FR3026669A1 - - Google Patents
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- Publication number
- FR3026669A1 FR3026669A1 FR1559366A FR1559366A FR3026669A1 FR 3026669 A1 FR3026669 A1 FR 3026669A1 FR 1559366 A FR1559366 A FR 1559366A FR 1559366 A FR1559366 A FR 1559366A FR 3026669 A1 FR3026669 A1 FR 3026669A1
- Authority
- FR
- France
- Prior art keywords
- clamping
- temperature
- force
- prestressing
- fiber
- 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.)
- Granted
Links
- 238000000034 method Methods 0.000 claims abstract description 26
- 238000004519 manufacturing process Methods 0.000 claims abstract description 22
- 239000003733 fiber-reinforced composite Substances 0.000 claims abstract description 20
- 239000000835 fiber Substances 0.000 claims description 45
- 239000000463 material Substances 0.000 claims description 37
- 230000001419 dependent effect Effects 0.000 claims description 34
- 230000000694 effects Effects 0.000 claims description 17
- 239000011159 matrix material Substances 0.000 claims description 8
- 238000010438 heat treatment Methods 0.000 claims description 5
- 238000012856 packing Methods 0.000 claims description 5
- 230000007423 decrease Effects 0.000 claims description 4
- 230000036316 preload Effects 0.000 claims description 4
- 239000002657 fibrous material Substances 0.000 claims description 3
- 238000002360 preparation method Methods 0.000 claims description 2
- 230000007935 neutral effect Effects 0.000 claims 6
- 230000005540 biological transmission Effects 0.000 claims 5
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 claims 4
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims 4
- 229910052782 aluminium Inorganic materials 0.000 claims 4
- 238000005056 compaction Methods 0.000 claims 4
- 230000003993 interaction Effects 0.000 claims 3
- 229910000831 Steel Inorganic materials 0.000 claims 2
- 229910052742 iron Inorganic materials 0.000 claims 2
- 239000010959 steel Substances 0.000 claims 2
- 230000003247 decreasing effect Effects 0.000 claims 1
- 239000012530 fluid Substances 0.000 claims 1
- 239000007788 liquid Substances 0.000 claims 1
- 230000001105 regulatory effect Effects 0.000 claims 1
- 238000005516 engineering process Methods 0.000 description 3
- 238000007493 shaping process Methods 0.000 description 3
- 229920002430 Fibre-reinforced plastic Polymers 0.000 description 1
- 239000002131 composite material Substances 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 239000011151 fibre-reinforced plastic Substances 0.000 description 1
- 239000012528 membrane Substances 0.000 description 1
- 239000011347 resin Substances 0.000 description 1
- 229920005989 resin Polymers 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
- 238000009755 vacuum infusion Methods 0.000 description 1
Classifications
-
- 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
- F16B2/00—Friction-grip releasable fastenings
- F16B2/02—Clamps, i.e. with gripping action effected by positive means other than the inherent resistance to deformation of the material of the fastening
- F16B2/06—Clamps, i.e. with gripping action effected by positive means other than the inherent resistance to deformation of the material of the fastening external, i.e. with contracting action
- F16B2/10—Clamps, i.e. with gripping action effected by positive means other than the inherent resistance to deformation of the material of the fastening external, i.e. with contracting action using pivoting jaws
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B25—HAND TOOLS; PORTABLE POWER-DRIVEN TOOLS; MANIPULATORS
- B25B—TOOLS OR BENCH DEVICES NOT OTHERWISE PROVIDED FOR, FOR FASTENING, CONNECTING, DISENGAGING OR HOLDING
- B25B5/00—Clamps
- B25B5/06—Arrangements for positively actuating jaws
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B25—HAND TOOLS; PORTABLE POWER-DRIVEN TOOLS; MANIPULATORS
- B25B—TOOLS OR BENCH DEVICES NOT OTHERWISE PROVIDED FOR, FOR FASTENING, CONNECTING, DISENGAGING OR HOLDING
- B25B5/00—Clamps
- B25B5/14—Clamps for work of special profile
-
- 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
- B29C70/54—Component parts, details or accessories; Auxiliary operations, e.g. feeding or storage of prepregs or SMC after impregnation or during ageing
- B29C70/541—Positioning reinforcements in a mould, e.g. using clamping means for the reinforcement
-
- 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
- F16B2/00—Friction-grip releasable fastenings
- F16B2/02—Clamps, i.e. with gripping action effected by positive means other than the inherent resistance to deformation of the material of the fastening
- F16B2/06—Clamps, i.e. with gripping action effected by positive means other than the inherent resistance to deformation of the material of the fastening external, i.e. with contracting action
- F16B2/12—Clamps, i.e. with gripping action effected by positive means other than the inherent resistance to deformation of the material of the fastening external, i.e. with contracting action using sliding jaws
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Composite Materials (AREA)
- Moulding By Coating Moulds (AREA)
- Casting Or Compression Moulding Of Plastics Or The Like (AREA)
Abstract
L'invention concerne un dispositif de serrage (1) pour la fixation d'objets (3) par serrage, qui comprend, outre un dispositif de précontrainte (17) pour produire une force de précontrainte, un organe supplémentaire de réglage (18) fonction de la température, permettant de compenser des processus de tassement engendrés par la température. L'invention concerne également un procédé pour fabriquer une pièce composite renforcée de fibres, qui est fixée à l'aide d'un tel dispositif de serrage (1).The invention relates to a clamping device (1) for fastening objects (3) by clamping, which comprises, in addition to a prestressing device (17) for producing a prestressing force, an additional adjusting member (18) depending on temperature, to compensate for settlement processes caused by temperature. The invention also relates to a method for manufacturing a fiber reinforced composite part, which is fixed by means of such a clamping device (1).
Description
Dispositif de serrage et procédé pour fabriquer une pièce composite renforcée de fibres L'invention concerne un dispositif de serrage pour serrer la fixation d'objets, notamment des préformes à base de fibres pour la fabrication d'une pièce ,eomposite renforcée de fibres. L'invention concerne également un procédé pour fabriquer une pièce composite renforcée de fibres, qui est formée par un matériau à base de fibres dans lequel a été infusé un matériau de matrice. 10 Des pièces en un matériau composite renforcé de fibres, appelées pièces composites renforcées de fibres, sont aujourd'hui incontournables dans le domaine aéronautique et aérospatial. Mais l'utilisation de tels matériaux est également de plus en plus plébiscitée dans le domaine automobile. On fabrique notamment des éléments structurels critiques, en des matières plastiques 15 renforcées de fibres, qui sont d'un poids minime grâce à leur résistance et leur rigidité, élevées pour un poids donné. Grâce aux propriétés anisotropes résultant de l'orientation des fibres des matériaux composites renforcés de fibres, les pièces peuvent être adaptées à des charges ou contraintes locales, en permettant ainsi une exploitation optimale du matériau dans l'optique d'une 20 construction allégée. Lors de la fabrication de pièces composites renforcées de fibres, il est fréquent d'introduire un matériau à base de fibres dans un outillage de mise en forme, à la suite de quoi un matériau de matrice, par exemple un système de résines, ayant 25 été infusé dans le matériau à base de fibres, est durci en étant mis en température et le cas échant en pression, ce qui permet de former une pièce intégrale. Le matériau à base de fibres utilisé pour la réalisation de la préforme à base de fibres, par exemple des semi-produits plats, peut être un matériau à base de fibres sec ou déjà pré-imprégné. Si l'on utilise un matériau à base de 30 fibres sec, le matériau de matrice est alors infusé à un instant ultérieur dans le matériau à base de fibres, par exemple par un procédé par infusion sous vide, puis est durci. Lors de la fabrication de pièces composites renforcées de fibres, on utilise très 35 souvent la technologie dite Open-Mould-technology, d'après laquelle le matériau à -base de fibres pour la fabrication de la préforme, y compris les substances auxiliaires nécessaires sous la forme d'aides à l'écoulement, de membranes d'aspiration et pour finir d'un film à vide, est appliqué sur un côté fixe d'outillage d'un outillage de mise en forme. La préforme à base de fibres n'est donc pas 40 formée et durcie dans un outillage de mise en forme globalement fermé. Au niveau d'éléments raidisseurs ou de raccords géométriques, on applique souvent des parties d'outillage de mise en forme supplémentaires en tant qu'appuis, sous l'enveloppe à vide ou sur l'enveloppe à vide, pour pouvoir maintenir également pendant la fabrication de la pièce composite renforcée de fibres la géométrie prédéfinie de la pièce à l'intérieur des tolérances.The invention relates to a clamping device for tightening the fastening of objects, in particular fiber-based preforms for the manufacture of a workpiece, a fiber-reinforced composite. The invention also relates to a method for manufacturing a fiber-reinforced composite part which is formed from a fiber-based material into which a matrix material has been infused. 10 Parts made of fiber-reinforced composite material, called composite fiber-reinforced parts, are today essential in the aeronautical and aerospace field. But the use of such materials is also increasingly popular in the automotive field. In particular, critical structural elements are made of fiber-reinforced plastics which are of minimal weight because of their strength and rigidity, which are high for a given weight. Due to the anisotropic properties resulting from the fiber orientation of the fiber reinforced composite materials, the parts can be adapted to local loads or stresses, thereby enabling optimum material utilization in the light of lighter construction. In the manufacture of fiber-reinforced composite parts, it is common to introduce a fiber-based material into a shaping tool, whereby a matrix material, for example a resin system, having a diameter of 25 to 25 μm, is used. has been infused into the fiber-based material, is cured by being warmed up and, if necessary, under pressure, thereby forming an integral part. The fiber-based material used for producing the fiber-based preform, for example flat semi-products, may be a dry or pre-impregnated fiber-based material. If a dry fiber material is used, the matrix material is then infused at a later time into the fiber material, for example by a vacuum infusion process, and then cured. In the manufacture of fiber-reinforced composite parts, the so-called open-mold technology is often used, according to which the fiber-base material for the manufacture of the preform, including the auxiliary substances required under the form of flow aids, suction membranes and finishing of a vacuum film, is applied to a fixed side of tooling of a forming tool. The fiber-based preform is thus not formed and cured in a generally closed shaping tool. At the level of stiffening elements or geometrical connections, additional forming tooling parts are often applied as supports, under the vacuum envelope or on the vacuum envelope, so that they can also be maintained during operation. manufacture of the fiber-reinforced composite part the predefined geometry of the part within the tolerances.
Au cours du processus de fabrication proprement dit, c'est-à-dire pendant l'opération de durcissement du matériau de matrice par mise en température et, le cas échéant sollicitation en pression, la préforme à base de fibres se trouvant entre les outils est comprimée, de sorte qu'il est nécessaire que les outillages de mise en forme suivent ce processus de tassement ou cet effet de tassement. io Dans la pratique, on utilise une pince de précontrainte où la précontrainte a été produite à l'aide d'une broche à ressort sur un bras de levier. Dans ce cas, il s'est toutefois avéré désavantageux qu'en raison du processus de tassement ou de l'effet de tassement pendant la mise- en température de la préforme, la 15 précontrainte était perdue partiellement, voire totalement, de sorte que les outils ne sont plus pressés l'un contre l'autre, et qu'en conséquence les tolérances de pièce exigées ne peuvent plus être respectées. En effet, en raison des températures élevées lors du processus de durcissement proprement dit, la tension de ressort diminue, de sorte que la précontrainte perdue sous l'effet du 20 processus de tassement ne peut plus être suffisamment compensée. En conséquence, le but de la présente invention consiste à indiquer un procédé amélioré pour fabriquer une pièce composite renforcée de fibres, notamment celui de la technologie dite Open-Mould-technology, ainsi qu'un dispositif de 25 pince de serrage à utiliser à cet effet, permettant de compenser de manière fiable dans le cadre du processus, les effets de tassement de la préforme à base de fibres, observés au cours du processus de fabrication. Le but recherché est atteint, conformément à l'invention, à l'aide d'un dispositif de 30 serrage pour la fixation d'objets par serrage, comprenant deux bras de serrage, qui présentent chacun, à une extrémité de serrage, un mors de serrage, au moyen desquels un objet peut être fixé par serrage, et qui sont montés mobiles l'un par rapport à l'autre par l'intermédiaire d'une articulation, le dispositif de serrage comprenant également un dispositif de précontrainte pour produire une 35 force de précontrainte pré-réglable, qui agit en tant que force de serrage sur les mors de serrage lorsqu'un objet est fixé au moyen du dispositif de serrage, caractérisé en ce qu'en plus du dispositif de précontrainte, il est prévu au moins un organe de réglage fonction de la température, qui, lors du réglage de la force de précontrainte au niveau du dispositif de précontrainte, présente un premier 40 état dans lequel l'organe de réglage fonction de la température ne produit pas de précontrainte supplémentaire, et qui, en cas d'augmentation de la température du milieu environnant le dispositif de serrage, passe dans un deuxième état dans lequel l'organe de réglage fonction de la température produit une force de précontrainte supplémentaire, basée sur l'effet de la dilatation thermique et agissant en tant que force de serrage sur les mors de serrage. Par ailleurs, le but recherché est atteint, conformément à l'invention, grâce à un procédé pour fabriquer une pièce composite renforcée de fibres, qui est formée par un matériau à base de fibres infusé avec un matériau de matrice, comprenant les étapes suivantes : a) fourniture et préparation d'un dispositif de serrage selon l'une desDuring the actual manufacturing process, i.e. during the curing operation of the matrix material by heating and, if appropriate, pressure loading, the fiber-based preform between the tools is compressed, so that the shaping tools must follow this settling process or this packing effect. In practice, a prestressing clamp is used where the prestressing has been produced by means of a spring pin on a lever arm. In this case, however, it has been disadvantageous that due to the settling process or the settling effect during preform warm-up, prestressing was partially or totally lost, so that The tools are no longer pressed against each other, and as a result the required part tolerances can no longer be met. In fact, because of the high temperatures during the curing process itself, the spring tension decreases, so that the prestressing lost under the effect of the settling process can no longer be sufficiently compensated. Accordingly, it is an object of the present invention to provide an improved method for making a fiber reinforced composite part, in particular that of the Open-Mold-technology technology, as well as a clamping device for use in this application. This allows the process to compensate reliably for the settling effects of the fiber-based preform observed during the manufacturing process. In accordance with the invention, the object of the invention is achieved by means of a clamping device for fastening objects by clamping, comprising two clamping arms, each having at one clamping end a jaw by means of which an object can be fixed by clamping, and which are mounted movable relative to each other by means of a hinge, the clamping device also comprising a prestressing device for producing a Pre-adjustable preload force, which acts as a clamping force on the clamping jaws when an object is attached by means of the clamping device, characterized in that in addition to the prestressing device, there is provided minus a temperature-dependent adjusting member, which, when adjusting the preload force at the prestressing device, has a first state in which the temperature-dependent adjusting member does not produce no additional prestress, and which, in case of increase of the temperature of the environment surrounding the clamping device, goes into a second state in which the temperature-dependent adjustment member produces an additional prestressing force, based on the effect of thermal expansion and acting as a clamping force on the clamping jaws. Furthermore, the object of the invention is achieved by a method for producing a fiber-reinforced composite part which is formed of a fiber-based material infused with a matrix material, comprising the steps of: a) supply and preparation of a clamping device according to one of
Claims (11)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE102014114377.9A DE102014114377B4 (en) | 2014-10-02 | 2014-10-02 | Clamping device and method for producing a fiber composite component |
DE102014114377.9 | 2014-10-02 |
Publications (2)
Publication Number | Publication Date |
---|---|
FR3026669A1 true FR3026669A1 (en) | 2016-04-08 |
FR3026669B1 FR3026669B1 (en) | 2019-04-05 |
Family
ID=55530969
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1559366A Active FR3026669B1 (en) | 2014-10-02 | 2015-10-02 | CLAMPING DEVICE AND METHOD FOR MANUFACTURING A FIBER REINFORCED COMPOSITE PIECE |
Country Status (2)
Country | Link |
---|---|
DE (1) | DE102014114377B4 (en) |
FR (1) | FR3026669B1 (en) |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2901012A (en) * | 1956-05-21 | 1959-08-25 | Douglas Aircraft Co Inc | Expansion or contraction compensating clamp |
WO1993005891A1 (en) * | 1991-09-27 | 1993-04-01 | Rotex, Inc. | Top cover clamp for screening machine |
WO2009036820A1 (en) * | 2007-09-17 | 2009-03-26 | Daimler Ag | Method for the production of a composite fiber component and apparatus for this purpose |
-
2014
- 2014-10-02 DE DE102014114377.9A patent/DE102014114377B4/en active Active
-
2015
- 2015-10-02 FR FR1559366A patent/FR3026669B1/en active Active
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2901012A (en) * | 1956-05-21 | 1959-08-25 | Douglas Aircraft Co Inc | Expansion or contraction compensating clamp |
WO1993005891A1 (en) * | 1991-09-27 | 1993-04-01 | Rotex, Inc. | Top cover clamp for screening machine |
WO2009036820A1 (en) * | 2007-09-17 | 2009-03-26 | Daimler Ag | Method for the production of a composite fiber component and apparatus for this purpose |
Also Published As
Publication number | Publication date |
---|---|
DE102014114377A1 (en) | 2016-04-07 |
FR3026669B1 (en) | 2019-04-05 |
DE102014114377B4 (en) | 2016-06-02 |
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