摘要:
There is provided a device for producing fibre-reinforced composite components from dry fibre components by means of an injection process for injecting curable matrix material, comprising a. a tool for arranging a dry fibre component; b. an envelope which is impermeable to gas and curable matrix material arranged on at least one side of the tool to form a space into which curable matrix material may be introduced to contact a dry fibre component arranged on the tool, the envelope sealing off the tool from the environment; c. an inlet for introducing curable matrix material into the space formed by the envelope; d. an outlet for removing gas from the space formed by the envelope so that curable matrix material may be drawn into the space to penetrate the dry fibre component arranged on the tool; and e. a patch formed from a membrane which is permeable to gas but impermeable to curable matrix material, the patch being associated with the outlet so that gas, but not curable matrix material, can be removed from the space formed by the envelope via the outlet; wherein the association between the outlet and the patch is stable at temperatures of at least 150° C. There is further provided a method for producing fibre-reinforced composite components by use of a device according to the invention.
摘要:
A manufacturing apparatus for constructing a 3D preform from carbon fibre tow (10), in which the tow is deposited by an AFP head (2400) onto a membrane (2204) which is conveyed to a forming cell (114) for diaphragm forming. Active tension control is provided with an offwind (102) combined with an accumulator (106) and compensator (108). The invention also provides a method of manufacture.
摘要:
The present invention concerns preforms made with a new intermediate material composed of a unidirectional layer of carbon fibers with a weight of 100 to 280 g/m2, associated on each of its faces, with a web of thermoplastic fibers having a thickness of 0.5 to 50 microns, preferably 3 to 35 microns, the intermediate material having a total thickness of 80 to 380 microns, preferably from 90 to 320 microns, and a process for manufacturing composite parts from such preforms and the resulting composite parts.
摘要:
The invention concerns a process for preparing a ribbon of reinforcement strands or filaments associated on each of its faces with a polymeric binder, said ribbon having a given width substantially constant over its entire length, in which the strands or filaments extend in a direction parallel to the length of the ribbon, wherein it comprises the following steps: a) adjustment of the ribbon width to the desired width thanks to a dimensioning device, b) association of the ribbon on each of its faces with a polymeric binder allowing the assurance of a homogenous cohesion of the ribbon, such that the total weight of the binder does not exceed 25% of the total weight of the obtained ribbon, as well as the ribbons obtainable by such a process.
摘要:
The present invention relates to a stack of fibrous materials including at least two unidirectional carbon fiber layers, each extending in different directions, wherein each one of the unidirectional layers is connected by means of at least one of the surfaces thereof to an adjacent web of thermoplastic fibers, at least one web being inserted between two consecutive unidirectional layers, characterized in that the link between each unidirectional layer and each adjacent web is provided by the web, by weld points which produce an intermittent overall weld, and in that said weld points also guarantee the cohesion of the stack, as well as the method for manufacturing same.
摘要:
An intermediate material made up of an array of individualized ribbons, each ribbon being composed of a tape of unidirectional reinforcing fibers associated, by adhesion, on each of its faces with a veil of thermoplastic fibers.
摘要:
The invention relates to a method of making a composite material in which at least one reinforcement thread is deposited on a surface according to a path having at least one curved area on the deposition surface, wherein the reinforcement thread is connected to the surface by a polymeric binder, characterized in that a twist is applied to the reinforcement thread before the deposition thereof at least in order to compensate the length differences of the extreme paths of the thread on either side of the width as measured in a direction parallel to the deposition surface: the invention also relates to the composite material thus obtained.
摘要:
The present invention relates to a method for applying spot transverse forces to an intermediate material composed of a layer of unidirectional reinforcing fibers associated on at least one of its faces to a layer of thermoplastic and/or thermosetting material that does not represent more than 10% of the total weight of the intermediate material, wherein the spot transverse forces are applied while the intermediate material is under tension in the direction of the unidirectional reinforcing fibers.
摘要:
The invention provides a method of manufacturing a preform (120) from a reinforcement fabric by depositing a first fibre layer (112) and depositing a second fibre layer (114) partially over the first layer before cutting a plurality of preforms from the reinforcement fabric.
摘要:
The invention relates to a blank for compression moulding a part in a compression mould comprising one or more moulding recesses, said blank comprising a body formed from a first moulding compound comprising a fibrous reinforcement material and a thermo-curable resin material, and a region located on the surface of the body formed from a second moulding compound; said second moulding compound comprising a fibrous reinforcement material and a thermo-curable resin material, and exhibiting increased flow at one or more temperatures between 20° C. and the cured Tg of the first moulding compound compared to the flow of the first moulding compound at the same temperature.