Method and associated apparatus for forming reinforced panel components - Patents.com

Abstract

To provide a method and device for forming a reinforced panel component.SOLUTION: There is provided a method of forming a reinforced panel component, comprising: engaging the reinforcing component having a joint surface with a first portion of a heated press machine; engaging an uncured panel component with an opposing second portion of the press machine; and engaging the uncured panel component in which the panel component has a joint surface that is complementary to the joint surface of the reinforced component with the opposing second portion of the press machine. A reinforcing panel is formed: by treating the joint surface of the reinforced component so that the joint surface of the reinforced component is effective for co-joining to the panel component; by actuating the press machine to direct the first portion and the second portion of the press machine toward each other, such that the joint surfaces of the reinforced component and the panel component are engaged complementarily under pressure; by heating the first portion and the second portion of the press machine to a curing temperature associated with the panel component to simultaneously co-join the joint surface of the reinforcement component and the panel component together; and by curing the panel component.SELECTED DRAWING: None

Description

[Technical field]

[0001] The present disclosure relates generally to stiffened panel components for aircraft. In particular, the present disclosure relates to methods and apparatus for forming stiffened panel components. [Background technology]

[0002] An aircraft generally includes an airframe, which may be considered an undercarriage, to which skin panels are attached to form a smooth aerodynamic outer surface. The wings of an aircraft also include an undercarriage, which is covered by skin panels. The undercarriage may include stringers, which together with longerons, formers, frames, ribs, spars, etc. form a structural framework. The skin panels are generally light and thin to minimize the weight of the aircraft and increase the payload and range of the aircraft. Because the skin panels are thin, they are generally flexible and require stiffening in conjunction with the undercarriage to prevent undesired movement, flexing, and vibration of the skin panels during flight.

[0003] Often, strengthening of skin panels is achieved by bonding stringers to the skin panels. However, bonding the stringers to the skin panels requires multiple process cycles that are time consuming and expensive. Thus, there is a need to reduce the cycle time and cost of bonding stringers to skin panels while minimizing the number and weight of parts when stringers are used to stiffen skin panels. Summary of the Invention

[0004] One embodiment of the present disclosure is directed to a method of forming a stiffened panel component for an aircraft or any similar application. As used herein, "stiffened panel component," "stiffened panel," and "stiffened component" all refer to the same component. In one particular embodiment, the method of forming the stiffened panel component includes co-bonding faying surfaces of a stiffening component and a panel component together substantially simultaneously (e.g., simultaneously or with only a small time difference) and applying heat and pressure to cure the panel component to form the stiffened panel component. Co-bonding the faying surfaces and curing the panel component substantially simultaneously advantageously reduces the typical cycle time and cost of bonding a stiffening component (e.g., a composite stringer) to a panel component (e.g., a composite skin panel) while minimizing the number of parts and the weight of the parts. For example, in one example, a typical cycle time of about 8-10 hours using an autoclave is reduced to about 20-50 minutes using the apparatus and methods disclosed herein.

[0005] Accordingly, the present disclosure provides, in one embodiment, a method of forming a reinforced panel, the method including engaging a reinforcing component with a first portion of a heated press, the reinforcing component having a faying surface, engaging an uncured panel component with an opposing second portion of the press, the panel component having a faying surface configured complementarily to the faying surface of the reinforcing component, treating the faying surface of the reinforcing component such that the faying surface of the reinforcing component is effective for co-bonding to the panel component, operating the press to orient the first and second portions of the press toward one another such that the faying surfaces of the reinforcing component and the panel component complementarily engage under pressure, and heating the first and second portions of the press to a cure temperature associated with the panel component to substantially simultaneously co-bond the faying surfaces of the reinforcing component and the panel component together, cure the panel component, and form a reinforced panel.

[0006] The present disclosure also provides, in another embodiment, a method of forming a reinforced component, the method including: placing a first component formed from a consolidated material on a first side of a heated press, the consolidated material having a joining surface; placing a second component formed from an unconsolidated material on an opposing second side of the heated press, the unconsolidated material having a joining surface configured complementary to the joining surface of the consolidated material; and placing a second component formed from an unconsolidated material on an opposing second side of the heated press, the unconsolidated material having a joining surface configured complementary to the joining surface of the consolidated material. the first and second sides of the press are oriented toward one another such that the faying surfaces of the consolidated material are effective for co-bonding to the unconsolidated material; operating the press to orient the first and second sides of the press toward one another such that the faying surfaces of the consolidated material and the unconsolidated material complementarily engage under pressure; and heating the first and second sides of the press to a curing temperature associated with the unconsolidated material to substantially simultaneously co-bond the faying surfaces of the consolidated material and the unconsolidated material together, cure the unconsolidated material, and form a reinforced component.

[0007] The present disclosure further provides, in another embodiment, an apparatus for forming a reinforced panel, the apparatus comprising: a first planar platen having a planar surface, a second planar platen having a planar surface adapted to engage a panel component, the second planar platen operable with the first planar platen to apply pressure between the first and second planar platens, and an intermediate insert adapted to engage a reinforcing component, the intermediate insert having a planar first surface engageable with a planar surface of the first or second planar platen and an opposing second surface engageable and conformal with the reinforcing component, whereby pressure applied between the first and second planar platens to the reinforcing component and the panel component is uniformly distributed throughout the reinforcing component, and at least the intermediate insert and the first or second planar platen are heated.

[0008] The above and other features, aspects, and advantages of the present disclosure will become apparent upon reading the following detailed description in conjunction with the accompanying drawings, which are briefly described below. The present disclosure includes any combination of two, three, four, or more elements described in the disclosure or recited in any one or more claims, regardless of whether such features or elements are expressly combined or otherwise recited in a particular embodiment or claim herein. This disclosure is intended to be read in its entirety such that any separable features or elements of the disclosure, in any of its aspects and embodiments, should be considered as intended to be combined unless the context of the disclosure dictates otherwise.

[0009] Having described embodiments of the present disclosure in general terms above, reference is now made to the accompanying drawings, which are not necessarily drawn to scale. [Brief description of the drawings]

[0010] [Figure 1] 1 illustrates a reinforced panel according to some embodiments of the present disclosure. [Diagram 2] 1 illustrates an apparatus for forming a reinforced panel according to some embodiments of the present disclosure. [Diagram 3] 1 illustrates a method of forming a reinforced panel according to some embodiments of the present disclosure. [Figure 4] 1 illustrates a method of forming a reinforced component according to some embodiments of the present disclosure. DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS

[0011] Some embodiments of the present disclosure will now be described more comprehensively below with reference to the accompanying drawings. The accompanying drawings show some, but not all, of the embodiments of the present disclosure. Indeed, various embodiments of the present disclosure may be embodied in many different forms and should not be construed as being limited to the embodiments set forth herein. Rather, these examples are provided so that this disclosure will be comprehensive and complete, and will fully convey the scope of the disclosure to those skilled in the art. For example, unless otherwise specified, referring to something as being "first," "second," etc. should not be construed as implying a particular order. Also, something that may be described as being above something else (unless otherwise specified) may instead be below, and vice versa. Similarly, something that may be described as being to the left of something else may instead be to the right, and vice versa. Like reference numerals refer to like elements throughout.

[0012] Embodiments of the present disclosure are generally directed to methods and associated apparatus for forming a stiffened panel component. As shown in FIG. 1, for example, a stiffened panel component 100 is formed from the methods and apparatus disclosed herein. The stiffened panel component 100 has a cross-section having a size / shape that is dependent on its application in an aircraft structure in a particular embodiment. For example, the stiffened panel component 100 has a cross-section defining a channel with or without flanges (e.g., a "bell" or "hat" shape), hooks or "J" shapes, or one or more vertical or horizontal components (e.g., a vertical component sandwiched between two horizontal components or an "I" shape, a vertical component with a horizontal component at one end or a "T" shape), although any other shapes, sizes, types, etc. may be accommodated by embodiments of the present disclosure. As shown in FIG. 1, the stiffened panel component is a hat-shaped stiffened panel component formed by substantially simultaneously co-bonding the faying surfaces of the stiffening component and the panel component together and curing the panel component, as will be described in more detail below.

[0013] As described herein, a reinforcing component is considered to be a composite reinforcing component, such as a composite reinforcement, in certain aspects. In that case, the composite reinforcing component is formed by molding, stamping, etc., a composite material. The composite material of the reinforcing component is composed of or includes a resin reinforced with a reinforcing material. The reinforcing material includes, but is not limited to, man-made or natural fibers, including carbon fiber, glass fiber, glass spheres, mineral fibers, or other reinforcing materials. When fibers are used as reinforcing materials, for example, the fibers may be continuous or chopped, unidirectional, randomly oriented, or in the form of a weave, such as, but not limited to, a plain weave, a houndstooth weave, a basket weave, or a twill weave. For example, the resin may include a thermoplastic material, including, but not limited to, polyphenylene sulfide, polyaryletherketone (PAEK), polyetherketoneketone (PEKK), polyetheretherketone (PEEK), polyimide, polyetherimide, polyamide, polyamide-imide, polyester, polybutadiene, polyurethane, polypropylene, polysulfone, polyethersulfone, polyphenylsulfone, polyacrylamide, polyketone, polyphthalamide, polyphenylene ether, polybutylene terephthalate, polyethylene, polyethylene terephthalate, polyester-polyarylate (e.g., VECTRAN®), polytetrafluoroethylene (PTFE), or other thermosetting resins. Alternatively, the resin may include a thermosetting material, including, but not limited to, epoxy resin, cyanate ester, benzoxazine, polyimide, bismaleimide, vinyl ester, polyurethane, polyurea, polyurethane / polyurea blend, polyester, or other thermosetting resins. Likewise, a panel component may in certain aspects be considered to be a composite panel component, such as a composite skin panel.In that case, the composite panel component is formed from one or more composite materials that are comprised of or include a resin reinforced with a reinforcing material metal as described with reference to the reinforcing component, a matrix composite with a polymer skin, a glass aluminum composite with a polymer skin, or a titanium aluminum composite with a polymer skin.

[0014] In some examples, the reinforcing component is considered to be a non-consolidated component while the panel component is considered to be a consolidated panel component. In particular, substantially simultaneously co-bonding respective faying surfaces of the reinforcing component and the panel component together and curing the panel component (e.g., performing the co-bonding and curing steps substantially simultaneously) results in consolidation of the reinforcing component and the panel component to form a reinforced panel. As used herein, a faying surface is one of two or more surfaces that are in direct or indirect contact with each other and are connected to each other via bolts, rivets, welding, soldering, bonding, etc.

[0015] Thus, the methods and apparatus disclosed herein advantageously reduce the costs and cycle times associated with forming a lightweight, stiff, reinforced panel component. This is accomplished through the utilization of a heated press having two platens operable with one another, which allows the reinforcement component and the panel component to be co-bonded at their respective bonding surfaces while the panel component is cured (e.g., performing the co-bonding and curing procedures substantially simultaneously). In doing so, the separate cycles of curing the panel component and then bonding the reinforcement component and the cured panel component are combined into a single cycle through the use of the heated press.

[0016] Figure 2 illustrates one embodiment of an apparatus, generally designated by reference numeral 200, in a closed position for forming a reinforced panel. In some embodiments, the reinforced panel is the reinforced panel 100 shown in Figure 1, or in some other embodiments, is another type of reinforced panel. Indeed, reinforced panels of any size, shape, material, etc. can be formed using the apparatus shown in Figure 2. In some embodiments, the apparatus 200 includes a heated press having a first portion and an opposing second portion that are brought into engagement with one another (e.g., the first and second portions of the press move between an open position and a closed position).

[0017] In some embodiments, the apparatus 200 includes a first planar platen 202 or first portion having a planar surface 204. A second planar platen 206 or second portion has a planar surface 208 adapted to engage a second component or panel component 210. The panel component 210 is a composite thermoset skin panel composed of fibers (e.g., carbon fibers, particles, etc.) and a polymer resin matrix. Other composite materials for the panel component 210 are also contemplated. Thermoset skins are hardened by a curing process that occurs by heating the thermoset skin to a curing temperature, by radiation, etc., and is accelerated by high pressure.

[0018] In particular, to initiate curing of the thermosetting skin, the second planar platen 206 is operable with the first planar platen 202 to apply pressure therebetween. For example, the two platens 202, 206 are operatively engaged with or brought into contact with one another (e.g., by operating each platen simultaneously, by operating only one platen, or by operating each platen at a different time), whereby pressure is applied to the platens as a normal force (e.g., the first planar platen 202 applies a normal force to the second planar platen 206, and the second planar platen 206 applies an opposing normal force to the first planar platen 202). The pressure is between about 50 and about 150 pounds per square inch (psi). In that case, in some cases, the amount of normal force applied depends on the surface area of ​​the planar platens.

[0019] An intermediate insert or press member 212 is engageable with a reinforcing component 214. In some embodiments, the reinforcing component 214 is a reinforcement material for a composite thermoplastic or thermoset composite. When the reinforcing component is a composite thermoplastic reinforcing component, the composite thermoplastic reinforcing component softens when heated to a melting temperature associated with the composite thermoplastic material and then hardens when cooled.

[0020] The intermediate insert or press member 212 has a planar first surface 216 engageable with the planar surface 204, 208 of the first or second planar platen 202, 206, and an opposing second surface 218 engageable and conformal with the reinforcing component 214. The intermediate insert or press member 212 is thereby considered to be configured complementary to the planar or press surfaces 204, 208. As shown in FIG. 2, the planar first surface 216 of the intermediate insert 212 engages with the first planar platen 202, while the second surface 218 engages and conformal with the reinforcing component 214. In particular, the second surface 218 of the intermediate insert 212 has a contour corresponding to the contour of the reinforcing component 214. For example, the contour of the reinforcing component 214 is based on the shape of the reinforcing component 214. In that case, the reinforcing component 214 has a cross section shaped like a "bell", "hat", "I", "J", or "T". Thereby, the second surface 218 has contours that correspondingly receive the reinforcing component so shaped. By providing contours on the second surface 218 of the intermediate insert 212, pressure applied to the reinforcing component 214 and the panel component 210 between the first planar platen 202 and the second planar platen 206 is uniformly distributed throughout the reinforcing component 214. The apparatus 200 further includes a heating element 220 associated with at least the intermediate insert 212 and the first planar platen 202 or the second planar platen 206. The heating element 220 is positionable to heat at least the intermediate insert 212 and the first platen 202 or the second platen 206 to substantially simultaneously co-bond the reinforcing component 214 and the panel component 210 together, cure the panel component 210, and form a reinforced panel (e.g., 100 in FIG. 1 ).

[0021] In some embodiments, the intermediate insert 212 and the first platen 202 or second platen 206 are heated via an electrical connection to a power source (not shown) of the apparatus 200 while the intermediate insert 212 and the first platen 202 or second platen 206 are operatively engaged with one another and under pressure. For example, activation of the power source directs an electric current to a heating element 220, such as a heating rod, embedded within, integral with, or otherwise coupled to the intermediate insert 212 and / or the first platen 202 or second platen 206. The intermediate insert 212 and the first platen 202 or second platen 206 are then heated by the heating element 220 to a curing temperature associated with the panel component 210. The curing temperature of the panel component 210 depends on the material of the panel component, where different materials have different curing temperatures. For example, the intermediate insert 212 and the first platen 202 or the second platen 206 are heated to a cure temperature of between about 250 degrees Fahrenheit (F°) and about 500 degrees Fahrenheit (F°) for between about 25 minutes and about 50 minutes, where the panel component is a composite thermoset, substantially simultaneously co-bonding the faying surfaces 222, 224 of the reinforcing component 214 and the panel component 210, respectively, to cure the panel component 210 and form a reinforced panel. The cure temperature associated with the panel component 210 is a temperature below the melting temperature associated with the reinforcing component 214. In this manner, heating the panel component 210 and the reinforcing component 214 does not melt the reinforcing components, while curing the panel component 210.

[0022] In some embodiments, the reinforcing component 214 is treated before the first and second planar platens 202, 206 are operatively engaged. In particular, the faying surface 222 of the reinforcing component 214 and / or the faying surface 224 of the panel component 210 are treated, such as via application of a film, energetic surface preparation, etc., such that the faying surfaces 222, 224 are available for co-bonding to the panel component 210. The type of treatment applied to the faying surfaces 222, 224 depends on the material of the reinforcing component 214.

[0023] For example, if the reinforcing component 214 is a composite thermoplastic reinforcing component, a thermoplastic film 226 is applied to the faying surface 222 of the thermoplastic reinforcing component such that the faying surface 222 is available for co-bonding to the panel component 210. The thermoplastic film 226 includes at least one of polyetherimide (PEI), polyphenylene sulfide, polyimide, polyamide, polyamide-imide, polyester, polybutadiene, polyurethane, polypropylene, polysulfone, polyethersulfone, polyphenylsulfone, polyacrylamide, polyketone, polyphthalamide, polyphenylene ether, polybutylene, polybutylene terephthalate, polyethylene, polyethylene terephthalate, polyester-polyarylate, polytetrafluoroethylene (PTFE), or any combination thereof.

[0024] In another embodiment, when the reinforcing component 214 is a composite thermoset reinforcing component, an adhesion promoting film 228 is applied to the faying surface 222 of the composite thermoset reinforcing component 214 and / or an energetic surface treatment 230 is performed on the faying surface 222 of the composite thermoset reinforcing component 214 to make the faying surface 222 available for co-bonding to the panel component 210. The adhesion promoting film is comprised of an unfilled partially highly epoxy resin. The energetic surface treatment includes performing a corona treatment, plasma treatment, flame treatment, etc. on the faying surface 222 of the composite thermoset reinforcing component 214 to make the faying surface 222 available for co-bonding to the panel component 210.

[0025] In some embodiments, a suction mechanism (not shown) is utilized to apply suction to the apparatus 200 to remove any air or volatile matter trapped within the uncured panel component 210. Removing the air or volatile matter ensures a strong co-bond between the reinforcing component 214 and the panel component 210. In that case, any air or volatile matter would prevent a strong, secure co-bond at the mating surfaces 222, 224.

[0026] 2 thus provides for the reinforcing component 214 and the panel component 210 to be co-bonded together while simultaneously curing the panel component 210. In some aspects, the time period for doing so is shorter than conventional bonding methods, thereby providing significant cost savings and efficiencies.

[0027] 3 illustrates one embodiment of a method for forming a reinforced panel, where the method is generally designated by the reference numeral 300. In some instances, the reinforced panel is a panel such as that shown in FIG 1. Moreover, method 300 is performed using an apparatus such as apparatus 200 of FIG 2.

[0028] In step 302, molding (e.g., continuous compression molding (CCM)) or stamping of material is performed to form a reinforcement component (e.g., element 214 of FIG. 2). In step 304, collating the uncured plies of the panel component (e.g., element 210 of FIG. 2) is performed. In step 306, an apparatus (e.g., a heated press such as apparatus 200 of FIG. 2) is preheated to a preheat temperature. The preheat temperature is below the cure temperature associated with the panel component. For example, the press is preheated to between about 225° F. and about 475° F.

[0029] In step 308, a reinforcing component having a joining surface is engaged with a first portion of a heated press (e.g., element 202 in FIG. 2). In step 310, an uncured panel component is engaged with an opposing second portion of the press (e.g., element 208 in FIG. 2). The panel component has a joining surface configured complementary to the joining surface of the reinforcing component. In step 312, the joining surface of the reinforcing component is treated to make it effective for co-bonding. Notably, step 312 is optional and depends on the material of the reinforcing component.

[0030] In step 314, suction is applied to the press to remove any air or volatiles trapped within the uncured panel component. In step 316, the press is actuated to orient the first and second portions of the press toward one another, thereby causing the faying surfaces of the reinforcing component and the panel component to complementarily engage under pressure. In step 318, the first and second portions of the press are heated to a cure temperature associated with the panel component to substantially simultaneously co-bond the faying surfaces of the reinforcing component and the panel component together, cure the panel component, and form a reinforced panel.

[0031] Yet a further method of forming a reinforced component is provided in Figure 4. The method is generally referred to by reference numeral 400. The reinforced component is a panel, such as that shown in Figure 1. Method 400 is carried out using an apparatus, such as apparatus 200 of Figure 2.

[0032] In a first step, 402, a first component formed from a consolidated object having a joining surface is placed on a first side of a heated press. In a second step, 404, a second component formed from an unconsolidated object is placed on an opposing second side of the heated press. The unconsolidated object has a joining surface configured complementary to the joining surface of the consolidated object. In a third step, 406, the joining surface of the consolidated object is treated to be effective for co-bonding to the unconsolidated object. In a fourth step, 408, the press is operated such that the first and second sides of the press are oriented toward one another, thereby causing the joining surfaces of the consolidated object and the unconsolidated object to complementary engage under pressure. In a fifth step, the first and second sides of the press are heated to a curing temperature associated with the unconsolidated object to substantially simultaneously co-bond the joining surfaces of the consolidated object and the unconsolidated object together, cure the unconsolidated object, and form a reinforced component.

[0033] In some embodiments, operating the press such that the first and second sides of the press are directed toward one another includes applying a pressure of between about 50 and about 150 pounds per square inch (psi) to the consolidated and unconsolidated materials between the first and second sides of the press.

[0034] In some further embodiments, heating the first and second sides of the press to a curing temperature includes heating the first and second sides of the press to between about 250° F. and about 500° F. for between about 25 minutes and about 50 minutes to substantially simultaneously co-bond the faying surfaces of the consolidated and unconsolidated materials together, cure the unconsolidated materials, and form the reinforced component.

[0035] Numerous modifications and other embodiments of the disclosure set forth herein will occur to one skilled in the art to which this disclosure pertains having the benefit of the teachings presented in the foregoing description and the associated drawings. It is to be understood, therefore, that the disclosure is not limited to the particular embodiments disclosed, and that modifications and other embodiments are intended to be included within the scope of the appended claims. Moreover, while the foregoing description and the associated drawings describe exemplary implementations in the context of certain example combinations of elements and / or functions, it should be recognized that alternative example implementations may provide various combinations of elements and / or functions without departing from the scope of the appended claims. That is, combinations of elements and / or functions different from those expressly described above are contemplated, for example, as may be set forth in some of the appended claims. Although specific terms have been employed herein, they are used in a generic and descriptive sense only and not for purposes of limitation.

[0036] Article 1. 1. A method of forming a reinforced panel, the method comprising: engaging a reinforcing component with a first portion of a heated press, the reinforcing component having a faying surface; engaging an uncured panel component with an opposing second portion of the press, the panel component having a faying surface configured complementarily to the faying surface of the reinforcing component; treating the faying surface of the reinforcing component so that the faying surface of the reinforcing component is effective for co-bonding to the panel component; operating the press to orient the first and second portions of the press toward one another such that the faying surfaces of the reinforcing component and the panel component complementarily engage under pressure; and heating the first and second portions of the press to a cure temperature associated with the panel component to substantially simultaneously co-bond the faying surfaces of the reinforcing component and the panel component together, cure the panel component, and form the reinforced panel. Article 2. 2. The method of claim 1, wherein the reinforcing component comprises a thermoplastic or thermoset reinforcement and the panel component comprises a thermosetting skin, and heating the first and second portions of the press to the cure temperature comprises heating the first and second portions of the press to a cure temperature associated with the thermosetting skin to substantially simultaneously co-bond the faying surfaces of the thermoplastic or thermoset reinforcement and the thermosetting skin together, cure the thermosetting skin, and form the reinforced panel. Article 3. 3. The method of claim 1 or 2, wherein operating the press to orient the first and second portions of the press toward one another includes applying a pressure of between about 50 and about 150 pounds per square inch (psi) to the reinforcement component and the panel component between the first and second portions of the press. Article 4. 4. The method of any one of clauses 1 to 3, wherein heating the first and second portions of the press to the curing temperature includes heating the first and second portions of the press to between about 250°F and about 500°F for between about 25 minutes and about 50 minutes to substantially simultaneously co-bond the faying surfaces of the reinforcing component and the panel component together, cure the panel component, and form the reinforced panel. Article 5. 5. The method of any one of clauses 1 to 4, wherein the reinforcing component is a thermoplastic reinforcement and treating the joining surface of the thermoplastic reinforcement comprises applying a thermoplastic film to the joining surface of the thermoplastic reinforcement such that the joining surface of the thermoplastic reinforcement is available for co-bonding to the panel component. Article 6. 6. The method of claim 5, wherein applying the thermoplastic film to the faying surface of the thermoplastic reinforcement includes applying a film of polyetherimide (PEI), polyphenylene sulfide, polyimide, polyamide, polyamide-imide, polyester, polybutadiene, polyurethane, polypropylene, polysulfone, polyethersulfone, polyphenylsulfone, polyacrylamide, polyketone, polyphthalamide, polyphenylene ether, polybutylene, polybutylene terephthalate, polyethylene, polyethylene terephthalate, polyester-polyarylate, polytetrafluoroethylene (PTFE), or any combination thereof, to the faying surface of the thermoplastic reinforcement. Article 7. 7. The method of any one of clauses 1 to 6, wherein the reinforcing component is a thermosetting reinforcement and treating the joining surface of the reinforcing component comprises one or both of applying an adhesion promoting film to the joining surface of the thermosetting reinforcement and performing an energetic surface treatment on the joining surface of the thermosetting reinforcement so that the joining surface of the thermosetting reinforcement is effective for co-bonding to the panel component. Article 8. 8. The method of claim 7, wherein performing the energetic surface treatment on the joining surface of the thermosetting reinforcement comprises performing a corona treatment, a plasma treatment, or a flame treatment on the joining surface of the thermosetting reinforcement so as to render the joining surface of the thermosetting reinforcement effective for co-bonding to the panel component. Article 9. 9. The method of any one of clauses 1 to 8, further comprising applying suction to the press to remove any air or volatile materials trapped within the uncured panel components. Article 10. 10. The method of any one of clauses 1-9, further comprising preheating the press to a preheated temperature, the preheated temperature being less than the cure temperature associated with the panel component. Article 11. 11. The method of any one of clauses 1 to 10, wherein engaging the reinforcement component with the first part of the heated press comprises engaging a press surface of the reinforcement component opposite the joining surface of the reinforcement component with a press member configured complementarily to the press surface. Article 12. 12. The method of any one of clauses 1 to 11, wherein heating the first and second parts of the press to the cure temperature associated with the panel component comprises heating the first and second parts of the press to the cure temperature associated with the panel component, the cure temperature being less than a cure temperature associated with the reinforcing component. Article 13. 13. The method of any one of clauses 1 to 12, wherein engaging the reinforcing element with the first portion of the heated press comprises engaging the reinforcing element having a cross-section shaped as a “bell”, “hat”, “I”, “J”, or “T” with the first portion of the heated press. Article 14. 14. The method of any one of clauses 1 to 13, further comprising molding or stamping a material to form the reinforcement component prior to engaging the formed reinforcement component with the first part of the heated press. Article 15. 15. The method of any one of clauses 1-14, further comprising sequencing at least one of the uncured plies of the panel component prior to engaging the plies with the second portion of the press. Article 16. 1. A method of forming a reinforced component, comprising: placing a first component formed from a consolidated material on a first side of a heated press, the consolidated material having a joining surface; and placing a second component formed from an unconsolidated material on an opposing second side of the heated press, the unconsolidated material having a joining surface configured complementary to the joining surface of the consolidated material. treating the faying surfaces of the consolidated material to render them effective for co-bonding to the unconsolidated material; operating the press to orient the first and second sides of the press toward one another such that the faying surfaces of the consolidated material and the unconsolidated material complementarily engage under pressure; and heating the first and second sides of the press to a curing temperature associated with the unconsolidated material to substantially simultaneously co-bond the faying surfaces of the consolidated material and the unconsolidated material together, cure the unconsolidated material, and form the reinforced component. Article 17. 17. The method of claim 16, wherein operating the press to orient the first side and the second side of the press toward one another includes applying a pressure of between about 50 and about 150 pounds per square inch (psi) to the consolidated and unconsolidated materials between the first and second sides of the press. Article 18. 18. The method of claim 16 or 17, wherein heating the first side and the second side of the press to the curing temperature includes heating the first side and the second side of the press to between about 250°F and about 500°F for between about 25 minutes and about 50 minutes to substantially simultaneously co-bond the faying surfaces of the consolidated and unconsolidated materials together, cure the unconsolidated materials, and form the reinforced component. Article 19. 19. The method of claim 16-18, wherein the unconsolidated material comprises a thermoplastic or thermoset reinforcement and the consolidated material comprises a thermosetting skin, and heating the first side and the second side of the press to the cure temperature comprises heating the first side and the second side of the press to a cure temperature associated with the thermosetting skin to substantially simultaneously co-bond the faying surfaces of the thermoplastic or thermoset reinforcement and the thermosetting skin together, cure the thermosetting skin, and form the stiffened panel. Article 20. 20. The method of any one of clauses 16 to 19, wherein the unconsolidated material is a thermoplastic reinforcement material, and treating the faying surface of the thermoplastic reinforcement material comprises applying a thermoplastic film to the faying surface of the thermoplastic reinforcement material such that the faying surface of the thermoplastic reinforcement material is available for co-bonding to the consolidated material. Article 21. 21. The method of claim 20, wherein applying the thermoplastic film to the faying surface of the thermoplastic reinforcement includes applying a film of polyetherimide (PEI), polyphenylene sulfide, polyimide, polyamide, polyamide-imide, polyester, polybutadiene, polyurethane, polypropylene, polysulfone, polyethersulfone, polyphenylsulfone, polyacrylamide, polyketone, polyphthalamide, polyphenylene ether, polybutylene, polybutylene terephthalate, polyethylene, polyethylene terephthalate, polyester-polyarylate, polytetrafluoroethylene (PTFE), or any combination thereof, to the faying surface of the thermoplastic reinforcement. Article 22. 22. The method of any one of clauses 16 to 21, wherein the non-consolidated material is a thermosetting reinforcement material, and treating the joining surface of the non-consolidated material comprises one or both of applying an adhesion promoting film to the joining surface of the thermosetting reinforcement material and performing an energetic surface treatment on the joining surface of the thermosetting reinforcement material so that the joining surface of the thermosetting reinforcement material is effective for co-bonding to the consolidated material. Article 23. 23. The method of claim 22, wherein performing the energetic surface treatment on the joining surfaces of the thermosetting reinforcement includes performing a corona treatment, a plasma treatment, or a flame treatment on the joining surfaces of the thermosetting reinforcement such that the joining surfaces of the thermosetting reinforcement are effective for co-bonding to the consolidated mass. Article 24. 24. The method of any one of clauses 16-23, further comprising applying suction to the press to remove any air or volatile materials trapped within the unset mass. Article 25. 25. The method of any one of clauses 16-24, further comprising preheating the press to a preheated temperature, the preheated temperature being less than the hardening temperature associated with the consolidated mass. Article 26. 1. An apparatus for forming a reinforced panel, comprising: a first planar platen having a planar surface; a second planar platen having a planar surface adapted to engage a panel component, the second planar platen being operable with the first planar platen to apply pressure between the first and second planar platens; and an intermediate insert adapted to engage a reinforcing component, the intermediate insert having a planar first surface engageable with the planar surface of the first or second planar platen and an opposing second surface engageable and conformal with the reinforcing component, whereby the pressure applied to the reinforcing component and the panel component between the first and second planar platens is uniformly distributed throughout the reinforcing component; and at least the intermediate insert and the first or second planar platen are heated. Article 27. The apparatus described in clause 26, further comprising a heating element associated with at least the intermediate insert and the first planar platen or the second planar platen, the heating element being positioned to heat at least the intermediate insert and the first planar platen or the second planar platen to substantially simultaneously co-bond and cure the reinforcing component and the panel component together, cure the panel component, and form the reinforced panel. Article 28. 28. The apparatus of claim 26 or 27, wherein the reinforcing component comprises a thermoplastic or thermoset reinforcement and the panel component comprises a thermoset skin. Article 29. 29. The apparatus of any one of clauses 26 to 28, wherein the reinforcing component is a thermoplastic reinforcement material. Article 30. 30. The apparatus of any one of clauses 26 to 29, wherein the reinforcing component is a thermoset reinforcing material.

Claims

1. 1. A method of forming a reinforced panel, comprising the steps of: engaging a reinforcement component with a first portion of a heated press, the reinforcement component having a joining surface; engaging an uncured panel component with an opposing second portion of the press, the uncured panel component having an interface surface configured complementary to the interface surface of the reinforcing component; treating the faying surfaces of the reinforced components such that the faying surfaces are effective for co-bonding to the uncured panel component; operating the press to orient the first and second portions of the press toward one another such that the faying surfaces of the reinforcement component and the uncured panel component complementarily engage under pressure; and heating the first and second portions of the press to a cure temperature associated with the uncured panel component, the cure temperature being less than a cure temperature associated with the reinforcing component, to simultaneously co-bond the faying surfaces of the reinforcing component and the uncured panel component together, curing the uncured panel component, and forming the reinforced panel.

2. 2. The method of claim 1, wherein the reinforcing component comprises a thermoplastic or thermoset stiffener and the uncured panel component comprises a thermosetting skin, and heating the first and second portions of the press to the cure temperature comprises heating the first and second portions of the press to a cure temperature associated with the thermosetting skin to simultaneously co-bond the faying surfaces of the thermoplastic or thermoset stiffener and the thermosetting skin together, cure the thermosetting skin, and form the stiffened panel.

3. 3. The method of claim 1 or 2, wherein operating the press to orient the first and second portions of the press toward one another comprises applying a pressure of between 50 pounds per square inch (psi) and 150 psi to the reinforcement component and the uncured panel component between the first and second portions of the press.

4. 4. The method of claim 1, wherein heating the first and second parts of the press to the curing temperature comprises heating the first and second parts of the press to between 250°F and 500°F for between 25 minutes and 50 minutes to simultaneously co-bond the faying surfaces of the reinforcing component and the uncured panel component together, cure the uncured panel component, and form the reinforced panel.

5. 5. The method according to claim 1, wherein the reinforcing component is a thermosetting reinforcement and treating the faying surface of the reinforcing component comprises one or both of applying an adhesion promoting film to the faying surface of the thermosetting reinforcement and performing an energetic surface treatment on the faying surface of the thermosetting reinforcement so that the faying surface of the thermosetting reinforcement is effective for co-bonding to the uncured panel component.

6. 6. The method of claim 5, wherein performing the energetic surface treatment on the joining surface of the thermosetting reinforcement comprises performing a corona treatment, a plasma treatment, or a flame treatment on the joining surface of the thermosetting reinforcement so that the joining surface of the thermosetting reinforcement is effective for co-bonding to the uncured panel component.

7. 7. The method of claim 1, further comprising applying suction to the press to remove air or volatiles trapped within the uncured panel components.

8. 8. The method of claim 1, further comprising preheating the press to a preheated temperature, the preheated temperature being less than the cure temperature associated with the uncured panel component.

9. 9. The method according to claim 1, wherein engaging the reinforcement component with the first part of the heated press comprises engaging a press surface of the reinforcement component opposite the joining surface of the reinforcement component with a press member configured complementarily to the press surface.

10. 10. The method of claim 1, wherein engaging the reinforcement component with the first portion of the heated press comprises engaging the reinforcement component with a cross-section shaped as a "bell", "hat", "I", "J", or "T" with the first portion of the heated press.

11. 11. The method of claim 1, further comprising molding or stamping a material to form a reinforcement component prior to engaging the formed reinforcement component with the first portion of the heated press.

12. 12. The method of claim 1, further comprising sequencing at least one of the uncured plies of the uncured panel component prior to engaging the plies with the second portion of the press.

13. 1. An apparatus for forming a reinforced panel, comprising: a first planar platen having a planar surface; a second planar platen having a planar surface adapted to engage a panel component, the second planar platen being operable with the first planar platen to apply pressure between the first planar platen and the second planar platen; an intermediate insert adapted to engage a reinforcing component, the intermediate insert having a planar first surface engageable with the planar surface of the first planar platen or the second planar platen and an opposing second surface engageable with and conforming to the reinforcing component, whereby the pressure applied to the reinforcing component and the panel component between the first planar platen and the second planar platen is uniformly distributed throughout the reinforcing component; An apparatus wherein at least the intermediate insert and the first planar platen or the second planar platen are heated to a cure temperature associated with the panel component, the cure temperature being less than a cure temperature associated with the reinforcing component.

14. 14. The apparatus of claim 13, further comprising a heating element associated with at least the intermediate insert and the first planar platen or the second planar platen, the heating element positioned to heat at least the intermediate insert and the first planar platen or the second planar platen to simultaneously co-bond and cure the reinforcing component and the panel component together, cure the panel component, and form the reinforced panel.

15. The apparatus of claim 13 or 14, wherein the reinforcing component comprises a thermoplastic or thermoset reinforcement material and the panel component comprises a thermoset skin.

16. An apparatus as described in any one of claims 13 to 15, wherein the reinforcing component is a thermoplastic reinforcing material.

17. An apparatus as described in any one of claims 13 to 16, wherein the reinforcing component is a thermosetting reinforcing material.

Images