Process and apparatus for controlling curing and thermoforming of resins and composites

Abstract: Composite materials (17) of reinforcing fibers are impregnated with polymeric matrices which may contain fillers and are then cured or thermoformed. As curing or thermoforming proceeds, dielectric detection is employed to closely monitor critical process events such as the release of volatiles, chemical reactions such as cross linking, melting and solidification. Curves are generated by plotting factors of the dielectric loss of the polymer matrix against time during the process; these plots have a distinctive shape or signature characteristic of the particular polymer matrix being processed. These distinctive features or signatures have been found to correlate with critical process events and are stored in a computer. During a cure cycle, the computer actuates the controls of the heating system so that the appropriate process actions or modifications will occur at the optimum time. The process controls are thereby adapted to produce an optimized high quality product.

Description: This invention relates to a new and improved process and apparatus for curing composites of polymeric resin impregnated fabric or fibrous reinforcement, the resin possibly containing fillers such as carbon black, graphite, mineral fillers, and the like. Typical fabrics and other fibrous reinforcements contemplated include those produced from graphite, carbon, fiberglass, ceramics, quartz, SiC, aramid, metal fibers such as Cu, AI, and steel, and mixtures thereof. Typical curable or thermoformable resins which may be employed to impregnate the fabric or fibrous reinforcements include phenolics, polyether ether ketones, polyimides, polyphenylene sulfides, polysulfones, polyesters, epoxies, polyethylene, polypropylene, nylon, bis-maleimides, PVC, polyamide-imides, furans, polyetherimides, ureas, urea-formaldehyde resins, melamines, polybenzimidazoles, etc., and mixtures thereof. Computer controlled processes and systems for curing graphite resin composites are well known, and typical publications in this field include: U.S. Patents 3,893,792; 3,925,139; 4,140,050; 4,236,109; 4,367,115; 4,373,092; 4,399,100; 4,423,191; 4,445,268; 4,449,697; 4,450,857; 4,486,996; 4,515,545; 4,559,810; 4,773,021; 4,777,431; 4,810,438; 4,828,472; 4,868,769; 5,032,525. A number of these prior art patents involve ultrasonic detection of the composite properties during the cure process, but ultrasonic detection does not have the desired effectiveness since it is superior in detecting structural anomalies, rather than gradual changes in physical state and cure reactions. Other patents involve the use of mathematical models, and still other patents, such as U.S. Patent 4,399,100 employ dielectric sensors to determine specific curing conditions, none of which address the ongoing nature of the curing or thermoforming process itself. US Patent 4,448,943 describes dielectric monitoring of a process to produce thermoplastic polymers but does not address a "signature" control process and apparatus for curing or cross-linking polymers used for composite technology systems. Furthermore, none of the prior art patents address the question of monitoring all of the critical process events such as the onset of reaction between the initial reactants, the completion of formation of the prepolymer, the onset and termination of the cross-linking reaction, the onset of melting and the completion of gelation. Consequently, these prior art patents do not adequately solve the problem of determining the most suitable time for applying heat and pressure to the curing system, and when to terminate the cure or thermoforming process. Also, the prior art does not show how to compensate the cure conditions for variations of the partially processed composite due to variations in its formulation from different manufacturers, and for differences in thicknesses of the composite materials. The prior art also does not compensate for additional variables which are introduced into the process by the nature of the curing equipment, tooling, thermal history, etc. Another problem of the prior art is that it attempts to determine actual values of the properties undergoing processing, such as viscosity, or to determine maxima and minima of these properties. However, such actual or absolute values of properties are difficult to measure under processing conditions due to variations in geometry of the measuring sensor such as the capacitor and the constantly changing environment including electrical noise within the processing equipment. It would be preferable to determine the characteristic shape or signature of the curve, since this would obviate the necessity of having to determine maximum or minimum values. Moreover, the prior art utilizes sensors which are buried within the composite and these sensors detect changes in the material only in their immediate vicinity, a condition which may not be typical of the laminate as a whole. Furthermore, after completion of the cure or thermoforming process, the sensors remain in the composite as undesirable artifacts. According to the invention, it has been found that curable and thermoformable composites produce distinctive dielectric loss response versus time curves during the cure or thermoforming process. In accordance with the invention there is provided a batch process for curing or thermoforming a resin with a fiber fabric or filler reinforcement to form a composite, the process comprising the steps of: (a) measuring curing or thermoforming conditions by dielectric means applied on opposite sides and through the portion of the composite, being cured during the cure or thermoforming process to produce a process curve for a specific resin which is correlated with physical and chemical changes in the resin; (b) automatically and repeatedly comparing the process curve for the specific resin with a computer-stored signature curve which is characteristic of the resin structure undergoing cure as it is being processed and which is correlated with physical changes in the resin and fabric or filler, the comparison being made at critical process events along the signature curve which are critical to the curing or thermoforming reaction; and, (c) applying reaction conditions in real time to the resin and fiber fabric or filler, including vacuum, venting, variations, in both temperature and pressure, and cooling to conform the process curve with the signature curve for the critical process events including release of volatiles, the onset of reaction between initial reactants, prepolymer formation, onset and termination of cross-linking, onset of melting and complete solidification to form the composite having fewer voids, improved uniform quality, with an increased yield and a reduced process cycle time. According to the invention there is provided also apparatus for curing or thermoforming a resin with a filler or fabric to produce a composite, comprising: (a) a reactor vessel; (b) heating, pressure, vacuum and venting means for applying curing or thermoforming reaction conditions to the reactor vessel; (c) reaction and reactor data collection means provided for the reactor, including thermal analysis, rheological analysis, dielectric measurements on opposite sides and through the portion of the composite being cured, heating, pressure, and vacuum measurements, and chemical and physical changes in the resin and fabric as measured by differential scanning calorimetry, viscosity and glass-transition temperature, the reaction and reactor data forming a process curve; and, (d) computerised control means comprising a processing unit and memory to store data which is suitable for: (i) receiving reaction and reactor data; (ii) storing signature features for a particular resin which define peaks, valleys, flats, rises and falls; (iii) automatically and repeatedly comparing the signature curve with reaction and reactor data representing an ongoing, real time curing or thermoforming reaction; and (iv) controlling means for heating, cooling, pressure, vacuum and venting along critical points on the process curve during the curing or thermoforming reaction to correlate the reaction with the signature curve features to form the composite with fewer voids, and improved uniform quality, with an increased yield and a reduced process cycle time, the controlling means including means for determining: volatile release, onset of reaction between initial reactants, prepolymer formation, onset and termination of cross-linking, onset of melting and completed solidification. preferred embodiments of the invention are disclosed in the dependent claims. Two components make up the total dielectric loss or impedance, viz., a resistive component and a capacitive component, and these two components are plotted separately versus time, each giving a distinctive curve. The shape of the curve is consistent, although it will vary in amplitude and time ordinate principally due to thickness, heating rate, degree of advancement and various other factors. The curve indicates distinctive process events which are characterised by PEAKS, VALLEYS, FLATS, RISES and FALLS, which can be correlated with chemical and physical changes occurring in the composite, as it is cured or thermoformed. Distinctive process events which are considered critical are then selected to obtain the highest quality in the finished product, but if there is uncertainty as to whether a process event is critical, this can be determined by experimentation, and will be discussed, infra. For this purpose, a dielectric loss curve having a particular distinctive shape is selected for the polymer composite being processed, and the shape of the curve is examined with a curve recognition computer program. The process cycle is divided into specific time/temperature segments and critical process events are selected within each segment. If a curve feature is not recognized, the sampling rate of the data and the sampling rate sensitivity is adjusted until the required features of the curve are invariably recognized. The above curve recognition process simulates an actual process occuring in real process equipment. The information developed in the simulation process is then programmed into a computer for controlling the operation of the autoclave, press or other equipment used to process the composite parts. In addition, the computer actuates the various autoclave operations and performs specific cure conditions based on readings of in-situ process control monitors. The actuation timing for the applications of these specific cure conditions by the process controls is based on the specific features of the dielectric curves. In this manner, standard or fixed process signature curve features are modified or adapted at critical points to correspond with the actual condition of the material being processed. The cure conditions which the computer is programmed to apply may include vacuum within a vacuum bag surrounding the composites, removal of volatiles, pressure (by using CO2, for example), temperature, cooling, and their respective application times, and on a real time basis. The entire system is usually run on a fully automatic computer controlled basis, but in case of sensor or equipment difficulties, the system may be run on a semi-automatic or manual basis, based on signature curve features. The invention will now be described in greater detail by way of example only with reference to the accompanying drawings, in which: Fig. 1 is a schematic representation of an autoclave which has been modified for the computer controlled curing of laminates, according to the invention; Fig. 2 is a schematic view in sectional side elevation showing the arrangement of a dielectric sensor, composite layers and lay-up components employed in fabricating a composite structure against a forming tool; FIG. 3. is an external view of an electrode, partly cut away, and suitable for dielectric monitoring of the composite during the cure process; FIGS. 4, 5 and 6 are graphs showing typical temperature versus time cure profile curves, respectively for polyether ether ketone, phenolic, and polyimide composites, all impregnated into various forms of graphite cloth; and, FIG. 7 is a program useful for controlling the cure cycle of a resin impregnated laminate. Initially, it is necessary to determine critical process events in a cure cycle, and for this purpose, thermal analysis (TGA), and dynamic rheological analysis (dielectric testing) were employed during the cure process. A number of cure runs were first made to produce sample laminates, and also to produce a series of dielectric curve shapes from which were obtained a standard cure cycle curve. The sample laminates were visually examined for defects and occasionally by ultrasonic scanning. Also, resin content, fiber volume, and void content were determined as well as flexural strength and short beam shear testing. If the results of these test showed the cured product failed to meet product specifications, or was of poor quality, the cure cycle was modified until laminates of suitable quality were produced. A number of cure runs were made (generally, not more than two being required) to produce a series of dielectric curve shapes from which were obtained a standard cure output curve with additional sample laminates being produced. Usually, critical process events are known to persons skilled in the art. However, to confirm that a process event is in fact critical, conditions around a particular event are varied, and if the resulting laminate is of good quality, then the particular process event is not critical. If in fact the conditions surrounding a process event are actually critical, then laminates taken from these surrounding process conditions will be inferior. Employing this procedure, an optimized processing curve for a particular manufactured part can be made which is adjusted at critical points based on the actual condition of the part being made. Since prior experience and background data are frequently, available, it may not be necessary to go through the entire procedure noted above to obtain an optimum processing curve. Consequently, the timing of specific curing and forming events such as the removal of volatile solvents, completion of certain chemical reactions, pressure application at suitable viscosity to obtain full consolidation, and the completion of the cure or thermoforming process can be controlled, preferably by a computer. FIG. 1. illustrates a typical autoclave vessel 9 which may be employed for curing or thermoforming purposes, using the conditions imposed by critical process events in the process cycle. The vessel was an existing autoclave which had been modified for the curing process and was capable at operating at 850 C and 17.56 kg/cm 2 (250 psi). The autoclave has an ellipsoidal shape, and comprises an exterior vessel wall 10, and an interior insulating wall 11, enclosing a vessel interior, and a door 12 at one end of the autoclave. A blower 13 and blower motor 14 are mounted at the opposite end of the autoclave, and function to blow over heaters 15 or a cooling coil 16 and onto a composite article 17 that is being processed. Temperature sensing elements 18, 19 and 20 are mounted within the autoclave to provide a reasonable temperature profile along the autoclave length, and temperature indicating controllers 21, 22 and 23 provide temperature control about midday of the autoclave. A pressure transducer 24 and pressure indicating controller 25 are provided to obtain pressure readings and supply pressure via say CO2, nitrogen, etc., to the autoclave. Vacuum sensing is provided by a vacuum transducer 29 along with a vacuum and venting control 27. A plurality of dielectric sensors 28, which are described in greater detail, infra, are mounted on the exterior of the laminate and provide dielectric loss curves to indicate progress of the curing reactions, changes of physical state such as melting and solidification, changes in viscosity and other physical or chemical occurrences in the polymer. Also, temperature sensing devices such as thermocouples are located at appropriate places on the composite part and tooling. Data from all of the sensors are fed into a computer (not shown) and this data is processed for comparison with optimum cure curves (e.g., FIGS. 4, 5 and 6). Output control data is fed from the computer to the temperature controls 21, 22 and 23, the pressure control 25, and the vacuum and venting control 27. FIG. 2 illustrates a lay-up configuration 30 in a silicone based envelope bag 31, for producing a cured composite part shaped to conform with a graphite tool 32. The overall part size was 660 x 610 mm (26 x 24 inches) and shaped as a partial frustrum typical of a structural, external airframe skin, and included flat portions, reinforcing ribs and a curved area. Graphite was selected for the tool 32 since it closely matched the coefficient of expansion of the graphite fiber reinforced composite, besides having dimensional stability, and resistance to the high temperature of the curing processes. The surface of the tool 32 was nickel plated to prevent damaging the graphite, and ten cure cycles at 385 C produced no visible damage to the tool. The envelope bag 31 was sealed to the surface of tool 32 by means of end seals 33, 34 and a double center seal 35. An assembly of film layers comprising breather material 36, a perforated release fabric 39, all of fiberglass, were placed on top of the composite lay-up 40. Layers of release fabric 41 and release film 42 were positioned between the composite lay-up 40 and the tool 32. At temperatures in excess of 260 C, use of polyimide film should be employed which does not exhibit dielectric activity such as ICI's polyimide UPILEX film. A dam portion 43 may be used to support the ends of envelope bag 31 and layers 36 and 37. The dielectric sensors 28, one sensor being shown in FIG. 3, are placed on top of the assembly of the film layers, and form a parallel plate condenser with the tool 32. This arrangement enables the electrodes to read through the laminate, compared to the action of buried electrodes which read only in the immediate vicinity of an electrode. Dielectric changes sensed during the cure process are converted into a voltage reading (e.g. 0 - 10 volts). A cable 44 connecting the electrodes 28 is passed through the autoclave wall using a teflon pressure gland. To reduce the effects of high temperature flow of teflon at temperatures exceeding about 288°C (550 F), the teflon coated cable was cushioned with fiberglass cloth and over-wrapped with KAPTON polyimide film for cure temperatures in excess of about 260°C (500 F). The sensor frequency was capable of functioning at 1,000 Hz - 10,000 Hz resistive signal gain and capacitive gain, and this enabled the cascading of five cascaded frequencies during a run for a given situation. The assembled dielectric sensor 28 comprises a metal foil electrode 45 having an active area of from 13 mm square to 25 mm square (about 1/2" square to about 1" square). Nickel electrodes are preferred to aluminum since aluminum electrodes tend to fail above say 230 C. The assembled sensor is shown in which the electrode 45 is surrounded by a suitably high temperature resistant polyimide insulating film 46 such as ICI's UPILEX material, together with an over-wrapping of insulating film 47 and bonded together with a polyimide adhesive primer. The sensor functioned up to about 400°C (750 F). When employed with phenolic cure systems, the UPILEX material tended to react with the phenolic resin, and hence the insulator was isolated from the phenolic resin with a layer of DuPont KAPTON polyimide film. As shown in FIG. 7, a typical program for producing laminates according to the invention, comprises receiving real time sensor and dielectric data 50 from the autoclave system and the part undergoing cure. For a specific resin having a unique cure or thermoform signature 51, the computer compares 52 the real time sensor and dielectric data with the stored cure or thermoform signature and looks for a rise, fall, peak, valley or flat. If a comparison 53 with the stored signature does not fulfil a rule requirement for a process change, the program idles back in the loop 53 - 50 until a process change is required. However, if a process change is required, a 'rule base' allotted pause time is set 54 for the controls of the autoclave to commence functioning. Following the requisite pause time, suitable modifications to the cure process by way of changes in temperature, pressure and vacuum are applied 55 by the autoclave controls. The program then proceeds to a feedback loop to determine if the cure has been completed 56. During this cure period, both sensor and dielectric data are fed back to the computer 50 for a signature comparison. The program continues looping between 56 and 50 until the signature comparison indicates the cure has been completed. The cure process then ends 56, the controls are turned off, and the autoclave is shut down 57. EXAMPLE 1. A sample of polyether ether ketone (ICI's PEEK) was impregnated into ICI's AS-4 unidirectional fiber array and the results selected from a range of 1 - 5 MHz, are illustrated in FIG. 4. Several plies of materials were laid up with several consolidation cycles, depending on thickness, and the temperature was raised (dark curve) until 385 C was reached. The critical event which was first reached was completion of melting, and the computer was programmed to recognize the well defined peak, followed by a flat and then to initiate cooling. Immediate cooling at this point not only can result in autoclave time reduction, but will reduce thermal degradation of the resin material, as compared with maintaining long process temperature hold times that are typical of the conservative prior art. It will be noted that a decrease in viscosity, indicating the onset of melting corresponded to an increase in dielectric values. A levelling off of the dielectric curve corresponds to complete melting. Several runs in which the computer made the decision to initiate cooling were made, and the quality of the parts (described in FIG. 2) were considered excellent. Ultrasonic (C scan) examination of the parts showed no significant voids, delaminations or flaws, and the properties of the thermoformed composite are given in Table 1, below. PROPERTY FLAT LAMINATES DEMONSTRATION PARTS (0,90)n; 16 Plies Quasi-Isotropic; 16 Plies Density 1.5954 1.5695 Fiber Volume 61.5% 63.93% Void Content 0.27% 0.85% Short Beam Shear: 1011 kg/cm 2 (14,376 psi) 600 kg/cm 2 (8,530 psi) ASTM 234, Ult. Str. 4-Point Flexure: 11,277 kg/cm 2 (160,406 psi) 8321 kg/cm 2 (118,366 psi) ASTM D790 Ult. Str. Modulus 5.98 x 10 5 kg/cm 2 (8.5 msi) 3.59 x 10 5 kg/cm 2 (5.1 msi) EXAMPLE 2. A sample of a phenolic composite was produced using Borden SC-1008 phenolic resin impregnated into T300, Style K135 graphite cloth sold by Ferro Corporation, and the graphic results of time versus temperature are shown in FIG. 5. Prior art processes for curing a phenolic composite, which are used as precursors to form ablative or carbon/carbon composite structures, involve raising the temperature to about 50 C - 60 C, and maintaining that temperature range until the solvents in the system are evaporated. This temperature range is maintained until the resin is 'staged', i.e., the molecular weight has increased to a higher level, as indicated by an increase in viscosity. The temperature is then increased to 177 C and held for about one hour or more to assure a complete cure. Full autoclave or press pressure is usually applied at some arbitrary point soon after the staging portion of the process. This prior art process cycle has been developed by trial and error, and is varied by individual operators according to the particular phenolic, and the size and thickness of the part undergoing curing. According to the invention, it has been discovered that the dielectric loss curves showed clear indications of the critical process events which the prior art has attempted to control. For example, evaporation of solvent is indicated by a small peak, and completion of this event is indicated by a flat portion of the curve, as shown in FIG. 5. Completion of the staging process is also indicated by a flat following a gentle rise in the curve. Heating is then resumed, and as the temperature rises, a marked decrease in viscosity occurs. The increase in temperature combined with low viscosity causes a rapid increase in cross linking chemical reactions leading to gelation. Thus, two competing phenomena occur simultaneously and rapidly, resulting in a very narrow processing window. Full autoclave pressure should therefore be applied within a processing window of about two to ten minutes after this rise in the dielectric loss curve. The application of full pressure within this narrow processing window is necessary for the preparation of a dense, void free composite. If pressure is applied too soon, the resin content of the product will be too low, but if pressure is applied too late, the product will be void filled, blistered and delaminated. Bearing in mind that the response time of the system is in the order of less than one second, there is no difficulty in applying pressure within the required time constraints. Initially, only a partial vacuum was applied to the interior of the vacuum bag until the solvent evaporation phase was complete. After solvent evaporation, and upon completion of the 'staging' phase, a temperature increase was applied as soon as the flat portion of the curve commenced. Pressure was then applied when commencement of the rise had been observed. Following completion of curing, indicated by a subsiding of a peak, and when the curve had attained a flat, cooling was commenced. Thus, all critical events were recognized and appropriate actions were taken in real time to provide an optimum cure. The process of this invention is therefore not only adaptive to the actual condition of the composite being cured but also eliminates unnecessary prolongation of various process phases, and this considerably reduces the overall process cycle. Flat panels with and without mineral fillers, were made using the process and apparatus of this invention, and all of these panels were of excellent quality. Three demonstration parts, representing a typical airframe skin structural part, were then made with the mineral filled material, and excellent quality was again obtained. One of these parts was converted to a carbon/carbon composite with excellent results. Test coupons were taken from the flat area of the 'as molded' demonstration parts, and the results are given in Table 2, below. PROPERTY DEMONSTRATION PARTS (0 - 90)n; 16 Plies Density 1.6372 Fiber Volume 45.58% Void Content **** Short Beam Shear 155 kg/cm 2 (2,208 psi) ASTM 234, Ult. Str. 4-Point Flexure: 1627 kg/cm 2 (23,143 psi) ASTM D790 Ult. Str. Modulus 2.76 x 10 5 kg/cm 2 (3.92 msi) ****Due to the proprietary nature of the inhibitor filler, the void content could not be determined, but ultrasonic C scans of the parts showed them to be dense and of good quality. EXAMPLE 3. Two different samples of phenolic prepregs were cured, one sample being from the Fiberite Corporation, and the other phenolic prepreg being from BASF/NARMCO. The dielectric traces differed in amplitude, and precise timing of events of FIG. 5, but they both exhibited the typical characteristic shape of the Borden SC-1008 resin. EXAMPLE 4. A high temperature PMR-15 polyimide resin was impregnated into T300, Style K135 graphite fiber cloth sold by the Ferro Corporation. The prepreg consisted of low molecular weight amid-acid prepolymers which increase in molecular weight rapidly in the temperature range of 80 C - 150 C with the release of condensation products, water and methanol. These reactions continue up to 250 C and are accompanied by imidization of the polymer with the elimination of water. Softening and melt flow of the imidized linear polymer occurs at about 175 C - 250 C. Cross linking reactions occur at about 250 C - 316 C, and FIG. 6 illustrates a general overview of the reaction. For this reason, prior art curing of PMR-15 is usually made at a maximum temperature of 330 C for several hours to ensure a complete cure. Using the process of this invention, the following cure procedure (dark curve - FIG. 6.) was adapted using a 5,000 Hz curve resistive loss since it had the most distinctive shape. 1. Apply 0.1034-0.1727 kg/cm 2 (3" - 5" Hg); 2. Increase the temperature 2 C/min. until the resistive curve (viscosity) shows a fall; 3. Maintain temperature until resistive curve becomes flat; 4. Apply full vacuum - minimum 0.9323 kg/cm 2 (27" Hg); 5. Apply further heat until 250 C at 2 C - 3 C per minute; 6. Wait for the resistive curve to become very flat; 7. Apply 13.03 kg/cm 2 (200 psig); 8. Increase temperature to 330 C and wait for a fall in the resistive trace; 9. Hold at temperature for 15 minutes; 10. Cool to 204 C; 11. Vent vacuum and release pressure gradually; and, 12. Continue cooling to 203 C, and conclude run. Procedures 1 - 6 would be used for elevated temperature consolidation (debulking) if required. Three flat panels 457 x 609 mm (18" x 24") and three demonstration parts as per FIG. 2 were produced, using the above described process, and all panels and parts were of excellent quality. The test results are given in Table 3, below. PROPERTY DEMONSTRATION PART (0 - 90)n;16 Plies Density 1.5862 Fiber Volume 61.2% Void Content less than 0.2% Short Beam Shear: 673.33 kg/cm 2 (9,578 psi) ASTM 234, Ult. Str. 4-Point Flexure: 8285.21 kg/cm 2 (117,855 psi) ASTM D790 Ult. Str. Modulus 3.41 x 10 5 kg/cm 2 (4.85 msi) The process and apparatus of this invention enables curing conditions to be optimized while reducing the possibility of damaging the laminate due to prolonged heating, and minimizing the residence time in the autoclave. Furthermore, excellent products can be produced, even if the manufacturing sources of the raw material are different. Moreover, many existing autoclaves, presses, and ovens can be modified without great cost since they are already equipped with computer controls. In summary, this invention insures the production of composite parts of uniform high quality as defined in the annexed claims, in spite of variations in raw material, pre-processing, tooling and equipment. Process cycles are significantly reduced, yields increased, and the technique applies an excellent quality control record of the process for each part. Past inspection operations which were normally intensively used to assure the quality of the part, may now be drastically reduced or eliminated.

Claims: A batch process for curing or thermoforming a resin with a fiber fabric or filler reinforcement to form a composite (17), the process comprising the steps of: (a) measuring (50) curing or thermoforming conditions by dielectric means (28) applied on opposite sides and through the portion of the composite (17) being cured during the cure or thermoforming process to produce a process curve for a specific resin which is correlated with physical and chemical changes in the resin; (b) automatically and repeatedly comparing (52, 53) the process curve for the specific resin with a computer-stored signature curve (51) which is characteristic of the resin structure undergoing cure as it is being processed and which is correlated with physical changes in the resin and fabric or filler, the comparison being made at critical process events along the signature curve which are critical to the curing or thermoforming reaction; and, (c) applying (55) reaction conditions in real time to the resin and fiber fabric or filler, including vacuum, venting, variations, in both temperature and pressure, and cooling to conform the process curve with the signature curve for the critical process events including release of volatiles, the onset of reaction between initial reactants, prepolymer formation, onset and termination of cross-linking, onset of melting and complete solidification to form the composite having fewer voids, improved uniform quality, with an increased yield and a reduced process cycle time. A process according to claim 1, wherein in step (b) the signature curve (51) defines peaks, valleys, flats, rises and falls which are correlated with physical and chemical changes in the resin fabric. A process according to claim 1 or claim 2, wherein in step (a) the physical and chemical changes in the resin and fabric are measured by differential scanning calorimetry, viscosity and glass transition temperature. A process according to any one of claims 1 to 3, wherein in step (b) the critical process events are determined by thermal analysis, rheological analysis and dielectric measurements. A process according to any one of claims 1 to 4, wherein in step (a) the dielectric means (28) comprises a plurality of dielectric sensors mounted on the composite (17). A process according to claim 5, wherein the dielectric measurements include resistance loss and capacitance loss at a sensor frequency of 1,000 to 10,000 Hz. A process according to claim 6, wherein the composite is formed on a tool (32) and dielectric means (28) includes the tool. A process according to claim 7, wherein the tool (32) comprises metal-coated graphite. A process according to any one of claims 1 to 8, wherein the resin is selected from phenolics, polyether ether ketones, polyimides, polyphenylene sulfides, polyesters, polysulfones, epoxies, polyethylenes, polypropylenes, nylons, bis-maleimides, PVC, polyamide-imides, urea-formaldehydes, furans, melamines, polyetherimides, ureas, polybenzimidazoles and mixtures of any two or more thereof. A process according to any one of claims 1 to 10, wherein the fabric or filler reinforcement is selected from mineral fillers, ceramics, carbon fibers, carbon black, graphite, fiberglass, quartz, SiC, aramid, metal fibers, Cu, Al, steel and mixtures of any two or more thereof. A process according to any one of claims 1 to 10, which is controlled by computer or semi-automatic means or on a manual basis. A process according to any one of claims 1 to 11, wherein the resin composite in the form of a lay-up (40) and dielectric means (28) are housed in a silicone bag (31). An apparatus for curing or thermoforming a resin with a filler or fabric to produce a composite (17), comprising: (a) a reactor vessel (9); (b) heating (15), pressure (25), vacuum and venting (13) means (27) for applying curing or thermoforming reaction conditions to the reactor vessel; (c) reaction and reactor data collection means provided for the reactor, including thermal analysis, rheological analysis, dielectric measurements (28) on opposite sides and through the portion of the composite being cured, heating (18, 19, 20), pressure (24), and vacuum (29) measurements, and chemical and physical changes in the resin and fabric as measured by differential scanning calorimetry, viscosity and glass-transition temperature, the reaction and reactor data forming a process curve; and, (d) computerised control means comprising a processing unit and memory to store data which is suitable for: (i) receiving reaction and reactor data; (ii) storing signature features for a particular resin which define peaks, valleys, flats, rises and falls; (iii) automatically and repeatedly comparing the signature curve with reaction and reactor data representing an ongoing, real time curing or thermoforming reaction; and (iv) controlling means for: heating (21, 22, 23), cooling (16), pressure (25), vacuum and venting (27) along critical points on the process curve during the curing or thermoforming reaction to correlate the reaction with the signature curve features to form the composite with fewer voids, and improved uniform quality, with an increased yield and a reduced process cycle time, the controlling means including means for determining: volatile release, onset of reaction between initial reactants, prepolymer formation, onset and termination of cross-linking, onset of melting and completed solidification. Apparatus according to claim 13, wherein the dielectric means comprises a plurality of sensors (28) adapted to be mounted on the composite. Apparatus according to claim 13 or claim 14, including a dielectric sensor array to provide dielectric measurements, comprising: (a) a plurality of sensor elements adapted to be positioned on the upper surface of the composite or resin undergoing curing or thermoforming, each sensor element comprising a metal foil having a high temperature durability, and being surrounded by an insulating film having temperature and reactive durability at the respective curing or thermoforming temperature; and, (b) a curing tool on which the composite is to be positioned, the sensor array and curing tool forming a parallel plate condenser on opposite sides of the composite or resin, and the sensor array being adapted to provide a detection signal in response to dielectric properties of the composite or resin, to enable the detection signal to control the thermoforming or curing process, the sensor array being removable from the surface of the composite or resin following completion of the process with minimal imprinting of the composite surface.

Inventors: CASTILLO ARTURO A, KELLER L BRIAN, CASTILLO, ARTURO A., KELLER, L. BRIAN
Applicants: SIGNATURE CONTROL SYSTEMS INC, SIGNATURE CONTROL SYSTEMS, INC.
Application year: 1992
Main classification: B29C35
IPC codes: G01N3, B29C35, G01N33