US20140159267A1 - System and method for forming composite articles - Google Patents

System and method for forming composite articles Download PDF

Info

Publication number
US20140159267A1
US20140159267A1 US14/232,723 US201214232723A US2014159267A1 US 20140159267 A1 US20140159267 A1 US 20140159267A1 US 201214232723 A US201214232723 A US 201214232723A US 2014159267 A1 US2014159267 A1 US 2014159267A1
Authority
US
United States
Prior art keywords
subsystem
tool
heater
fluid
tank
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
Application number
US14/232,723
Other languages
English (en)
Inventor
Robert W. Murch
Gary R. Lownsdale
Douglas L. Bartolotti
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Plasan Carbon Composites Inc
Original Assignee
Plasan Carbon Composites Inc
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Plasan Carbon Composites Inc filed Critical Plasan Carbon Composites Inc
Priority to US14/232,723 priority Critical patent/US20140159267A1/en
Assigned to PLASAN CARBON COMPOSITES, INC. reassignment PLASAN CARBON COMPOSITES, INC. ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: LOWNSDALE, GARY R., BARTOLOTTI, DOUGLAS S., MURCH, ROBERT W.
Assigned to PLASAN CARBON COMPOSITES, INC. reassignment PLASAN CARBON COMPOSITES, INC. CORRECTIVE ASSIGNMENT TO CORRECT THE TO REMOVE INCORRECT SERIAL NUMBER 12/048,832 AND CORRECT MIDDLE INITIAL OF DOUGLAS BARTOLOTTI FROM "S." TO "L." (AS SIGNED) PREVIOUSLY RECORDED ON REEL 029078 FRAME 0919. ASSIGNOR(S) HEREBY CONFIRMS THE ASSIGNMENT. Assignors: LOWNSDALE, GARY R., BARTOLOTTI, DOUGLAS L., MURCH, ROBERT W.
Publication of US20140159267A1 publication Critical patent/US20140159267A1/en
Assigned to FIRST MIDWEST BANK, AS ADMINISTRATIVE AGENT reassignment FIRST MIDWEST BANK, AS ADMINISTRATIVE AGENT SECURITY INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: PLASAN CARBON COMPOSITES, INC.
Abandoned legal-status Critical Current

Links

Images

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C35/00—Heating, cooling or curing, e.g. crosslinking or vulcanising; Apparatus therefor
    • B29C35/007—Tempering units for temperature control of moulds or cores, e.g. comprising heat exchangers, controlled valves, temperature-controlled circuits for fluids
    • 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
    • B29C35/00—Heating, cooling or curing, e.g. crosslinking or vulcanising; Apparatus therefor
    • B29C35/02—Heating or curing, e.g. crosslinking or vulcanizing during moulding, e.g. in a mould
    • B29C35/0288—Controlling heating or curing of polymers during moulding, e.g. by measuring temperatures or properties of the polymer and regulating the process
    • B29C35/0294—Controlling heating or curing of polymers during moulding, e.g. by measuring temperatures or properties of the polymer and regulating the process using tempering units for temperature control of moulds or cores

Definitions

  • the present invention generally relates to a system and method for forming composite articles, and more specifically to a thermal system and method for forming carbon fiber composite articles.
  • Carbon fiber composite (CFC) articles typically comprise two or more layers of a carbon fiber mat comprising carbon fiber filaments, which are impregnated by a plastic resin, in a final cured state.
  • Conventional methods for forming CFC articles include vacuum bag molding, pressure molding, Virtual Engineered Composites (VEC) molding, autoclave molding, and resin transfer molding (RTM).
  • VEC Virtual Engineered Composites
  • RTM resin transfer molding
  • Newer automotive industry regulations including the Corporate Average Fuel Economy (CAFE), Head Impact Characteristic (HIC), and Pedestrian Protection, represent a challenge to conventional materials used in automobiles, such as steel.
  • CFC articles include an excellent combination of physical properties including strength, weight, and energy absorption. As such, CFC articles are able to meet these newer requirements, such as requirements for mass reduction and energy absorption.
  • CFC articles Unfortunately, a major issue with conventional CFC articles is the amount of time it takes to manufacture CFC articles relative to conventional articles, such as those made out of steel. In addition, it can be time consuming and difficult to achieve CFC articles with aesthetically pleasing surfaces, such as “Class A” surfaces. As such, there remains an opportunity to provide improved methods and systems for forming CFC articles.
  • the present invention provides a thermal system for rapidly heating and cooling a mold surface of a tool.
  • the thermal system comprises a heater-subsystem in fluid communication with the tool.
  • the heater-subsystem comprises a heater for heating a first thermal fluid, a tank in fluid communication with the heater and containing a mass of heated first thermal fluid, and a three-way valve.
  • the three-way valve is in fluid communication i) between the tank and the heater for re-circulating the first thermal fluid from the tank to the heater and ii) between the tank and the tool for directing the first thermal fluid from the tank to the tool.
  • the thermal system further comprises an exchanger-subsystem in fluid communication with the heater-subsystem and the tool.
  • the exchanger-subsystem comprises an exchanger for cooling the first thermal fluid returning from the tool, and a three-way valve.
  • the three-way valve is in fluid communication i) between the exchanger and the heater-subsystem for sending the first thermal fluid from the tool back to the heater-subsystem and ii) between the exchanger and the tool for directing the first thermal fluid from the tool to the exchanger.
  • the thermal system further comprises a chiller-subsystem in fluid communication with the exchanger-subsystem.
  • the chiller-subsystem comprises a chiller to cool a second thermal fluid, a tank in fluid communication with the chiller and containing a mass of cooled second thermal fluid, and a three-way valve.
  • the three-way valve is in fluid communication i) between the tank and the chiller for re-circulating the second thermal fluid from the tank to the chiller and ii) between the tank and the exchanger-subsystem for directing the second thermal fluid from the tank to the exchanger.
  • the tool can be used for forming a composite article, such as a carbon fiber composite article.
  • the present invention also provides a method of rapidly heating and cooling the mold surface of the tool.
  • the method comprises the steps of providing the heater-subsystem, providing the exchanger-subsystem, providing the chiller-subsystem, and providing a controller.
  • the controller is in communication with the tool and the subsystems for instructing the subsystems.
  • the method further comprises the step of directing the mass of heated first thermal fluid from the tank of the heater-subsystem to the tool via the controller to heat the mold surface of the tool from a first temperature (T 1 ) to a second temperature (T 2 ) within a first period of time (Tt 1 ).
  • the method further comprises the step of directing the mass of heated first thermal fluid from the tank of the heater-subsystem to the mold surface of the tool via the controller to maintain the mold surface at T 2 for a second period of time (Tt 2 ).
  • the method further comprises the step of directing the mass of cooled second thermal fluid from the tank of the chiller-subsystem to the exchanger-subsystem via the controller to cool the first thermal fluid returning from the tool from T 2 to a third temperature (T 3 ) within a third period of time (Tt 3 ).
  • the mold surface of the tool heats at a rate of greater than about 60° F. ( ⁇ 33° C.) per minute and cools at a rate of greater than about 40° F. ( ⁇ 22° C.) per minute.
  • Tt 1 +Tt 2 +Tt 3 is no greater than about 20 minutes.
  • the present invention provides various benefits over conventional systems and methods for forming composite articles.
  • conventional methods such as autoclaving, generally have cycle times that are well over an hour, typically cycle times of 75 minutes or longer.
  • Such cycle times are the times in which the composite articles are formed within the autoclave (e.g. during cure of a resin).
  • preforms are disposed on tools, the tools are loaded into the autoclave, vacuum bags (or other vacuum means) are attached to the tools, the autoclave is closed, vacuum is applied, and the autoclave is heated and pressurized with nitrogen gas (N 2 ) for an extended period of time, e.g. 75+ minutes, to form the composite articles.
  • N 2 is generally required to prevent flash fires in the autoclave due to exotherms. Additional time associated with loading, closing, opening, and unloading the autoclave further decreases output.
  • the autoclave takes a long time to heat and requires the use of N 2 for safety reasons. As such, energy costs associated with the autoclave tends to be high. In order to increase output of composite articles, autoclaves tend to be large in size, thereby having a large footprint. Such sizing of the autoclave also requires a large number of heavy and expensive tools, further adding to capital and manufacturing costs.
  • Autoclaves are also prone to making scrap parts. For example, if vacuum fails (or is interrupted) on one (or more) of the tools while in the autoclave, the composite article will cure in an improper configuration, e.g. a non-consolidated form. The vacuum cannot be reestablished until after the cure cycle is complete, which is too late to save the composite article. As such, the composite article(s) with vacuum problems must be scrapped after being removed from the autoclave.
  • Composite articles formed in autoclaves also tend to suffer from surfaces blemishes, such as pits of various location, diameter and depth. Such surface blemishes must be removed during finishing steps of the composite article, such as by filling and sanding, further adding to manufacturing costs.
  • the thermal system and method of the present invention provide one or more benefits over the prior art.
  • the present invention provides for excellent temperature control relative to conventional autoclaving systems and methods.
  • the present invention can provide reduced cycle times relative to autoclave cycles, which provides for increased output. Reduced energy costs may also be appreciated.
  • a reduced footprint may be provided by the thermal system relative to large autoclaves.
  • the same or similar chemistries and/or materials generally used for conventional autoclave methods, e.g. resins, may generally be used with the present invention, therefore not requiring chemistry or material redesign.
  • the present invention generally provides composite articles which have excellent surface properties that generally match those of carbon composite articles formed in an autoclave. For example, surface blemishes (e.g. pits) are generally reduced in number and/or severity. In addition or alternatively, the present invention generally provides composite articles which have excellent mechanical properties that match or exceed those of carbon composite articles formed in an autoclave.
  • FIG. 1 is a schematic view of a thermal system having a heater-subsystem, a valve, a controller, a press, a tool disposed within the press, and a pressure tank;
  • FIG. 2 is a schematic view of another embodiment of the thermal system having a heater-subsystem, a chiller-subsystem, valves, the controller, the press, the tool disposed within the press, and the pressure tank;
  • FIG. 3 is a partially exploded perspective view of the tool, a vacuum canopy, and a preform of a composite article disposed between the tool and vacuum canopy;
  • FIG. 4 is a cross-sectional end-view of the tool having a mold surface and tubing, the vacuum canopy attached to the tool, and the preform of the composite article disposed between the mold surface and vacuum canopy;
  • FIG. 5 is a perspective view of a support table, the tool disposed on the support table, the vacuum canopy disposed on the tool, and the press having a platform and a cover;
  • FIG. 6 is an enlarged perspective view detailing portions of the press and tool illustrated in FIG. 5 , with the press including a carrier and rams for moving the tool in and out of the press;
  • FIG. 7 is a partial cross-sectional end-view of the press having a cavity defined between the platform and the cover, the tool having the mold surface and tubing, the vacuum canopy attached to the tool, and the preform of the composite article disposed between the mold surface and vacuum canopy;
  • FIG. 8 is a perspective simplified environmental view of another embodiment of the press, support tables, and composite articles, with technicians disposing a preform of the composite article on a mold surface of the tool disposed on one of the support tables;
  • FIG. 9 is a cross-sectional side-view of a mandrel having a mandrel surface and tubing, with pieces of a carbon fiber sheet being disposed on the mandrel surface, and a vacuum sheet being disposed over the pieces on the mandrel surface;
  • FIG. 10 is a flow chart generally illustrating additional, optional, manufacturing steps for forming the composite article
  • FIG. 11 is a graph illustrating temperature, pressure, vacuum and heater profiles over time for an invention example of the composite article using the thermal system and press;
  • FIG. 12 is another graph illustrating temperature, pressure, and vacuum profiles over time for another invention example of the composite article using the thermal system and press;
  • FIG. 13 is another graph illustrating temperature, pressure, and vacuum profiles over time for another invention example of the composite article using the thermal system and press;
  • FIG. 14 is a graph illustrating temperature, pressure, vacuum and heater profiles over time for a comparative example of a composite article using a conventional autoclave
  • FIG. 15 is a perspective view of a tool-connection system operatively connected to the tool, with the tool-connection system including connections for feed and return of thermal fluid to and from the tubing of the tool, connections for a vacuum and static line for pressure monitoring, and a connection for a resistive thermal device (RTD) for temperature monitoring and providing feedback;
  • the tool-connection system including connections for feed and return of thermal fluid to and from the tubing of the tool, connections for a vacuum and static line for pressure monitoring, and a connection for a resistive thermal device (RTD) for temperature monitoring and providing feedback;
  • RTD resistive thermal device
  • FIG. 16 is a perspective view of a press-connection system operatively connected to the cover of the press for coupling with the tool-connection system shown in FIG. 15 , with the press-connection system including connections for feed and return of thermal fluid through the cover of the press and to and from the tubing of the tool, connections for a vacuum and static line for pressure monitoring, and a connection for a RTD for temperature monitoring and providing feedback;
  • FIG. 17 is a partial cross-sectional side-view of the press having the cavity defined between the platform and the cover, with the tool-connection system and the press-connection system coupled together such that thermal fluid can be communicated to and from the tool with the thermal system;
  • FIG. 18 is a schematic view of another embodiment of the thermal system having a heater-subsystem, a chiller-subsystem, an exchanger-subsystem, valves, the controller, the press, the tool disposed within the press, and the pressure tank.
  • a thermal system is generally shown at 20 .
  • the thermal system 20 is hereinafter simply referred to as the system 20 .
  • the system 20 can be used for forming various types of articles.
  • the system 20 is useful for forming composite articles 22 , such as carbon fiber reinforced plastics 22 or carbon fiber composite (CFC) articles 22 .
  • CFC articles 22 are useful in many industries, such as in the automotive, marine, military defense, aeronautical, aerospace, and medical equipment industries.
  • the system 20 is especially useful for forming “Class A” CFC body panels 22 across entire vehicle platforms.
  • body panels 22 and related parts include hoods, fenders, roofs, rockers, splitters, roof bows, dive planes, wings, mirror caps, deflectors, etc.
  • CFC articles 22 include deck-lids, battery applications, control arms, bumpers, cradles/sub-frames, and other structural components.
  • the system 20 is not limited to forming any particular type of composite article 22 , or composite articles 22 for a particular industry, and such composite articles 22 can be of various sizes, shapes, and use. The composite articles 22 are described further below.
  • the system 20 is useful for heating and cooling a mold surface 24 of a tool 26 .
  • the system 20 is useful for heating and cooling a fluid, with the fluid used for directly (or nearly directly) heating and cooling the mold surface 24 of the tool 26 .
  • the system 20 can be used in combination with or separate from the methods of the present invention. The invention methods are described further below, and can be used in combination with or separate from the system 20 .
  • the tool 26 can be a portion of a mold (e.g. a two-piece mold) where the tool 26 is a top mold and another tool is a bottom mold, or vice versa.
  • the tool 26 is typically a one-piece mold 26 (e.g. an open mold).
  • the system 20 is generally associated with at least one type of the tool 26 , but may be associated with two or more different types of tools 26 , which can be the same as or different from each other.
  • the tool 26 can be of various types, albeit possibly being modified for communicating with the system 20 .
  • the tool 26 is of the type (or similar to the type) generally used in conventional autoclaves.
  • the system 20 is not typically associated with an autoclave. In other words, the system 20 is generally free of an autoclave, as are the invention methods.
  • the tool 26 is of the type generally used for vacuum molding (or forming). In another embodiment, the tool 26 is of the type generally used for resin transfer molding (RTM). It is to be appreciated that other types of tools 26 can also be used.
  • the mold surface 24 and the tool 26 may be unitary, i.e., a single body.
  • the mold surface 24 and the tool 26 are separate pieces joined together, e.g. by fasteners, by welding, etc.
  • different mold surfaces 24 may be used with different tools 26 or vice versa. This allows for interchangeability between different mold surfaces 24 and/or different tools 26 for forming different types of composite articles 22 .
  • the mold surface 24 of the tool 26 can be configured to have various shapes. Typically, the mold surface 24 is configured in a shape corresponding to a particular composite article 22 being made, e.g. a hood, a fender, a spoiler, etc. The mold surface 24 is not limited to any particular shape.
  • the mold surface 24 of the tool 26 is typically formed from a metallic material, which is useful for heat transfer, such as nickel, steel, etc.
  • the mold surface 24 comprises a nickel alloy 22 .
  • the mold surface 24 is generally rigid and inflexible (which is different from a rubber or “bladder” type mold surface).
  • Metallic mold surfaces 24 generally have a high thermal conductivity, which allows for rapid heating and cooling of the mold surface 24 . This is especially true when utilized along with the system 20 .
  • the mold surface 24 can be of various thicknesses, typically of from about 5 to about 20, from about 7.5 to about 15, or from about 10 to about 12.5, mm. Suitable mold surfaces 24 are commercially available from a variety of suppliers.
  • mold surfaces 24 include those commercially available from Weber Manufacturing Team of Midland, Ontario, Canada, such as nickel shell mold surfaces 24 ; Visioneering Inc. of Fraser, Mich.; and Models & Tools Inc. of Troy, Mich., such as mold surfaces 24 formed from Invar (or “64FeNi”).
  • the tool 26 typically includes tubing 28 for communicating the fluid.
  • the tubing 28 includes at least one input 30 for communicating fluid to the tubing 28 and at least one outlet 32 for communicating fluid from the tubing 28 .
  • the tubing 28 is proximal or directly in contact with the mold surface 24 to expedite heat transfer between the tubing 28 and the mold surface 24 .
  • the tubing 28 is useful for direct (rather than indirect) heating or cooling of the mold surface 24 .
  • the tubing 28 may be formed into the tool 26 itself (such as by boring within the tool 26 ), or attached within the tool 26 proximal the mold surface 24 , either to the tool 26 and/or to the mold surface 24 .
  • the tubing 28 can be attached (e.g. to the mold surface 24 ) in various fashions, such as by welding, fasteners, etc.
  • the tubing 28 can be arranged in various patterns and may be of equal or varying diameters. For example, if the mold surface 24 is complex in shape, a portion of the tubing 28 can be concentrated in more critical areas of the mold surface 24 to ensure proper heating and cooling of those areas. As alluded to above, the mold surface 24 may be of various configurations, and can be substantially planar, three-dimensional, or a combination of shapes. The tubing 28 can be configured likewise to provide for direct heating of the mold surface 24 .
  • the tool 26 may have one or more fasteners 34 , e.g. clamps 34 , for attaching a vacuum canopy 36 to the tool 26 . Various types of fasteners 34 may be employed.
  • the vacuum canopy 36 is described further below. In other embodiments, a conventional vacuum bag (not shown) can be utilized.
  • the tubing 28 of the tool 26 is connected to piping 38 of the system 20 for communicating the fluid to and from the tool 26 and to and from the system 20 for heating and cooling the mold surface 24 .
  • piping 38 Various types can be employed.
  • the piping 38 should be capable of handling the temperatures and pressures present in the system 20 .
  • the piping 38 can be of various diameters.
  • the piping 38 can have a diameter of from about 0.5 to about 4, about 0.75 to about 3, about 1 to about 2, or about 2, inches (or about 1.3 to about 10, about 1.9 to about 7.6, about 2.5 to about 5, or about 5, cm), outer diameter (OD).
  • the tubing 28 may have more than one input 30 and output 32 .
  • Suitable tools 26 are commercially available from a variety of suppliers. Specific examples of tools 26 include those commercially available from Weber Manufacturing Team, such as nickel shell tooling.
  • the fluid carried within the system 20 is typically a heat transfer fluid, which may also be referred to as a thermal fluid.
  • a thermal fluid e.g. thermal oil
  • Water may be used elsewhere in the system 20 , and combinations of thermal oil and water may be used in certain embodiments.
  • Suitable fluids are commercially available from a variety of suppliers. Specific examples of fluids include those commercially available from Mokon of Buffalo, N.Y., including DELF450 and DELF600. Further examples of fluids include those commercially available from Multitherm of Malvern, Pa., including PG-1 and IG-4; from Paratherm Corp.
  • the fluid should be capable of handling the temperatures of the system 20 , and may include a blend of two or more different fluids. Typically, the system 20 is closed-loop; however, at times, the system 20 may have some amount of fluid added thereto or withdrawn therefrom.
  • the system 20 comprises a heater-subsystem 40 .
  • the heater-subsystem 40 is in fluid communication with the tool 26 .
  • the heater-subsystem 40 is useful for heating the mold surface 24 of the tool 26 .
  • the heater-subsystem 40 can also be used for cooling the mold surface 24 of the tool 26 .
  • the heater-subsystem 40 comprises a heater 42 .
  • the heater 42 is useful for heating the fluid within the system 20 .
  • Various types of heaters 42 can be employed.
  • the heater 42 should be capable of heating the fluid to temperatures of at least about 3° F. ( ⁇ 16° C.) to about 350° F. ( ⁇ 177° C.), or upwards of about 600° F. ( ⁇ 315° C.) to about 650° F. ( ⁇ 343° C.). Generally, the hotter the fluid coming into the tool 26 , the quicker the mold surface 24 heats.
  • the heater 42 should also be capable of delivering various outputs of the fluid.
  • Suitable outputs are from about 10 to about 120, from about 20 to about 100, from about 40 to about 90, or about 60, gallons per minute (gpm) (or about 38 to about 454, about 76 to about 379, about 151 to about 341, or about 227, liters per minute).
  • Suitable heaters 42 are commercially available from a variety of suppliers. Specific examples of heaters 42 include those commercially available from Mokon, including the HTF Series, e.g. the HTF 500 Series, the HTF 600 Series, the HTF HF-2 Series, and the ST Series, heaters. Gas fired heaters, such as those commercially available from Fulton Boiler Works, Inc. of Pulaski, N.Y., can also be used, e.g. a Fulton FT-0320-C Thermal Fluid Heater. As used herein, a tilde character ( ⁇ ) is meant to represent an approximation based, for example, on unit conversion from US to SI units.
  • the heater-subsystem 40 further comprises a tank 44 .
  • the tank 44 of the heater-subsystem 40 is useful for containing a mass of heated fluid.
  • the tank 44 of the heater-subsystem 40 serves as a heat buffer in the system 20 , as described further below.
  • the tank 44 of the heater-subsystem 40 is in fluid communication with the heater 42 .
  • Various types of tanks can be employed as the tank 44 of the heater-subsystem 40 .
  • the tank 44 of the heater-subsystem 40 should be capable of holding fluid at temperatures of at least about 300° F. ( ⁇ 157° C.) to about 350° F. ( ⁇ 177° C.), and upwards of about 600° F. ( ⁇ 315° C.) to about 650° F. ( ⁇ 343° C.).
  • the tank 44 of the heater-subsystem 40 should be rated for more than the highest temperature output of the heater 42 .
  • the heater-subsystem 40 comprises two of more tanks (not shown).
  • the mass of fluid contained in one tank 44 may be at a different temperature than that of another tank 44 . This may be useful for buffering the system 20 with masses of heated fluid at different temperatures.
  • the tank 44 is typically separate from the heater 42 , i.e., the tank 44 is distinguishable from an “internal” tank of the heater 42 , if present.
  • the tank 44 of the heater-subsystem 40 is insulated, either itself, and/or with a supplemental layer of insulation, to prevent cooling of the mass of heated fluid contained therein by the ambient environment.
  • Various types of insulation means can be employed.
  • the tank 44 of the heater-subsystem 40 can be wrapped with an insulated jacket.
  • Piping 38 of the system 20 , or portions thereof, should also be wrapped or covered for purposes of insulation and safety.
  • the piping 38 running from the heater-subsystem 40 to the tool 26 can be insulated to prevent heat loss, burns, fires, etc.
  • the tank 44 of the heater-subsystem 40 can be of various sizes and shapes. It may be useful to reduce the surface area to volume ratio (SA:V) of the tank 44 of the heater-subsystem 40 to reduce heat loss; however, this is not required.
  • the tank 44 of the heater-subsystem 40 should be sized to hold of from about 50 to about 250, from about 100 to about 225, from about 100 to about 200, or from about 100 to about 150, gallons of the fluid (or about 189 to about 946, from about 378 to about 852, from about 378 to about 757, or from about 378 to about 568, liters of the fluid). Generally, a larger size tank 44 provides for a greater heat buffer in the system 20 .
  • Reference to the mass of heated fluid associated with the tank 44 of the heater-subsystem 40 may refer to a portion to an entirety of the heated fluid contained within the tank 44 at a given instance.
  • the masses of fluid described herein may also be referred to as stored (thermal) energy masses.
  • the heater-subsystem 40 further comprises a valve 46 in fluid communication between the tank 44 of the heater-subsystem 40 and the heater 42 .
  • valves 46 can be employed.
  • the valve 46 is a three-way valve 46 .
  • the three-way valve 46 of the heater-subsystem 40 is useful for re-circulating the fluid between the tank 44 of the heater-subsystem 40 and the heater 42 . This arrangement is useful for initially forming, maintaining, and/or recharging the mass of heated fluid in the tank 44 of the heater-subsystem 40 .
  • fluid returning from the tool 26 can be fed to the heater 42 and then to the tank 44 of the heater-subsystem 40 to maintain or recharge the mass of heated fluid.
  • the heated fluid may then be held or re-circulated in one or more passes between the heater 42 and the tank 44 of the heater-subsystem 40 to further increase or maintain temperature of the mass of heated fluid.
  • the heater 42 can't keep up with demands of the tool 26 and/or the system 20 , where the mass of heated fluid serves as a buffer for the heater 42 to catch-up or recover. This is also useful for maintaining a near steady-state temperature of the fluid within the heater-subsystem 40 to meet ongoing demands of the tool 26 and the system 20 .
  • the three-way valve 46 of the heater-subsystem 40 is also in fluid communication between the tank 44 of the heater-subsystem 40 and the tool 26 .
  • the three-way valve 46 of the heater-subsystem 40 is also useful for directing the fluid from the tank 44 of the heater-subsystem 40 to the tool 26 .
  • This is especially useful for rapidly heating the mold surface 24 of the tool 26 as further described below.
  • the mass of heated fluid (or a portion thereof) can be fed to the tool 26 to rapidly heat the mold surface 24 .
  • the mass of heated fluid provided by the tank 44 of the heater-subsystem 40 provides for a rapid change in temperature relative to what the heater 42 could achieve on its own by providing only heated fluid on demand.
  • the heater 42 may be burdened during ramping up of the mold surface 24 temperature and will take time to recover.
  • the mass of heated fluid provides for a drastic change in temperature in a very short period of time, i.e., a maximum ⁇ T in the mold surface 24 , without putting the entire heating burden on the heater 42 .
  • the three-way valve 46 of the heater-subsystem 40 is in fluid communication i) between the tank 44 and the heater 42 for re-circulating a first thermal fluid from the tank 44 to the heater 42 and ii) between the tank 44 and the tool 26 for directing the first thermal fluid from the tank 44 to the tool 26 .
  • the heater-subsystem 40 may include a tank bypass line 39 in this or other embodiments.
  • a related embodiment of the system 20 further comprises a chiller-subsystem 48 .
  • the system 20 comprises the heater- and chiller-subsystems 40 , 48 .
  • the chiller-subsystem 48 is in fluid communication with the tool 26 .
  • the chiller-subsystem 48 is useful for cooling the mold surface 24 of the tool 26 .
  • the heater-subsystem 40 may be used for cooling the mold surface 24 of the tool 26
  • the chiller-subsystem 48 can also be used for further cooling the mold surface 24 .
  • the heater-subsystem 40 is used only for heating the mold surface 24
  • the chiller-subsystem 48 is used only for cooling the mold surface 24 .
  • the chiller-subsystem 48 is used in another location of the system 20 .
  • the subsystems 40 , 48 are separate from each other; however, in other embodiments, the subsystems 40 , 48 are in fluid communication with each other, i.e., they share the fluid of the system 20 .
  • the chiller-subsystem 48 comprises a chiller 50 .
  • the chiller 50 is useful for cooling the fluid within the system 20 .
  • Various types of chillers 50 can be employed.
  • the chiller 50 should be capable of cooling the fluid to temperatures of at least about 50° F. ( ⁇ 10° C.) to about 80° F. ( ⁇ 27° C.), and downwards of about ⁇ 10° F. ( ⁇ 23° C.) to about 20° F. ( ⁇ 7° C.).
  • the chiller 50 should also be capable of delivering various outputs of fluid, such as from about 10 to about 150, from about 20 to about 125, from about 30 to about 100, from about 40 to about 75, ton chilling (where 1 ton chilling is about 12,000 BTUs per hour).
  • Suitable chillers 50 are commercially available from a variety of suppliers. Specific examples of chillers 50 include those commercially available from Mokon, including the Iceman Series, e.g. the Iceman SC Series, the Iceman LT Series, the Iceman Dual Circuit, and the Iceman Full Range.
  • the chiller-subsystem 48 further comprises a tank 52 .
  • the tank 52 of the chiller-subsystem 48 is useful for containing a mass of cooled fluid.
  • the tank 52 of the chiller-subsystem 48 is in fluid communication with the chiller 50 .
  • Various types of tanks can be employed as the tank 52 of the chiller-subsystem 48 .
  • the tank 52 of the chiller-subsystem 48 should be able to hold fluid at temperatures of about ⁇ 30° F. ( ⁇ 34° C.) to about ⁇ 10° F. ( ⁇ 23° C.), or upwards of about 20° F. ( ⁇ 7° C.) to about 50° F. ( ⁇ 10° C.).
  • the tank 52 of the chiller-subsystem 48 should be rated for less than the lowest temperature output of the chiller 50 .
  • the chiller-subsystem 48 comprises two of more tanks (not shown).
  • the mass of fluid contained in one tank 52 may be at a different temperature than that of another tank 52 . This may be useful for buffering the system 20 with masses of cooled fluid at different temperatures.
  • the tank 52 of the chiller-subsystem 48 should be insulated, either itself, and/or with a supplemental layer of insulation, to prevent heating of the mass of cooled fluid contained therein by the ambient environment.
  • Various types of insulation means can be employed as like described above with the tank 44 of the heater-subsystem 40 .
  • the tank 52 of the chiller-subsystem 48 can be of various sizes and shapes. It may be useful to reduce the SA:V of the tank 52 of the chiller-subsystem 48 to reduce heat gain; however, this is not required.
  • the tank 52 of the chiller-subsystem 48 should be of a size to hold of from about 50 to about 200, from about 75 to about 150, or from about 100 to about 125, gallons of the fluid (or about 189 to about 946, from about 378 to about 852, from about 378 to about 757, or from about 378 to about 568, liters of the fluid). Generally, a larger size tank 52 provides for a greater cooling buffer in the system 20 .
  • Reference to the mass of cooled fluid associated with the tank 52 of the chiller-subsystem 48 may refer to a portion to an entirety of the cooled fluid contained in the tank 52 at a given instance.
  • the tank 52 is typically separate from the chiller 50 , i.e., the tank 52 is distinguishable from an “internal” tank of the chiller 50 , if present.
  • the chiller-subsystem 48 further comprises a valve 54 in fluid communication between the tank 52 of the chiller-subsystem 48 and the chiller 50 .
  • valves 54 can be employed.
  • the valve 54 is a three-way valve 54 .
  • the three-way valve 54 of the chiller-subsystem 48 is useful for re-circulating the fluid between the tank 52 of the chiller-subsystem 48 and the chiller 50 . This arrangement is useful for initially forming, maintaining, and/or recharging the mass of cooled fluid in the tank 52 of the chiller-subsystem 48 .
  • fluid returning from the tool 26 can be fed to the chiller 50 and then to the tank 52 of the chiller-subsystem 48 to maintain or recharge the mass of cooled fluid.
  • the cooled fluid may then be held or re-circulated in one or more passes between the chiller 50 and the tank 52 of the chiller-subsystem 48 to further decrease or maintain temperature of the mass of cooled fluid.
  • the chiller 50 can't keep up with demands of the tool 26 and/or the system 20 , where the mass of cooled fluid serves as a buffer for the chiller 50 to catch-up or recover. This is also useful for maintaining a near steady-state temperature of the fluid within the chiller-subsystem 48 to meet ongoing demands of the tool 26 and the system 20 .
  • the three-way valve 54 of the chiller-subsystem 48 is also in fluid communication between the tank 52 of the chiller-subsystem 48 and the tool 26 .
  • the three-way valve 54 of the chiller-subsystem 48 is also useful for directing the fluid from the tank 52 of the chiller-subsystem 48 to the tool 26 .
  • This is especially useful for rapidly cooling the mold surface 24 of the tool 26 as further described below.
  • the mass of cooled fluid (or a portion thereof) can be fed to the tool 26 to rapidly cool the mold surface 24 .
  • the mass of cooled fluid provided by the tank 52 of the chiller-subsystem 48 provides for a rapid change in temperature relative to what the chiller 50 could achieve on its own by providing only cooled fluid on demand.
  • the chiller 50 may be burdened during ramping down of the mold surface 24 temperature and will take time to recover.
  • the mass of cooled fluid provides for a drastic change in temperature in a very short period of time, i.e., a maximum ⁇ T in the mold surface 24 , without putting the entire cooling burden on the chiller 50 .
  • the three-way valve 54 of the chiller-subsystem 48 is in fluid communication i) between the tank 52 and the chiller 50 for re-circulating a second thermal fluid from the tank 52 to the chiller 50 and ii) between the tank 52 and an exchanger-subsystem 49 for directing the second thermal fluid from the tank to an exchanger 51 .
  • the chiller-subsystem 48 may include the tank bypass line 39 in this or other embodiments.
  • the second thermal fluid is water.
  • the system 20 further comprises the exchanger-subsystem 49 .
  • the exchanger-subsystem 49 comprises the (heat) exchanger 51 .
  • the exchanger 51 can be of various types, such as a shell-and-tube, a shell-and-plate, etc.
  • the exchanger-subsystem 49 further comprises a valve 53 .
  • the valve 53 is a three-way valve 53 .
  • the system 20 typically includes at least one pump 55 .
  • the pump 55 is useful for circulating the fluid within the system 20 when the heater-subsystem 40 and chiller-subsystem 48 are closed off from the tool 26 , such as when recharging. Otherwise, the heater 42 can generally provide suitable pumping for the system 20 .
  • the exchanger 51 and three-way valve 53 of the exchanger-subsystem are useful for indirectly introducing cooled fluid to the tool 26 .
  • cooled fluid does not go directly to the tool 26 , but to the exchanger 51 wherein the cooled fluid is used to reduce the temperature of the heated fluid that is in direct contact with the tool 26 .
  • this can provide for a smaller closed loop to be established thereby allowing the closed loop to be “set” to a fixed temperature via temperature feedback of the fluid in the loop and control of the valves 46 , 53 , 54 .
  • the valves 46 , 53 , 54 can be set such that the fluid flows through a check valve 57 via the pump 55 and around the smaller closed loop. Additional aspects of this embodiment are described further below.
  • the three-way valve 53 is in fluid communication i) between the exchanger 51 and the heater-subsystem 40 for sending the first thermal fluid from the tool 26 back to the heater-subsystem 40 and ii) between the exchanger 51 and the tool 26 for directing the first thermal fluid from the tool 26 to the exchanger 51 .
  • the first thermal fluid is shared between the heater-subsystem 40 and the exchanger-subsystem 49
  • the second thermal fluid is shared between the chiller-subsystem 48 and the exchanger-subsystem 49
  • the first thermal fluid is kept separate from the second thermal fluid.
  • the first thermal fluid is thermal oil and the second thermal fluid is water, i.e., they are different from one another.
  • the system 20 is typically in communication with a controller 56 .
  • the controller 56 is typically in communication with at least one of the subsystems 40 , 48 , 49 and the tool 26 , more typically in communication with all of the subsystems 40 , 48 , 49 and the tool 26 .
  • Various types of controllers 56 can be employed.
  • the controller 56 is a programmable logic controller (PLC) 56 , which may also be referred to as a programmable controller 56 .
  • PLC programmable logic controller
  • the controller 56 can communicate to components of the system 20 by various methods, such as by wire, by wireless, etc.
  • the system 20 further comprises a valve 58 , which is in addition to the valves 46 , 53 , 54 of the subsystems 40 , 48 , 49 .
  • valves 58 can be employed.
  • the valve 58 is a three-way valve 58 .
  • the three-way valve 58 of the system 20 is in fluid communication between the tool 26 and both of the subsystems 40 , 48 .
  • the three-way valve 58 is also in communication with the controller 56 .
  • the three-way valve 58 of the system 20 is useful for directing the fluid to the heater-subsystem 40 or to the chiller-subsystem 48 after returning from the tool 26 .
  • the controller 56 can direct fluid from the tool 26 to each of the subsystems 40 , 48 by controlling the three-way valve 58 of the system 20 , along with the three-way valves 46 , 54 of each of the subsystems 40 , 48 .
  • the three-way valve 58 may optionally be utilized, i.e., as a supplemental valve 58 , such as in place of the check valve 57 .
  • valves 46 , 53 , 54 , 58 may generally be referred to herein, the same flow control may be achieved by a combination of different types of valves and piping 38 arrangements which “mimic” a three-way valve.
  • a combination of two-way valves and piping 38 may be utilized to achieve the same flow control as achieved by a three-way valve.
  • a plugged four-way valve may be utilized in place of a three-way valve.
  • Such alternate arrangements for achieving the same (or similar) flow control are contemplated as being equivalent in function as the three-way valves 46 , 53 , 54 , 58 described herein.
  • the controller 56 is also useful for controlling flow of fluid in the system 20 .
  • the controller 56 can control a combination of the valves 58 of the system 20 , the valves 46 , 53 , 54 of the subsystems 40 , 48 , 49 the heater 42 , the chiller 50 , and/or the heat exchanger 49 , to direct fluid at various temperatures to and from the tool 26 .
  • the controller 56 is especially useful for directing the masses of the heated and cooled fluid from each of the subsystems 40 , 48 . Specifically, the controller 56 is useful for directing the mass of heated fluid from the tank 44 of the heater-subsystem 40 to rapidly heat the mold surface 24 of the tool 26 . The controller 56 is also useful for directing the mass of cooled fluid from the tank 52 of the chiller-subsystem 48 to rapidly cool the mold surface 24 of the tool 26 either directly to the tool 26 , such as in FIG. 2 , or indirectly via the exchanger-subsystem 51 , such as in FIG. 18 .
  • the controller 56 controls the three-way valves 46 , 53 , 54 , 58 to direct fluid from at least one of the tanks 44 , 52 to the tool 26 to heat or cool the mold surface 24 of the tool 26 .
  • the controller 56 controls the three-way valves 46 , 53 , 54 , 58 to re-circulate fluid in the other subsystem 40 , 48 to maintain the mass of heated or cooled fluid in the tank 44 , 52 of the other subsystem 40 , 48 .
  • Re-circulating the fluid in the subsystem 40 , 48 can start before, after, or during heating or cooling of the mold surface 24 with the other subsystem 40 , 48 .
  • the controller 56 can also be used to control fluid in the exchanger-subsystem 49 .
  • the controller 56 can direct the fluid in the system 20 by opening and closing the three-way valves 46 , 53 , 54 , 58 in particular orders and/or at particular times.
  • the three-way valves 46 , 53 , 54 , 58 may be opened and/or closed simultaneously and/or concurrently. While not shown, the controller 56 may also be in communication with other valves in the system 20 to control flow of the fluid.
  • the controller 56 can be programmed to manipulate the subsystems 40 , 48 , 49 in various manners.
  • the controller 56 is generally programmed to instruct the three-way valve 46 of the heater-subsystem 40 at certain times such that the first thermal fluid re-circulates between the heater 42 and the tank 44 and bypasses the tool 26 to maintain the mass of heated first thermal fluid in the heater-subsystem 40 .
  • the controller 56 is generally programmed to instruct the three-way valve 46 of the heater-subsystem 40 such that the first thermal fluid is directed from the heater-subsystem 40 and to the tool 26 to heat the mold surface 24 of the tool 26 .
  • the controller 56 is generally programmed to instruct the three-way valve 54 of the chiller-subsystem 48 at certain times such that the second thermal fluid re-circulates between the chiller 50 and the tank 52 and bypasses the exchanger-subsystem 49 to maintain the mass of cooled second thermal fluid in the chiller-subsystem 48 .
  • the controller 56 is generally programmed to instruct the three-way valve 54 of the chiller-subsystem 48 such that the second thermal fluid is directed from the chiller-subsystem 48 to the exchanger-subsystem 49 to cool the first thermal fluid returning from the tool 26 and entering the exchanger-subsystem 51 .
  • the controller 56 is generally programmed to instruct the three-way valve 53 of the exchanger-subsystem 49 at certain times such that the first thermal fluid returning from the tool 26 is directed to the heater-subsystem 40 and bypasses the exchanger-subsystem 51 to reheat the first thermal fluid within the heater-subsystem 40 .
  • the controller 56 is generally programmed to instruct the three-way valve 53 of the exchanger-subsystem 49 such that the first thermal fluid returning from the tool 26 is directed to the exchanger-subsystem to cool the first thermal fluid via the second thermal fluid from the chiller-subsystem 48 .
  • the fluid may be directed into the tool 26 in a countercurrent fashion relative to a coolest or warmest area of the mold surface 24 .
  • the controller 56 can direct heated fluid to this location to expedite temperature change of the location based on a large initial temperature gradient.
  • concurrent flow arrangements can be useful, such as for maintaining a temperature gradient across the mold surface 24 , or there may be instances where a combination of countercurrent and concurrent flow arrangements can be used.
  • flow within the tubing 28 of the tool 26 is turbulent to promote greater thermal transfer between the mold surface 24 and the fluid within the tubing 28 . Turbulence may be imparted by various means, such as by use of helically corrugated piping 38 and/or tubing 28 .
  • the system 20 may include one or more additional types of valves for regulating flow of the fluid within the system 20 .
  • one or more ball valves may be present for stopping/starting flow of the fluid in a portion of the system 20 .
  • one or more gate valves and/or check valves may be present for preventing backflow of the fluid in a portion of the system 20 .
  • one or more globe valves may be present for regulating flow rate of the fluid in a portion of the system 20 . If employed, the additional valves may be disposed in various locations of the system 20 .
  • valves of the system 20 may be manipulated in various ways, such as pneumatically, manually, electrically, magnetically, etc. In certain embodiments, electrical control is employed, pneumatic control is employed, or combinations thereof.
  • the system 20 can further comprise a relief valve 60 .
  • the relief valve 60 may also be referred to as a pressure relief valve 60 , a pressure safety valve 60 , or a safety valve 60 .
  • Various types of relief valves 60 can be employed.
  • the relief valve 60 is typically in fluid communication between the subsystems 40 , 48 , 49 and the tool 26 .
  • the relief valve 60 is useful for relieving pressure of the fluid in the system 20 . For example, an upset in the system 20 may increase pressure of the fluid to an unsafe or undesirable level. As such, the relief valve 60 can compensate for such an occurrence by releasing a portion of the fluid in the system 20 to return the pressure of the fluid to a safe or desired level.
  • the controller 56 may be in communication with the relief valve 60 to shut down the system 20 in the event that the relief valve 60 activates to prevent damage to the system 20 , press 64 , etc.
  • the system 20 may further comprise a strainer (not shown).
  • a strainer (not shown).
  • Various types of strainers can be employed.
  • the strainer useful for straining the fluid to prevent clogging or other issues in the system 20 over time.
  • the strainer can also be useful for imparting and/or maintaining turbulent flow of the fluid.
  • the system 20 may further comprise one or more pumps 55 .
  • pumps 55 Various types of pumps can be employed, such as those generally used for moving heat transfer fluids.
  • the heater 42 and chiller 50 generally provide sufficient pumping of the fluid.
  • the mold surface 24 of the tool 26 can be heated at various rates.
  • the rate of heating may be linear or curvilinear.
  • the rate of heating can increase at a decreasing rate, increase at an increasing rate, be substantially constant, or combinations thereof.
  • the mold surface 24 heats at a rate of greater than about 60, greater than about 70, greater than about 80, greater than about 90, or greater than about 100, ° F. per minute (or greater than ⁇ 33, greater than ⁇ 39, greater than ⁇ 44, greater than ⁇ 50, or greater than ⁇ 56, ° C. per minute).
  • the mold surface 24 can be heated at a rate upwards of about 300, about 250, about 225, or about 200, ° F. per minute ( ⁇ 167, ⁇ 39, ⁇ 125, or ⁇ 111, ° C. per minute).
  • the mold surface 24 of the tool 26 can be cooled at various rates.
  • the rate of cooling may be linear or curvilinear.
  • the rate of cooling can increase at a decreasing rate, increase at an increasing rate, be substantially constant, or combinations thereof.
  • the mold surface 24 cools at a rate of greater than about 40, greater than about 50, greater than about 60, greater than about 70, greater than about 80, greater than about 90, or greater than about 100, ° F. per minute (or greater than ⁇ 22, greater than ⁇ 28, greater than ⁇ 33, greater than ⁇ 39, greater than ⁇ 44, greater than ⁇ 50, or greater than ⁇ 56, ° C. per minute).
  • the mold surface 24 can be cooled at a rate upwards of about 200, about 175, or about 150, ° F. per minute ( ⁇ 111, ⁇ 97, or ⁇ 83, ° C. per minute).
  • the present invention further provides a method.
  • the method is useful for heating and cooling the mold surface 24 of the tool 26 .
  • the method comprises the step of providing the heater-subsystem 40 .
  • the method further comprises the step of providing the chiller-subsystem 48 .
  • the method further comprises the step of providing the exchanger-subsystem 49 .
  • the method further comprises the step of providing the controller 56 .
  • the method further comprises the step of providing the tool 26 .
  • the tool 26 can be provided manually or automatically.
  • the tool 26 may be provided by a technician or by a robot (not shown).
  • the tool 26 and subsystems 40 , 48 , 49 can be as described above.
  • the method further comprises the step of directing the mass of heated fluid from the tank 44 of the heater-subsystem 40 to the tool 26 .
  • the mass of heated fluid can be directed by the controller 56 communicating with the subsystems 40 , 48 , 49 and the three-way valve 58 of the system 20 as described above.
  • T 1 can be various temperatures.
  • T 1 can be the temperature of the mold surface 24 at startup, i.e., the mold surface 24 can be at ambient (or room) temperature.
  • T 1 can be the temperature of the mold surface 24 after a previous cycle of heating and cooling.
  • the mold surface 24 may be hotter (or cooler) than ambient temperature.
  • T 1 is from about 50 to about 125, from about 75 to about 125, from about 90 to about 125, or from about 100 to about 120, ° F. ( ⁇ 10 to ⁇ 52, ⁇ 24 to ⁇ 52, ⁇ 32 to ⁇ 52, or ⁇ 38 to ⁇ 49, ° C.).
  • Tt 1 can be various time periods. Typically, Tt 1 is short relative to subsequent time periods of heating and cooling. However, Tt 1 may also be longer than or equal to one or more subsequent time periods of heating and cooling. Typically, Tt 1 is from about 1 to about 25, from about 1 to about 20, from about 1 to about 15, from about 1 to about 10, from about 2.5 to about 10, from about 2.5 to about 7.5, or from about 4 to about 6, minutes.
  • T 2 can be various temperatures.
  • T 2 can be the maximum temperature of the mold surface 24 reached during heating.
  • T 2 is from about 250 to about 400, from about 250 to about 375, from about 275 to about 375, from about 300 to about 375, or from about 325 to about 350, ° F. ( ⁇ 121 to ⁇ 204, ⁇ 121 to ⁇ 191, ⁇ 135 to ⁇ 191, ⁇ 149 to ⁇ 191, or ⁇ 163 to ⁇ 177, ° C.).
  • the mass of heated fluid in the tank 44 of heater-subsystem 40 is at a temperature of about T 2 or higher. It is useful when the mass of the heated fluid is at least about 50° F. (10° C.) higher than T 2 to facilitate heat transfer between the mass and the mold surface 24 of the tool 26 , and more typically much higher than T 2 .
  • the mass of heated fluid in the tank 44 of the heater-subsystem 40 is at a temperature of from about 250 to about 600, from about 300 to about 550, from about 350 to about 500, or from about 400 to about 450, ° F. ( ⁇ 121 to ⁇ 316, ⁇ 149 to ⁇ 288, ⁇ 177 to ⁇ 260, or ⁇ 204 to ⁇ 232, ° C.). Due to the mass of heated fluid, the system 20 can rapidly heat the mold surface 24 of the tool 26 as described above.
  • the method further comprises the step of directing fluid from the heater-subsystem 40 to the mold surface 24 of the tool 26 .
  • the fluid can be directed by the controller 56 communicating with the subsystems 40 , 48 and the three-way valve 58 of the system 20 .
  • the fluid maintains the mold surface 24 at about T 2 for a second period of time (Tt 2 ).
  • the mold surface 24 can be maintained at T 2 or at an acceptable tolerance level, e.g. Tt 2 ⁇ 15° F. ( ⁇ 9° C.). Maintaining the mold surface 24 at about T 2 for Tt 2 is useful for curing resin of the composite article 22 . It is also believed to be useful for increasing surface properties of the composite article 22 .
  • Thermostat modulation can be used for staying within the tolerance level.
  • Tt 2 can be various time periods. Typically, Tt 2 is shorter than Tt 1 . However, Tt 2 may also be longer than or equal to Tt 1 or a subsequent time period. Typically, Tt 2 is from about 1 to about 25, from about 1 to about 20, from about 1 to about 15, from about 1 to about 10, from about 1 to about 7.5, from about 1 to about 5, or from about 1 to about 2.5, minutes.
  • the method further comprises the step of maintaining the mold surface 24 of the tool 26 at an intermediate temperature (T 1-2 ) of between T 1 and T 2 . Typically, this step occurs prior to heating the mold surface 24 of the tool 26 to T 2 .
  • T 1-2 can be maintained by only feeding a portion of the mass of heated fluid to the mold surface 24 and/or by controlling overall temperature of the heater-subsystem 40 .
  • the fluid maintains the mold surface 24 at about T 1-2 for a portion of Tt 1 (Tt ⁇ 1 ).
  • the fluid can be directed by the controller 56 communicating with the subsystems 40 , 48 and the three-way valve 58 of the system 20 .
  • the mold surface 24 can be maintained at T 1-2 or at an acceptable tolerance level, e.g. T 1-2 ⁇ 15° F. ( ⁇ 9° C.). It is believed that maintaining the mold surface 24 at about T 1-2 for Tt 2 is useful for consolidating the composite article 22 . For example, resin of the composite article 22 reaches its minimum viscosity and/or thins to more readily flow into the carbon fiber mat of the composite article 22 . Such consolidation is believed to be useful for achieving mechanical properties and improving the Class A surface of body panels of the composite article 22 , if formed. Thermostat modulation can be used for staying within the tolerance level.
  • T 1-2 can be various temperatures.
  • T 1-2 can be in the middle of T 1 and T 2 , closer to T 1 , or closer to T 2 .
  • T 1-2 is from about 100 to about 350, from about 150 to about 325, from about 200 to about 300, from about 225 to about 275, or from about 235 to about 265, ° F. ( ⁇ 38 to ⁇ 177 , ⁇ 66 to ⁇ 163, ⁇ 93 to ⁇ 149, ⁇ 107 to ⁇ 135, or ⁇ 113 to ⁇ 129, ° C.).
  • Tt ⁇ 1 can be various time periods, provided it is less than Tt 1 .
  • Tt 1-2 is longer than Tt 2 .
  • Tt 1-2 may also be shorter than or equal to Tt 2 or a subsequent time period.
  • Tt ⁇ 1 is from about 1 to less than about 25, from about 1 to about 20, from about 1 to about 15, from about 1 to about 10, from about 1 to about 7.5, from about 1 to about 5, or from about 1 to about 2.5, minutes. In certain embodiments, Tt ⁇ 1 is from 1 to less than 10 minutes.
  • the method further comprises the step of directing the mass of cooled fluid from the tank 52 of the chiller-subsystem 48 to the tool 26 to cool the mold surface 24 of the tool 26 from about T 2 to a third temperature (T 3 ) within a third period of time (Tt 3 ).
  • the heater-subsystem 40 is used to cool the mold surface 24 in a similar manner. Typically, either one of these steps occurs after maintaining the mold surface 24 of the tool 26 at T 2 for Tt 2 .
  • the mass of cooled fluid can be directed by the controller 56 communicating with the subsystems 40 , 48 and the three-way valve 58 of the system 20 . In other embodiments, such as the one of FIG.
  • the method further comprises the step of directing the mass of cooled second thermal fluid from the tank 52 of the chiller-subsystem 48 to the exchanger-subsystem 49 via the controller 56 to cool the mold surface 24 of the tool 26 from T 2 to T 3 within Tt 3 .
  • T 3 can be various temperatures.
  • T 3 can be the temperature of the mold surface 24 at startup, i.e., the mold surface 24 can be at ambient (or room) temperature.
  • T 3 is generally higher than ambient temperature.
  • T 3 is from about 75 to about 150, from about 85 to about 140, from about 90 to about 130, or from about 100 to about 120, ° F. ( ⁇ 24 to ⁇ 66, ⁇ 29 to ⁇ 60, ⁇ 32 to ⁇ 54, or ⁇ 38 to ⁇ 49, ° C.).
  • Tt 3 can be various time periods. Typically, Tt 3 is long relative to previous time periods of heating. However, Tt 3 may also be longer than or equal to one or more previous time periods of heating. Typically, Tt 3 is from about 1 to about 25, from about 1 to about 20, from about 1 to about 15, from about 1 to about 10, from about 2.5 to about 10, from about 2.5 to about 7.5, or from about 4 to about 6, minutes.
  • the mass of cooled fluid in the tank 52 of chiller-subsystem 48 is at a temperature of about T 3 or lower. It is useful when the mass of the cooled fluid is at least about 50° F. lower than T 3 to facilitate heat transfer between the mold surface 24 of the tool 26 and the mass. In certain embodiments, the mass of the cooled fluid in the tank 52 of the chiller-subsystem 48 is at a temperature of from about 35 to about 70, about 40 to about 60, about 45 to about 55, or about 50, ° F. ( ⁇ 1.7 to ⁇ 21, ⁇ 4.4 to ⁇ 16, ⁇ 7 to ⁇ 13, or ⁇ 10, ° C.). As such, the system 20 can rapidly cool the mold surface 24 of the tool 26 with the mass of cooled fluid.
  • the method is useful for heating the mold surface 24 of the tool 26 .
  • the mold surface 24 of the tool 26 heats at a rate of greater than about 60, about 70, about 80, about 90, about 100, about 110, about 120, about 130, about 140, about 150, about 160, about 170, or about 180, ° F. per minute (greater than ⁇ 33, greater than ⁇ 39, greater than ⁇ 44, greater than ⁇ 50, greater than ⁇ 56, greater than ⁇ 61, greater than ⁇ 67, greater than ⁇ 72, greater than ⁇ 78, greater than ⁇ 83, greater than ⁇ 89, greater than ⁇ 94, or greater than ⁇ 100, ° C. per minute).
  • the method is useful for cooling the mold surface 24 of the tool 26 .
  • the mold surface 24 of the tool 26 cools at a rate of greater than about 40, about 50, about 60, about 70, about 80, about 90, about 100, about 110, about 120, about 130, about 140, about 150, about 160, about 170, or about 180, ° F. per minute (greater than ⁇ 33, greater than ⁇ 39, greater than ⁇ 44, greater than ⁇ 50, greater than ⁇ 56, greater than ⁇ 61, greater than ⁇ 67, greater than ⁇ 72, greater than ⁇ 78, greater than ⁇ 83, greater than ⁇ 89, greater than ⁇ 94, or greater than ⁇ 100, ° C. per minute).
  • the controller 56 can be programmed with various control schemes to heat and cool the mold surface 24 using the subsystems 40 , 48 , 49 and three-way valve 58 of the system 20 , if utilized.
  • the controller 56 can be programmed to open or close one or more of the three-way valves 46 , 53 , 54 , 58 at certain times and/or at certain temperatures of the mold surface 24 .
  • Such control methodology is useful for directing the fluid to the tool 26 and/for re-circulating the fluid as described above.
  • control schemes of the controller 56 may be modeled off of control schemes generally used with autoclaves.
  • the controller 56 is programmed such that Tt 1 ⁇ Tt 2 or Tt 1 ⁇ Tt 2 . In further embodiments, the controller 56 is programmed such that Tt 1 ⁇ Tt 3 or Tt 1 ⁇ Tt 3 .
  • Tt 1 +Tt 2 +Tt 3 is no greater than about 30, about 25, about 20, about 19, about 18, about 17.5, about 17, about 15, about 14, about 13.5, about 13, about 12.5, about 12, about 11, about 10, about 7.5, about 5, about 2.5, or about 2, minutes.
  • Tt 1 +Tt 2 +Tt 3 is no greater than about 20 minutes, no greater than about 19 minutes, no greater than about 18 minutes, or no greater than about 17 minutes, and can be downwards of about 15, about 10, or about 5, minutes. Due to the direct heating and cooling of the mold surface 24 of the tool 26 via the system 20 , cycle time of making the composite articles 22 is greatly reduced relative to conventional methods, such as autoclaving.
  • the controller 56 typically measures temperature of the mold surface 24 by feedback from one or more resistive thermal device (RTD) (not shown) disposed proximal the mold surface 24 .
  • RTD resistive thermal device
  • the controller 56 can also measure temperature of the fluid by one or more RTDs disposed in or proximal the piping 38 at one or more locations and/or by one or more RTDs disposed in or proximal the subsystems 40 , 48 , 49 .
  • RTD resistive thermal device
  • the present invention further provides a method of forming the composite article 22 .
  • the method comprises the step of providing the tool 26 .
  • the tool 26 can be as described above.
  • the method further comprises the step of providing a preform 62 .
  • the preform 62 can be provided manually or automatically.
  • the preform 62 comprises a carbon fiber mat and a resin.
  • Various types of carbon fiber mat can be employed, such as a continuous fiber mat.
  • the carbon fiber mat may also be referred to as a fabric or a braid.
  • the carbon fiber mat can include one or more layers of fibers, typically at least two layers of fibers.
  • the carbon fibers can be of various types, such as standard modulus, intermediate modulus, high modulus, or high strength, carbon fibers. In certain embodiments, the carbon fibers are unidirectional.
  • the carbon fiber mat can be substantially dry and/or a pre-preg.
  • the carbon fiber mat is a carbon fiber pre-preg, which may also be referred to as a prepreg.
  • Suitable carbon fiber mats are commercially available from a variety of suppliers. Specific examples of carbon fiber mats include those commercially available from Toray Carbon Fibers America, Inc. of Flower Mound, Tex., including the TORAYCA® Series, e.g. TORAYCA® T700S; and from Toray Composites (America), Inc., of Tacoma, Wash. Further specific examples of carbon fiber mats include those commercially available from Advanced Composites Group of Tulsa, Okla.; and from Grafil, Inc. of Sacramento, Calif., including the GRAFIL Series and the PYROFILTM Series, e.g. PYROFILTM TR30S.
  • thermosetting resins include epoxy resins.
  • the resin comprises an epoxy resin.
  • the resin can include (or be mixed) with one or more hardeners to promote cure of the resin.
  • hardeners can be employed.
  • the resin should be capable of curing in the time periods described above to utilize the rapid heating and cooling provided by the system 20 . Suitable resins are commercially available from a variety of suppliers.
  • resins include those commercially available from Huntsman International LLC of Salt Lake City, Utah; from Toray Carbon Fibers America, Inc.; from Toray Composites (America), Inc., including G83 pre-preg resin; and from Advanced Composites Group, including MTM57 pre-preg resin.
  • the composite article 22 may be formed from a pre-preg, which is a carbon fiber mat previously infused with a resin, being either wet or dry, typically slightly wet. It is to be appreciated that if the pre-preg is employed, additional resin being the same or different from that of the pre-preg may be employed to form the composite article 22 . Alternatively, just the resin provided with the pre-preg can be employed as the resin. Various types of pre-pregs can be employed. Specific examples of pre-pregs or pre-preg systems include those commercially available from Toray Composites (America), Inc., such as PC7831-190-1000; and from Advanced Composites Group, such as MTM57/CF3238.
  • the method further comprises the step of disposing the preform 62 on the mold surface 24 of the tool 26 .
  • the preform 62 may be disposed manually or automatically.
  • the method further comprises the step of heating the mold surface 24 of the tool 26 from T 1 to T 2 within Tt 1 .
  • T 1 , T 2 , and Tt 1 can be as described above. Heating the mold surface 24 is useful for thinning the resin of the preform 62 . As such, the resin is better able to flow around, into, and within the carbon fiber mat.
  • the mold surface 24 , and therefore, the preform 62 can be heated with the system 20 as described above.
  • the method further comprises the step of applying pressure to the preform 62 .
  • Pressure may be applied by various means. Typically, pressure is applied by a press 64 , as described further below. The pressure is applied from a first pressure (P 1 ) to a second pressure (P 2 ).
  • Pressure can be applied at various rates.
  • the rate of pressurizing may be linear or curvilinear.
  • the rate of pressurizing can increase at a decreasing rate, increase at an increasing rate, be substantially constant, or combinations thereof.
  • pressure is applied at a rate of greater than about 0.1, greater than about 0.2, greater than about 0.3, greater than about 0.4, greater than about 0.5, greater than about 0.6, greater than about 0.7, greater than about 0.8, greater than about 0.9, greater than about 1, greater than about 1.1, greater than about 1.2, greater than about 1.3, greater than about 1.4, greater than about 1.5, or greater than about 2, pounds per square inch (psi) per second (sec) (where 1 psi/sec is ⁇ 2.07 kPa/sec).
  • P 1 can be various pressures.
  • P 1 can be standard atmospheric pressure ( ⁇ 14.7 psi).
  • P 1 is from about 0 to about 5, from about 0 to about 1, from about 0 to about 0.5, from about 0 to about 0.25, or from about 0 to about 0.1, psi gauge (psig) (where 1 psig is ⁇ 2.07 kPa gauge).
  • P 2 can be various pressures.
  • P 2 can be the maximum pressure reached during pressurizing.
  • P 2 is from about 50 to about 150, from about 60 to about 140, from about 70 to about 130, from about 80 to about 120, from about 90 to about 110, or about 100, psig.
  • the pressure is applied within a first period of time (Pt 1 ). Applying the pressure is useful for consolidating the preform 62 , especially after the resin has thinned via application of heat.
  • Pt 1 can be various time periods. Typically, Pt 1 is short relative to subsequent time periods of pressurizing or depressurizing. However, Pt 1 may also be longer than or equal to one or more subsequent time periods of pressurizing or depressurizing. Typically, Pt 1 is from about 1 to about 25, from about 1 to about 20, from about 1 to about 15, from about 1 to about 10, from about 2.5 to about 10, from about 2.5 to about 7.5, or from about 4 to about 6, minutes.
  • the method further comprises the step of maintaining pressure at about P 2 for a second period of time (Pt 2 ).
  • the pressure can be maintained at P 2 or at an acceptable tolerance level, e.g. P 2 ⁇ 10 psi (wherein 1 psi is ⁇ 2.07 kPa). Maintaining the pressure at about P 2 for Pt 2 is useful for further consolidation and curing the resin of the composite article 22 . Modulation can be used for staying within the tolerance level.
  • Pt 2 can be various time periods. Typically, Pt 2 is shorter than Pt 1 . However, Pt 2 may also be longer than or equal to Pt 1 or a subsequent time period. Typically, Pt 2 is from about 1 to about 25, from about 1 to about 20, from about 1 to about 15, from about 1 to about 10, from about 1 to about 7.5, from about 1 to about 5, or from about 1 to about 2.5, minutes.
  • the method further comprises the step of maintaining pressure at an intermediate pressure (P 1-2 ) of between P 1 and P 2 for a portion of Pt 1 (Pt ⁇ 1 ) prior to P 2 .
  • This step occurs prior to pressurizing to P 2 .
  • the pressure can be maintained at P 1-2 or at an acceptable tolerance level, e.g. P 1-2 ⁇ 10 psi. It is believed that maintaining the pressure at about P 1-2 for Pt ⁇ 1 is useful for consolidating the composite article 22 .
  • the resin can be at its minimum viscosity or thinned to more readily flow within the carbon fiber mat of the preform 62 . Modulation can be used for staying within the tolerance level.
  • P 1-2 can be various pressures.
  • P 1-2 can be in the middle of P 1 and P 2 , closer to P 1 , or closer to P 2 .
  • P 1-2 is from about 25 to about 125, from about 35 to about 115, from about 45 to about 105, from about 50 to 100, from about 55 to about 95, from about 65 to about 85, or about 75, psig.
  • Pt ⁇ 1 can be various time periods, provided it is less than Pt 1 .
  • Pt 1-2 is longer than Pt 2 .
  • Pt 1-2 may also be shorter than or equal to Pt 2 or a subsequent time period.
  • Pt ⁇ 1 is from about 1 to less than about 25, from about 1 to about 20, from about 1 to about 15, from about 1 to about 10, from about 1 to about 7.5, from about 1 to about 5, or from about 1 to about 2.5, minutes.
  • the method further comprises the step of reducing pressure on the composite article 22 .
  • the method further comprises the step of cooling the mold surface 24 of the tool 26 to drop the mold surface 24 from about T 2 to T 3 within Tt 3 .
  • the mold surface 24 of the tool 26 can be cooled with the system 20 as described above.
  • the method further comprises the step of removing the composite article 22 from the mold surface 24 of the tool 26 .
  • the composite article 22 may be removed manually or automatically.
  • the system 20 can be used to heat and cool the mold surface 24 of the tool 26 .
  • the controller 56 can be programmed with various control schemes to heat and cool the mold surface 24 using the subsystems 40 , 48 , 49 and three-way valve 58 of the system 20 , if utilized.
  • the controller 56 can also be programmed to apply and remove pressure to the composite article 22 at various times and/or at various temperatures.
  • pressure can be applied by various means.
  • a pressure tank 66 is used along with the press 64 to apply pressure to the composite article 22 . It is to be appreciated that reference to the composite article 22 herein may also refer to the preform 62 depending on its degree of formation.
  • the controller 56 is programmed such that Tt 1 ⁇ Tt 2 or Tt 1 ⁇ Tt 2 . In further embodiments, the controller 56 is programmed such that Tt 1 ⁇ Tt 3 or Tt 1 ⁇ Tt 3 . The total of Tt 1 +Tt 2 +Tt 3 is as described above. In certain embodiments, the controller 56 is programmed such that Pt 1 ⁇ Pt 2 or Pt 1 ⁇ Pt 2 . In further embodiments, the controller 56 is programmed such that Pt 1 ⁇ Tt 1 or Pt 1 ⁇ Tt 1 . In yet further embodiments, the controller 56 is programmed such that Pt 2 ⁇ Tt 1 or Pt 2 ⁇ Tt 1 . Typically, (Pt 1 +Pt 2 ) ⁇ (Tt 1 +Tt 2 +Tt 3 ). Said another way, the total time for heating and cooling generally defines the total cycle time for forming the composite article 22 .
  • Timing for each of the temperature and pressure time periods can be changed to alter surface and/or mechanical properties of the composite article 22 .
  • Specific heating, cooling, pressurizing, and depressurizing profiles, for making different types of composite articles 22 can be determined via routine experimentation. Examples of specific profiles are illustrated in FIGS. 11 , 12 , and 13 , which are described further below.
  • cycle time of making the composite article 22 is greatly reduced relative to conventional methods, e.g. autoclaving.
  • the present invention provides another method.
  • the method is useful for forming the composite article 22 .
  • the method comprises the steps of providing the tool 26 and the preform 62 .
  • the tool 26 and preform 62 can be as described above.
  • the method further comprises the step of providing the press 64 .
  • the press 64 can be situated proximal or distal each of the system 20 , the pressure tank 66 , and/or the controller 56 .
  • the subsystems 40 , 48 , 49 of the system 20 can be situated proximal or distal each other. If utilized, the exchanger-subsystem 49 is typically proximal the press 64 .
  • the controller 56 can be situated proximal or distal each of the subsystems 40 , 48 , 49 and the pressure tank 66 . As such, the system 20 offers flexibility in laying out each of its components.
  • the press 64 has a platform 68 and a cover 70 facing the platform 68 .
  • the platform 68 of the press 64 is useful for supporting the tool 26 .
  • the method further comprises the step of contacting (or coupling) the platform 68 with the cover 70 to define a cavity 72 between the cover 70 and the platform 68 .
  • the cavity 72 may also be referred to as a plenum.
  • the cover 70 and/or the platform 68 include a peripheral seal 74 , such as a peripheral gasket 74 , such that the cavity 72 is airtight. In this way, the cavity 72 is operable to maintain a pressurized and/or temperature controlled environment about the tool 26 .
  • Various types of seals 74 can be employed.
  • the cover 70 is generally rigid and inflexible (which is different from a rubber or “bladder” type mold surface).
  • Various types of presses 64 can be employed.
  • the press 64 should be capable of handling the pressures described herein. Suitable presses 64 are commercially available from a variety of suppliers. Specific examples of presses 64 include those available from Globe Machine Manufacturing Company of Tacoma, Wash.
  • the method further comprises the step of disposing the preform 62 on the mold surface 24 of the tool 26 .
  • the method further comprises the step of disposing the vacuum canopy 36 on the tool 26 to define an envelope (not shown) between the vacuum canopy 36 and the mold surface 24 of the tool 26 .
  • the preform 62 and the vacuum canopy 36 may be disposed manually or automatically.
  • the vacuum canopy 36 may also be referred to as a bag 36 or a sheet 36 .
  • the vacuum canopy 36 can be formed from various materials, such as a polymeric material, e.g. a silicone.
  • the vacuum canopy 36 can include a peripheral seal 78 , e.g. a peripheral gasket 78 , to assist in forming the envelope.
  • putty 78 can be used.
  • Various types of seals 78 and/or putty 78 can be employed.
  • the envelope is airtight.
  • the vacuum canopy 36 can include a peripheral frame 80 for adding rigidity and easing handling of the vacuum canopy 36 . Handles (not shown) may be attached to the peripheral frame 80 for moving the vacuum canopy 36 .
  • Clasps 82 can also be attached to the peripheral frame 80 to interact with the fasteners 34 of the tool 26 .
  • the clasps 82 and fasteners 34 are useful for maintaining orientation of the vacuum canopy 36 on the tool 26 .
  • a release sheet (not shown) may be disposed between the vacuum canopy 36 and the preform 62 to prevent sticking.
  • a release sheet or coating (not shown) may also be applied to the mold surface 24 to prevent the composite article 22 from sticking.
  • Various types of release sheets and/or coatings may be employed.
  • the release sheet may be formed from various materials, such as a polymeric film.
  • the method further comprises the step of disposing the tool 26 under the cover 70 such that it is within the cavity 72 of the press 64 once established.
  • the tool 26 is generally disposed under the cover 70 of the press 64 prior to contacting the cover 70 to the platform 68 to establish the cavity 72 .
  • the tool 26 generally takes up at least about 33%, at least about 50%, at least about 66%, at least about 75%, at least about 80%, at least about 85%, or at least about 90%, of the overall volume of the cavity 72 , when disposed therein. As such, the remaining volume of the cavity 72 is typically small relative to the overall volume when the tool 26 is present. Inserts, partitions, or blocks (not shown) can be used to take up additional volume in the cavity, if desired.
  • a support table 84 is disposed next to the press 64 .
  • the support table 84 is useful for holding, loading, and unloading the tool 26 .
  • Another support table 84 may be used on an opposite side of the press 64 for unloading, or just one support table 84 may be used.
  • a carrier 86 is disposed adjacent the platform 68 .
  • the carrier 86 is generally on a chained track 88 and includes at least one hook 90 to engage the tool 26 , and typically includes one hook 90 for engaging each side of the tool 26 .
  • the carrier 86 is useful for pulling the tool 26 from the support table 84 onto the platform 68 of the press 64 , and under the cover 70 of the press 64 .
  • the carrier 86 moves the tool 26 a majority of the way under the cover 70 , the carrier 86 moves out of the way of the cover 70 .
  • the cover 70 then lowers down over the platform 68 to engage (or couple to) the platform 68 and define the cavity 72 .
  • Pistons 92 and/or gears 94 can be used to move the cover 70 of the press 64 up and down into place.
  • rams 96 disposed on the cover 70 extend into the cover 70 and the cavity 72 .
  • the rams 96 engage with receivers 98 on the tool 26 and push the tool 26 further on the platform 68 to substantially center the tool 26 within the cavity 72 .
  • the tool 26 is generally aligned such that it is in fluid communication with the system 20 .
  • Such fluid communication from the tool 26 to the system 20 can be routed through the cover 70 and/or through the platform 68 of the press 64 .
  • the press 64 can include one or more sensors (not shown) to ensure proper location of the tool 26 prior to lowering the cover 70 and/or prior to heating the mold surface 24 .
  • the system 20 includes a connection system for automatically coupling the press 64 and the tool 26 .
  • the connection system is useful for communicating the thermal fluid to and from the tool 26 via the system 20 .
  • a tool-connection system 200 for the tool 26 is shown.
  • the tool-connection system 200 includes a plurality of connections for connecting various elements to the tool 26 , such as fluid feeds, fluid returns, and sensors. Said another way, the tool-connection system 200 can provide various services to the tool 26 , and optionally, to the cavity 72 of the press 64 .
  • the elements provide services and communication with the tool 26 . These elements are generally in communication with the tool 26 , such as being in fluid communication with the tubing 28 of the tool 26 .
  • the tool-connection system 200 includes a resistive thermal device (RTD) male connector 202 for temperature monitoring and feedback of the tool 26 .
  • the tool-connection system 200 also includes a first alignment bushing 204 , a thermal fluid intake valve 206 for feeding thermal fluid to the tool 26 from the inlet 30 , a male locking pin 208 , a thermal fluid exhaust valve 210 for returning the thermal fluid from the tool 26 out the outlet 32 , a second alignment bushing 212 , and a vacuum connector 214 and static connector 216 for pressure monitoring of the tool 26 .
  • RTD resistive thermal device
  • the tool-connection system 200 also includes a first alignment bushing 204 , a thermal fluid intake valve 206 for feeding thermal fluid to the tool 26 from the inlet 30 , a male locking pin 208 , a thermal fluid exhaust valve 210 for returning the thermal fluid from the tool 26 out the outlet 32 , a second alignment bushing 212 , and a vacuum connector 214 and static connector 216 for pressure monitoring of the tool 26 .
  • the press-connection system 218 includes a plurality of connections for connecting various elements to the press 64 , such as fluid feeds, fluid returns, and sensors. These elements are generally in communication with the system 20 , such as being in fluid communication with the piping 38 of the system 20 .
  • the press-connection system 218 includes a RTD female connector 220 for temperature monitoring and feedback of the tool 26 .
  • the press-connection system 218 also includes a thermal fluid exhaust valve 222 for feeding thermal fluid to the tool 26 from the inlet 30 , a thermal fluid intake valve 224 for returning the thermal fluid from the tool 26 out the outlet 32 , a first alignment pin 226 , a vacuum connector 228 and a static connector 230 for pressure monitoring of the tool 26 , a female locking ring 230 operated by hydraulic actuators, and a second alignment pin 232 .
  • the press 64 is depicted during a press cycle to form a composite article 22 .
  • the press 64 and tool 26 have a pressure and temperature profile which is imparted in part by the press-connection system 218 and the tool-connection system 200 in combination with the system 20 .
  • connection between the tool 26 and cover 70 of the press 64 is done automatically after the cover 70 closes.
  • the tool-connection system 200 and the press-connection system 218 couple and engage with one another after the tool 26 enters the press 64 .
  • the rams 96 are used to push the connection systems 200 , 218 together.
  • the carrier 86 can later be used to pull the connection systems 200 , 218 apart.
  • the tool-connection system 200 is operatively connected to the tool 26 , and the press-connection system 218 is in fluid communication with the heater-subsystem 40 and the exchanger-subsystem 49 .
  • the connection systems 200 , 218 couple together for feeding and receiving the first thermal fluid to and from the tool 26 .
  • the press-connection system 218 is operatively connected to the tubing 28 of the tool 26 for heating and cooling the mold surface 26 with the first thermal fluid.
  • the press-connection system 218 is operatively connected through the cover 70 and/or the platform 68 of the press 64 into the cavity 72 for coupling with the tool-connection system 200 while the tool 26 is disposed within the cavity 70 of the press 64 for heating and cooling the mold surface 26 with the first thermal fluid.
  • Such a “quick-connect/disconnect” configuration provides for manufacturing versatility, such as allowing for multiple tool 26 variations to be utilized with no affiliated change over time.
  • various configurations of tools 26 can be utilized and simply “plugged into” the press 64 via the connection systems 200 , 218 . This also allows for a fast change out of the tools 26 in the system 20 .
  • Tool 26 changes can occur in a time frame of 5 minutes, as fast as 2 minutes and as long as 10 minutes.
  • typical tool changes in compression molding of fiber reinforced plastic parts can take 4 hours.
  • the controller 56 may be implemented using shared processing devices and/or individual processing devices.
  • Processing devices may include microprocessors, micro-controllers, digital signal processors, microcomputers, central processing units, field programmable gate arrays, programmable logic devices, state machines, logic circuitry, analog circuitry, digital circuitry, and/or any device that manipulates signals (analog and/or digital) based on operational instructions.
  • the memory may be a single memory device or a plurality of memory devices.
  • Such a memory device may be a read-only memory, random access memory, volatile memory, non-volatile memory, static memory, dynamic memory, flash memory, and/or any device that stores digital information.
  • the baseband processing module implements one or more of its functions via a state machine, analog circuitry, digital circuitry, and/or logic circuitry
  • the memory storing the corresponding operational instructions is embedded with the circuitry comprising the state machine, analog circuitry, digital circuitry, and/or logic circuitry.
  • the method further comprises the step of applying vacuum to the vacuum canopy 36 thereby evacuating the envelope to retain the preform 62 adjacent the mold surface 24 of the tool 26 .
  • This is useful for keeping the preform 62 in contact with the mold surface 24 for heating and cooling.
  • Vacuum may be applied by various methods.
  • a vacuum pump (not shown) can be connected to the tool 26 which draws air from the mold surface 24 .
  • vacuum is tested prior to disposing the tool 26 within the cavity 72 to ensure a proper seal of the vacuum canopy 36 on the tool 26 .
  • the fasteners 34 and clasps 82 are useful for aligning the vacuum canopy 36 on the tool 26 .
  • the vacuum pump can be in fluid communication with the tool through the cover 70 and/or through the platform 68 of the press 64 .
  • Vacuum can be applied at various pressures, such as from about 10 to about 35, or about 12.5 to about 32.5, or about 15 to about 30, in Hg.
  • the method further comprises the step of heating the mold surface 24 of the tool 26 from T 1 to T 2 within Tt 1 . This is useful for thinning the resin of the preform 62 .
  • T 1 , T 2 , and Tt 1 can be as described above.
  • the system 20 can be used for heating the mold surface 24 .
  • the method further comprises the step of pressurizing the cavity 72 of the press 64 from P 1 to P 2 within Pt 1 . This is useful for consolidating the preform 62 .
  • P 1 , P 2 , and Pt 1 can be as described above.
  • the method further comprises the step of providing the pressure tank 66 .
  • the pressure tank 66 is in fluid communication with the cavity 72 of the press 64 to pressurize and/or depressurize the cavity 72 of the press 64 .
  • Such fluid communication can be through the cover 70 and/or through the platform 68 of the press 64 .
  • the gas is recycled from the cavity 72 after use. In other embodiments, the gas is vented from the cavity 72 after use, rather than being recycled.
  • the pressure tank 66 can contain various compressed gases. Typically, the pressure tank 66 contains compressed air, such that the cavity 72 of the press 64 is pressurized with air. In certain embodiments, the pressure tank 66 is free of compressed nitrogen gas (N 2 ). It is to be appreciated that air can include ⁇ 78% N 2 . While air is typically used to pressurize the cavity 72 , other types of gases may also be used.
  • the pressure tank 66 may be a stand alone pressurized tank containing the compressed gas or be part of an air compressor.
  • the pressure tank 66 and/or air compressor may be of various types.
  • the pressure tank 66 and/or air compressor should be capable of handling and delivering the pressures associated with the cavity 72 of the press 64 .
  • the pressure tank 66 should be able to pressurize the cavity 72 of the press 64 to at least 150 psig in no more than 120 seconds.
  • Suitable pressure tanks 66 and air compressors are commercially available from a variety of suppliers. Specific examples of air compressors include those commercially available from Sullair® of Michigan City, Ind., including the Sullair® Stationary Air Power Systems, e.g. the Sullair® 2200, the Sullair® 3700, the Sullair® 4500, and the Sullair® 7500.
  • the pressure tank 66 can be in fluid communication with a dryer (not shown).
  • the dryer is useful for removing moisture from the compressed gas sent to or returned from the cavity 72 of the press 64 .
  • the dryer may be of various types. Suitable dryers are commercially available from a variety of suppliers. Specific examples of dryers include those commercially available from BEKO Technologies Corp. of Atlanta, Ga., including the Drypoint® Series, e.g. the Drypoint® RA.
  • the method further comprises the steps of providing the system 20 and providing the controller 56 for heating and cooling of the mold surface 24 of the tool 26 , as well as for pressurizing and depressurizing the cavity 72 .
  • the controller 56 can be in communication with the pressure tank 66 and the press 64 with the controller 56 controlling the pressure tank 66 and/or the press 64 to pressurize or depressurize the cavity 72 .
  • the controller 56 typically measures pressure of the cavity 72 by feedback from one or more pressure sensors (not shown) disposed within the cavity 72 .
  • the controller 56 is typically programmed to set certain pressures at certain times and/or temperatures.
  • the method further comprises the step of maintaining the mold surface 24 of the tool 26 at about T 2 for Tt 2 . This is useful for curing the resin.
  • the method can further comprise the step of maintaining the mold surface 24 of the tool 26 at T 1-2 for Tt ⁇ 1 prior to heating the mold surface 24 of the tool 26 to T 2 .
  • the method further comprises the step of maintaining the cavity 72 of the press 64 at about P 2 for Pt 2 . This is useful for further consolidating and curing of the composite article 22 .
  • the method further comprises the step of cooling the mold surface 24 of the tool 26 to drop the mold surface 24 from about T 2 to T 3 within Tt 3 .
  • the controller 56 , the system 20 , and the pressure tank 66 can be used for these steps.
  • the method further comprises the step of depressurizing the cavity 72 of the press 64 .
  • the cavity 72 is depressurized back to P 1 over a third period to time (Pt 3 ).
  • the cavity 72 of the press 64 can be depressurized at various rates.
  • the rate of depressurizing may be linear or curvilinear.
  • the rate of depressurizing can increase at a decreasing rate, increase at an increasing rate, be substantially constant, or combinations thereof.
  • depressurizing is at a rate of greater than about 0.1, greater than about 0.2, greater than about 0.3, greater than about 0.4, greater than about 0.5, greater than about 0.6, greater than about 0.7, greater than about 0.8, greater than about 0.9, greater than about 1, greater than about 1.1, greater than about 1.2, greater than about 1.3, greater than about 1.4, or greater than about 1.5, psi per second.
  • the cavity 72 can be depressurized at a rate upwards of about 100, about 75, about 50, about 25, or about 10, psi per second.
  • Pt 3 can be various time periods. Typically, Pt 3 is short relative to previous time periods of pressurizing. However, Pt 3 may also be longer than or equal to one or more previous time periods of pressurizing. Typically, Pt 3 is from about 1 to about 25, from about 1 to about 20, from about 1 to about 15, from about 1 to about 12.5, from about 1 to about 10, from about 1 to about 7.5, from about 1 to about 5, or from about 1 to about 2, minutes. Typically, (Pt 1 +Pt 2 +Pt 3 ) ⁇ (Tt 1 +Tt 2 +Tt 3 ).
  • the method can further comprise the step of maintaining the cavity 72 of the press 64 at P 1-2 for Pt ⁇ 1 prior to pressurizing the cavity 72 of the press 64 to P 2 .
  • the method further comprises the step of separating the cover 70 and the platform 68 of the press 64 .
  • pressure in the cavity 72 is reduced prior to separating the cover 70 and platform 68 to prevent damage to the peripheral seal 74 and/or composite article 22 .
  • the pressure tank 66 can be used to depressurize the cavity 72 .
  • the press 64 can vent the compressed gas to the atmosphere in a rapid or controlled manner.
  • the method can further comprise the step of maintaining vacuum on the vacuum canopy 36 . This is typically done while the cavity 72 of the press 64 is pressurized.
  • the method further comprises the step of removing the tool 26 from the press 64 .
  • the carrier 86 can be used to push or pull the tool 26 from the platform 68 back to the support table 84 or another support table 84 .
  • FIG. 8 another embodiment of the press 64 is shown.
  • One support table 84 can be used for loading and one support table 84 can be used for unloading.
  • different tools 26 can be used to load the press 64 rather than using the previously unloaded tool 26 . This is not to say that a previously unloaded tool 26 cannot be loaded into the press 64 at a later time.
  • the method further comprises the step of removing the vacuum canopy 36 from the tool 26 .
  • the vacuum canopy 36 may be removed manually or automatically.
  • the method further comprises the step of removing the composite article 22 from the mold surface 24 of the tool 26 .
  • the composite article 22 may be removed manually or automatically.
  • the composite article 22 is at a temperature which can be handled by gloved (or bare) hand.
  • the total of Tt 1 +Tt 2 +Tt 3 is as described above.
  • the present invention also provides a method of forming a preform 62 .
  • the method may be referred to as a layup (or lay-up) method.
  • the preform 62 may be used with the system 20 and/or invention methods described above to form the composite article 22 .
  • the method comprises the step of providing a mandrel 100 having a mandrel surface 102 .
  • Various types of mandrels 100 can be employed. Suitable mandrels 100 are commercially available from a variety of suppliers. Specific examples of mandrels 100 include those commercially available from Models & Tools Inc.
  • the mandrel surface 102 of the mandrel 100 is complimentary to the mold surface 24 of the tool 26 .
  • the surfaces 24 , 102 may be in a female/male configuration.
  • the mandrel 100 can be similar to the tool 26 .
  • the mandrel can have tubing 104 for conveying a fluid.
  • the tubing 104 includes at least one input 106 for communicating fluid to the tubing 104 and at least one outlet 108 for communicating fluid from the tubing 104 .
  • the tubing 104 is proximal or directly in contact with the mandrel surface 102 to expedite heat transfer.
  • the tubing 104 is useful for direct (rather than indirect) heating or cooling of the mandrel surface 102 .
  • the tubing 104 may be formed into the mandrel 100 itself (such as by boring), or attached within the mandrel 100 proximal the mold surface 24 , either to the tool 26 and/or to the mold surface 24 .
  • the tubing 104 can be arranged in various patterns and may be of equal or varying diameters, as like described above for the tool 26 .
  • the tubing 104 of the mandrel 100 is connected to piping (not shown) for communicating the fluid to and from the mandrel 100 .
  • the mandrel 100 can be in fluid communication with the system 20 for heating or cooling the mandrel surface 102 .
  • the mandrel 100 can be in fluid communication with another type of system (not shown), such as a conventional oil- or water-based heating and/or cooling system, typically a water-based system.
  • the method further comprises the steps of providing pieces of a carbon fiber sheet 110 and providing the resin.
  • the pieces of carbon fiber sheet 110 can be of various types, such as pieces 110 comprising the pre-pregs and/or carbon fiber mats described above.
  • the resin can be of various types, such as the epoxies described above.
  • the resin has a “tack” temperature, which is described further below.
  • the method further comprises the step of heating the mandrel surface 102 to a first temperature.
  • the first temperature promotes adhesion of the resin to the mandrel surface 102 during preparation of the preform 62 .
  • the first temperature generally corresponds to the tack temperature of the resin, where the resin adheres to both the mandrel surface 102 and to itself, such as adhesion between layers of the pieces 110 .
  • the tack temperature can be determined via testing or by reference to technical literature of the resin, such as from MSDS or technical data sheets.
  • a typical test for determining tack involves placing a gloved finger or tool on a layer of the resin, and pulling the finger or tool away to determine at which point in temperature the resin adheres to the finger or tool when pulled away.
  • the first temperature is typically of from about 100 to about 175, from about 110 to about 155, or from about 125 to about 140, ° F. ( ⁇ 38 to ⁇ 79, ⁇ 43 to ⁇ 68, or ⁇ 52 to ⁇ 60, ° C.).
  • the method typically comprises the step of applying the resin to the mandrel surface 102 of the mandrel 100 to form a resin layer (not shown).
  • the resin may be applied by various methods. For example, the resin may be applied by hand or robotic spraying, brushing, pouring, rolling, etc. Prior to applying the resin, a release liner or coating may be applied to the mandrel surface 102 to prevent sticking of the preform 62 .
  • the method further comprises the step of arranging the pieces 110 on the resin layer to form a carbon fiber mat.
  • the pieces 110 may be laid in a uniform layer and/or may overlap one another. Multiple layers of the pieces 110 can be arranged to build up thickness of the carbon fiber mat, and optionally, additional resin can be applied between the layers of the pieces 110 .
  • the method typically comprises the step of applying additional resin on top of the carbon fiber mat.
  • the method further comprises the step of disposing a vacuum sheet 112 on the mandrel 100 to define an envelope (not shown) between the vacuum sheet 112 and the mandrel surface 102 of the mandrel 100 .
  • putty 114 is applied around a periphery of the mandrel 100 for making the envelope airtight.
  • the putty 114 may be applied by various methods, such as by hand, robotic dispenser, etc.
  • a release liner or coating may be applied between the vacuum sheet 112 and the preform 62 to prevent sticking.
  • the vacuum sheet 112 may be configured similar to or the same as the vacuum sheet 36 described above with the tool 26 . In other words, the vacuum sheet 112 may include a peripheral seal (not shown).
  • the method further comprises the step of applying vacuum to the vacuum sheet 112 thereby evacuating the envelope to retain the preform 62 adjacent the mandrel surface 102 of the mandrel 100 .
  • This is useful for consolidating the pieces 110 and further form the preform 62 .
  • This is also useful for keeping the preform 62 in contact with the mandrel surface 102 during heating and cooling.
  • Vacuum can be applied at various pressures, such as from about 10 to about 35, from about 12.5 to about 32.5, or from about 15 to about 30, inches Hg.
  • the method further comprises the step of cooling the mandrel surface 102 to a second temperature.
  • the second temperature allows the preform 62 to be released from the mandrel surface 102 .
  • the second temperature is typically cooler than the first temperature, and generally corresponds to either a non-tack or less tacky temperature of the resin.
  • the second temperature is typically from about 35 to about 100, about 40 to about 75, or about 40 to about 50, ° F. ( ⁇ 1.7 to ⁇ 38, ⁇ 4 to ⁇ 24, or ⁇ 4 to ⁇ 10, ° C.).
  • Heating and cooling of the mandrel surface 102 can be controlled manually, or automatically, such as by another controller (not shown).
  • the method further comprises the steps of removing the vacuum sheet 112 from the mandrel 100 and removing the removing the preform 62 from the mandrel surface 102 . These steps can be manual or automatic.
  • the mandrel 100 can be attached to a manual or robotic arm (not shown), such that the mandrel 100 can be movable from a preparation position to a molding position.
  • a preparation position the preform 62 is formed on the mandrel 100 , with the mandrel surface 102 set at the first temperature to hold the preform 62 in place.
  • the mandrel 100 can then move to the molding position, where the temperature of the mandrel surface 102 is set to the second temperature, thereby allowing release of the preform 62 from the mandrel surface 102 .
  • the preform 62 can then be disposed on the mold surface 24 of the tool 26 for further processing, such as directly moving or dropping the preform 62 from the mandrel 100 onto the mold surface 24 .
  • the preform 62 can be stored or queued for later use in either the same or a different location.
  • various steps may be carried out before and/or after formation of the composite article 22 in the press 64 . These steps can be used in various orders and combinations. These additional steps are merely examples, and are not to be construed as limitations of the present invention.
  • the pieces 110 for the preform 62 can be provided by a “kit cut” process.
  • a pre-preg sheet can be cut into the pieces 110 using computer driven cutting tables, which use data from a computer aided drafting (CAD) system and/or from digitized patterns and drawings.
  • the kit cut process may utilize a computer numerically controlled (CNC) work cell, which includes of a series of CNC and machining tools. Patterns and molds can be made on-site, but may also be supplemented by 3 rd parties, if needed. Similar to other raw materials, the pieces 110 can be cold stored in a freezer to preserve them in advance of a lay-up process.
  • CNC computer numerically controlled
  • the pieces 110 can be used to form preforms 62 with the mandrel 100 as described above. While automation is possible, the use of hand lay-up generally allows for designing composite articles 22 with different strength requirements throughout the composite article 22 by laying down a kit of the pieces 110 that is unique to each mandrel 100 . In addition, hand lay-up can reduce material cost by eliminating unnecessary extra build-up of the resin.
  • the composite articles 22 After formation of the composite articles 22 via the press 64 and after removal from the tool 24 , they can be provided to a trim process.
  • the composite articles 22 may be mechanically trimmed and/or drilled by a robotic router. The use of the robotic router facilitates consistent accuracy as well as timely turnaround.
  • the composite articles 22 may then be provided to a sub-assembly and bonding process.
  • Composite articles 22 that may require bonding are prepped following the trim process and placed in a bonding cell where they are CNC bonded.
  • the use of a robotic bonding cell provides a consistent adhesive path for bond accuracy as well as quick turnaround.
  • the composite articles 22 may then be provided to a finishing process.
  • the composite articles 22 can be robotically or hand sanded. It is believed that while automated technology can streamline the finishing process, use of hand sanding helps to ensure Class A surface quality, if desired. Technicians identify and repair minor surface blemishes of the composite articles 22 , if present.
  • the composite articles 22 may then be provided to a prime process.
  • the composite articles 22 can enter a paint line system for a high volume low pressure (HVLP) primer (or clear coat) application.
  • HVLP high volume low pressure
  • the composite articles 22 may be washed prior to prevent contamination.
  • Composite articles 22 having exposed carbon fiber weave can be clear coated and shipped directly to a customer, while composite articles 22 which require color can be primed and may be sent to a 3 rd party, e.g. an OEM approved supplier, to be painted before reaching a customer.
  • the composite articles 22 may then be provided to a final inspection process.
  • the composite articles 22 can be gauged and visually inspected to ensure dimensional quality.
  • Clear coated composite articles 22 can be provided to a finesse stage where they are polished to a jewel like finish before a final visual inspection prior to shipment to the customer.
  • the composite articles 22 formed from the invention methods have excellent mechanical properties and/or surface properties.
  • the composite articles 22 can have near Class A surfaces, with little to no surface blemishes relative to composite articles formed via conventional autoclaving methods. More specifics of the composite articles 22 are described in the examples immediately below.
  • PCT/US2011/059434 entitled “THERMAL PROCESSING AND CONSOLIDATION SYSTEM AND METHOD”
  • International Application No. PCT/US2011/062836 entitled “METHOD AND SYSTEM FOR FORMING COMPOSITE ARTICLES”; all of which are incorporated herein by reference in their entirety to the extent they do not conflict with the general scope of the present invention.
  • Comparative examples of composites articles are made by using a conventional autoclave and autoclaving method.
  • Invention examples of composites articles are made by using and the system and method of the present invention. Additional information regarding these examples is provided in Table I below and the subsequent description.
  • the preforms are formed by conventional lay-up methods.
  • the preforms are shaped into car hoods.
  • the carbon fiber mat is an exposed weave pre-preg, and the resin is a “quick cure” epoxy resin, which are both commercially available from Toray Composites (America), Inc. of Tacoma, Wash.
  • the preforms are loaded into tool and covered with a vacuum sheet.
  • the tools are the same in configuration and material. Vacuum is established and confirmed.
  • the tools are disposed into the autoclave or press, respectively.
  • the autoclave is closed and the started.
  • the press is closed and started.
  • the press is in fluid communication with the invention system.
  • each of the TCs in FIG. 14 refers to a temperature at a specific point on the mold surface of the tool.
  • the autoclave fails to uniformly heat the mold surface at constant temperatures. It is believed that this lack of uniform heat soaking imparts the composite articles formed in the autoclave with various problems, such as surface blemishes.
  • FIG. 11 specific parameters including temperature and pressure ramps and dwells for the press can be better appreciated.
  • FIG. 12 illustrates a second invention example (not shown in Table I above).
  • FIG. 13 illustrates a third invention example (also not shown in Table I above).
  • the invention system is capable of rapidly heating the mold surface in a short period of time.
  • a dwell is not required to reach a peak temperature. Instead, the peak temperature can be quickly reached within a very short period of initial time based on the rapid heating capability of the invention system.
  • temperature of the mold surface of the tool ramps from T 1 to T 1-2 using the heater-subsystem and controller. Specifically, the controller directs a portion of the mass of heated fluid from the tank of the heater-subsystem to the tool using the valves until T 1-2 is reached.
  • T 1-2 the controller stops flow from the tank by using the valves and the heater-subsystem begins to re-circulate to recharge the mass of heated fluid.
  • T 1-2 is maintained at an acceptable tolerance level by the controller modulating additional flow of the mass of heated fluid to the tool, as needed.
  • the resin is at or near its lowest viscosity. Having the resin at such a viscosity allows any trapped air or resin byproducts created during cure of the resin (e.g. steam) to evacuate from the composite article.
  • the cavity of the press is pressurized to P 1-2 .
  • the controller directs the pressure tank to provide compressed air to the cavity. Once P 1-2 is reached, the controller stops flow from the pressure tank. P 1-2 is maintained at an acceptable tolerance level by the controller modulating additional flow of compressed air to the cavity, as needed.
  • the controller directs another portion (or all of) the mass of heated fluid to the tool until the mold surfaces reaches T 2 .
  • T 2 the controller stops flow from the tank by using the valves and the heater-subsystem begins to re-circulate to recharge the mass of heated fluid.
  • T 2 is maintained at an acceptable tolerance level by the controller modulating additional flow of the mass of heated fluid to the tool, as needed.
  • the resin is at or near its cure temperature. It is believed that having the resin at such a temperature imparts the composite article with excellent surface and mechanical properties. This temperature can be determined via testing or by reference to technical literature of the resin, such as from MSDS or technical data sheets.
  • the cavity of the press is pressurized to P 2 .
  • the controller directs the pressure tank to provide compressed air to the cavity. Vacuum is maintained while pressure is applied. Once P 2 is reached, the controller stops flow from the pressure tank. P 2 is maintained at an acceptable tolerance level by the controller modulating additional flow of compressed air to the cavity, as needed.
  • the controller directs the press to depressurize. Specifically, the press begins to vent the compressed air to the atmosphere over Pt 3 .
  • the press may do a complete “dump” of the air, i.e., air does not need to be released at a controlled rate.
  • the controller directs a portion of the mass of cooled fluid from the tank of the chiller-subsystem to the tool using the valves until T 3 is reached.
  • the controller Prior to or while the heater-subsystem was previously being used, the controller directed the chiller-subsystem to form and maintain the mass of cooled fluid using the valves, tank, and chiller. While the chiller-subsystem is being used, the controller directs the heater-subsystem to recharge and maintain the mass of heated fluid using the valves, tank, and heater. As such, the system is ready for a subsequent cycle immediately after a short period of time.
  • the controller directs a portion of the mass of cooled fluid from the tank of the chiller-subsystem to the exchanger-subsystem using the valves until T 3 is reached.
  • the controller Prior to or while the heater-subsystem was previously being used, the controller directed the chiller-subsystem to form and maintain the mass of cooled fluid using the valves, tank, and chiller. While the chiller-subsystem is being used, the controller directs the heater-subsystem to recharge and maintain the mass of heated fluid using the valves, tank, and heater. As such, the system is ready for a subsequent cycle immediately after a short period of time.
  • the tools are removed from the autoclave and press. Performance of each cycle is evaluated on an appearance basis of the composite articles formed via each method. Specifically, the composite articles are removed from the tools and their surfaces are wiped with white talcum powder to highlight surface blemishes. Pits and/or dry-lines present on the surface of the composite articles are highlighted by the talcum powder. Specifically, such defects are seen as white dots (pits) or white streaks (dry-lines). A pit or dry-line is where the resin has not properly flowed during the cycle thereby leaving a void on the surface.
  • the composite articles made by the invention system and method have excellent surface properties relative to those made by the autoclave. Specifically, the composite articles formed via the invention system and method have an ⁇ 85 to 90% reduction in the amount of pits and dry-lines relative to those formed in the autoclave. In addition, the composite articles formed via the invention system and method have an ⁇ 85% to 90% reduction in the severity (depth/width) of pits and dry-lines relative to those formed in the autoclave. Such defects have to be repaired (filled and sanded) in order for the surface of the composite article to be considered Class A.
  • the invention system and method also has over an ⁇ 80% reduction in cycle time relative to the autoclave process (13 mins vs. 72 mins).
  • the tools are over 30% cooler in temperature after being removed from the press relative to those removed from the autoclave: ⁇ 120° F. ( ⁇ 49° C.) vs. ⁇ 180° F. ( ⁇ 82° C.).
  • the invention system and method allows for a significant reduction in cycle time and overall manufacturing time while providing higher quality composite articles, as compared to those formed using the autoclave.
  • any ranges and subranges relied upon in describing various embodiments of the present invention independently and collectively fall within the scope of the appended claims, and are understood to describe and contemplate all ranges including whole and/or fractional values therein, even if such values are not expressly written herein.
  • One of skill in the art readily recognizes that the enumerated ranges and subranges sufficiently describe and enable various embodiments of the present invention, and such ranges and subranges may be further delineated into relevant halves, thirds, quarters, fifths, and so on.
  • a range “of from 0.1 to 0.9” may be further delineated into a lower third, i.e., from 0.1 to 0.3, a middle third, i.e., from 0.4 to 0.6, and an upper third, i.e., from 0.7 to 0.9, which individually and collectively are within the scope of the appended claims, and may be relied upon individually and/or collectively and provide adequate support for specific embodiments within the scope of the appended claims.
  • a range such as “at least,” “greater than,” “less than,” “no more than,” and the like, it is to be understood that such language includes subranges and/or an upper or lower limit.
  • a range of “at least 10” inherently includes a subrange of from at least 10 to 35, a subrange of from at least 10 to 25, a subrange of from 25 to 35, and so on, and each subrange may be relied upon individually and/or collectively and provides adequate support for specific embodiments within the scope of the appended claims.
  • an individual number within a disclosed range may be relied upon and provides adequate support for specific embodiments within the scope of the appended claims.
  • a range “of from 1 to 9” includes various individual integers, such as 3, as well as individual numbers including a decimal point (or fraction), such as 4.1, which may be relied upon and provide adequate support for specific embodiments within the scope of the appended claims.
US14/232,723 2011-07-28 2012-07-30 System and method for forming composite articles Abandoned US20140159267A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US14/232,723 US20140159267A1 (en) 2011-07-28 2012-07-30 System and method for forming composite articles

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US201161574151P 2011-07-28 2011-07-28
US14/232,723 US20140159267A1 (en) 2011-07-28 2012-07-30 System and method for forming composite articles
PCT/US2012/048832 WO2013016728A1 (en) 2011-07-28 2012-07-30 Thermal system and method for rapidly forming composite articles

Related Parent Applications (1)

Application Number Title Priority Date Filing Date
PCT/US2012/048832 A-371-Of-International WO2013016728A1 (en) 2011-07-28 2012-07-30 Thermal system and method for rapidly forming composite articles

Related Child Applications (1)

Application Number Title Priority Date Filing Date
US15/292,228 Continuation US10493666B2 (en) 2011-07-28 2016-10-13 System and method for forming composite articles

Publications (1)

Publication Number Publication Date
US20140159267A1 true US20140159267A1 (en) 2014-06-12

Family

ID=46640776

Family Applications (2)

Application Number Title Priority Date Filing Date
US14/232,723 Abandoned US20140159267A1 (en) 2011-07-28 2012-07-30 System and method for forming composite articles
US15/292,228 Expired - Fee Related US10493666B2 (en) 2011-07-28 2016-10-13 System and method for forming composite articles

Family Applications After (1)

Application Number Title Priority Date Filing Date
US15/292,228 Expired - Fee Related US10493666B2 (en) 2011-07-28 2016-10-13 System and method for forming composite articles

Country Status (5)

Country Link
US (2) US20140159267A1 (ja)
EP (1) EP2736693B1 (ja)
JP (1) JP6050351B2 (ja)
KR (1) KR20140053143A (ja)
WO (1) WO2013016728A1 (ja)

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2016111785A1 (en) * 2015-01-07 2016-07-14 Massachusetts Institute Of Technology Production of composite parts
GB2535193A (en) * 2015-02-12 2016-08-17 Zodiac Seats Uk Ltd Tool for curing a composite component
US9676124B2 (en) 2010-12-01 2017-06-13 Plasan Carbon Composites, Inc. Method and system for forming composite articles
US20180224149A1 (en) * 2017-02-07 2018-08-09 Schneider Electric It Corporation Cooling system with reduced pressure drop
US20180229402A1 (en) * 2017-02-10 2018-08-16 Divergent Technologies, Inc. Methods for producing panels using 3d-printed tooling shells
US10493666B2 (en) 2011-07-28 2019-12-03 Plasan Carbon Composites, Inc. System and method for forming composite articles
US10913833B2 (en) * 2015-09-04 2021-02-09 Gurit (Uk) Ltd. Prepregs and production of composite material using prepregs
US11318659B2 (en) 2018-04-25 2022-05-03 Nike, Inc. System and methods for thermoforming articles
US20220143875A1 (en) * 2019-02-28 2022-05-12 Lm Wind Power A/S A flexible preform mould for manufacturing a preform for a wind turbine blade
US11400673B2 (en) 2015-11-11 2022-08-02 Nike, Inc. Articles of wear and processes for making the same
US11590686B2 (en) * 2018-04-25 2023-02-28 Nike, Inc. System and methods for thermoforming articles

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
AT520890B1 (de) * 2018-02-01 2020-03-15 Wittmann Kunststoffgeraete Temperiergerät und Verfahren zum Steuern und Regeln eines Temperiergeräts für ein
WO2020041886A1 (en) * 2018-08-30 2020-03-05 Husky Injection Molding Systems Ltd. Melt dispenser for plastic molding
TWM589091U (zh) * 2019-10-04 2020-01-11 正鴻科技有限公司 以四向電子閥對工具機之構件提供升降溫效果的輔助裝置

Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3167811A (en) * 1960-04-14 1965-02-02 Robert A Kraus Apparatus for forming thin wall articles of manufacture from expandable fusible plastic
US3525098A (en) * 1965-06-15 1970-08-18 Thermovox Gmbh Kunstsfoffmasch Process and device for heating and/or cooling moulds
US3556201A (en) * 1968-03-25 1971-01-19 Konus Kessel Ges Fur Warmetech Method and apparatus for heating and cooling presses and the like
US3880227A (en) * 1972-06-13 1975-04-29 Thermovox Gmbh Arrangement for heating and cooling a double-walled mold
US5437304A (en) * 1992-03-30 1995-08-01 Delcroix; Jean-Louis Device for alternate admission of a liquid or a pressurized gas to one or more moulds used in plastics processing
US20030085491A1 (en) * 2001-11-07 2003-05-08 Fuji Photo Film Co., Ltd. Heat exchange apparatus for a metal mold
US20080111280A1 (en) * 2006-11-14 2008-05-15 Samsung Electronics Co., Ltd. Temperature control system for mold and injection molding method using the same
US20090218729A1 (en) * 2008-02-29 2009-09-03 Pelley Kenneth A Method and apparatus to form a spherical end of an elongated cylindrical tube

Family Cites Families (45)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2620635A (en) * 1950-09-09 1952-12-09 Erwin W Mautner Cooling system and control
US3190944A (en) * 1963-05-31 1965-06-22 Davidson Rubber Company Inc Method of mold temperature control
US3259175A (en) * 1964-06-15 1966-07-05 Robert A Kraus Heating and cooling system for molds
US3334383A (en) 1965-11-03 1967-08-08 Lockheed Aircraft Corp Molding apparatus
BE795718A (fr) * 1972-02-23 1973-06-18 Decca Ltd Procede et appareil pour la fabrication d'enregistrements profiles
US4125526A (en) 1973-01-02 1978-11-14 Goodyear Aerospace Corporation Vacuum blanket curing method
US4593056A (en) 1985-06-21 1986-06-03 Union Carbide Corporation Epoxy/aromatic amine resin systems containing aromatic trihydroxy compounds as cure accelerators
JPS62208918A (ja) * 1986-03-11 1987-09-14 Hitachi Ltd 金型温度調節装置
JPS63251207A (ja) 1987-04-07 1988-10-18 Ashida Seisakusho:Kk プリント配線板の成形方法及びその装置
JPH01125609U (ja) * 1988-02-12 1989-08-28
JPH0243011A (ja) 1988-08-03 1990-02-13 Nissan Motor Co Ltd 繊維強化複合部材の製造方法
JPH0791784B2 (ja) 1989-07-17 1995-10-04 タイガースポリマー株式会社 マットの製造方法
US5360671A (en) 1990-07-06 1994-11-01 The University Of Akron Thermoplastic polymides and composites therefrom
US5209889A (en) 1991-10-10 1993-05-11 Gencorp Inc. Method for operation of shuttle assembly for use in an injection molding machine
US5362221A (en) 1992-08-17 1994-11-08 General Electric Company Manufacturing device with an automatic self-aligning connector for attachment to a docking station
FR2694906B1 (fr) 1992-08-20 1994-09-23 Acb Presse pour le formage d'une pièce en matériau composite comportant des renforts fibreux dans une matrice en polymère.
US5328979A (en) 1992-11-16 1994-07-12 The University Of Akron Thermoplastic copolyimides and composites therefrom
US5354195A (en) 1992-12-23 1994-10-11 United Technologies Corporation Composite molding apparatus for high pressure co-cure molding of lightweight honeycomb core composite articles having ramped surfaces utilizing low density, stabilized ramped honeycomb cores
JP3027895B2 (ja) 1993-02-02 2000-04-04 トヨタ自動車株式会社 樹脂基複合材料の成形方法
JPH1015944A (ja) 1996-07-05 1998-01-20 Taiho Kogyo Kk 成形型の加熱冷却装置
JP2000176940A (ja) 1998-12-21 2000-06-27 Yokohama Rubber Co Ltd:The 蒸気加熱成形方法及びその装置
JP2002220538A (ja) 2000-03-28 2002-08-09 Mazda Motor Corp 成形用ガラス長繊維強化樹脂材料、該樹脂材料を射出成形してなる射出成形品及び該樹脂材料を用いた成形方法
US20020025423A1 (en) 2000-07-21 2002-02-28 Dreher Michael A. Method of fabricating a composite part including a resin impregnated fiber shell and an expandable syntactic foam core
CN100396472C (zh) 2001-01-25 2008-06-25 快速科技有限公司 复合金属部件的生产、成型和粘结系统
JP2005205876A (ja) * 2003-12-25 2005-08-04 Innotech Corp 加熱冷却装置
JP5105704B2 (ja) * 2004-12-07 2012-12-26 株式会社シスコ 熱プレス用又は加熱冷却用金型の加熱冷却システム及び加熱冷却方法
JP4550762B2 (ja) * 2005-09-22 2010-09-22 株式会社スター精機 金型温度調節装置
US20090256290A1 (en) 2005-10-27 2009-10-15 Polytec Holding Ag RSM (Rapid Shell Moulding) Rapid Moulding Process
FR2913089B1 (fr) 2007-02-22 2010-11-26 Staubli Sa Ets Element de raccord a soupape d'obturation et raccord incorporant un tel element
DE102007026099A1 (de) 2007-06-05 2008-12-11 Airbus Deutschland Gmbh Vorrichtung und Verfahren zum Bearbeiten einer Faserverbundstruktur
JP2009137075A (ja) * 2007-12-04 2009-06-25 Autonetworks Technologies Ltd 射出成形方法及び金型温度調節装置
FR2927143B1 (fr) 2008-02-06 2010-03-19 Staubli Sa Ets Element femelle de raccord et raccord rapide incorporant un tel element
FR2928787B1 (fr) 2008-03-12 2012-06-22 Staubli Sa Ets Element femelle de connecteur et connecteur comprenant un tel element femelle
FR2933162B1 (fr) 2008-06-30 2010-08-20 Staubli Sa Ets Element de raccord a griffes et raccord incorporant un tel element
FR2933155B1 (fr) 2008-06-30 2010-08-27 Staubli Sa Ets Ensemble de connexion et procede de connexion d'un tel ensemble
FR2944297B1 (fr) 2009-04-10 2011-04-08 Staubli Sa Ets Dispositif d'assemblage, ensemble de deux pieces assemblees par un tel dispositif et lame de machine de formation de la foule comprenant un tel ensemble
FR2945101B1 (fr) 2009-04-30 2011-05-20 Staubli Sa Ets Nourrice de distribution ou de collecte de fluide et installation de moulage comprenant une telle nourrice
FR2948435B1 (fr) 2009-07-23 2011-08-12 Staubli Sa Ets Element femelle de raccord et raccord rapide incorporant un tel element
FR2950949B1 (fr) 2009-10-01 2012-06-22 Staubli Sa Ets Element femelle de raccord rapide et raccord rapide incorporant un tel element
FR2950950B1 (fr) 2009-10-01 2012-12-07 Staubli Sa Ets Element femelle de raccord rapide et raccord rapide incorporant un tel element
US8633327B2 (en) 2010-03-24 2014-01-21 Dow Global Technologies Inc. Process for preparing divinylarene dioxides
FR2965887B1 (fr) 2010-10-08 2012-11-30 Staubli Sa Ets Dispositif de raccord avec verrouillage par griffes filetees et raccord comprenant un tel dispositif
WO2012061768A2 (en) 2010-11-05 2012-05-10 Lightweight Labs, Llc Thermal processing and consolidation system and method
EP2646215A1 (en) 2010-12-01 2013-10-09 Plasan Carbon Composites, Inc. Method and system for forming composite articles
EP2736693B1 (en) 2011-07-28 2017-02-22 Plasan Carbon Composites, Inc. Thermal system and method for rapidly forming composite articles

Patent Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3167811A (en) * 1960-04-14 1965-02-02 Robert A Kraus Apparatus for forming thin wall articles of manufacture from expandable fusible plastic
US3525098A (en) * 1965-06-15 1970-08-18 Thermovox Gmbh Kunstsfoffmasch Process and device for heating and/or cooling moulds
US3556201A (en) * 1968-03-25 1971-01-19 Konus Kessel Ges Fur Warmetech Method and apparatus for heating and cooling presses and the like
US3880227A (en) * 1972-06-13 1975-04-29 Thermovox Gmbh Arrangement for heating and cooling a double-walled mold
US5437304A (en) * 1992-03-30 1995-08-01 Delcroix; Jean-Louis Device for alternate admission of a liquid or a pressurized gas to one or more moulds used in plastics processing
US20030085491A1 (en) * 2001-11-07 2003-05-08 Fuji Photo Film Co., Ltd. Heat exchange apparatus for a metal mold
US20080111280A1 (en) * 2006-11-14 2008-05-15 Samsung Electronics Co., Ltd. Temperature control system for mold and injection molding method using the same
US20090218729A1 (en) * 2008-02-29 2009-09-03 Pelley Kenneth A Method and apparatus to form a spherical end of an elongated cylindrical tube

Cited By (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9676124B2 (en) 2010-12-01 2017-06-13 Plasan Carbon Composites, Inc. Method and system for forming composite articles
US10493666B2 (en) 2011-07-28 2019-12-03 Plasan Carbon Composites, Inc. System and method for forming composite articles
WO2016111785A1 (en) * 2015-01-07 2016-07-14 Massachusetts Institute Of Technology Production of composite parts
US10576701B2 (en) 2015-01-07 2020-03-03 Massachusetts Institute Of Technology Production of composite parts
US11305499B2 (en) 2015-02-12 2022-04-19 Safran Seats GB Limited Tool for curing a composite component
GB2535193A (en) * 2015-02-12 2016-08-17 Zodiac Seats Uk Ltd Tool for curing a composite component
US11724469B2 (en) 2015-02-12 2023-08-15 Safran Seats GB Limited Tool for curing a composite component
US11505642B2 (en) 2015-09-04 2022-11-22 Gurit (Uk) Ltd. Prepregs and production of composite material using prepregs
US10913833B2 (en) * 2015-09-04 2021-02-09 Gurit (Uk) Ltd. Prepregs and production of composite material using prepregs
US11400673B2 (en) 2015-11-11 2022-08-02 Nike, Inc. Articles of wear and processes for making the same
US11692727B2 (en) * 2017-02-07 2023-07-04 Uniflair S.P.A. Cooling system with reduced pressure drop
US20180224149A1 (en) * 2017-02-07 2018-08-09 Schneider Electric It Corporation Cooling system with reduced pressure drop
US11247367B2 (en) 2017-02-10 2022-02-15 Divergent Technologies, Inc. 3D-printed tooling shells
US10759090B2 (en) * 2017-02-10 2020-09-01 Divergent Technologies, Inc. Methods for producing panels using 3D-printed tooling shells
US20180229402A1 (en) * 2017-02-10 2018-08-16 Divergent Technologies, Inc. Methods for producing panels using 3d-printed tooling shells
US11318659B2 (en) 2018-04-25 2022-05-03 Nike, Inc. System and methods for thermoforming articles
US11590686B2 (en) * 2018-04-25 2023-02-28 Nike, Inc. System and methods for thermoforming articles
US11826945B2 (en) 2018-04-25 2023-11-28 Nike, Inc. System and methods for thermoforming articles
US11890803B2 (en) 2018-04-25 2024-02-06 Nike, Inc. System and methods for thermoforming articles
US20220143875A1 (en) * 2019-02-28 2022-05-12 Lm Wind Power A/S A flexible preform mould for manufacturing a preform for a wind turbine blade

Also Published As

Publication number Publication date
US20170297233A1 (en) 2017-10-19
US10493666B2 (en) 2019-12-03
KR20140053143A (ko) 2014-05-07
JP2014524860A (ja) 2014-09-25
EP2736693B1 (en) 2017-02-22
WO2013016728A1 (en) 2013-01-31
JP6050351B2 (ja) 2016-12-21
EP2736693A1 (en) 2014-06-04

Similar Documents

Publication Publication Date Title
US10493666B2 (en) System and method for forming composite articles
US9676124B2 (en) Method and system for forming composite articles
KR102037237B1 (ko) 열처리 강화 시스템 및 방법
US10105911B2 (en) End of arm tooling
JP6784728B2 (ja) 熱処理及び固化システム並びにその方法
EP3628475B1 (en) System and method for manufacturing composite structures
US20210187873A1 (en) Mold and trim tool
US20200094490A1 (en) System and method for manufacturing composite structures
US11135784B2 (en) System and method for manufacturing composite structures
US9987832B2 (en) Honeycomb sandwich panel paint ready surface
NL2021878B1 (en) System and method for manufacturing composite structures
EP3628476B1 (en) System and method for manufacturing composite structures
NL2021876B1 (en) System and method for manufacturing composite structures
CN113771465A (zh) 用于固化复合材料的方法和系统和相关的抗微裂复合材料
Steyer et al. Mass production of fibre-reinforced plastic components for structural applications
Kruckenberg Manufacturing and tooling cost factors

Legal Events

Date Code Title Description
AS Assignment

Owner name: PLASAN CARBON COMPOSITES, INC., VERMONT

Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNORS:MURCH, ROBERT W.;LOWNSDALE, GARY R.;BARTOLOTTI, DOUGLAS S.;SIGNING DATES FROM 20120919 TO 20120925;REEL/FRAME:029078/0919

AS Assignment

Owner name: PLASAN CARBON COMPOSITES, INC., VERMONT

Free format text: CORRECTIVE ASSIGNMENT TO CORRECT THE TO REMOVE INCORRECT SERIAL NUMBER 12/048,832 AND CORRECT MIDDLE INITIAL OF DOUGLAS BARTOLOTTI FROM "S." TO "L." (AS SIGNED) PREVIOUSLY RECORDED ON REEL 029078 FRAME 0919. ASSIGNOR(S) HEREBY CONFIRMS THE ASSIGNMENT;ASSIGNORS:MURCH, ROBERT W.;LOWNSDALE, GARY R.;BARTOLOTTI, DOUGLAS L.;SIGNING DATES FROM 20120919 TO 20120925;REEL/FRAME:033080/0028

AS Assignment

Owner name: FIRST MIDWEST BANK, AS ADMINISTRATIVE AGENT, ILLIN

Free format text: SECURITY INTEREST;ASSIGNOR:PLASAN CARBON COMPOSITES, INC.;REEL/FRAME:037645/0707

Effective date: 20160129

STCB Information on status: application discontinuation

Free format text: ABANDONED -- FAILURE TO RESPOND TO AN OFFICE ACTION