WO1989005718A1 - Process and compression mould for manufacture of composite parts - Google Patents
Process and compression mould for manufacture of composite parts Download PDFInfo
- Publication number
- WO1989005718A1 WO1989005718A1 PCT/SE1988/000682 SE8800682W WO8905718A1 WO 1989005718 A1 WO1989005718 A1 WO 1989005718A1 SE 8800682 W SE8800682 W SE 8800682W WO 8905718 A1 WO8905718 A1 WO 8905718A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- mould
- tool
- manufacture
- stages
- mould half
- Prior art date
Links
- 239000002131 composite material Substances 0.000 title claims abstract description 8
- 238000004519 manufacturing process Methods 0.000 title claims description 9
- 238000000034 method Methods 0.000 title abstract description 21
- 238000007906 compression Methods 0.000 title description 2
- 230000006835 compression Effects 0.000 title description 2
- 239000000463 material Substances 0.000 claims abstract description 26
- 239000004033 plastic Substances 0.000 claims abstract description 15
- 229920003023 plastic Polymers 0.000 claims abstract description 15
- 238000003825 pressing Methods 0.000 claims description 7
- 239000000203 mixture Substances 0.000 claims description 6
- 239000007788 liquid Substances 0.000 claims description 4
- 230000003014 reinforcing effect Effects 0.000 claims description 3
- 238000005507 spraying Methods 0.000 claims description 3
- 239000000047 product Substances 0.000 description 7
- 239000003365 glass fiber Substances 0.000 description 3
- 238000002347 injection Methods 0.000 description 3
- 239000007924 injection Substances 0.000 description 3
- 229920005989 resin Polymers 0.000 description 3
- 239000011347 resin Substances 0.000 description 3
- 239000007921 spray Substances 0.000 description 3
- PPBRXRYQALVLMV-UHFFFAOYSA-N Styrene Chemical compound C=CC1=CC=CC=C1 PPBRXRYQALVLMV-UHFFFAOYSA-N 0.000 description 2
- 239000000835 fiber Substances 0.000 description 2
- 238000000465 moulding Methods 0.000 description 2
- 229920000728 polyester Polymers 0.000 description 2
- 241000282326 Felis catus Species 0.000 description 1
- 230000006978 adaptation Effects 0.000 description 1
- 239000000945 filler Substances 0.000 description 1
- 239000007789 gas Substances 0.000 description 1
- 239000011521 glass Substances 0.000 description 1
- 239000013067 intermediate product Substances 0.000 description 1
- 239000011159 matrix material Substances 0.000 description 1
- 239000002994 raw material Substances 0.000 description 1
- 230000002787 reinforcement Effects 0.000 description 1
- 239000012779 reinforcing material Substances 0.000 description 1
- 239000002904 solvent Substances 0.000 description 1
- 239000007858 starting material Substances 0.000 description 1
- 238000003860 storage Methods 0.000 description 1
- 229920001187 thermosetting polymer Polymers 0.000 description 1
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
- 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
- B29C70/30—Shaping 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
- B29C70/34—Shaping 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
- B29C70/345—Shaping 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
-
- 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
- B29C43/00—Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor
- B29C43/02—Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor of articles of definite length, i.e. discrete articles
- B29C43/04—Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor of articles of definite length, i.e. discrete articles using movable moulds
- B29C43/06—Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor of articles of definite length, i.e. discrete articles using movable moulds continuously movable in one direction, e.g. mounted on chains, belts
- B29C43/08—Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor of articles of definite length, i.e. discrete articles using movable moulds continuously movable in one direction, e.g. mounted on chains, belts with circular movement, e.g. mounted on rolls, turntables
-
- 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
- B29C43/00—Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor
- B29C43/02—Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor of articles of definite length, i.e. discrete articles
- B29C43/14—Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor of articles of definite length, i.e. discrete articles in several steps
-
- 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
- B29C43/00—Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor
- B29C43/32—Component parts, details or accessories; Auxiliary operations
- B29C43/36—Moulds for making articles of definite length, i.e. discrete articles
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
- B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
- B29C70/28—Shaping operations therefor
- B29C70/40—Shaping or impregnating by compression not applied
- B29C70/42—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles
- B29C70/46—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using matched moulds, e.g. for deforming sheet moulding compounds [SMC] or prepregs
- B29C70/461—Rigid movable compressing mould parts acting independently from opening or closing action of the main mould
-
- 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
- B29C43/00—Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor
- B29C43/02—Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor of articles of definite length, i.e. discrete articles
- B29C43/14—Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor of articles of definite length, i.e. discrete articles in several steps
- B29C2043/141—Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor of articles of definite length, i.e. discrete articles in several steps for making single layer articles
- B29C2043/144—Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor of articles of definite length, i.e. discrete articles in several steps for making single layer articles using different moulds, i.e. the layer is compressed in consecutive steps by using different moulds for each portion of the article
-
- 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
- B29C43/00—Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor
- B29C43/32—Component parts, details or accessories; Auxiliary operations
- B29C43/36—Moulds for making articles of definite length, i.e. discrete articles
- B29C43/361—Moulds for making articles of definite length, i.e. discrete articles with pressing members independently movable of the parts for opening or closing the mould, e.g. movable pistons
- B29C2043/3615—Forming elements, e.g. mandrels or rams or stampers or pistons or plungers or punching devices
- B29C2043/3621—Forming elements, e.g. mandrels or rams or stampers or pistons or plungers or punching devices a plurality of individual elements acting on the material in the same or diferent directions, e.g. making tubular T-joints, profiles
-
- 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
- B29C2791/00—Shaping characteristics in general
- B29C2791/001—Shaping in several steps
-
- 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
- B29C41/00—Shaping by coating a mould, core or other substrate, i.e. by depositing material and stripping-off the shaped article; Apparatus therefor
- B29C41/02—Shaping by coating a mould, core or other substrate, i.e. by depositing material and stripping-off the shaped article; Apparatus therefor for making articles of definite length, i.e. discrete articles
- B29C41/08—Coating a former, core or other substrate by spraying or fluidisation, e.g. spraying powder
-
- 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
- B29C43/00—Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor
- B29C43/006—Pressing and sintering powders, granules or fibres
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
- B29K2105/00—Condition, form or state of moulded material or of the material to be shaped
- B29K2105/06—Condition, form or state of moulded material or of the material to be shaped containing reinforcements, fillers or inserts
- B29K2105/12—Condition, form or state of moulded material or of the material to be shaped containing reinforcements, fillers or inserts of short lengths, e.g. chopped filaments, staple fibres or bristles
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
- B29L2031/00—Other particular articles
- B29L2031/30—Vehicles, e.g. ships or aircraft, or body parts thereof
- B29L2031/3005—Body finishings
- B29L2031/3017—Floor coverings
Definitions
- the present invention relates to a method for manufac ⁇ turing composite components, in which a mixture of plastics material and reinforcing material is pressed between mould halves.
- the invention also relates to a mould tool for carrying out the method, said tool comprising first and second mould halves which can be brought together so as to define a mould cavity there ⁇ between.
- vehicle parts have been produced from composite materials within the vehicle manufacturing industry for some considerable time. This manufacture is primarily concerned with such vehicle body parts as wings, engine covers, rear deak lids (boot covers) and like vehicle parts made from reinforced thermo ⁇ etting resins, prefer ⁇ ably reinforced polyester plastics, and then primarily in respect of motor vehicles which are produced in relatively small numbers.
- Other methods generally known in the art for manufacturing vehicle parts such as those afore- mentioned include wet pressing, injection and SMC-pre ⁇ ing methods. The two first mentioned methods are used in con ⁇ junction with preform glass-fibre reinforcements in which the glass fibres have been bonded together to form a readily handled body having a shape which conforms to that of the finished product.
- this preform is placed in the bottom part of a mould and wetted with liquid plastic, which is poured over the preform with the form open, whereafter the mould is closed.
- the plastic is injected into the mould cavity subsequent to closing the mould.
- SMC-pressing methods there is used a starting material which comprises a mixture of fibres. resin and filler, which forms a leather-like sheet. A number .of such sheets are placed on part of a otrld sur- . face and flow plastically during the pressure ⁇ ha.se, to fill the mould cavity.
- a common feature of the aforedescribed methods is that they require the provision of an intermediate product, which consequently requires the provision of intermediate . storage facilities, and none of these methods is suitable for direct application in the series manufacture of com ⁇ ponents which have large surfaces.
- the plastics material first applied will begin to harden before the mould is closed, unless a slowly hardening plastics mixture is used. This would render the process too long for rational series produc ⁇ tion.
- he injection method is also too slow to fulfil present day requirements of rational production processes.
- the SMC-method is encumbered with a multiple of drawbacks, one of which is that the spread of mechanical strength values throughout the finished product is too excessive, due to unfavourable material flow.
- the object of the present invention is to provide a method which can be used to manufacture composite products having large surfaces, and particularly surfaces which are seve ⁇ ral square meters in area, e.g. complete vehicle floors, while avoiding the drawbacks of the aforesaid methods and while enabling such products to be produced rationally and in series.
- a mould tool for carrying out the method will have at least one mould half which is divided into several sepa ⁇ rate parts which can be moved individually in relation to the other mould half, so that the tool can be closed in stages, as material is sprayed onto the mould surface of the other mould half.
- Figure 1 is a perspective view of a bottom mould half and a robot spray.
- Figure 2 is a schematic, perspective view illustrating the various steps of the inventive method, and
- Figure 3 is a sketch which illustrates the constructional principles of a mould tool.
- the reference 1 identifies a bottom mould half or mould part of a mould tool which is refer ⁇ enced generally with 2 and which has an upper mould half 3 which is divided into four mutually separate mould parts 4, 5, 6 and 7.
- the mould part ⁇ 1, 3 define therebetween a mould cavity for moulding a floor laminate consisting, for' instance, of a polyester plastic reinforced with glass , fibre.
- a robot 8 equipped with a spray/fiber cutter 9 sprays a plastics mixture admixed with glass fibres directly onto the mould surface 10 of the bottom mould half.
- Respective mould quarters 4-7 are lowered onto and pressed against the bottom mould half 1 and the material thereon rhythmically, in time with the application of material onto said bottom mould half.
- mould pressure in the order of 0.1 bar, can be achieved by loading the mould part ⁇ 4-7 individually - with the aid of pre ⁇ sure exerting devices (not shown), e.g. compressed air piston-cylinder devices, in principle the same manner as that employed with conventional press tables.
- pre ⁇ sure exerting devices e.g. compressed air piston-cylinder devices
- Lower mould pressures can be achieved, by suitable adaptation of the weight of the mould parts 4-7, such that it will suffice simply to lower the mould part ⁇ into place on the bottom mould half.
- the reference po ⁇ . 1 indicates the ⁇ tep at which material is charged to the bottom mould half.
- po ⁇ . 2 indicates the step in which the material is compacted subsequent to all four mould parts having been placed in position with the aid of a crane 11,
- po ⁇ . 3 indicates the step in which the material is hardened, and
- pos. 4 indi- cates the step in which the finished floor laminate 12 is removed from the mould, subsequent to lifting away the top mould half.
- Figure 3 illustrates schematically a mould tool whose top mould half 13 is divided into five mould parts 14, 15. 16, 17. 18, which are located sequentially in the longitudinal direction of the tool.
- the mould parts are provided with guides and force exerting devices, for instance hydraulic or compressed air piston-cylinder de ⁇ vices for displacing the mould part ⁇ in the direction of the arrows shown in the Figure, and in opposite directions.
- the robot 8 When applying material to the mould surface 10 of the bottom mould half 1, the robot 8 begins, by spraying material onto a region of the surface located opposite the mould part 14. Immediately this region of the surface has been coated with material, the mould part 14 is pressed against the material on the oppositely located region of the mould surface 10. Charging and pressing of material is carried out sequentially and in stages, in a corresponding manner (from left to right as seen in Figure 3), until finally the terminal mould part 18 is pressed against the underlying mould surface.
- the mould part ⁇ 4-7 and 14-18 respectively may be cold or heated, depending on the type of plastics material to be moulded and on desired hardening times.
- the heat transfer between mutually adjacent moulds can be limited as far as po ⁇ sible, by providing the ⁇ ides of the mould parts with recesses 20, so that the mould part ⁇ will only present small contacting surfaces therebetween, as illustrated in Figure 3.
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Composite Materials (AREA)
- Casting Or Compression Moulding Of Plastics Or The Like (AREA)
- Moulding By Coating Moulds (AREA)
- Reinforced Plastic Materials (AREA)
- Compositions Of Macromolecular Compounds (AREA)
- Moulds For Moulding Plastics Or The Like (AREA)
Abstract
A method and mould tool for producing plastic composite products having large surface areas, e.g. floors for automotive vehicles. A batch of material comprising plastics material which has fibres admixed therewith is sprayed onto a mould surface (10) on one mould half (1). A second multi-part half (13) is pressed in stages against the material, as the material is charged to the mould surface.
Description
Process and compression mould for manufacture of composite parts
The present invention relates to a method for manufac¬ turing composite components, in which a mixture of plastics material and reinforcing material is pressed between mould halves. The invention also relates to a mould tool for carrying out the method, said tool comprising first and second mould halves which can be brought together so as to define a mould cavity there¬ between.
Certain vehicle parts have been produced from composite materials within the vehicle manufacturing industry for some considerable time. This manufacture is primarily concerned with such vehicle body parts as wings, engine covers, rear deak lids (boot covers) and like vehicle parts made from reinforced thermoεetting resins, prefer¬ ably reinforced polyester plastics, and then primarily in respect of motor vehicles which are produced in relatively small numbers. Other methods generally known in the art for manufacturing vehicle parts such as those afore- mentioned include wet pressing, injection and SMC-preεεing methods. The two first mentioned methods are used in con¬ junction with preform glass-fibre reinforcements in which the glass fibres have been bonded together to form a readily handled body having a shape which conforms to that of the finished product. In the case of the wet pressing method, this preform is placed in the bottom part of a mould and wetted with liquid plastic, which is poured over the preform with the form open, whereafter the mould is closed. In the case of injection methods, the plastic is injected into the mould cavity subsequent to closing the mould. When applying SMC-pressing methods there is used a starting material which comprises a mixture of fibres.
resin and filler, which forms a leather-like sheet. A number .of such sheets are placed on part of a otrld sur- . face and flow plastically during the pressure ρha.se, to fill the mould cavity.
A common feature of the aforedescribed methods is that they require the provision of an intermediate product, which consequently requires the provision of intermediate . storage facilities, and none of these methods is suitable for direct application in the series manufacture of com¬ ponents which have large surfaces. When using the" wet pressing method to produce large surface components, there is a risk that the plastics material first applied will begin to harden before the mould is closed, unless a slowly hardening plastics mixture is used. This would render the process too long for rational series produc¬ tion. he injection method is also too slow to fulfil present day requirements of rational production processes. The SMC-method is encumbered with a multiple of drawbacks, one of which is that the spread of mechanical strength values throughout the finished product is too excessive, due to unfavourable material flow.
The object of the present invention is to provide a method which can be used to manufacture composite products having large surfaces, and particularly surfaces which are seve¬ ral square meters in area, e.g. complete vehicle floors, while avoiding the drawbacks of the aforesaid methods and while enabling such products to be produced rationally and in series.
This object is achieved in accordance with the invention by spraying onto a mould surface of one mould half a batch of material which comprises a liquid plastics mixture having reinforcing fibres admixed therewith, and by press¬ ing the mould batch in stages between said mould surface and another, multi-part mould half.
A mould tool for carrying out the method will have at least one mould half which is divided into several sepa¬ rate parts which can be moved individually in relation to the other mould half, so that the tool can be closed in stages, as material is sprayed onto the mould surface of the other mould half.
This combination of the known "spray-up" technique with εtagewise pressing of the material affords several advan- tageε. The fact that both fibres and liquid matrix mate¬ rial (plastics) are charged directly to the moulding tool eliminates the need to store semi-manufactured products or preforms and thus provides the shortest route from raw materials to finished product. The fact that the material is pressed in stages means that said material need only lie against the mould surfaces for a very short period of time before being compressed. This enables large surface components to be produced from reactive quick-setting thermosetting resin systems, therewith resulting in short process times. The departure of gases, such as styrene and solvent, from the mould batch is restricted, since the whole of the mould batch is never exposed, therewith bene- fitting the environment.
The method according to the invention is described below with reference to the accompanying drawing, in which Figure 1 is a perspective view of a bottom mould half and a robot spray. Figure 2 is a schematic, perspective view illustrating the various steps of the inventive method, and
Figure 3 is a sketch which illustrates the constructional principles of a mould tool.
In Figures 1 and 2 the reference 1 identifies a bottom mould half or mould part of a mould tool which is refer¬ enced generally with 2 and which has an upper mould half 3
which is divided into four mutually separate mould parts 4, 5, 6 and 7. The mould partε 1, 3 define therebetween a mould cavity for moulding a floor laminate consisting, for' instance, of a polyester plastic reinforced with glass , fibre.
As illustrated in Figures 1 and 2, a robot 8 equipped with a spray/fiber cutter 9 sprays a plastics mixture admixed with glass fibres directly onto the mould surface 10 of the bottom mould half. Respective mould quarters 4-7 are lowered onto and pressed against the bottom mould half 1 and the material thereon rhythmically, in time with the application of material onto said bottom mould half. The
. requisite "mould pressure", in the order of 0.1 bar, can be achieved by loading the mould partε 4-7 individually - with the aid of preεsure exerting devices (not shown), e.g. compressed air piston-cylinder devices, in principle the same manner as that employed with conventional press tables. Lower mould pressures can be achieved, by suitable adaptation of the weight of the mould parts 4-7, such that it will suffice simply to lower the mould partε into place on the bottom mould half.
In Figure 1, the reference poε. 1 indicates the εtep at which material is charged to the bottom mould half. poε. 2 indicates the step in which the material is compacted subsequent to all four mould parts having been placed in position with the aid of a crane 11, poε. 3 indicates the step in which the material is hardened, and pos. 4 indi- cates the step in which the finished floor laminate 12 is removed from the mould, subsequent to lifting away the top mould half.
Figure 3 illustrates schematically a mould tool whose top mould half 13 is divided into five mould parts 14, 15. 16, 17. 18, which are located sequentially in the longitudinal
direction of the tool. Although not shown, the mould parts are provided with guides and force exerting devices, for instance hydraulic or compressed air piston-cylinder de¬ vices for displacing the mould partε in the direction of the arrows shown in the Figure, and in opposite directions.
When applying material to the mould surface 10 of the bottom mould half 1, the robot 8 begins, by spraying material onto a region of the surface located opposite the mould part 14. Immediately this region of the surface has been coated with material, the mould part 14 is pressed against the material on the oppositely located region of the mould surface 10. Charging and pressing of material is carried out sequentially and in stages, in a corresponding manner (from left to right as seen in Figure 3), until finally the terminal mould part 18 is pressed against the underlying mould surface.
The mould partε 4-7 and 14-18 respectively may be cold or heated, depending on the type of plastics material to be moulded and on desired hardening times. The heat transfer between mutually adjacent moulds can be limited as far as poεsible, by providing the εides of the mould parts with recesses 20, so that the mould partε will only present small contacting surfaces therebetween, as illustrated in Figure 3.
In addition to those advantages mentioned in the afore¬ going, the division of a mould half into separate sections in the aforedescribed manner affords the additional advan¬ tage of enabling the moulded product to be given a pro¬ nounced undercut, as will be seen from the part 21 located opposite the mould part 14.
Claims
1. A method for producing composite material components, in which a plastics mixture admixed with reinforcing mate¬ rial is pressed between mould halves, characterized by spraying a material batch comprising liquid plastic having reinforcing fibres admixed therewith onto a mould surface on one mould half, and pressing material charged to the mould in stages between said mould surface and a mould surface on a further, multi-part mould half.
2. A mould tool for producing composite material com¬ ponents, comprising first and second mould halves which can be brought together to define a mould cavity there¬ between, characterized in that at least one mould half (3; 13) is divided into several separate parts (4-7; 14-18) which are movable individually in relation to the other mould half (1), such as to enable the mould tool to be closed in stages as material iε applied to the mould surface (10) of the other mould half.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SE8705017A SE460271B (en) | 1987-12-16 | 1987-12-16 | PROCEDURE AND FORMING TOOL FOR PREPARATION OF COMPOSITION PARTS |
SE8705017-5 | 1987-12-16 |
Publications (1)
Publication Number | Publication Date |
---|---|
WO1989005718A1 true WO1989005718A1 (en) | 1989-06-29 |
Family
ID=20370612
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/SE1988/000682 WO1989005718A1 (en) | 1987-12-16 | 1988-12-14 | Process and compression mould for manufacture of composite parts |
Country Status (2)
Country | Link |
---|---|
SE (1) | SE460271B (en) |
WO (1) | WO1989005718A1 (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO1999017914A1 (en) * | 1997-10-02 | 1999-04-15 | Borealis Gmbh | Differentiated pressing process |
WO2017051383A1 (en) * | 2015-09-25 | 2017-03-30 | Sabic Global Technologies B.V. | Method of molding using mold inserts and apparatus therefor |
US9890764B2 (en) * | 2014-03-26 | 2018-02-13 | General Electric Company | Trailing edge cap for a rotor blade and method of manufacturing same |
WO2019081904A1 (en) * | 2017-10-23 | 2019-05-02 | Mclaren Automotive Limited | Moulding arrangement |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR1175022A (en) * | 1957-05-13 | 1959-03-19 | Renault | Improvements in the manufacture of fiber preforms |
US3901641A (en) * | 1971-06-24 | 1975-08-26 | Alusuisse | Compacting step by step |
US4514353A (en) * | 1983-06-29 | 1985-04-30 | International Paper Company | Apparatus and method for forming a multi-compartmented tray from a sheet material |
-
1987
- 1987-12-16 SE SE8705017A patent/SE460271B/en not_active IP Right Cessation
-
1988
- 1988-12-14 WO PCT/SE1988/000682 patent/WO1989005718A1/en unknown
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR1175022A (en) * | 1957-05-13 | 1959-03-19 | Renault | Improvements in the manufacture of fiber preforms |
US3901641A (en) * | 1971-06-24 | 1975-08-26 | Alusuisse | Compacting step by step |
US4514353A (en) * | 1983-06-29 | 1985-04-30 | International Paper Company | Apparatus and method for forming a multi-compartmented tray from a sheet material |
Cited By (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO1999017914A1 (en) * | 1997-10-02 | 1999-04-15 | Borealis Gmbh | Differentiated pressing process |
US9890764B2 (en) * | 2014-03-26 | 2018-02-13 | General Electric Company | Trailing edge cap for a rotor blade and method of manufacturing same |
WO2017051383A1 (en) * | 2015-09-25 | 2017-03-30 | Sabic Global Technologies B.V. | Method of molding using mold inserts and apparatus therefor |
US11117299B2 (en) | 2015-09-25 | 2021-09-14 | Sabic Global Technologies B.V. | Method of molding using mold inserts and apparatus therefor |
WO2019081904A1 (en) * | 2017-10-23 | 2019-05-02 | Mclaren Automotive Limited | Moulding arrangement |
CN111491772A (en) * | 2017-10-23 | 2020-08-04 | 迈凯轮汽车有限公司 | Molding apparatus |
GB2567699B (en) * | 2017-10-23 | 2022-02-09 | Mclaren Automotive Ltd | Moulding arrangement |
CN111491772B (en) * | 2017-10-23 | 2022-06-14 | 迈凯轮汽车有限公司 | Molding apparatus |
EP3700729B1 (en) * | 2017-10-23 | 2023-07-26 | McLaren Automotive Limited | Moulding arrangement |
Also Published As
Publication number | Publication date |
---|---|
SE8705017L (en) | 1989-06-17 |
SE8705017D0 (en) | 1987-12-16 |
SE460271B (en) | 1989-09-25 |
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