EP0510097A1 - Process of forming fiber reinforced molded plastic articles and preforms therefor using a photosetting binder - Google Patents

Process of forming fiber reinforced molded plastic articles and preforms therefor using a photosetting binder

Info

Publication number
EP0510097A1
EP0510097A1 EP91903515A EP91903515A EP0510097A1 EP 0510097 A1 EP0510097 A1 EP 0510097A1 EP 91903515 A EP91903515 A EP 91903515A EP 91903515 A EP91903515 A EP 91903515A EP 0510097 A1 EP0510097 A1 EP 0510097A1
Authority
EP
European Patent Office
Prior art keywords
fibers
preform
mold
photohardenable
coated
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.)
Withdrawn
Application number
EP91903515A
Other languages
German (de)
French (fr)
Inventor
Rudolph Henry Boeckeler
Kenneth Austin Seroogy
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.)
Freeman Chemical Corp
Original Assignee
Freeman Chemical Corp
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 Freeman Chemical Corp filed Critical Freeman Chemical Corp
Publication of EP0510097A1 publication Critical patent/EP0510097A1/en
Withdrawn legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29BPREPARATION OR PRETREATMENT OF THE MATERIAL TO BE SHAPED; MAKING GRANULES OR PREFORMS; RECOVERY OF PLASTICS OR OTHER CONSTITUENTS OF WASTE MATERIAL CONTAINING PLASTICS
    • B29B11/00Making preforms
    • B29B11/14Making preforms characterised by structure or composition
    • B29B11/16Making preforms characterised by structure or composition comprising fillers or reinforcement
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/28Shaping operations therefor
    • B29C70/30Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core
    • B29C70/34Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core and shaping or impregnating by compression, i.e. combined with compressing after the lay-up operation
    • B29C70/345Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core and shaping or impregnating by compression, i.e. combined with compressing after the lay-up operation using matched moulds
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/003Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts characterised by the matrix material, e.g. material composition or physical properties
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C2791/00Shaping characteristics in general
    • B29C2791/001Shaping in several steps

Definitions

  • the invention relates to the art of making fiber reinforced molded articles. Specifically, the invention relates to an improved process for forming fiber preforms for use in molding such articles in which an ultraviolet light, poly erizable, photohardenable composition is employed as a preform binder.
  • preforms formed of glass or other fibers is a proven method of incorporating reinforcing fibers into complex shaped molds.
  • Such preforms have been used for a number of years in the art of forming molded articles utilizing matched die compression molds.
  • glass fibers are used as the reinforcing material, it has been common practice to chop glass fiber roving into shorter lengths.
  • the fibers were then deposited onto preform molds which often were in the shape of a specially designed screen having a size, shape and configuration conforming to that of the part to be molded. Even distri ⁇ bution of the chopped glass fibers on the preform mold has been achieved by use of a vacuum behind the screen.
  • the placement of holes and baffling the screen have also been utilized to control such distribution.
  • the binders used to bond the fibers together into a preform which can be handled have been of a heat curable type.
  • binder compositions are based on unsaturated polyester resins dispersed or dissolved in water. Commonly, such resins are diluted to a 5 to 7% solids concentration. This composition is sprayed on fibers and the binder composition is subsequently cured at elevated temperatures.
  • a forced air oven is required for curing in which temperatures in the 350° to 500 °F (175°C to 260°C) range are utilized.
  • the length of the curing cycle typically ranges between 20 seconds and several minutes, depending on the thickness of the preform and the air flow through the preform in the oven.
  • Various manual and automated methods have been used for this purpose. After curing, the preforms are moved from the screen, allowed to cool to ambient temperature, and then stored until they are used for molding.
  • the oven must have a relatively large exhaust stack to vent out the water vapor laden air. While it is possible to introduce heat exchangers to reduce some of the energy losses, this is not commonly done and, in any event, creates the need for additional equipment to deal with the condensed water vapor.
  • water vapor present in the exhaust air there are often volatile organic compounds also pre ⁇ sent which are vaporized or atomized from the glass and binders in the oven. Because the legally allowable limits for such emissions are constantly being reduced, the in ⁇ stallation of expensive scrubbing equipment or, alterna ⁇ tively, the development of new preform binders and/or glass fiber sizing technology, is required.
  • the present invention involves the use of ultraviolet light to cure a UV activated polymeric binder at or near* ambient temperatures.
  • the present invention thus eliminates the problems heretofore encountered with smoke generation and volatile organic compound emissions, reduces the difficulty of cleaning the equipment and, most importantly, greatly reduces the energy consumption of the process.
  • a further advantage of the present invention is the achievement of an enormous increase in the speed of preform production by greatly reducing the time required to cure the preforms.
  • An important object of the invention is to provide a very rapid and low energy consuming method for making fiber preforms which utilizes 100% solids or very high solid content ultraviolet curable thermoset binders.
  • a further object of the invention is to provide a low energy consuming method of rapidly bonding or attaching fiber appendages to existing preforms.
  • the present invention achieves the foregoing objects and advantages by providing a method of making fiber reinforced molded articles, which method may include the steps of first applying a layer of reinforcing fibers against a preform mold surface which has a configuration corresponding to that of the final molded article. The method then includes the step of coating the fibers with an ultraviolet light curable composition which contains a photohardenable material that is polymerizable under UV light and a polymerization photoinitiator. The fibers are coated to a degree sufficient to coat the individual fibers without filling the interstices among the fibers. 0 The thus coated fibers are then exposed to ultraviolet light to cure the composition. The resulting preform has the strength to be handled and stored for later use if desired, or transported in commerce.
  • the preform When used, the preform is placed in a mold with a de ⁇ formable plastic material.
  • the fiber preform and the plastic material are then molded together to form an article which consists of the plastic material containing the fibers therein as a fiber reinforcement.
  • the fiber reinforced plastic article is then removed from the mold and processed further in accordance with conventional practice.
  • any of the common UV curable resins and monomers may be used as the photohardenable material in practicing the invention.
  • suitable materials are unsaturated polyesters, ethacrylated and acrylated urethanes, methacrylated and acrylated epoxies, polyester acrylates, polyether acrylates, compositions containing allyl unsaturated and cationically polymerizable monomers and polymers in which UV radiation is used to unblock a cationic catalyst.
  • the photohardenable composition to the fibers on the mold is accomplished by spraying, roll coat application or transfer roll coat application, or other common coating transfer methods.
  • a number of layers of glass matt may be treated individually and subsequently stacked to form a multilayered preform. It is also possible to coat several layers simultaneously and then cure them together.
  • the amount of photohardenable material varies somewhat with the type of photohardenable material used as well with the type of fiber employed.
  • the UV curable binder generally comprises between 0.2 and 15% by weight of the total glass fibers.
  • the preferred binder content is in the 3 to 5% by weight range.
  • various other fibers such as carbon fibers, ceramic fibers, metal fibers, and plastic fibers such as polyester, polyethylene, aramide and other nylon fibers, may be used.
  • the speed and uniformity of UV curing is improved significantly by the use of fibers which are optically clear and, thus, capable of transmitting ultraviolet light through them.
  • the photohardenable binder composition can be further formulated with fillers, pigments, dyes and additives to improve rheology, adhesion to the fibers, cure rate and other process parameters.
  • the shape of the preform is constructed by wrapping glass fibers around a mandrel or mold of a desired shape to preconstructed matt ⁇ of chopped or continuous fibers, woven or non-woven fabrics, unidirectional or bidirectional stitched matts, or matts with sandwiched construction.
  • the reinforcing fibers may be continuous or chopped.
  • continuous or chopped glass fibers may be placed in a mold formed of a screen which is preferably transparent to UV radiation.
  • the preferred screen materials are glass or clear plastic, but other metallic or non-metallic materials may be substituted if desired.
  • the screen or mandrel is preselected to conform to the shape of the finished article. However, in some cases it may be desirable to preform several components or sections of the finished article individually, and to later combine the sections into a final composite article.
  • the composition containing the photohardenable material is preferably 100% reactive. In any event, it should be a high solid content composition which contains a photoinitiator.
  • the composition should be responsive to and harden when subjected to UV radiation in the range of from 200 nm (nanometers) to 500 nm. The preferred range is from 250 nm to 400 nm.
  • Any source of UV radiation commonly used for curing thin films may be employed.
  • Preferred sources are those with intensities of 200 watts or greater. Examples of such radiation sources are medium and high pressure
  • mercury vapor lamps and electrodeless mercury vapor lamps.
  • Examples of such units are those manufactured by Ashdee Corp., (Evansville, Indiana) and Fusion Systems, Inc. (Rockville, Maryland). Particularly advantageous for complex shapes are those sources which spread their energy
  • Preforms prepared in accordance with the invention can be used to make various reinforced plastic articles.
  • the plastic employed may either be thermoplastic or thermoset- ting.
  • Examples of the finished articles are items used in the transportation, construction, furniture, recreational, marine, agricultural, and electrical industries.
  • the fin- ished articles are made by placing the preform together with a thermosetting or thermoplastic material in an enclosed mold zone having a shape conforming to the finished product. The materials in the mold zone are then heated and compressed to form the molded shape. If the plastic deformable material is a thermoplastic, the material can be preheated to its deformation temperature and then forced within the mold cavity containing the preform to form the molded shape and thereafter allowed to cool and solidify. If a thermosetting plastic material is used, the plastic composition can be mixed, placed in the mold and heated to cure within the mold.
  • the mold may be heated by any available conventional means, such as microwave, hot oil, steam, radiant heaters, sonic heaters, or the like.
  • Thermosetting materials include but are not limited to polyester, epoxy, polyurethane, polyisocyanurate, polyurea and phenolic molding resins.
  • thermosetting mixture is one containing approximately 55% by weight styrene containing polyester resin, 44% by weight calcium carbonate and 0.5% by weight of a benzoyl peroxide catalyst mixture and 0.5% for an internal mold release composition.
  • Such mixtures can be molded at pressures of approximately 200 to 2,000 psi (14 to 140 Kg per square centimeters) in a mold cavity heated to approximately 300° F (150°C) and will cure within the mold in approximately 1-2 minutes.
  • the resulting glass composite was stiff and held its shape well. No odor of uncured resin could be detected.
  • a small piece of woven glass was bonded (stitched) 10 onto the composite using the same procedure.
  • the binder constituted 4.5% of the total weight of the treated glass.
  • Flat sheets of treated glass were exposed to ultraviolet radiation emitted by one 200 watt per inch mercury vapor lamp in an Ashdee UV cure unit.
  • the glass matt was passed under the UV lamp at a rate of 100 feet (30.5m) per minute (approximately 0.4 second exposure). Upon exiting from the UV unit, the matt was stiff and no odor of uncured resin could be detected.
  • One layer of glass matt treated with the composition of Example 2 was wrapped around a steel cylinder of 2 inch (5.1cm) diameter and secured with clear adhesive tape. The part was rotated under the 200 watt per inch lamp for 1-2 seconds. Upon removal of the tape and cylinder, the glass matt was rigid and held its cylindrical shape.
  • the UV curable binder system of Example 2 was applied to continuous strand glass by drawing down a film onto a glass plate, placing the glass fiber onto the film and rolling the glass with a hard rubber printer's roller to distribute the binder.
  • the binder contents varied from 3% to 5% by weight of the total glass.
  • the molded glass was then exposed by passing through the mold ultraviolet light emitted by a 118 watt per centimeter electrodeless lamp (Fusion Systems, Inc. "H bulb"). After 15-30 seconds of exposure, the glass was rigid, non-tacky and retained its molded shape after removal of the acrylic mold.
  • a 118 watt per centimeter electrodeless lamp Fusion Systems, Inc. "H bulb”
  • Example 4 The procedure of Example 4 was followed except the source of ultraviolet light is a 400 watt mercury vapor lamp with an elliptical reflector manufactured by Dr. Hoenle, West Germany. The glass was rigid, non-tacky and held its shape after removal from the mold.
  • EXAMPLE 6 The procedure of Example 4 was followed except the source of ultraviolet light is a 400 watt mercury vapor lamp with an elliptical reflector manufactured by Dr. Hoenle, West Germany. The glass was rigid, non-tacky and held its shape after removal from the mold.
  • Example 4 The procedure of Example 4 was followed except the source of ultraviolet light is high pressure mercury short arc lamp with an output of 100 milliwatts/cm2 and light was delivered by a flexible optical light guide.
  • the unit was manufactured by National Engineered Fiber Optics Systems, Inc.
  • the glass was rigid, non-tacky and held its shape after 15-30 seconds exposure.
  • Examples 4, 5 and 6 were repeated with a binder consisting of 70 parts epoxy acrylate oligomer (CHEMPOL® 19-6600, Freeman Chemical Corporation), 25 parts tripropylene glycol diacrylate (CL Industries, Georgetown, Illinois), 2 parts benzildimethyl ketal (Irgacure 651, Ciba Geigy Corporation), 3 parts N-methyl diethanolamine and 5 parts methyl ethyl ketone.
  • the binder is a clear, colorless liquid with viscosity of 450 cps at 25°C.
  • Examples 4, 5 and 6 were repeated with a polymerizable resin produced from combining acrylic acid, the diglycidyl ether of 1,4 butane diol and 3,3', 4,4' benzophenone tetracarboxylic dianhydride (BTDA) .
  • the resin so prepared is a product of Freeman Chemical Corporation and is designated CHEMPOL® 19-4837.
  • the glass composite was rigid, non-tacky and held its shape after removal from the acrylic mold.
  • a 3" x 5" triangular-shaped appendage was "stitched" onto the glass composite of Example 7 by applying a band of the binder system of Example 1 to the point at which the fin-shaped appendage makes contact with the bumper beam and exposing the binder to the optical wand delivered UV radiation from a 100 milliwatt per sq. cm. high pressure mercury vapor short arc lamp (Efos unit) . After 5-10 seconds exposure, the fin was tightly bonded to the bumper beam-shaped glass composite.
  • Example 7 The composition of Example 7 was applied to three layers of continuous strand glass matt by spraying
  • Example 10 The procedure of Example 10 was followed for treating and curing of preform binder. Three layer panels of glass with binder contents of 0%, 4.6%, 6.8% and 8.4% were thusly prepared. Each of the three layers of glass were placed in the RTM mold described in Example 10.

Abstract

Cette invention concerne un procédé pour fabriquer des articles moulés renforcés par des fibres et des préformes destinées à être utilisées dans la fabrication d'articles moulés de ce type. Ce procédé comprend les étapes suivantes: l'application d'une couche de fibres de renforcement, préférablement des fibres de verre, sur la surface d'un moule de préforme dont la configuration correspond au moins partiellement à l'article final moulé; l'enduction des fibres avec une composition durcissant à la lumière ultraviolette qui comprend un matériau photodurcissable polymérisant sous l'effet de la lumière ultraviolette et un photoinitiateur de polymérisation; l'exposition des fibres enrobées, à la lumière ultraviolette pour durcir la composition; et le retrait de la préforme, résultant de l'opération, de la surface du moule de préforme. La préforme est ensuite utilisée en la plaçant, ainsi qu'un matériau plastique déformable, dans un moule, où un article contenant du plastique renforcé par les fibres est alors formé.This invention relates to a process for making fiber reinforced molded articles and preforms for use in the manufacture of such molded articles. This method comprises the following steps: applying a layer of reinforcing fibers, preferably glass fibers, to the surface of a preform mold, the configuration of which corresponds at least partially to the final molded article; coating the fibers with an ultraviolet light curing composition which comprises a photocurable material curing under the effect of ultraviolet light and a curing photoinitiator; exposing the coated fibers to ultraviolet light to cure the composition; and removing the preform, resulting from the operation, from the surface of the preform mold. The preform is then used by placing it, along with a deformable plastic material, in a mold, where an article containing fiber reinforced plastic is then formed.

Description

PROCESS OF FORMING FIBER REINFORCED MOLDED PLASTIC ARTICLES AND PREFORMS THEREFORE USING A PHOTOSETTING BINDER
Cross Reference to Related Applications, If Any:
This application is a continuation in part of co-pending application Serial No. 07/463,388 filed January 11, 1990.
BACKGROUND OF THE INVENTION
Field of -the Invention
The invention relates to the art of making fiber reinforced molded articles. Specifically, the invention relates to an improved process for forming fiber preforms for use in molding such articles in which an ultraviolet light, poly erizable, photohardenable composition is employed as a preform binder.
The use of preforms formed of glass or other fibers is a proven method of incorporating reinforcing fibers into complex shaped molds. Such preforms have been used for a number of years in the art of forming molded articles utilizing matched die compression molds. When glass fibers are used as the reinforcing material, it has been common practice to chop glass fiber roving into shorter lengths. The fibers were then deposited onto preform molds which often were in the shape of a specially designed screen having a size, shape and configuration conforming to that of the part to be molded. Even distri¬ bution of the chopped glass fibers on the preform mold has been achieved by use of a vacuum behind the screen. The placement of holes and baffling the screen have also been utilized to control such distribution.
Heretofore, the binders used to bond the fibers together into a preform which can be handled have been of a heat curable type. Typically, such binder compositions are based on unsaturated polyester resins dispersed or dissolved in water. Commonly, such resins are diluted to a 5 to 7% solids concentration. This composition is sprayed on fibers and the binder composition is subsequently cured at elevated temperatures. Typically, a forced air oven is required for curing in which temperatures in the 350° to 500 °F (175°C to 260°C) range are utilized. The length of the curing cycle typically ranges between 20 seconds and several minutes, depending on the thickness of the preform and the air flow through the preform in the oven. Various manual and automated methods have been used for this purpose. After curing, the preforms are moved from the screen, allowed to cool to ambient temperature, and then stored until they are used for molding.
There are a number of disadvantages to these conventional methods of manufacturing preforms. Firstly, the procedures are relatively slow, in that typically the preform requires 1 to 3 minutes in the oven to cure, and UP to an additional 30 seconds to cool down sufficiently for removal from the screen. Secondly, the heating required often bakes the over sprayed binder to a point that makes it very difficult to clean the preform screens and associated equipment. However, more importantly, the process is very energy intensive. Large motors are required to produce sufficient vacuum behind the screen and, thus, the airflow to and through the screen requires a large amount of energy. The high temperatures required to cure the binder and the high air flow required within the oven to remove the water and cure the binder is also highly energy intensive. In addition, the oven must have a relatively large exhaust stack to vent out the water vapor laden air. While it is possible to introduce heat exchangers to reduce some of the energy losses, this is not commonly done and, in any event, creates the need for additional equipment to deal with the condensed water vapor. In addition to water vapor present in the exhaust air, there are often volatile organic compounds also pre¬ sent which are vaporized or atomized from the glass and binders in the oven. Because the legally allowable limits for such emissions are constantly being reduced, the in¬ stallation of expensive scrubbing equipment or, alterna¬ tively, the development of new preform binders and/or glass fiber sizing technology, is required.
It is an object of the present invention to overcome these problems by providing a new process of manufacturing preforms in which the curing can be performed at ambient temperatures. More specifically, the present invention involves the use of ultraviolet light to cure a UV activated polymeric binder at or near* ambient temperatures. The present invention thus eliminates the problems heretofore encountered with smoke generation and volatile organic compound emissions, reduces the difficulty of cleaning the equipment and, most importantly, greatly reduces the energy consumption of the process. A further advantage of the present invention is the achievement of an enormous increase in the speed of preform production by greatly reducing the time required to cure the preforms. An important object of the invention is to provide a very rapid and low energy consuming method for making fiber preforms which utilizes 100% solids or very high solid content ultraviolet curable thermoset binders. A further object of the invention is to provide a low energy consuming method of rapidly bonding or attaching fiber appendages to existing preforms.
The present invention achieves the foregoing objects and advantages by providing a method of making fiber reinforced molded articles, which method may include the steps of first applying a layer of reinforcing fibers against a preform mold surface which has a configuration corresponding to that of the final molded article. The method then includes the step of coating the fibers with an ultraviolet light curable composition which contains a photohardenable material that is polymerizable under UV light and a polymerization photoinitiator. The fibers are coated to a degree sufficient to coat the individual fibers without filling the interstices among the fibers. 0 The thus coated fibers are then exposed to ultraviolet light to cure the composition. The resulting preform has the strength to be handled and stored for later use if desired, or transported in commerce.
-~, Alternatively, it is an object of the present invention to provide a method of making fiber reinforced molded articles by coating the reinforcing fibers with an ultraviolet light composition, placing the coated fibers against a preform mold surface and curing them with ultraviolet light.
When used, the preform is placed in a mold with a de¬ formable plastic material. The fiber preform and the plastic material are then molded together to form an article which consists of the plastic material containing the fibers therein as a fiber reinforcement. The fiber reinforced plastic article is then removed from the mold and processed further in accordance with conventional practice.
Any of the common UV curable resins and monomers may be used as the photohardenable material in practicing the invention. Examples of suitable materials are unsaturated polyesters, ethacrylated and acrylated urethanes, methacrylated and acrylated epoxies, polyester acrylates, polyether acrylates, compositions containing allyl unsaturated and cationically polymerizable monomers and polymers in which UV radiation is used to unblock a cationic catalyst.
Application of the photohardenable composition to the fibers on the mold is accomplished by spraying, roll coat application or transfer roll coat application, or other common coating transfer methods. In a further aspect of the invention, a number of layers of glass matt may be treated individually and subsequently stacked to form a multilayered preform. It is also possible to coat several layers simultaneously and then cure them together. The amount of photohardenable material varies somewhat with the type of photohardenable material used as well with the type of fiber employed. In the case of glass fiber preforms, the UV curable binder generally comprises between 0.2 and 15% by weight of the total glass fibers. The preferred binder content is in the 3 to 5% by weight range.
In addition to glass fibers, various other fibers, such as carbon fibers, ceramic fibers, metal fibers, and plastic fibers such as polyester, polyethylene, aramide and other nylon fibers, may be used. The speed and uniformity of UV curing is improved significantly by the use of fibers which are optically clear and, thus, capable of transmitting ultraviolet light through them.
If desired, peroxides and/or metallic dryers may be incorporated in the photohardenable composition to improve curing of any areas which may not receive sufficient UV radiation. In accordance with conventional practice, the photohardenable binder composition can be further formulated with fillers, pigments, dyes and additives to improve rheology, adhesion to the fibers, cure rate and other process parameters.
The shape of the preform is constructed by wrapping glass fibers around a mandrel or mold of a desired shape to preconstructed mattε of chopped or continuous fibers, woven or non-woven fabrics, unidirectional or bidirectional stitched matts, or matts with sandwiched construction. The reinforcing fibers may be continuous or chopped. Alternatively, continuous or chopped glass fibers may be placed in a mold formed of a screen which is preferably transparent to UV radiation. The preferred screen materials are glass or clear plastic, but other metallic or non-metallic materials may be substituted if desired. Generally, the screen or mandrel is preselected to conform to the shape of the finished article. However, in some cases it may be desirable to preform several components or sections of the finished article individually, and to later combine the sections into a final composite article.
The composition containing the photohardenable material is preferably 100% reactive. In any event, it should be a high solid content composition which contains a photoinitiator. The composition should be responsive to and harden when subjected to UV radiation in the range of from 200 nm (nanometers) to 500 nm. The preferred range is from 250 nm to 400 nm.
5
Any source of UV radiation commonly used for curing thin films may be employed. Preferred sources are those with intensities of 200 watts or greater. Examples of such radiation sources are medium and high pressure
10 mercury vapor lamps and electrodeless mercury vapor lamps. Examples of such units are those manufactured by Ashdee Corp., (Evansville, Indiana) and Fusion Systems, Inc. (Rockville, Maryland). Particularly advantageous for complex shapes are those sources which spread their energy
I**** over a large area, such as pulse lamps with multidirectional reflectors (similar to units manufactured by 1ST America, Nashville, Tennessee). Especially suitable for concentrating energy when it is desired to attach a small appendage to a larger preform are sources
2 directing energy by means of a flexible optical wand.
National Engineered Fiber Optic Systems, Inc. of Buffalo, New York, and Uvex, Inc. of Mountain View, California are suppliers of optical wand UV delivery systems.
25 Preforms prepared in accordance with the invention can be used to make various reinforced plastic articles. The plastic employed may either be thermoplastic or thermoset- ting. Examples of the finished articles are items used in the transportation, construction, furniture, recreational, marine, agricultural, and electrical industries. The fin- ished articles are made by placing the preform together with a thermosetting or thermoplastic material in an enclosed mold zone having a shape conforming to the finished product. The materials in the mold zone are then heated and compressed to form the molded shape. If the plastic deformable material is a thermoplastic, the material can be preheated to its deformation temperature and then forced within the mold cavity containing the preform to form the molded shape and thereafter allowed to cool and solidify. If a thermosetting plastic material is used, the plastic composition can be mixed, placed in the mold and heated to cure within the mold. The mold may be heated by any available conventional means, such as microwave, hot oil, steam, radiant heaters, sonic heaters, or the like.
Thermosetting materials include but are not limited to polyester, epoxy, polyurethane, polyisocyanurate, polyurea and phenolic molding resins.
An example of a thermosetting mixture is one containing approximately 55% by weight styrene containing polyester resin, 44% by weight calcium carbonate and 0.5% by weight of a benzoyl peroxide catalyst mixture and 0.5% for an internal mold release composition. Such mixtures can be molded at pressures of approximately 200 to 2,000 psi (14 to 140 Kg per square centimeters) in a mold cavity heated to approximately 300° F (150°C) and will cure within the mold in approximately 1-2 minutes.
The invention will further be illustrated by means of the following examples wherein all parts referred to are by weight, unless otherwise noted.
EXAMPLE 1
An ultraviolet curable binder containing 70 parts of urethane diacrylate oligomer (CHEMPOL® 19-4830, a product of Freeman Chemical Corporation), 25 parts trimethylolpropane trimethacrylate (Sartomer Co. SR 350), 2 parts 2-hydroxy-2-methyl-l-phenyl-propane-l-one (E.
Merck, Darocure 1173), 3 parts N-methyldiethanolamine and 5 parts methyl ethyl ketone was applied to continuous strand glass at a concentration of approximately 3 grams binder per 33 grams glass. Four layers of treated glass were sandwiched in an acrylic mold and exposed for 30 seconds on each side to 400 watts UV radiation from a portable Hoenle mercury vapor ultraviolet lamp having a UV output of 400 watts.
The resulting glass composite was stiff and held its shape well. No odor of uncured resin could be detected.
A small piece of woven glass was bonded (stitched) 10 onto the composite using the same procedure.
EXAMPLE 2
15 An ultraviolet curable epoxy acrylate resin (CHEMPOL®
19-4837) prepared in accordance with the teaching of U.S. Patent No. 4,216,306, issued August 5, 1980, and assigned to the assigner of the present invention, and containing benzophenone photoinitiator coreacted on its backbone and
20 having a viscosity of 4900 cps at 25°C was applied to con¬ tinuous strand whirl matt glass by spraying or transferring from a thin film on polyester sheet.
By weighing the glass before and after treating with 25 resin, it was determined that the binder constituted 4.5% of the total weight of the treated glass. Flat sheets of treated glass were exposed to ultraviolet radiation emitted by one 200 watt per inch mercury vapor lamp in an Ashdee UV cure unit. The glass matt was passed under the UV lamp at a rate of 100 feet (30.5m) per minute (approximately 0.4 second exposure). Upon exiting from the UV unit, the matt was stiff and no odor of uncured resin could be detected.
EXAMPLE 3
One layer of glass matt treated with the composition of Example 2 was wrapped around a steel cylinder of 2 inch (5.1cm) diameter and secured with clear adhesive tape. The part was rotated under the 200 watt per inch lamp for 1-2 seconds. Upon removal of the tape and cylinder, the glass matt was rigid and held its cylindrical shape.
EXAMPLE 4
The UV curable binder system of Example 2 was applied to continuous strand glass by drawing down a film onto a glass plate, placing the glass fiber onto the film and rolling the glass with a hard rubber printer's roller to distribute the binder. The binder contents varied from 3% to 5% by weight of the total glass.
Four layers of the thusly treated glass were sandwiched in a two-part clear acrylic mold in the shape of an automotive bumper beam 24 inches (61cm) in length, three inches (7.6cm) in width and three inches (7.6cm) in height.
The molded glass was then exposed by passing through the mold ultraviolet light emitted by a 118 watt per centimeter electrodeless lamp (Fusion Systems, Inc. "H bulb"). After 15-30 seconds of exposure, the glass was rigid, non-tacky and retained its molded shape after removal of the acrylic mold.
EXAMPLE 5
The procedure of Example 4 was followed except the source of ultraviolet light is a 400 watt mercury vapor lamp with an elliptical reflector manufactured by Dr. Hoenle, West Germany. The glass was rigid, non-tacky and held its shape after removal from the mold. EXAMPLE 6
The procedure of Example 4 was followed except the source of ultraviolet light is high pressure mercury short arc lamp with an output of 100 milliwatts/cm2 and light was delivered by a flexible optical light guide. The unit was manufactured by National Engineered Fiber Optics Systems, Inc. The glass was rigid, non-tacky and held its shape after 15-30 seconds exposure.
EXAMPLE 7
The application and curing procedures of Examples 4, 5 and 6 were repeated with a binder consisting of 70 parts epoxy acrylate oligomer (CHEMPOL® 19-6600, Freeman Chemical Corporation), 25 parts tripropylene glycol diacrylate (CL Industries, Georgetown, Illinois), 2 parts benzildimethyl ketal (Irgacure 651, Ciba Geigy Corporation), 3 parts N-methyl diethanolamine and 5 parts methyl ethyl ketone. The binder is a clear, colorless liquid with viscosity of 450 cps at 25°C.
After 15-30 seconds exposure, the glass composite was rigid, non-tacky and held the shape of the mold. EXAMPLE 8
The application and curing procedures of Examples 4, 5 and 6 were repeated with a polymerizable resin produced from combining acrylic acid, the diglycidyl ether of 1,4 butane diol and 3,3', 4,4' benzophenone tetracarboxylic dianhydride (BTDA) . The resin so prepared is a product of Freeman Chemical Corporation and is designated CHEMPOL® 19-4837.
After 30-45 seconds, the glass composite was rigid, non-tacky and held its shape after removal from the acrylic mold.
EXAMPLE 9
A 3" x 5" triangular-shaped appendage was "stitched" onto the glass composite of Example 7 by applying a band of the binder system of Example 1 to the point at which the fin-shaped appendage makes contact with the bumper beam and exposing the binder to the optical wand delivered UV radiation from a 100 milliwatt per sq. cm. high pressure mercury vapor short arc lamp (Efos unit) . After 5-10 seconds exposure, the fin was tightly bonded to the bumper beam-shaped glass composite. EXAMPLE 10
The composition of Example 7 was applied to three layers of continuous strand glass matt by spraying
5 with a low pressure spray gun manufactured by Croix Air Products, Inc. Binder content was 6% by weight. The treated glass was exposed for 8 seconds to ultraviolet radiation of a 200 watt per inch mercury vapor lamp (Ashdee Model 25H/2A UV curing unit). Next, the cured in treated glass was placed into an 45.7cm x 45.7cm x 0.32cιr. aluminum resin transfer mold. A 2 part epoxy molding resin based on a diglycidyl ether of biεphenol A (Epon 828) and 1,2 diaminocyclohexane hardner (Shell Chemical Co.) was injected into the RTM mold under low pressure.
15
After maintaining the mold temperture at 66°C for 1 hour, the hardening panel was removed from the mold and post cured for 2 hours at 135°C. Physical properties were determined and compared to a control panel prepared
20 with 3 layers of untreated glass. Results are summarized in Table I.
EXAMPLE 11
The procedure of Example 10 was followed for treating and curing of preform binder. Three layer panels of glass with binder contents of 0%, 4.6%, 6.8% and 8.4% were thusly prepared. Each of the three layers of glass were placed in the RTM mold described in Example 10.
Next, a dicyclopentadiene-based polyester molding resin, (Stypol 40-0824 from Freeman Chemical
Corp. ) was injected under low pressure into the mold held at 54°C. The hardened panel was removed from the mold after 60 seconds and post hardened for 2 hours at 135°C. Physical properties of treated and untreated glass reinforced polyester composites are shown in Table II.
TABLE I
PHYSICAL PROPERTIES OF GLASS REINFORCED
EPOXY MOLDING COMPOUND
% PREFORM BINDER
PROPERTY 0 6
Shore D Hardness 86 86
Impact Strength (Convert to Metric)
Izod Notched (lib/in.) 10.33 8.97
Izod unnotched (lib/in.) 9.52 13.53
Flexural Strength (PSI) 1093.0 1465.8
Flexural Modulus (PSI) 52358.0 61390.4
Tensile Strength (PSI) 735.9 645.0
Tensile Modulus (PSI) 41157.2 43224.5
% Tensile Elongation 3.19 2.78
Heat Distortion Temperature (°C) >140 >140 TABLE II
PHYSICAL PROPERTIES OF GLASS REINFORCED POLYESTER
MOLDING COMPOUND
% BINDER
PROPERTY 4_;_6 6_;_8 8_;_4
Shore D Hardness 86 86 86 85
Impact Strength
(Note must convert to metric for Foreign Filing)
IZOD Notched (lb./in. ) 11.98 14..48 14.40 14.92
IZOD Unnotched (lb./in.) 16.27 22.38 18.99 18.96
Flexural Strength (PSI) 1669.5 2395.5 1922.6 1761.9
Flexural Modulus (PSI) 75611.4 87868.3 82800.1 73958.6
Tensile Strength (PSI) 831.7 920.2 1025.0 958.7
Tensile Modulus (PSI) 61695.7 64885.0 64895.2 57074.6
% Tensile Elongation 2.45 2.45 2.87 2.87
Heat Distortion Temp. (°C) >140 >140 >140 >140

Claims

What is claimed is:
1. A method of making fiber reinforced molded articles comprising: a. applying a layer of reinforcing fibers on a preform mold surface which has a configuration corresponding to at least a portion of the final molded article, b. coating at least some of said fibers with an
10 ultraviolet light curable composition which contains a photohardenable material polymerizable under UV light and a polymerization photoinitiator, to a degree sufficient to coat said fibers without filling the interstices among said fibers,
jc c. exposing said coated fibers to UV light to cure said composition, d. removing the resulting preform from said preform mold surface, e. placing said preform and a deformable plastic 20 material in a mold, f. molding said preform and said plastic material together to form an article comprising said plastic with said fibers contained therewithin as a reinforcement, and, g. removing the resulting fiber reinforced 25 plastic article from said mole.
2. A method according to Claim 1, wherein uncoated reinforcing fibers are initially applied to the mold surface and then coated with said ultraviolet light curable composition prior to exposure to said UV light source.
3. A method according to Claim 1, wherein said reinforcing fibers are pre-coated with said ultraviolet light curable composition prior to being applied to said preform mold surface prior to exposure to said UV light source.
4. A method according to Claim 1, wherein said photohardenable composition is selected from the group consisting of unsaturated polyesters, methacrylated urethanes, acrylated urethanes, acrylated epoxies, methacrylated epoxies, polyether acrylate resins, polyether methacrylate resins, acrylated polyesters, methacrylated polyesters, compositions containing allyl unsaturated and cationically polymerizable compositions containing a blocked cationic catalyst which can be unblocked by UV radiation, or mixtures of the above photohardenable compositions and polyethylenically unsaturated organic monomers.
5. A method according to Claim 1, wherein said pre¬ form mold comprises a screen or a material transparent to UV radiation having a shape conforming to that of the part to be molded.
6. A method according to Claim 1, wherein said pre¬ form mold comprises a mandrel around which said fibers are deposited.
7. A method according to Claim 1, wherein said fibers are optically clear.
8. A method according to Claim 1, wherein said fibers are glass fibers, and said photohardenable composition is coated thereon in an amount of about .0.2 to 15% by weight of said fibers.
9. A method according to Claim 1, wherein said compo¬ sition also contains a peroxide curable material and a peroxide catalyst.
10. A method of making fiber reinforcement preform for use in making fiber reinforced molded articles comprising: a. applying a layer of reinforcing fibers on a preform mold surface which has a configuration corres¬ ponding to at least a portion of the final molded article. b. coating said fiber-εlwith an ultraviolet light curable composition which contains a photohardenable mate¬ rial polymerizable under UV light and a polymerization photoinitiator, to a degree sufficient to coat said fibers without filling the interstices among said fibers, c. exposing said coated fibers to UV light to cure said composition, d. removing the resulting preform from said pre¬ form mold surface.
11. A method according to Claim 10, wherein uncoated reinforcing fibers are initially applied to the mold sur¬ face and then coated with said ultraviolet light curable composition prior to exposure to said UV light source.
12. A method according to Claim 10, wherein said rein¬ forcing fibers are pre-coated with said ultraviolet light curable composition prior to being applied to said preform mold surface prior to exposure to said UV light source.
13. A method according to Claim 10, wherein said photohardenable composition is selected from the group consisting of unsaturated polyesters, methacrylated urethanes, acrylated urethanes, acrylated epoxies, methacrylated epoxies, polyether acrylates, polyether methacrylates, acrylated polyester resins, compositions containing allyl unsaturation and cationically polymer¬ izable compositions containing a blocked cationic catalyst which can be unblocked by UV radiation, or mixtures of the above photohardenable compositions and polyethylenically unsaturated organic monomers.
14. A method according to Claim 10, wherein said pre¬ form mold comprises a screen or transparent mold having a shape conforming to that of the part to be molded.
15. A method according to Claim 10, wherein said pre¬ form mold comprises a mandrel around which said fibers are deposited.
16. A method according to Claim 10, wherein said fibers are optically clear.
17. A method according to Claim 10, wherein said fi¬ bers are glass fibers, and said photohardenable compoεi- tion is coated thereon in an amount of about 0.2 to 15% by weight of said fibers.
18. A method according to Claim 10, wherein said com¬ position also contains a peroxide curable material and a peroxide catalyst.
EP91903515A 1990-01-11 1990-12-19 Process of forming fiber reinforced molded plastic articles and preforms therefor using a photosetting binder Withdrawn EP0510097A1 (en)

Applications Claiming Priority (4)

Application Number Priority Date Filing Date Title
US46338890A 1990-01-11 1990-01-11
US463388 1990-01-11
US60999790A 1990-11-07 1990-11-07
US609997 1990-11-07

Publications (1)

Publication Number Publication Date
EP0510097A1 true EP0510097A1 (en) 1992-10-28

Family

ID=27040639

Family Applications (1)

Application Number Title Priority Date Filing Date
EP91903515A Withdrawn EP0510097A1 (en) 1990-01-11 1990-12-19 Process of forming fiber reinforced molded plastic articles and preforms therefor using a photosetting binder

Country Status (6)

Country Link
EP (1) EP0510097A1 (en)
JP (1) JPH05505352A (en)
KR (1) KR920703286A (en)
AU (1) AU660407B2 (en)
CA (1) CA2073682C (en)
WO (1) WO1991010547A1 (en)

Families Citing this family (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0620091B1 (en) * 1990-07-12 1996-08-14 The C.A. Lawton Company Method and apparatus for making structural reinforcement preforms including energetic basting and stitching
US5192387A (en) * 1990-11-05 1993-03-09 The C.A. Lawton Company Method of making preforms
US5217654A (en) * 1992-01-30 1993-06-08 The C. A. Lawton Company Two-stage mat forming preforming and molding process
ZA93819B (en) * 1992-02-24 1993-10-15 Cook Composites & Polymers Process of making a rigid multi-layer preform
FR2700171B1 (en) * 1993-01-07 1995-02-24 Vetrotex France Sa Process for the preparation of glass-resin prepregs intended for the manufacture of composite parts.
FI102945B (en) * 1995-02-24 1999-03-31 Stick Tech Oy Prepreg, a process for its preparation, a composite based on the aforementioned prereg and its use
US5882462A (en) * 1996-02-02 1999-03-16 Dow-United Technologies Composite Products Method for fabricating a corrugated composite channel
WO1999015323A1 (en) * 1997-09-19 1999-04-01 Dow-United Technologies Composite Products, Inc. Method for fabricating a corrugated composite channel
KR20020088794A (en) * 2001-05-21 2002-11-29 유림산업 주식회사 Reinforced plastic have granite pattern and manufacture method thereof
DE10161773A1 (en) * 2001-12-15 2003-06-26 Bayerische Motoren Werke Ag Method for producing a three-dimensionally shaped fiber composite plastic component
ATE458624T1 (en) * 2004-03-30 2010-03-15 Asahi Kasei Chemicals Corp HOLLOW CYINDRICAL PRESSURE ELEMENT
TW200716361A (en) * 2005-07-27 2007-05-01 Mitsubishi Heavy Ind Ltd Rtm process
DE102006048920B3 (en) * 2006-10-10 2008-05-21 Fraunhofer-Gesellschaft zur Förderung der angewandten Forschung e.V. Preparing light-weight component, useful e.g. in vehicle, comprises pre-impregnating semi-fabricated product having e.g. glass and electrically conductive fiber, inserting product into heatable molding tool, applying pressure and hardening
DE102008028865B4 (en) * 2008-06-19 2015-04-02 Airbus Defence and Space GmbH Process for the production of fiber composite profile components, as well as use of such manufactured fiber composite profile components
JP2012001665A (en) * 2010-06-18 2012-01-05 Asahi Organic Chemicals Industry Co Ltd Sheet material, piping member, and method of manufacturing sheet material

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US442587A (en) * 1890-12-09 Fender for street-cars
SE420991B (en) * 1978-02-13 1981-11-16 Scandinavian Glasfiber Ab KIT FOR PREPARATION OF FORMULA OF GLASS FIBER ARMED HARDWARE
DE2931737A1 (en) * 1979-08-04 1981-02-26 Basf Ag METHOD FOR PRODUCING MOLDED BODIES FROM UNSATURATED POLYESTER RESINS
US4692291A (en) * 1980-04-14 1987-09-08 Union Carbide Corporation Molding method using fast curing fiber reinforced, low viscosity thermosetting resin
DE3109424A1 (en) * 1981-03-12 1982-10-28 Herbert 7140 Ludwigsburg Schreiber METHOD FOR THE PRODUCTION OF FIBER REINFORCED PLASTIC OBJECTS AND PREPREG FOR ITS IMPLEMENTATION AND ITEMS OBTAINED THEREOF
DE3636755A1 (en) * 1986-10-29 1988-05-05 Basf Ag METHOD FOR PRODUCING HOLLOW BODIES

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
See references of WO9110547A1 *

Also Published As

Publication number Publication date
WO1991010547A1 (en) 1991-07-25
JPH05505352A (en) 1993-08-12
CA2073682C (en) 2002-02-19
AU7220391A (en) 1991-08-05
CA2073682A1 (en) 1991-07-12
AU660407B2 (en) 1995-06-29
KR920703286A (en) 1992-12-17

Similar Documents

Publication Publication Date Title
AU660407B2 (en) Process of forming fiber reinforced molded plastic articles and preforms therefor using a photosetting binder
US5382148A (en) Two-stage mat forming, preforming and molding apparatus
JP3121461B2 (en) Mat production method and its equipment
JP4969717B2 (en) Manufacturing method of composite parts subjected to strong stress
EP0380591B1 (en) Fiber/resin composites, and method of making the same
US20030175520A1 (en) Formed composite structural members and methods and apparatus for making the same
JP2004510842A (en) Sheet (SMC) molding compound with vented structure for trapped gas
JP2003260717A (en) Method for manufacturing hollow reinforced resin composite material article
KR850001250B1 (en) Process of fiber reinforced thermoplastics resins
AU654884B2 (en) Method for making preforms
JP3754525B2 (en) Decorative molding sheet, method for producing the same, and method for producing fiber reinforced thermoplastic resin foam using the decorative molding sheet
JP3115023B2 (en) Manufacturing method of fiber reinforced resin molded product
JPH01176531A (en) Manufacture of molding having protective layer
US20040094875A1 (en) Method for making a composite construction panel
KR101725523B1 (en) Process Of Producing Carbon Fiber Prepreg And Process Of Producing Carbon Fiber Thrmoplastic Composite Using PhotoThermosetting
JP4295742B2 (en) Continuous molding method of fiber reinforced plastic sheet
TW209872B (en)
KR100236895B1 (en) Mat forming process and apparatus
JP2000210963A (en) Energy beam emitting type continuously molding machine and fiber-reinforced plastic plate-like molding
JPH0137259B2 (en)
US20040094874A1 (en) Method for making a composite construction panel
JP2554708B2 (en) Method for manufacturing long composite molded body
JPS62773B2 (en)
JPH0788998A (en) Fiber-reinforced thermoplastic resin laminated body
JPH07164543A (en) Manufacture of fiber reinforced resin composite

Legal Events

Date Code Title Description
PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

Free format text: ORIGINAL CODE: 0009012

17P Request for examination filed

Effective date: 19920708

AK Designated contracting states

Kind code of ref document: A1

Designated state(s): AT BE CH DE DK ES FR GB GR IT LI LU NL SE

17Q First examination report despatched

Effective date: 19940222

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: THE APPLICATION IS DEEMED TO BE WITHDRAWN

18D Application deemed to be withdrawn

Effective date: 19960426