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ES2721153T3 - Procedimiento y sistema para insertar un elemento de inserción en un producto de panel - Google Patents

Procedimiento y sistema para insertar un elemento de inserción en un producto de panel Download PDF

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Publication number
ES2721153T3
ES2721153T3 ES12775017T ES12775017T ES2721153T3 ES 2721153 T3 ES2721153 T3 ES 2721153T3 ES 12775017 T ES12775017 T ES 12775017T ES 12775017 T ES12775017 T ES 12775017T ES 2721153 T3 ES2721153 T3 ES 2721153T3
Authority
ES
Spain
Prior art keywords
filling
insertion element
recess
sealing
intermediate space
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
ES12775017T
Other languages
English (en)
Inventor
Stefan Kögl
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.)
RUAG Schweiz AG
Original Assignee
RUAG Schweiz AG
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 RUAG Schweiz AG filed Critical RUAG Schweiz AG
Application granted granted Critical
Publication of ES2721153T3 publication Critical patent/ES2721153T3/es
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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
    • B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
    • B29C65/48—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding
    • 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
    • B29C31/00—Handling, e.g. feeding of the material to be shaped, storage of plastics material before moulding; Automation, i.e. automated handling lines in plastics processing plants, e.g. using manipulators or robots
    • B29C31/04—Feeding of the material to be moulded, e.g. into a mould cavity
    • B29C31/041—Feeding of the material to be moulded, e.g. into a mould cavity using filling or dispensing heads placed in closed moulds or in contact with mould walls
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16B—DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
    • F16B13/00—Dowels or other devices fastened in walls or the like by inserting them in holes made therein for that purpose
    • F16B13/14—Non-metallic plugs or sleeves; Use of liquid, loose solid or kneadable material therefor
    • F16B13/141—Fixing plugs in holes by the use of settable 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
    • B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
    • B29C65/48—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding
    • B29C65/52—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding characterised by the way of applying the adhesive
    • B29C65/54—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding characterised by the way of applying the adhesive between pre-assembled parts
    • B29C65/542—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding characterised by the way of applying the adhesive between pre-assembled parts by injection
    • 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
    • B29C66/725—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 being hollow-walled or honeycombs
    • B29C66/7252—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 being hollow-walled or honeycombs hollow-walled
    • B29C66/72525—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 being hollow-walled or honeycombs hollow-walled comprising honeycomb cores
    • 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
    • B29C66/725—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 being hollow-walled or honeycombs
    • B29C66/7254—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 being hollow-walled or honeycombs honeycomb structures
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B37/00—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding
    • B32B37/12—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by using adhesives
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B37/00—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding
    • B32B37/14—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by the properties of the layers
    • B32B37/142—Laminating of sheets, panels or inserts, e.g. stiffeners, by wrapping in at least one outer layer, or inserting into a preformed pocket
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
    • B64C1/066—Interior liners
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16B—DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
    • F16B11/00—Connecting constructional elements or machine parts by sticking or pressing them together, e.g. cold pressure welding
    • F16B11/006—Connecting constructional elements or machine parts by sticking or pressing them together, e.g. cold pressure welding by gluing
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16B—DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
    • F16B5/00—Joining sheets or plates, e.g. panels, to one another or to strips or bars parallel to them
    • F16B5/01—Joining sheets or plates, e.g. panels, to one another or to strips or bars parallel to them by means of fastening elements specially adapted for honeycomb panels

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Robotics (AREA)
  • Casting Or Compression Moulding Of Plastics Or The Like (AREA)
  • Lining Or Joining Of Plastics Or The Like (AREA)
  • Connection Of Plates (AREA)
  • Investigating Strength Of Materials By Application Of Mechanical Stress (AREA)

Abstract

Procedimiento para fabricar un dispositivo de producto de panel (10), en particular para una aeronave o un vehículo espacial, proporcionándose un producto previo de panel (11) con al menos una escotadura (12) formada en una superficie de panel (13), con una delimitación (14) y al menos un elemento de inserción (20) previsto para anclar en una de las escotaduras (12), que comprende los siguientes pasos: - inserción automatizada del elemento de inserción (20) en la escotadura (12) del producto previo de panel (11), y - llenado automatizado de un espacio intermedio (16) entre el elemento de inserción (20) y la delimitación (14) de la escotadura (12) con un fluido de llenado (15) que se endurece o es endurecible, caracterizado por que el elemento de inserción (20) se une de manera separable, antes de la inserción en la escotadura (12), a una instalación de sellado y de posicionamiento (40, 140) según una de las reivindicaciones 6 - 14, y por que el paso del llenado del espacio intermedio (16) comprende los siguientes pasos: - sellar el espacio intermedio (16), - llenar el espacio intermedio (16) con el fluido de llenado (15) a través de la abertura de llenado (43, 143) de la instalación de sellado y de posicionamiento (40, 140) hasta que el espacio intermedio está lleno esencialmente por completo del fluido de llenado (44, 144), y - dejar salir fluido de llenado (15) excedente del espacio intermedio (16) a través de la abertura de salida (44, 20 144) de la instalación de sellado y de posicionamiento (40, 140).
ES12775017T 2012-10-17 2012-10-17 Procedimiento y sistema para insertar un elemento de inserción en un producto de panel Active ES2721153T3 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
PCT/EP2012/070549 WO2014060027A1 (de) 2012-10-17 2012-10-17 Verfahren und system zum einsetzen eines einsatzelements in ein paneelprodukt, das damit hergestellte paneelprodukt sowie verfahren und system zum ausführen eines zugtests am eingesetzten einsatzelement

Publications (1)

Publication Number Publication Date
ES2721153T3 true ES2721153T3 (es) 2019-07-29

Family

ID=47045031

Family Applications (1)

Application Number Title Priority Date Filing Date
ES12775017T Active ES2721153T3 (es) 2012-10-17 2012-10-17 Procedimiento y sistema para insertar un elemento de inserción en un producto de panel

Country Status (14)

Country Link
US (1) US10377087B2 (es)
EP (1) EP2909004B1 (es)
JP (1) JP6243434B2 (es)
CN (1) CN104853899B (es)
AU (1) AU2012392268A1 (es)
ES (1) ES2721153T3 (es)
HK (1) HK1209689A1 (es)
HU (1) HUE043099T2 (es)
IL (1) IL238334A0 (es)
IN (1) IN2015DN04168A (es)
PL (1) PL2909004T3 (es)
PT (1) PT2909004T (es)
RU (1) RU2015117922A (es)
WO (1) WO2014060027A1 (es)

Families Citing this family (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9702394B2 (en) * 2015-07-13 2017-07-11 The Boeing Company Floating, bottom-filled and twist insert and methods for use thereof
US10626992B2 (en) * 2015-11-30 2020-04-21 The Boeing Company Sealant containment assembly, system, and method
DE102015122950B4 (de) * 2015-12-30 2024-06-06 Fraunhofer-Gesellschaft zur Förderung der angewandten Forschung e.V. Verbundanker
PT3464911T (pt) 2016-05-31 2021-09-28 Ruag Schweiz Ag Sistema de insertos, inserto e conjunto de painéis
DE102016214366A1 (de) * 2016-08-03 2018-02-08 Bayerische Motoren Werke Aktiengesellschaft Verfahren zur Herstellung einer Anordnung mit einer Faserverbundwerkstoff aufweisenden Struktur und einem Lasteinleitungselement
EP3384996A4 (en) * 2016-11-25 2019-04-17 Mitsubishi Electric Corporation AUTOMATIC FILLING DEVICE
CA3053726C (en) 2017-03-28 2021-10-26 Ruag Schweiz Ag Insert for a composite structure
CN112424487B (zh) * 2018-09-05 2022-08-23 Nok株式会社 连结装置和密封装置
CN110900948A (zh) * 2018-09-17 2020-03-24 汉达精密电子(昆山)有限公司 一种凸柱结构及其制造方法
FR3091668B1 (fr) 2019-01-15 2021-01-22 Ecole Superieure Des Tech Industrielles Avancees Estia Effecteur terminal robotique de pose automatique d’inserts dans un panneau en matériau composite du type sandwich à âme alvéolaire
GB2582631A (en) * 2019-03-28 2020-09-30 Airbus Operations Ltd A joint for an aircraft assembly
FR3097141B1 (fr) * 2019-06-12 2021-05-14 Secam Dispositif de remplissage d’une substance durcissable dans un insert assemblé dans un trou d’un panneau sandwich
CN112373717B (zh) * 2020-10-30 2022-10-11 哈尔滨飞机工业集团有限责任公司 一种飞机变曲度焊接件结构装配方法
CN113879559B (zh) * 2021-10-12 2023-08-15 北京机电工程研究所 飞行器蒙皮静态力加载装置及蒙皮动强度试验方法
CN115071177B (zh) * 2022-06-22 2024-03-08 沈阳飞机工业（集团）有限公司 一种含嵌块的蜂窝夹层复合材料制件制造及检验工装

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DE3519679A1 (de) * 1985-06-01 1986-12-04 Beitz, Wolfgang, Prof.Dr.-Ing. Verfahren zur herstellung loesbarer verbindungen (schrauben-, formschluessige welle-nabe- und linienhafte formschlussverbindungen) durch formelemente aus klebstoff
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Also Published As

Publication number Publication date
CN104853899A (zh) 2015-08-19
IN2015DN04168A (es) 2015-10-16
AU2012392268A1 (en) 2015-06-04
EP2909004A1 (de) 2015-08-26
IL238334A0 (en) 2015-06-30
EP2909004B1 (de) 2019-01-23
US10377087B2 (en) 2019-08-13
WO2014060027A1 (de) 2014-04-24
HUE043099T2 (hu) 2019-08-28
HK1209689A1 (en) 2016-04-08
US20160001501A1 (en) 2016-01-07
PL2909004T3 (pl) 2019-09-30
PT2909004T (pt) 2019-05-22
JP6243434B2 (ja) 2017-12-06
CN104853899B (zh) 2017-12-08
RU2015117922A (ru) 2016-12-10
JP2016503352A (ja) 2016-02-04

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