal flux by controlling or regulating the temperature of the joining tools
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00—General aspects of processes or apparatus for joining preformed parts
    • B29C66/90—Measuring or controlling the joining process
    • B29C66/96—Measuring or controlling the joining process characterised by the method for implementing the controlling of the joining process
    • B29C66/961—Measuring or controlling the joining process characterised by the method for implementing the controlling of the joining process involving a feedback loop mechanism, e.g. comparison with a desired value
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
    • B29K2105/00—Condition, form or state of moulded material or of the material to be shaped
    • B29K2105/06—Condition, form or state of moulded material or of the material to be shaped containing reinforcements, fillers or inserts
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
    • B29K2307/00—Use of elements other than metals as reinforcement
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
    • B29L2031/00—Other particular articles
    • B29L2031/30—Vehicles, e.g. ships or aircraft, or body parts thereof
    • B29L2031/3076—Aircrafts

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Fluid Mechanics (AREA)
  • Composite Materials (AREA)
  • Chemical & Material Sciences (AREA)
  • Architecture (AREA)
  • Civil Engineering (AREA)
  • Structural Engineering (AREA)
  • Moulding By Coating Moulds (AREA)
  • Reinforced Plastic Materials (AREA)
  • Lining Or Joining Of Plastics Or The Like (AREA)

Abstract

1. Способ по меньшей мере частичного восстановления или по меньшей мере частичной замены элемента усиления (10) конструкции из волокнистого композита (8), имеющий следующие этапы:размещение по меньшей мере одного волокнистого слоя (11) на части поверхности элемента усиления (10) и/или по меньшей мере одной заменяющей части элемента усиления (10), изготовленной из такого же материала и с такой же структурой слоев, на части поверхности усиления конструкции из волокнистого композита (8);размещение по меньшей мере одного мата давления (4), адаптированного к контуру элемента усиления (10) над по меньшей мере одним волокнистым слоем (11) и/или по меньшей мере одной заменяющей части элемента усиления (10), причем по меньшей мере один мат давления (4) опирается на фиксирующую раму (3) и зафиксирован в желательном положении фиксирующей рамой (3), адаптированной к контуру элемента усиления (10);поддержка конструкции из волокнистого композита (8) в области, противоположной фиксирующей раме (3), посредством контропоры (5);приложение среды давления к по меньшей мере одному мату давления (4) для прижатия его к элементу усиления (10) и фиксирующей раме (3) иотверждение по меньшей мере одного волокнистого слоя (11) и/или по меньшей мере одной заменяющей части элемента усиления (10).2. Способ по п.1, отличающийся тем, что по меньшей мере один волокнистый слой (11) и/или по меньшей мере одну заменяющую часть элемента усиления (10) предварительно формуют перед тем, как ее размещают и прикрепляют клеем в неотвержденном, частично отвержденном или полностью отвержденном состоянии.3. Способ по п.1, отличающийся тем, что после этапа размещения по меньшей мере одного воло�

Claims (13)

1. Способ по меньшей мере частичного восстановления или по меньшей мере частичной замены элемента усиления (10) конструкции из волокнистого композита (8), имеющий следующие этапы:
размещение по меньшей мере одного волокнистого слоя (11) на части поверхности элемента усиления (10) и/или по меньшей мере одной заменяющей части элемента усиления (10), изготовленной из такого же материала и с такой же структурой слоев, на части поверхности усиления конструкции из волокнистого композита (8);
размещение по меньшей мере одного мата давления (4), адаптированного к контуру элемента усиления (10) над по меньшей мере одним волокнистым слоем (11) и/или по меньшей мере одной заменяющей части элемента усиления (10), причем по меньшей мере один мат давления (4) опирается на фиксирующую раму (3) и зафиксирован в желательном положении фиксирующей рамой (3), адаптированной к контуру элемента усиления (10);
поддержка конструкции из волокнистого композита (8) в области, противоположной фиксирующей раме (3), посредством контропоры (5);
приложение среды давления к по меньшей мере одному мату давления (4) для прижатия его к элементу усиления (10) и фиксирующей раме (3) и
отверждение по меньшей мере одного волокнистого слоя (11) и/или по меньшей мере одной заменяющей части элемента усиления (10).
2. Способ по п.1, отличающийся тем, что по меньшей мере один волокнистый слой (11) и/или по меньшей мере одну заменяющую часть элемента усиления (10) предварительно формуют перед тем, как ее размещают и прикрепляют клеем в неотвержденном, частично отвержденном или полностью отвержденном состоянии.
3. Способ по п.1, отличающийся тем, что после этапа размещения по меньшей мере одного волокнистого слоя (11) и/или по меньшей мере одной заменяющей части элемента усиления (10), кроме того предусмотрены этапы:
покрытия по меньшей мере одного волокнистого слоя (11) и/или по меньшей мере одной заменяющей части элемента усиления (10) вакуумной пленкой (12а) и
герметизации области отрицательного давления, ограниченной вакуумной пленкой (12а), и конструкции из волокнистого композита (8), причем область отрицательного давления откачивают на этапе приложения среды давления к по меньшей мере одному мату давления (4).
4. Способ по п.1, отличающийся тем, что на этапе отверждения по меньшей мере одного волокнистого слоя (11) и/или по меньшей мере одной заменяющей части осуществляют нагрев в соответствии с температурой отверждения системы смоляной матрицы волокнистого слоя (11) и/или по меньшей мере одной заменяющей части.
5. Способ по п.4, отличающийся тем, что нагрев осуществляют посредством по меньшей мере одного нагревательного элемента (6), который интегрирован в мат давления (4), прикреплен к последнему и/или расположен между матом давления (4) и по меньшей мере одним волокнистым слоем (11) и/или по меньшей мере одной заменяющей частью как отдельный компонент.
6. Способ по п.5, отличающийся тем, что нагрев, кроме того, осуществляют по меньшей мере одним нагревательным элементом (7, 7a) контропоры, расположенным в и/или на контропоре (5).
7. Соединительное устройство (1) для соединения по меньшей мере одного волокнистого слоя (11), размещенного на по меньшей мере одной части поверхности элемента усиления, с элементом усиления (10) и/или для соединения по меньшей мере одной заменяющей части, изготовленной из такого же материала и с такой же структурой слоев элемента усиления (10), на части поверхности усиления конструкции из волокнистого композита (8) с упомянутой конструкцией из волокнистого композита, включающее:
по меньшей мере один мат давления (4), который адаптирован к контуру элемента усиления (10), и который имеет по меньшей мере одну камеру давления (18) для среды давления, к которой может быть приложено давление, и размещен над по меньшей мере одним волокнистым слоем (11) и/или по меньшей мере одной заменяющей частью элемента усиления (10);
фиксирующую раму (3), адаптированную к контуру элемента усиления (10), для поддержки и фиксации мата давления (4); и
контропору (5) для установки конструкции из волокнистого композита (8), причем по меньшей мере одна фиксирующая рама (3) имеет первое фиксирующее устройство (22, 23, 24) для фиксации горизонтальных областей мата давления (4) и второе фиксирующее устройство (26) для фиксации элемента усиления (10), и причем второе фиксирующее устройство (26) снабжено по меньшей мере одним боковым фиксирующим элементом (27) для боковой фиксации элемента усиления (10).
8. Соединительное устройство (1) по п.7, отличающееся тем, что по меньшей мере один мат давления (4) имеет по меньшей мере один элемент усиления (17) в жестких на изгиб областях.
9. Соединительное устройство (1) по п.7, отличающееся тем, что по меньшей мере один мат давления (4) имеет шарнирную часть (20).
10. Соединительное устройство (1) по п.7, отличающееся тем, что предусмотрен по меньшей мере один нагревательный элемент (6), интегрированный в мат давления (4) и/или прикрепленный к нему так, чтобы быть адаптированным к контуру элемента усиления (10).
11. Соединительное устройство (1) по п.7, отличающееся тем, что по меньшей мере один нагревательный элемент (6) расположен между матом давления (4) и по меньшей мере одним волокнистым слоем (11) и/или по меньшей мере одной заменяющей частью как отдельный компонент так, чтобы быть адаптированным к контуру элемента усиления (10).
12. Соединительное устройство (1) по п.10, отличающееся тем, что по меньшей мере один нагревательный элемент (7) контропоры расположен в и/или на контропоре (5).
13. Соединительное устройство (1) по п.7, отличающееся тем, что поверхности давления, передающие теплоту, которые находятся в контакте с по меньшей мере одним волокнистым слоем, расположенным на элементе усиления (10), и/или по меньшей мере одной новой заменяющей частью элемента усиления (10) и/или конструкции из волокнистого композита (8), снабжены металлической фольгой (33) для равномерного распределения теплоты.
RU2011133776/05A 2009-02-23 2010-02-23 Способ по меньшей мере частичного восстановления или замены усиливающего элемента конструкции из волокнистого композита и соответствующее соединительное устройство RU2487799C2 (ru)

Applications Claiming Priority (5)

Application Number Priority Date Filing Date Title
US20831409P 2009-02-23 2009-02-23
US61/208,314 2009-02-23
DE102009001075.0 2009-02-23
DE200910001075 DE102009001075A1 (de) 2009-02-23 2009-02-23 Verfahren zum zumindest teilweise Nachbearbeiten oder Ersetzen eines Versteifungselementes einer Faserverbundstruktur und zugehörige Anbindvorrichtung
PCT/EP2010/052251 WO2010094808A2 (de) 2009-02-23 2010-02-23 Verfahren zum zumindest teilweise nachbearbeiten oder ersetzen eines versteifungselementes einer faserverbundstruktur und zugehörige anbindvorrichtung

Publications (2)

Publication Number Publication Date
RU2011133776A true RU2011133776A (ru) 2013-03-27
RU2487799C2 RU2487799C2 (ru) 2013-07-20

Family

ID=42538246

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2011133776/05A RU2487799C2 (ru) 2009-02-23 2010-02-23 Способ по меньшей мере частичного восстановления или замены усиливающего элемента конструкции из волокнистого композита и соответствующее соединительное устройство

Country Status (7)

Country Link
US (1) US8726965B2 (ru)
EP (1) EP2408610B1 (ru)
CN (1) CN102325647B (ru)
CA (1) CA2752871C (ru)
DE (1) DE102009001075A1 (ru)
RU (1) RU2487799C2 (ru)
WO (1) WO2010094808A2 (ru)

Families Citing this family (26)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102010045210B4 (de) * 2010-09-13 2012-06-28 Premium Aerotec Gmbh Vakuumaufbau zur Druckbeaufschlagung eines Bauteils während seiner Herstellung, und Verfahren zur Herstellung eines Bauteils
DE102011115049B4 (de) 2010-11-10 2015-04-09 Piekenbrink Composite Gmbh Beheizbare Vakuumhauben-Vorrichtung
DE102010053569B4 (de) * 2010-12-06 2012-07-26 Airbus Operations Gmbh Verfahren zur Reparatur eines Flugzeugstrukturbauteils
DE102011004775B4 (de) 2011-02-25 2012-10-25 Airbus Operations Gmbh Verfahren zum Herstellen einer Verbindung, Verbindung sowie Luft- oder Raumfahrzeug
DE102011014999A1 (de) * 2011-03-25 2012-09-27 Waldemar Piekenbrink GFK - Modell- und Formenbau, Produktions- und Vertriebs GmbH Beheizbare Vakuumhauben-Vorrichtung
FR2980732B1 (fr) 2011-10-04 2013-10-11 Airbus Operations Sas Procede et dispositif pour le soudage d'un raidisseur thermoplastique
FR2983264B1 (fr) * 2011-11-29 2016-04-01 Mecano I D Piece d'assemblage
FR2987305B1 (fr) * 2012-02-29 2017-02-10 Daher Aerospace Procede et dispositif pour le soudage a haute temperature d'un raidisseur sur un panneau composite a matrice thermoplastique
US9649785B2 (en) 2012-08-15 2017-05-16 The Boeing Company Portable Curing System
US9523431B2 (en) * 2013-05-31 2016-12-20 The Boeing Company Sealing and testing segmented tools
RU2542311C1 (ru) * 2013-07-17 2015-02-20 Открытое акционерное общество Научно-производственное объединение "Искра" Способ подготовки к работе вулканизационного оборудования
DE102013222106A1 (de) * 2013-10-30 2015-05-13 Airbus Operations Gmbh Aushärtungswerkzeug für Schalenbauteile und Verfahren zum Aushärten von Schalenbauteilen
CN103770346B (zh) * 2014-01-07 2016-05-04 杭州华聚复合材料有限公司 一种热塑性蜂窝板的修复方法
US10093068B2 (en) 2014-07-08 2018-10-09 Polycorp Ltd. Method and system for providing a rubber lining
US9545778B2 (en) * 2014-08-04 2017-01-17 The Boeing Company System and method for applying pressure to structural components
JP6463094B2 (ja) * 2014-11-25 2019-01-30 三菱重工業株式会社 接合装置及び接合方法
DE102015211671A1 (de) * 2015-06-24 2016-12-29 Airbus Operations Gmbh Verfahren und Vorrichtung zur Herstellung eines Bauteils unter Verwendung einer Vakuumfolie
GB201511402D0 (en) * 2015-06-30 2015-08-12 Short Brothers Plc Repair including a chamfered bracket and a chamfered bracket component for reinforcing a damaged structural element made from composite materials
US10836001B2 (en) 2016-07-08 2020-11-17 Sikorsky Aircraft Corporation Mobile pressure tool for rotor blade processes
CN106181885B (zh) * 2016-09-09 2017-05-31 安徽山鹰纸业股份有限公司 一种造纸机干部稳纸风箱拆装装置
CN109789650A (zh) * 2016-09-27 2019-05-21 庞巴迪公司 用复合修复帽修复复合桁条的方法
US10710319B2 (en) 2017-08-02 2020-07-14 The Boeing Company Controlling application of forces to different portions of object surface using bladder
US10710320B2 (en) * 2017-08-02 2020-07-14 The Boeing Company Controlling application of forces to different portions of object surface using flexible wall
DE102018110123A1 (de) * 2018-04-26 2019-10-31 Airbus Operations Gmbh Verfahren zum Herstellen eines dreidimensionalen Vorformlings aus Verstärkungsfasern
US11542086B2 (en) * 2018-08-06 2023-01-03 Better Packages, Inc. Packaging apparatus for film inflation and method thereof
FR3121382B1 (fr) * 2021-03-30 2023-11-17 Safran Aircraft Engines Réparation d’une pièce en matériau composite

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2187672A (en) * 1986-01-17 1987-09-16 Advanced Composite Components Moulding fibre-reinforced articles
DE4101854C1 (en) * 1991-01-23 1992-06-11 Deutsche Airbus Gmbh, 2000 Hamburg, De Repair device for CFK monolith with double-T stringer - includes three part aluminium@ heater with electrically heated rod(s) in core section
JPH10146898A (ja) * 1996-11-15 1998-06-02 Honda Motor Co Ltd 繊維強化複合材の成形方法
IL151541A0 (en) * 2000-03-03 2003-04-10 Quickstep Technologies Pty Ltd Production, forming, bonding, joining and repair system for composite and metal components
DE10013409C1 (de) * 2000-03-17 2000-11-23 Daimler Chrysler Ag Verfahren und Vorrichtung zur Herstellung von faserverstärkten Bauteilen mittels eines Injektionsverfahrens
DE102007004312B4 (de) * 2007-01-29 2014-08-21 Airbus Operations Gmbh Verfahren zur Herstellung eines Faserverbundbauteils für ein Luft- oder Raumfahrzeug
DE102007026099A1 (de) 2007-06-05 2008-12-11 Airbus Deutschland Gmbh Vorrichtung und Verfahren zum Bearbeiten einer Faserverbundstruktur
DE102007061431B4 (de) * 2007-12-20 2013-08-08 Airbus Operations Gmbh Verfahren zur Versteifung eines Faserverbundbauteils sowie Vakuummatte und Anordnung zur Herstellung eines versteiften Faserverbundbauteils

Also Published As

Publication number Publication date
CN102325647A (zh) 2012-01-18
WO2010094808A4 (de) 2011-02-17
US8726965B2 (en) 2014-05-20
EP2408610B1 (de) 2012-12-19
DE102009001075A1 (de) 2010-09-09
US20120061006A1 (en) 2012-03-15
CN102325647B (zh) 2014-01-08
CA2752871A1 (en) 2010-08-26
WO2010094808A3 (de) 2010-12-29
RU2487799C2 (ru) 2013-07-20
EP2408610A2 (de) 2012-01-25
CA2752871C (en) 2017-03-21
WO2010094808A2 (de) 2010-08-26

Similar Documents

Publication Publication Date Title
RU2011133776A (ru) Способ по меньшей мере частичного восстановления или замены усиливающего элемента конструкции из волокнистого композита и соответствующее соединительное устройство
CA2784378C (en) Double vacuum cure processing of composite parts
US20110232837A9 (en) Method for producing an orthesis
KR101787783B1 (ko) 고온 복합재료 공구
JP2010528899A (ja) 繊維複合構造部材の処理装置及び繊維複合構造部材の処理方法
JP7093299B2 (ja) 熱プレス装置および金属樹脂複合体の成形方法
RU2008116590A (ru) Способ и устройство для приклеивания компонентов к композитному формованному изделию
CN110494617B (zh) Frp材料与结构体的粘合结构和粘合方法
KR20120099677A (ko) 섬유강화재로 부품을 제조하는 방법
JP5148466B2 (ja) 複合材料の修理方法
JP6100579B2 (ja) ハニカムコアサンドイッチパネルの修理方法、および修理装置
US10322552B2 (en) Composite repair armature
EP3305511B1 (en) System and method for curing polymer matrix composite parts in manufacturing and repairing processes
JP6154670B2 (ja) 繊維強化プラスチック部材の成形方法及び成形装置
US20200180240A1 (en) Method and device for consolidating a composite fiber structure
JP2001038752A (ja) 複合材曲面パネルの成形装置及び成形方法
JP2014008735A (ja) 繊維強化プラスチック製ハニカムコアの製造方法
JP2017035848A (ja) 複合材部品の修理方法及び複合材部品の製造方法
WO2012157327A1 (ja) Ｒｔｍ成形方法及びｒｔｍ成形装置
JPH0419111A (ja) コンクリート製成形型の表面補強方法
JP6724667B2 (ja) 複合材料の成形方法および複合材料の成形装置
JP2023061443A (ja) 複合材の接着方法
US20130052565A1 (en) Applying a seal to a fuel cell component
JP2020159092A (ja) 支柱を補強または補修する方法及びシステム
JP2012006337A (ja) 繊維強化複合材の製造方法

Legal Events

Date Code Title Description
MM4A The patent is invalid due to non-payment of fees

Effective date: 20180224