CA2055436A1 - System and method for monitoring pressure during the production of fiber reinforced polymers - Google Patents
System and method for monitoring pressure during the production of fiber reinforced polymersInfo
- Publication number
- CA2055436A1 CA2055436A1 CA002055436A CA2055436A CA2055436A1 CA 2055436 A1 CA2055436 A1 CA 2055436A1 CA 002055436 A CA002055436 A CA 002055436A CA 2055436 A CA2055436 A CA 2055436A CA 2055436 A1 CA2055436 A1 CA 2055436A1
- Authority
- CA
- Canada
- Prior art keywords
- pressure
- composite material
- force sensing
- laminate
- sensing resistor
- 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.)
- Abandoned
Links
Classifications
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01L—MEASURING FORCE, STRESS, TORQUE, WORK, MECHANICAL POWER, MECHANICAL EFFICIENCY, OR FLUID PRESSURE
- G01L5/00—Apparatus for, or methods of, measuring force, work, mechanical power, or torque, specially adapted for specific purposes
- G01L5/0061—Force sensors associated with industrial machines or actuators
- G01L5/0076—Force sensors associated with manufacturing machines
- G01L5/008—Force sensors integrated in an article or a dummy workpiece
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- 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
- B29C43/20—Making multilayered or multicoloured articles
- B29C43/203—Making multilayered 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
- 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
- B29C43/56—Compression moulding under special conditions, e.g. vacuum
-
- 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
- B29C43/58—Measuring, controlling or regulating
-
- 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
- B29C70/342—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 isostatic pressure
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
- B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
- B29C70/28—Shaping operations therefor
- B29C70/54—Component parts, details or accessories; Auxiliary operations, e.g. feeding or storage of prepregs or SMC after impregnation or during ageing
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B37/00—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding
- B32B37/10—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by the pressing technique, e.g. using action of vacuum or fluid pressure
-
- 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
- B29C43/58—Measuring, controlling or regulating
- B29C2043/5808—Measuring, controlling or regulating pressure or compressing force
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2309/00—Parameters for the laminating or treatment process; Apparatus details
- B32B2309/12—Pressure
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B41/00—Arrangements for controlling or monitoring lamination processes; Safety arrangements
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Analytical Chemistry (AREA)
- Composite Materials (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Moulding By Coating Moulds (AREA)
- Casting Or Compression Moulding Of Plastics Or The Like (AREA)
Abstract
Disclosed is a system and method of monitoring exerted pressure during the production of composite material laminates that utilizes a thin, low cost, durable, temperature resistant force sensing resistor (50). The sensor (50) can be embedded directly on the surface of the composite laminate (42), or can be positioned between layers of the composite laminate (42). Alternatively, the sensor (50) is built into or mounted on a tool (46) or die used to form or exert pressure on the laminate (42). In all of these cases, the force sensing resistor (50) monitors the pressure experienced by the laminate (42) during processing of the laminate (42).
Description
W~90/1~25 -1- 2 ~ ~ 1 3 ~ PCT/US90/0~89 SYSTEM AND METHOD ~OR MONITORING PRESSURE DURING
THE PRODUCTION OF FI~ER REINFORCED POLYMERS
BACKGROUND OF THE INVENTION
The present invention relates to a system and method for monitoring pressure exerted on materials during the production of fiber reinforced polymer composites and more particularly to a system and method - for monitoring pressure exerted on fiber reinforced polymer composites through the use of a force sensing lo resistor in either the composite or the tool or die.
Use of fiber reinforced polymer has seen a dramatic increase in recent years as the demand for high performance plastics in commercial, industrial and military applications has risen. The benefits of composite materials, such as high strength and stiffness, low weight, resistance to fatigue and corrosion, make these materials extremely attractive in applications ran~ing from aircraft to bridges. New fabrication technologies have opened the door to low cost processing, allowing hundreds of new companies to enter production. Composites manufacturing, however, requires a careful monitoring control of the many complex processes common to every composite molding operation.
Most composite production processes start with the assembly of individual layers of fiber and matrix material. The basic materials used to construct the laminate can be in any number of forms including dry fiber and liquid resin, sheets of fiber impregnated with matrix material, sprayed mixtures of resin and matrix, as well as other combinations. The matrix materials can include thermosetting types, which undergo irreversible chemical reactions as they cure to form a rigid laminate, or thermoplastics, which can be repeatedly heated, melted and reconsolidated.
THE PRODUCTION OF FI~ER REINFORCED POLYMERS
BACKGROUND OF THE INVENTION
The present invention relates to a system and method for monitoring pressure exerted on materials during the production of fiber reinforced polymer composites and more particularly to a system and method - for monitoring pressure exerted on fiber reinforced polymer composites through the use of a force sensing lo resistor in either the composite or the tool or die.
Use of fiber reinforced polymer has seen a dramatic increase in recent years as the demand for high performance plastics in commercial, industrial and military applications has risen. The benefits of composite materials, such as high strength and stiffness, low weight, resistance to fatigue and corrosion, make these materials extremely attractive in applications ran~ing from aircraft to bridges. New fabrication technologies have opened the door to low cost processing, allowing hundreds of new companies to enter production. Composites manufacturing, however, requires a careful monitoring control of the many complex processes common to every composite molding operation.
Most composite production processes start with the assembly of individual layers of fiber and matrix material. The basic materials used to construct the laminate can be in any number of forms including dry fiber and liquid resin, sheets of fiber impregnated with matrix material, sprayed mixtures of resin and matrix, as well as other combinations. The matrix materials can include thermosetting types, which undergo irreversible chemical reactions as they cure to form a rigid laminate, or thermoplastics, which can be repeatedly heated, melted and reconsolidated.
-2- 57CI`/US90/02489 rj ~ '` ' The manufacturing of a composite laminate, regardless of the fiber type and polymer matrix, requires the application of heat and pressure. Heat is required to either polymerize a thermosetting resin s system (cure) or melt a thermoplastic system ~such as Ultem). Application of pressure is required to consolidate the laminate to eliminate voids in the form of trapped air or volatiles that are generated during the cure. Without careful consideration of both the temperature history or pressure profile of the composite part during processing, the ability to produce high quality parts is severely crippled. For this reason, the reinforced plastics industry has spent a large portion of its research funds developing sophisticated hardware to monitor the state of a composite laminate during fabrication. Instruments for monitoring cure state of thermosetting and thermoplastic resins abound.
Differential scanning calorimetry (DSC), thermograimetric analysis (TGA), thermemechanical analysis (TMA), parallel plate rheometers, dielectric-electrics, ultrasonics, and fiberoptics are only a few of the sensing and measurement technologies that have been applied to research and production of composite materials. None of these monitoring instruments have proven, however, to be useful in monitoring the pressure ! exerted on or between the layers of the composite material.
Composite structures, unlike their metallic counterparts, are built up rather than "machined down".
This difference permits the integration of embedded sensors for use in such diverse applications as adaptive structures which actively damp vibrations or maintain precise geometry over a broad temperature and loading spectrum to structures which monitor the health of the structure in order to warn when damage is present.
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WO90~ PCT/US90/0~4X9 -3- 2~ 3~
Embedded sensors have also recently been used in process technology as ~ell. Thin dielectric cure sensors and thermocouples are routinely laminated between plies in the composite to provide feedback for control of autoclaves and hot presses during processing. Fiber optic cables provide similar information in the autoclave and may also serve a second purpose in the structure as a health monitoring device, communications link or strain indicator.
A missing link in composites processing is a pressure monitoring device that can be embedded in the laminate. In-situ pressure monitoring during process development and during production is extremely important for a number of reasons. Referring to Fig. 1, in a typical laminate consolidation and cure process used in autoclave molding, in resin transfer molding and in filament winding operations, several layers of disposable materials are used to provide high surface quality, absorb excess resin and provide even vacuum distribution. The materials are sealed beneath the nylon film. The area between the caul sheet 14 (or mold surface) and the vacuum bag 16 is evacuated with a vacuum pump (not shown) to approximately 20 inches ~9 or less. The vacuum draws volatiles out of the laminate 12 and provides the necessary pressure gradient between the autoclave and the laminate 12. In autoclave processing, if a vacuum bag 16 breaks or loses its seal, the net force consolidating the part becomes zero and the laminate will not be of acceptable quality after the cure. The part, which may require several weeks to prepare for cure, is then scrapped.
A record of the pressure versus time history of each component is often required to verify the quality of every high performance composite part made. A sensor capable of indicating loss of vacuum pressure would ;
WO9~ 5 PCTJUS90/0~9 ob~La~sly bè a valuable quality control and process monitoring tool. It is possible that early warning of vacuum loss could allow the problem to be repaired or laminate damage minimized. A knowledge of the pressure history during cure is also an important consideration.
Pressure may be varied at di~ferent times during a normal autoclave cure cycle.
In complex tool situations, thermal expansion of metal tooling is used to provide laminate pressurization. Shrink wrap films are often applied to filament wound vessels, radomes and cylinders to apply pressure when heated. Matched dies are used for consolidation in compression molding of composite materials. In all these applications, the actual applied pressure on the laminate is virtually unknown and is unmeasurable by previous existing techniques.
Lamination pressure will typically vary from point to point in large complex dies. A reliable pressure sensing system would be a valuable asset in measuring such applied pressure.
Pultrusion technology has also emer~ed as one of the most rapidly growing (by volume) manufacturing processes for reinforced polymer materials. Referring to Fig. 2, in pultrusion manufacturing, fibers 22 and resins 24 are pulled through a heated die 26 and cured.
Fibers are impregnated with resin by either pulling them through a resin bath or by direct injection at the entrance of the die. The part undergoes an extremely complex series of chemical reactions and thermal expansion, leading to wild excursions in volumetric dimension. Changes in material volume lead to pressure variation within the die which affects consolidation of the laminate. A variety of facto~s including temperature, formulation of resin, volume of fibers, pulling speed and die design influence the pressure ' W090~1~25 PCT/US90tO248~
~5~ 2~7~
profile of the part during cure. The complex interaction o~ the parameters and their effect on laminate pressure cannot be readily analyzed nor can the results be veriEied until a continuous pressure measurement can be determined. Currently, temperature proiles are obtained by passing a thin thermocouple through the die. An example of a temperature profile of an epoxy resin system is shown in Fig. 3. A cross-section of the die is shown on the plot to illustrate the relative position of the thermocouple in the die.
The die temperature is approximately 150 C. The exothermic reaction produces higher resin temperatures.
- The combination of both a thermal profile and pressure profile would unlock the answers to many important lS questions regarding the process conditions within a pultrusion die.
It is therefore a principal object of the present invention to provide a system and method of monitoring exerted pressure during the production of composite material laminate.
Another object of the present invention is to provide a system and method of monitoring exerted ! pressure on a manufactured laminate utilizing a force sensing device either in the laminate or on a tool or die used to manufacture the laminateO
It is another object of the present invention is to provide a composite material laminate or a laminate forming tool including a pressure sensing device for providing a record of pressure versus time history of the composite material laminate.
Yet another object of the present invention is to produce a composite material laminate with a low cost, durable, low profile, temperature resistant pressure sensor embedded therein.
,, WO90/1~25 PCr/US90/0~8 20~ 5a'~ -6-Still another object of the present invention is to provide tools or dies for creating a composite material laminate that include a deviee for measurinq pressure exerted on the composite material laminate created by the tool or die during production.
SUMMARY OF THE INVENTION
Accordingly, a system and method of monitoring exerted pressure during the production of composite material laminates utilizes a thin, low cost, durable, temperature resistant force sensing resistor. The - sensor can be embedded directly on the surface of the composite laminate, or can be positioned between layers of the composite laminate. In this way, the force sensing resistor monitors the pressure experienced by the laminate during processing of the laminate.
Alternatively, the sensor is built into or mounted on a tool or die used to form or exert pressure on the laminate.
These and other features and objects of the present invention will become more fully understood from following the detailed description which should be read in light of the accompanying drawings.
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BRIE~ DESCRIPTION OF THE DRAWINGS
Fig. l is layup of a prior art preimpregnated composite material laminate constructed out of a Yariety of auxiliary materials;
~ ig. 2 is a diagrammatic view of a prior art pultrusion processing system;
Fig. 3 is a graph of a thermal profile of a graphite/epoxy part generated using a prior art thermocouple passed through the die with the materials used for creating a composite, WO9~1~25 PCT/US90/0248~
~7~ 2 0 ~ ~ ~ 3 6 Pigs. 4(a)-4(d) are perspective views of alternate embodiments of the positioning of a sensor in the system of the present invention;
Fig. S is a schematic view of a device for use in calibrating the force sensing resistor utilized in the composite material laminate of the present invention;
Eig. 6 is a perspective view of a force sensing resistor placed between layers of a composite material laminate of the present invention;
~ig. 7 is diagrammatic view of pultrusion die through which a force sensing resistor will be pulled with the materials for creating a composite material laminate according to the present invention;
Fig. 8 shows use of a force sensing resistor mounted on a tool of the present invention used in an autoclave.
DETAILED DESCRIPTION_OF T~E PREFERRED EMBODIMENTS
In a preferred embodiment, in order to measure the pressure exerted on a composite laminate manufactured throu~h the use of autoclave molding, compression molding, resin injection molding, pultrusion, reaction injection molding, press molding and other procedures, a thin force sensing resistor is embedded between laminate ¦ layers of the product during assembly of its layers or is placed between the surface of the composite laminate and the tool against which the composite is cured. In some cases, layers of disposable materials are positioned between the composite product and the tool, and the sensor can be placed in these layers as well. A
suitable resistor is described in U.S. Patent No.
4,301,337, the teachings of which are incorporated - herein by reference. In preferred embodiments, the resistor, however, includes one pressure switch rather j than the two desrribed in this patent.
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i L
WV90/1~25 PCT/VS~0/0~8 ~95rj ~T~ force sensing resistor, ~hich was developed to i generate tones in an electronic musical device, is a dual switch that is actuated in response to a single touch force. In its commercial form, this force sensing j 5 resistor, which is sold by Interlink Electronics of Santa 3arbara, California under the designation Forcing Sensing Resistor or FS~, has a thickness of less than O.5 mm, has good dynamic and pressure ranges and has minimum temperature sensitivity. In particular, the force sensing resistor is available in thicknesses ranging from 0.005 to 0.050 inches. As will be more fully described below, this thin profile allows the force sensing resistor to be implanted inside a ! laminate, placed on the surface of a laminate, placed within supporting cure materials of a laminate, placed on a laminate forming tool, or built permanently below the surface of the tool.
This force sensing resistor is also available in a variety of surface areas. Sensors with surface areas from less than 0.5 to more than 5,000 square cm are ` currently available with other sizes possible for speci~l applications. This range of surface areas j allows the device to be used for many different types of pressure monitoring applications. The use of a sensor with a small surface area in the present invention allows pressure at a point to be measured, and the use of a sensor with a large surface area allows the measurement o~ average pressures or the determination of the distribution of pressure over a large area. The sensor in its commerical form can be used in temperatures up to 300F and it is possible to special order the sensor so that it can operate at temperatures approaching 800. Such temperature ranges are appropriate for many plastics, composites and chemical manufacturing, testing and service conditions. Anotùer .
, r WO90/1~25 PCT/VS90/024~9 -9- 2~3~3~
advantage of the sensor is that it can be tailored to be sensitive to a variety of pressure ranges of interest to the material processing industry. The sensitivity of the sensor to changes in operating temperatures is small. For many applications such as monitoring the loss of vacuum pressure, temperature sensitivity can be ignored. For more percise measurements, temperature effects can be accounted for by simple calibration and curve fittings. The resistor (or sensor) can remain a permanent part of the composite after the consolidation and cure of the material has been completed (and therefore lost during the production process) or, if properly positioned, it can be removed during a trimming operation.
The creation of the composite laminate with an - embedded sensor will now be described in detail. During the layup of uncured laminate, a force sensing resistor 50 is placed between material layers 42 at locations in the laminate (Fig. 6) and/or the surrounding trim, scrape or follower materials, where measurement of the processing pressure is desired. Alternatively, the force sensing resistor can be placed between layers of supporting material 44 (~ig. 4a), placed directly between the laminate 42 and the tool 46 (Fig. 4b), placed on the tool 46 away from the composite laminate 42 (Fig. 4c) or permanently built into the processing tool 46 slightly below the tool surface (Fig. 4d).
Because of the very thin profile of the sensors and leads, the surface imperfection at the sensor location from the build-up of additional thickness is minimized.
The thinness of the force sensing resistor also improves its ability to accurately measure the pressure in the laminate, especially when manufacturing techniques such as press molding, matched die molding and pultrusion, which apply load to the surface by closing or otherwise .
W090/13~2~ ~ P~T/US~0/0~89 S~ 10-controlling the thickness of the laminate as it cures, are employed. Thick points, caused by thick sensors, in a laminate would locally contact the sur~aces with more force. Therefore, the thinness of the force sensing resistor becomes an important feature of the present invention that allows this force sensing resistor to be used as part of a composite laminate.
Prior to positioning the sensor in the system of the present invention ~e.g. between layers of unprocessed laminate), the sensor may need to be calibrated. The calibration can be obtained from non-spec-fic data supplied by the sensor manufacturer, or each sensor can be individually calibrated. The force sensing resistor operates by changing its electrical resistance in a way that is directly and repeatedly related to applied surface pressure. Calibration of the sensor, for those applications requiring more detailed and accurate pressure readings, can be accomplished by applying a series of known pressures to the surface of the force sensor resistor and measuring its resistance at each of these pressures.
~ ig. 5 shows one possible method for obtaining a pressure versus sensor output curve for individual sensors when detailed calibration is required. The force sensing resistor 50 is placed on a base plate 52, and a thin plastic film 54 with its edges sealed against air leaks covers the force sensing resistor 50. A top plate 56 ic placed over the force sensing resistor 50 and base plate 52. Air lines 5~ connected to the top plate 56 apply a variable air pressure from a variable air pressure source 60 under control of gauge 62 to the force sensing resistor 50. An ohm meter 64 measures the resistance.
WO90/1~25 PCT/VS90/O~B9 2 ~ 3 ~
Referring to Fig. 6, after the force sensing resistor 50 has been calibrated, lead wires 64 must be connected to the sensor. These lead wires may be connected by soldering, bonding, crimping or mechanical S fastening. Leads must be long enough to reach the laminate, following a possibly convoluted path to reach the outside of the tooling used to form the laminate, exit the machinery used to apply pressure and temperature to the laminate as it cures and finally connect to the device 66 used to monitor the signal from the force sensing reslstor. Care should be taken to select leads that can withstand the temperature and pressure conditions to which the leads are exposed during the laminate processing. In particular, the melting temperature of the insulation on the leads should be higher than the maximum processing temperature.
Ater the sensor has been positioned between layers of unprocessed laminate, wires from the sensor should be strung to the exterior of the mold and loading machine.
It is often desirable to run the leads through the laminate in a direction parallel to the principal fiber direction of the adjacent layers of the material so the leads can nest in the most unobtrusive manner possible between the reinforcing fibers when pressure is applied.
In addition, if the sensor and leads are not located in a position that will be trimmed from the finished laminate prior to its use, care should be taken to insure that the sensors and leads do not compromise the structural performance of the laminate. The leads from the force sensing resistor are attached to a device for measuring the resistance of the force sensing resistor.
The force sensing resistor responds to pressure applied to its surface by changing its resistance in relation to applied loads. The simplest device for W090~1~25 PCT/US90/0~89 2~ 3 ~ -12-measuring the resistance of the sensor, and thus in~erring the pressure by correlating the resistance reading to pressure using the calibration curves determined for the force sensing resistor, is a simple s ohm meter. By measuring the resistance of the sensor, the pressure at that point in the laminate can be determined.
Once the force sensing resistor has been positioned in the unprocessed laminate, pressure and temperature are applied to the laminate. Process pressure can be applied using any of a variety of standard methods used by the composite material processing industry including, autoclave methods, hydraulic presses, matched tooling, expanding tooling, compression molding machines, etc.
As pressure is applied to the laminate, the applied pressure is monitored by reading resistance and correlating the readings with applied pressure. This pressure in the laminate can be read directly from analog meters as a resistance; it can be converted electronically to pressure by applying the proper calibration equations relating pressure to resistance;
it can be converted by the use of look-up tables; or it can be read in digital form using a computer to both display and record the data. In some cases it may be necessary to monitor temperature changes and account for its effect on the sensor.
In an alternate embodiment of the present invention shown in ~ig. 4(d)~ the force sensing resistor can be permanently embedded for monitoring pressure at a surface of material forming tools or other tools and equipment used for the production or testing of composite material laminates or other plastic, chemical or metal products. In this embodiment, the sensor is built permanently into the tool 46 or equipment, either on or slightly below the surface, rather than into the WO90/1~ PCT/US90/0~89 -13- 2~5`~
part being manufactured. The tool can be constructed from a number of materials including composite material, metal, plastic, ceramic and other materials or combination of materials. Protective surfaces such as sprayed metal, plastics and other materials could be used to coat the sensor and provide a smooth tool surface. When employed in this fashion, the sensor will become a permanent part of the tool. It could be used to measure pressure during the production of multiple parts from the same tool, rather than being expendable.
Multiple sensors can be built into the surface of each tool to measure the pressure distribution at a variety of points in the product.
In this embodiment, the calibration and the connection of the sensors would be accomplished as described above in connection with the embodiment of Fiys. 5-6, except that the sensor need not necessarily be implanted between layers of composite material, but could instead be positioned directly on the solid surface of the tool. In this embodiment, unlike the embodiment described above and shown in Figs. 5-6, the force sensing resistors would be reusable Referring now to another alternate embodiment shown in Fig. 7, the force sensing resistor is utilized in a special composite materi~l processing method known as pultrusion. Pultrusion is currently used mostly for production of parts having a constant cross section.
Fiber and resin materials 70 are pulled through a pultrusion die 72 at a continuous and steady speed by a variety of mechanical systems. The resin is cured inside the die as it moves through.
~ hen employing the thin force sensing resistor 50, that has been described above, to measure to pultrusion - process pressures, the resistor is calibrated as described above in connection with ~ig. 5, and the leads WO90/l~S PCT/US90~89 '?~ 14-are attached to the sensor in the manner described above. Care should be taken to assure that the leads are long enough to reach the electronic device that will be used to monitor the sensor output to the die entrance and through the die, possibly a distance of 10 feet or more. The leads from the force sensing resistor 50 to the device that measures the resistance of the force sensing resistor 50 are also attached in the same way as described above in connection with the embodiment of Fig. 5.
The force sensing resistor 50 is placed between layers of material prior to the entrance of the material 70 to the pultrusion die. Leads 64 applied to the force sensing resistor are positioned in a way that they will not bind as they are pulled into and through the pultrusion die 72, but instead will feed smoothly without knots, kinks or folds. In Fig. 7, material 70 is fed into the pultrusion die 72, and the finished product 74 exits to the right of the pultrusion die as shown in Fig. 7. The force sensing resistor 50 is initially positioned near the entrance to the die 72 with the leads 64 spooled at the side ready to feed in as the material pulls the force sensing resistor through the system. ~hile Fig. 7 illustrates a pultrusion die using a resin injection method to wet out the materials, ~n almost identical approach could be used if a wet bath or through bath wet out method is used.
Applied pressure is monitored by reading resistance and correlating the reading with applied pressure as described above in connection with the embodiments of Figs. 5-6. As the force sensing resistor is pulled through the pultrusion die, a continuous read out of resistance tpressure) can be measured and recorded. ~y noting the time that each reading is taken, it is possible to calculate the position in the die with which WO90/1~25 PCl/US90/0~8~
2~3~3~
the pressure reading corresponds. When the sensor exits the pultrusion die with the now consolidated and cured laminate the leads should be cut from the entrance end of the die.
In the alternate embodiment of the present - invention shown in Fig. 8, a heated and pressurized vessel known as an autoclave is used to apply pressure to a laminate 80 through a vacuum bag 82 and an exterior pressurized atmosphere. The successful manufacture of composite parts in an autoclave requires that the integrity of the vacuum bag be maintained throughout the process. Loss of the vacuum can result in destruction of the part i~ the failure is not rapidly attended. The force sensing resistor 50 is used as a simple vacuum integrity sensor. When used as a vacuum integrity sensor, the sensor end leads 64 are calibrated and prepared as described above in connection with other embodiments. The sensor is then placed on the surface of the production tool 84, or within layers of auxiliary cure materials in a position where it will be contained inside the vacuum bag 82. The force sensor resistor S0 is sealed inside the vacuum bag 82 using standard bag preparation techniques with the leads 64 extending outside the Dag 82 through a vacuum tight seal. The lead wires are lead to a device 66 that can monitor the resistance of the force sensing resistor 50. The reading of the force sensing resistor 50 prior to applying the vacuum to the vacuum bag is noted and this reading represents the zero pressure value. The vacuum is then applied to the bag and a new reading from the sensor is noted. This reading represents the value that should be maintained throughout the process if vacuum integrity in the bag is maintained. The reading from the sensor is monitored during autoclave processing. If the value drops below a previously selected limit, W090t1~25 ~ pCT/~S90/0~8 indicating an unacceptable leak in the vacuum integrity of the bag, corrective action should be taken in time to save a part that would otherwise be improperly cured.
The foregoing invention has been described with reference to its preferred embodiments. Various alterations and modifications will occur to those skilled in the art. All such variations and modifications are intended to fall within the scope of the appended claims.
Differential scanning calorimetry (DSC), thermograimetric analysis (TGA), thermemechanical analysis (TMA), parallel plate rheometers, dielectric-electrics, ultrasonics, and fiberoptics are only a few of the sensing and measurement technologies that have been applied to research and production of composite materials. None of these monitoring instruments have proven, however, to be useful in monitoring the pressure ! exerted on or between the layers of the composite material.
Composite structures, unlike their metallic counterparts, are built up rather than "machined down".
This difference permits the integration of embedded sensors for use in such diverse applications as adaptive structures which actively damp vibrations or maintain precise geometry over a broad temperature and loading spectrum to structures which monitor the health of the structure in order to warn when damage is present.
.
.
WO90~ PCT/US90/0~4X9 -3- 2~ 3~
Embedded sensors have also recently been used in process technology as ~ell. Thin dielectric cure sensors and thermocouples are routinely laminated between plies in the composite to provide feedback for control of autoclaves and hot presses during processing. Fiber optic cables provide similar information in the autoclave and may also serve a second purpose in the structure as a health monitoring device, communications link or strain indicator.
A missing link in composites processing is a pressure monitoring device that can be embedded in the laminate. In-situ pressure monitoring during process development and during production is extremely important for a number of reasons. Referring to Fig. 1, in a typical laminate consolidation and cure process used in autoclave molding, in resin transfer molding and in filament winding operations, several layers of disposable materials are used to provide high surface quality, absorb excess resin and provide even vacuum distribution. The materials are sealed beneath the nylon film. The area between the caul sheet 14 (or mold surface) and the vacuum bag 16 is evacuated with a vacuum pump (not shown) to approximately 20 inches ~9 or less. The vacuum draws volatiles out of the laminate 12 and provides the necessary pressure gradient between the autoclave and the laminate 12. In autoclave processing, if a vacuum bag 16 breaks or loses its seal, the net force consolidating the part becomes zero and the laminate will not be of acceptable quality after the cure. The part, which may require several weeks to prepare for cure, is then scrapped.
A record of the pressure versus time history of each component is often required to verify the quality of every high performance composite part made. A sensor capable of indicating loss of vacuum pressure would ;
WO9~ 5 PCTJUS90/0~9 ob~La~sly bè a valuable quality control and process monitoring tool. It is possible that early warning of vacuum loss could allow the problem to be repaired or laminate damage minimized. A knowledge of the pressure history during cure is also an important consideration.
Pressure may be varied at di~ferent times during a normal autoclave cure cycle.
In complex tool situations, thermal expansion of metal tooling is used to provide laminate pressurization. Shrink wrap films are often applied to filament wound vessels, radomes and cylinders to apply pressure when heated. Matched dies are used for consolidation in compression molding of composite materials. In all these applications, the actual applied pressure on the laminate is virtually unknown and is unmeasurable by previous existing techniques.
Lamination pressure will typically vary from point to point in large complex dies. A reliable pressure sensing system would be a valuable asset in measuring such applied pressure.
Pultrusion technology has also emer~ed as one of the most rapidly growing (by volume) manufacturing processes for reinforced polymer materials. Referring to Fig. 2, in pultrusion manufacturing, fibers 22 and resins 24 are pulled through a heated die 26 and cured.
Fibers are impregnated with resin by either pulling them through a resin bath or by direct injection at the entrance of the die. The part undergoes an extremely complex series of chemical reactions and thermal expansion, leading to wild excursions in volumetric dimension. Changes in material volume lead to pressure variation within the die which affects consolidation of the laminate. A variety of facto~s including temperature, formulation of resin, volume of fibers, pulling speed and die design influence the pressure ' W090~1~25 PCT/US90tO248~
~5~ 2~7~
profile of the part during cure. The complex interaction o~ the parameters and their effect on laminate pressure cannot be readily analyzed nor can the results be veriEied until a continuous pressure measurement can be determined. Currently, temperature proiles are obtained by passing a thin thermocouple through the die. An example of a temperature profile of an epoxy resin system is shown in Fig. 3. A cross-section of the die is shown on the plot to illustrate the relative position of the thermocouple in the die.
The die temperature is approximately 150 C. The exothermic reaction produces higher resin temperatures.
- The combination of both a thermal profile and pressure profile would unlock the answers to many important lS questions regarding the process conditions within a pultrusion die.
It is therefore a principal object of the present invention to provide a system and method of monitoring exerted pressure during the production of composite material laminate.
Another object of the present invention is to provide a system and method of monitoring exerted ! pressure on a manufactured laminate utilizing a force sensing device either in the laminate or on a tool or die used to manufacture the laminateO
It is another object of the present invention is to provide a composite material laminate or a laminate forming tool including a pressure sensing device for providing a record of pressure versus time history of the composite material laminate.
Yet another object of the present invention is to produce a composite material laminate with a low cost, durable, low profile, temperature resistant pressure sensor embedded therein.
,, WO90/1~25 PCr/US90/0~8 20~ 5a'~ -6-Still another object of the present invention is to provide tools or dies for creating a composite material laminate that include a deviee for measurinq pressure exerted on the composite material laminate created by the tool or die during production.
SUMMARY OF THE INVENTION
Accordingly, a system and method of monitoring exerted pressure during the production of composite material laminates utilizes a thin, low cost, durable, temperature resistant force sensing resistor. The - sensor can be embedded directly on the surface of the composite laminate, or can be positioned between layers of the composite laminate. In this way, the force sensing resistor monitors the pressure experienced by the laminate during processing of the laminate.
Alternatively, the sensor is built into or mounted on a tool or die used to form or exert pressure on the laminate.
These and other features and objects of the present invention will become more fully understood from following the detailed description which should be read in light of the accompanying drawings.
..
BRIE~ DESCRIPTION OF THE DRAWINGS
Fig. l is layup of a prior art preimpregnated composite material laminate constructed out of a Yariety of auxiliary materials;
~ ig. 2 is a diagrammatic view of a prior art pultrusion processing system;
Fig. 3 is a graph of a thermal profile of a graphite/epoxy part generated using a prior art thermocouple passed through the die with the materials used for creating a composite, WO9~1~25 PCT/US90/0248~
~7~ 2 0 ~ ~ ~ 3 6 Pigs. 4(a)-4(d) are perspective views of alternate embodiments of the positioning of a sensor in the system of the present invention;
Fig. S is a schematic view of a device for use in calibrating the force sensing resistor utilized in the composite material laminate of the present invention;
Eig. 6 is a perspective view of a force sensing resistor placed between layers of a composite material laminate of the present invention;
~ig. 7 is diagrammatic view of pultrusion die through which a force sensing resistor will be pulled with the materials for creating a composite material laminate according to the present invention;
Fig. 8 shows use of a force sensing resistor mounted on a tool of the present invention used in an autoclave.
DETAILED DESCRIPTION_OF T~E PREFERRED EMBODIMENTS
In a preferred embodiment, in order to measure the pressure exerted on a composite laminate manufactured throu~h the use of autoclave molding, compression molding, resin injection molding, pultrusion, reaction injection molding, press molding and other procedures, a thin force sensing resistor is embedded between laminate ¦ layers of the product during assembly of its layers or is placed between the surface of the composite laminate and the tool against which the composite is cured. In some cases, layers of disposable materials are positioned between the composite product and the tool, and the sensor can be placed in these layers as well. A
suitable resistor is described in U.S. Patent No.
4,301,337, the teachings of which are incorporated - herein by reference. In preferred embodiments, the resistor, however, includes one pressure switch rather j than the two desrribed in this patent.
-- .
i L
WV90/1~25 PCT/VS~0/0~8 ~95rj ~T~ force sensing resistor, ~hich was developed to i generate tones in an electronic musical device, is a dual switch that is actuated in response to a single touch force. In its commercial form, this force sensing j 5 resistor, which is sold by Interlink Electronics of Santa 3arbara, California under the designation Forcing Sensing Resistor or FS~, has a thickness of less than O.5 mm, has good dynamic and pressure ranges and has minimum temperature sensitivity. In particular, the force sensing resistor is available in thicknesses ranging from 0.005 to 0.050 inches. As will be more fully described below, this thin profile allows the force sensing resistor to be implanted inside a ! laminate, placed on the surface of a laminate, placed within supporting cure materials of a laminate, placed on a laminate forming tool, or built permanently below the surface of the tool.
This force sensing resistor is also available in a variety of surface areas. Sensors with surface areas from less than 0.5 to more than 5,000 square cm are ` currently available with other sizes possible for speci~l applications. This range of surface areas j allows the device to be used for many different types of pressure monitoring applications. The use of a sensor with a small surface area in the present invention allows pressure at a point to be measured, and the use of a sensor with a large surface area allows the measurement o~ average pressures or the determination of the distribution of pressure over a large area. The sensor in its commerical form can be used in temperatures up to 300F and it is possible to special order the sensor so that it can operate at temperatures approaching 800. Such temperature ranges are appropriate for many plastics, composites and chemical manufacturing, testing and service conditions. Anotùer .
, r WO90/1~25 PCT/VS90/024~9 -9- 2~3~3~
advantage of the sensor is that it can be tailored to be sensitive to a variety of pressure ranges of interest to the material processing industry. The sensitivity of the sensor to changes in operating temperatures is small. For many applications such as monitoring the loss of vacuum pressure, temperature sensitivity can be ignored. For more percise measurements, temperature effects can be accounted for by simple calibration and curve fittings. The resistor (or sensor) can remain a permanent part of the composite after the consolidation and cure of the material has been completed (and therefore lost during the production process) or, if properly positioned, it can be removed during a trimming operation.
The creation of the composite laminate with an - embedded sensor will now be described in detail. During the layup of uncured laminate, a force sensing resistor 50 is placed between material layers 42 at locations in the laminate (Fig. 6) and/or the surrounding trim, scrape or follower materials, where measurement of the processing pressure is desired. Alternatively, the force sensing resistor can be placed between layers of supporting material 44 (~ig. 4a), placed directly between the laminate 42 and the tool 46 (Fig. 4b), placed on the tool 46 away from the composite laminate 42 (Fig. 4c) or permanently built into the processing tool 46 slightly below the tool surface (Fig. 4d).
Because of the very thin profile of the sensors and leads, the surface imperfection at the sensor location from the build-up of additional thickness is minimized.
The thinness of the force sensing resistor also improves its ability to accurately measure the pressure in the laminate, especially when manufacturing techniques such as press molding, matched die molding and pultrusion, which apply load to the surface by closing or otherwise .
W090/13~2~ ~ P~T/US~0/0~89 S~ 10-controlling the thickness of the laminate as it cures, are employed. Thick points, caused by thick sensors, in a laminate would locally contact the sur~aces with more force. Therefore, the thinness of the force sensing resistor becomes an important feature of the present invention that allows this force sensing resistor to be used as part of a composite laminate.
Prior to positioning the sensor in the system of the present invention ~e.g. between layers of unprocessed laminate), the sensor may need to be calibrated. The calibration can be obtained from non-spec-fic data supplied by the sensor manufacturer, or each sensor can be individually calibrated. The force sensing resistor operates by changing its electrical resistance in a way that is directly and repeatedly related to applied surface pressure. Calibration of the sensor, for those applications requiring more detailed and accurate pressure readings, can be accomplished by applying a series of known pressures to the surface of the force sensor resistor and measuring its resistance at each of these pressures.
~ ig. 5 shows one possible method for obtaining a pressure versus sensor output curve for individual sensors when detailed calibration is required. The force sensing resistor 50 is placed on a base plate 52, and a thin plastic film 54 with its edges sealed against air leaks covers the force sensing resistor 50. A top plate 56 ic placed over the force sensing resistor 50 and base plate 52. Air lines 5~ connected to the top plate 56 apply a variable air pressure from a variable air pressure source 60 under control of gauge 62 to the force sensing resistor 50. An ohm meter 64 measures the resistance.
WO90/1~25 PCT/VS90/O~B9 2 ~ 3 ~
Referring to Fig. 6, after the force sensing resistor 50 has been calibrated, lead wires 64 must be connected to the sensor. These lead wires may be connected by soldering, bonding, crimping or mechanical S fastening. Leads must be long enough to reach the laminate, following a possibly convoluted path to reach the outside of the tooling used to form the laminate, exit the machinery used to apply pressure and temperature to the laminate as it cures and finally connect to the device 66 used to monitor the signal from the force sensing reslstor. Care should be taken to select leads that can withstand the temperature and pressure conditions to which the leads are exposed during the laminate processing. In particular, the melting temperature of the insulation on the leads should be higher than the maximum processing temperature.
Ater the sensor has been positioned between layers of unprocessed laminate, wires from the sensor should be strung to the exterior of the mold and loading machine.
It is often desirable to run the leads through the laminate in a direction parallel to the principal fiber direction of the adjacent layers of the material so the leads can nest in the most unobtrusive manner possible between the reinforcing fibers when pressure is applied.
In addition, if the sensor and leads are not located in a position that will be trimmed from the finished laminate prior to its use, care should be taken to insure that the sensors and leads do not compromise the structural performance of the laminate. The leads from the force sensing resistor are attached to a device for measuring the resistance of the force sensing resistor.
The force sensing resistor responds to pressure applied to its surface by changing its resistance in relation to applied loads. The simplest device for W090~1~25 PCT/US90/0~89 2~ 3 ~ -12-measuring the resistance of the sensor, and thus in~erring the pressure by correlating the resistance reading to pressure using the calibration curves determined for the force sensing resistor, is a simple s ohm meter. By measuring the resistance of the sensor, the pressure at that point in the laminate can be determined.
Once the force sensing resistor has been positioned in the unprocessed laminate, pressure and temperature are applied to the laminate. Process pressure can be applied using any of a variety of standard methods used by the composite material processing industry including, autoclave methods, hydraulic presses, matched tooling, expanding tooling, compression molding machines, etc.
As pressure is applied to the laminate, the applied pressure is monitored by reading resistance and correlating the readings with applied pressure. This pressure in the laminate can be read directly from analog meters as a resistance; it can be converted electronically to pressure by applying the proper calibration equations relating pressure to resistance;
it can be converted by the use of look-up tables; or it can be read in digital form using a computer to both display and record the data. In some cases it may be necessary to monitor temperature changes and account for its effect on the sensor.
In an alternate embodiment of the present invention shown in ~ig. 4(d)~ the force sensing resistor can be permanently embedded for monitoring pressure at a surface of material forming tools or other tools and equipment used for the production or testing of composite material laminates or other plastic, chemical or metal products. In this embodiment, the sensor is built permanently into the tool 46 or equipment, either on or slightly below the surface, rather than into the WO90/1~ PCT/US90/0~89 -13- 2~5`~
part being manufactured. The tool can be constructed from a number of materials including composite material, metal, plastic, ceramic and other materials or combination of materials. Protective surfaces such as sprayed metal, plastics and other materials could be used to coat the sensor and provide a smooth tool surface. When employed in this fashion, the sensor will become a permanent part of the tool. It could be used to measure pressure during the production of multiple parts from the same tool, rather than being expendable.
Multiple sensors can be built into the surface of each tool to measure the pressure distribution at a variety of points in the product.
In this embodiment, the calibration and the connection of the sensors would be accomplished as described above in connection with the embodiment of Fiys. 5-6, except that the sensor need not necessarily be implanted between layers of composite material, but could instead be positioned directly on the solid surface of the tool. In this embodiment, unlike the embodiment described above and shown in Figs. 5-6, the force sensing resistors would be reusable Referring now to another alternate embodiment shown in Fig. 7, the force sensing resistor is utilized in a special composite materi~l processing method known as pultrusion. Pultrusion is currently used mostly for production of parts having a constant cross section.
Fiber and resin materials 70 are pulled through a pultrusion die 72 at a continuous and steady speed by a variety of mechanical systems. The resin is cured inside the die as it moves through.
~ hen employing the thin force sensing resistor 50, that has been described above, to measure to pultrusion - process pressures, the resistor is calibrated as described above in connection with ~ig. 5, and the leads WO90/l~S PCT/US90~89 '?~ 14-are attached to the sensor in the manner described above. Care should be taken to assure that the leads are long enough to reach the electronic device that will be used to monitor the sensor output to the die entrance and through the die, possibly a distance of 10 feet or more. The leads from the force sensing resistor 50 to the device that measures the resistance of the force sensing resistor 50 are also attached in the same way as described above in connection with the embodiment of Fig. 5.
The force sensing resistor 50 is placed between layers of material prior to the entrance of the material 70 to the pultrusion die. Leads 64 applied to the force sensing resistor are positioned in a way that they will not bind as they are pulled into and through the pultrusion die 72, but instead will feed smoothly without knots, kinks or folds. In Fig. 7, material 70 is fed into the pultrusion die 72, and the finished product 74 exits to the right of the pultrusion die as shown in Fig. 7. The force sensing resistor 50 is initially positioned near the entrance to the die 72 with the leads 64 spooled at the side ready to feed in as the material pulls the force sensing resistor through the system. ~hile Fig. 7 illustrates a pultrusion die using a resin injection method to wet out the materials, ~n almost identical approach could be used if a wet bath or through bath wet out method is used.
Applied pressure is monitored by reading resistance and correlating the reading with applied pressure as described above in connection with the embodiments of Figs. 5-6. As the force sensing resistor is pulled through the pultrusion die, a continuous read out of resistance tpressure) can be measured and recorded. ~y noting the time that each reading is taken, it is possible to calculate the position in the die with which WO90/1~25 PCl/US90/0~8~
2~3~3~
the pressure reading corresponds. When the sensor exits the pultrusion die with the now consolidated and cured laminate the leads should be cut from the entrance end of the die.
In the alternate embodiment of the present - invention shown in Fig. 8, a heated and pressurized vessel known as an autoclave is used to apply pressure to a laminate 80 through a vacuum bag 82 and an exterior pressurized atmosphere. The successful manufacture of composite parts in an autoclave requires that the integrity of the vacuum bag be maintained throughout the process. Loss of the vacuum can result in destruction of the part i~ the failure is not rapidly attended. The force sensing resistor 50 is used as a simple vacuum integrity sensor. When used as a vacuum integrity sensor, the sensor end leads 64 are calibrated and prepared as described above in connection with other embodiments. The sensor is then placed on the surface of the production tool 84, or within layers of auxiliary cure materials in a position where it will be contained inside the vacuum bag 82. The force sensor resistor S0 is sealed inside the vacuum bag 82 using standard bag preparation techniques with the leads 64 extending outside the Dag 82 through a vacuum tight seal. The lead wires are lead to a device 66 that can monitor the resistance of the force sensing resistor 50. The reading of the force sensing resistor 50 prior to applying the vacuum to the vacuum bag is noted and this reading represents the zero pressure value. The vacuum is then applied to the bag and a new reading from the sensor is noted. This reading represents the value that should be maintained throughout the process if vacuum integrity in the bag is maintained. The reading from the sensor is monitored during autoclave processing. If the value drops below a previously selected limit, W090t1~25 ~ pCT/~S90/0~8 indicating an unacceptable leak in the vacuum integrity of the bag, corrective action should be taken in time to save a part that would otherwise be improperly cured.
The foregoing invention has been described with reference to its preferred embodiments. Various alterations and modifications will occur to those skilled in the art. All such variations and modifications are intended to fall within the scope of the appended claims.
Claims (15)
[received by the International Bureau on 16 October 1990 (16.10.90);
original claims 1-8 replaced by amended claims 1-8, new claims 9-15 added (4 pages)]
1. (Amended) A system for measuring pressure exerted during the production of a composite material laminate, said system comprising:
fiber material and polymer matrix material mixed together to form a composite material through the application of heat and pressure;
a force sensing resistor positioned within the system for measuring process pressure applied to said composite material while the composite material is being produced;
means for measuring resistances sensed by said force sensing resistor.
fiber material and polymer matrix material mixed together to form a composite material through the application of heat and pressure;
a force sensing resistor positioned within the system for measuring process pressure applied to said composite material while the composite material is being produced;
means for measuring resistances sensed by said force sensing resistor.
2. (Amended) The system for measuring pressure of claim 1 wherein said force sensing resistor is embedded in a surface of said composite material laminate for meausring the process pressure applied to a surface of said composite material.
3. (Amended) The system for measuring pressure of claim 1 further comprising layers of composite material laminate and wherein said force sensing resistor is positioned between two of said layers of said composite material laminate.
4. (Amended) The system for measuring pressure of claim 1 wherein said system further comprises a forming tool for exerting pressure on said composite material and wherein said force sensing resistor is embedded in said forming tool below a protective layer on a surface of the forming tool.
5. (Amended) The system for measuring pressure of claim 1 wherein said system further comprises:
a forming tool for exerting pressure on said composite material, and at least two layers of cure supporting materials;
and wherein said force sensing resistor is positioned between said two layers of cure supporting materials.
a forming tool for exerting pressure on said composite material, and at least two layers of cure supporting materials;
and wherein said force sensing resistor is positioned between said two layers of cure supporting materials.
6. (Amended) The system for measuring the pressure the claim 1 wherein said system further comprises a forming tool for exerting pressure on said composite material, and wherein said force sensing resistor is placed on a surface of said forming tool between said forming tool and said composite material.
7. (Amended) The system for measuring pressure of claim 1 wherein said system further comprises:
a forming tool for exerting pressure on said composite material;
a vacuum bag that encloses said composite material;
and wherein said force sensing resistor is positioned within said vacuum bag out of contact with said laminate.
a forming tool for exerting pressure on said composite material;
a vacuum bag that encloses said composite material;
and wherein said force sensing resistor is positioned within said vacuum bag out of contact with said laminate.
8. (Amended) A method for measuring pressure exerted during the production of a composite material laminate, said method comprising the steps of:
mixing fiber material and polymer material together to form a composite material through the application of heat and pressure;
positioning a force sensing resistor relative to said mixed materials so as to enable said force sensing resistor to measure a pressure experienced by said mixed materials while the composite material is being produced;
measuring the resistance sensed by said force sensing resistor;
converting said resistance into a corresponding pressure reading indicating the pressure experienced by said mixed materials while the composite material is being produced.
mixing fiber material and polymer material together to form a composite material through the application of heat and pressure;
positioning a force sensing resistor relative to said mixed materials so as to enable said force sensing resistor to measure a pressure experienced by said mixed materials while the composite material is being produced;
measuring the resistance sensed by said force sensing resistor;
converting said resistance into a corresponding pressure reading indicating the pressure experienced by said mixed materials while the composite material is being produced.
9. (New) The system for measuring pressure of claim 1 wherein said force sensing resister has a thickness between 0.005 inches and 0.50 inches.
10. (New) The system for measuring pressure of claim 1 wherein said sensor has an appropriate surface area and is positioned within said system at a location appropriate to allow the measurement of pressure applied to a single small area of said composite material.
11. (New) The system for measuring pressure of claim 1 wherein said sensor has an appropriate surface area and is positioned within said system at a location appropriate to allow the measurement of average pressures.
12. (New) The system for measuring pressure of claim 1 wherein said sensor has an appropriate surface area and is positioned within said system at a location appropriate to allow the determination of the distribution of pressure over an entire area.
13. (New) The system for measuring pressure of claim 1 wherein said force sensing resistor changes its electrical resistance in direct relationshp to pressure applied to a surface of said resistor.
14. (New) The system for measuring pressure of claim 1 wherein said composite material is produced in a pultrussion die and said force sensing resistor is positioned between layers of composite material laminate before said layers are pulled through said die.
15. (New) A system for measuring pressure exerted during the production of a composite material laminate, said system comprising:
fiber material and polymer matrix material mixed together to form a composite material through the application of heat and pressure;
a force sensing means, positioned within the system for measuring process pressure experienced by said composite material while the composite material is being produced; said force sensing means having a thickness between 0.005 and 0.050 inches and a surface area greater than 0.5 cm means for measuring resistances sensed by said force sensing resistor.--
fiber material and polymer matrix material mixed together to form a composite material through the application of heat and pressure;
a force sensing means, positioned within the system for measuring process pressure experienced by said composite material while the composite material is being produced; said force sensing means having a thickness between 0.005 and 0.050 inches and a surface area greater than 0.5 cm means for measuring resistances sensed by said force sensing resistor.--
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|---|---|---|---|
| US34882289A | 1989-05-08 | 1989-05-08 | |
| US348,822 | 1989-05-08 |
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|---|---|
| CA2055436A1 true CA2055436A1 (en) | 1990-11-09 |
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|---|---|---|---|
| CA002055436A Abandoned CA2055436A1 (en) | 1989-05-08 | 1990-05-04 | System and method for monitoring pressure during the production of fiber reinforced polymers |
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| EP (1) | EP0472590A4 (en) |
| JP (1) | JPH04505135A (en) |
| CA (1) | CA2055436A1 (en) |
| WO (1) | WO1990013425A1 (en) |
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| US4140050A (en) * | 1977-10-27 | 1979-02-20 | Formica Corporation | Method and apparatus for controlling rate related manufacturing operations using a reaction simulation technique |
| DE3038288C1 (en) * | 1980-10-10 | 1982-04-08 | Robert Bürkle GmbH & Co, 7290 Freudenstadt | Device for determining the pour point of resin laminates in the production of multilayer printed circuit boards |
| US4515545A (en) * | 1981-07-09 | 1985-05-07 | Applied Polymer Technology, Inc. | Control system for processing composite material |
| US4486996A (en) * | 1982-05-19 | 1984-12-11 | Luis Alejos | Construction-panel prefabrication method, panels thus made and equipment for implementing said method |
| US4502857A (en) * | 1983-04-04 | 1985-03-05 | The Goodyear Tire & Rubber Company | Green tire-to-mold contact time detection, analysis, and control |
| US4773021A (en) * | 1987-07-31 | 1988-09-20 | General Electric Company | Adaptive model-based pressure control and method of resin cure |
-
1990
- 1990-05-04 JP JP2507815A patent/JPH04505135A/en active Pending
- 1990-05-04 WO PCT/US1990/002489 patent/WO1990013425A1/en not_active Application Discontinuation
- 1990-05-04 CA CA002055436A patent/CA2055436A1/en not_active Abandoned
- 1990-05-04 EP EP19900907685 patent/EP0472590A4/en not_active Withdrawn
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108692846A (en) * | 2018-05-09 | 2018-10-23 | 中南大学 | A kind of hot-press solidifying composite product and mold interface stress monitoring system |
Also Published As
| Publication number | Publication date |
|---|---|
| JPH04505135A (en) | 1992-09-10 |
| EP0472590A4 (en) | 1992-05-27 |
| EP0472590A1 (en) | 1992-03-04 |
| WO1990013425A1 (en) | 1990-11-15 |
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| Date | Code | Title | Description |
|---|---|---|---|
| EEER | Examination request | ||
| FZDE | Discontinued |