STRUCTURAL PANEL AND METHOD TO PRODUCE IT

Abstract: A process for fabricating panels of a core material with thermoplastic resin facings. The core material is either foam or a honeycomb structure from aramid paper. A belt press machine provides a means for rapid heating and cooling such that the core will not degrade. Since the process is so rapid, aramid fibers can be used to reinforce the resin facings without deleterious decomposition of the fibers under the temperatures used to heat the panels during forming.

Description: TI TLE Structural panel and method to produce it BACKGROUND OF THE INVENTION This invention relates to a method for rapidly forming structural panels having a core faced with thermoplastic resin facings. In the manufacture of composite panels with resin facing material bonded to core structures, it has been the practice to use facing materials made with thermosetting resins which are cured as the panel is consolidated in an autoclave, oven or press which is a costly and a time-consuming operation. Attempts to use high performance thermoplastic resin sheet material as facings for these panels require higher processing temperatures than thermoset resins. This leads to decomposition of core materials and to panels with low adhesion between the facings and the core material when the facings are resin reinforced with fibers. SUMMARY OF THE INVENTION According to the method of this invention, a composite structure is formed from a core and ε thermoplastic resin sheet material by bonding the thermoplastic resin sheet material to at least one side of the core by passing the core and the thermoplastic resin sheet material in mating surface contact through a belt press for a residence time of less than 2.3 min. under a positive pressure, while heating the core and the thermoplastic sheet material to a temperature of from about 480°F to a out 710°F in the belt press and cooling the core and the sheet material in the belt press while maintaining said positive pressure. The residence time and process temperature are adjusted to give optimum resin impregnation while minimizing core or organic fiber facing reinforcement degradation. Another embodiment of the invention is a panel formed by the .above method that includes a core member and a fiber reinforced thermoplastic resin sheet material bonded to at least one side of the core member to form a facing therefor. The thermoplastic resin is between 30 to about 65 weight percent of the facing. The peel strength or adhesion between the facing and the core is greater than 10 lbs./3" sample. Useful cores are honeycomb structures of aramid paper, aluminum or glass fibers and foams such as poly ethacrylimide and polyetherimide foams or polyurethaneε and polyisocyanurate foams. Suitable thermoplastic resins include polyesters, polyamides, copolyamides polyolefins and polyetherketoneketone (PEKK) both amorphous and se icrystalline . The polyaryletherketone resin consists of repeating units (as disclosed in U.S. Patent No. 4,937,135) of 1,4 phenylene groups (T, terephthalyl groups) and 1,3 phenylene groups (I, isophthalyl groups); the T:I ratio being 50:50 to 80:20, preferably 60:40 to 70:30. Polyetheretherketone (PEEK) Stabar™ from ICI, polyetherimide (PEI) Ultem™ from GE, and polyethersulfone (PES) Radel τκ X from Amoco. The ratio of resin to reinforcement can vary. Such properties as peel strenqth increase linearlv with increasing resin content. However, extra resin adds weight to the finished panel which is un es ra e n aerospace app ca ons. e preferred resin contents are similar tc the corresponding thermoset values for self-bonding prepregs, i.e. about 50% by weight for c - reinforcement with fabrics of Kevlar™ aramid fibers, about 45% by weight for woven carbon fiber facings and about 40% by weight for fiberglass facings. For panels with maximum bending stiffness, the thermoplastic resin and fiber 0 reinforcement may be consolidated in a separate step under high pressure before bonding to the core in the method described above. Useful fibers for reinforcing the thermoplastic resin facings are carbon, aramid and 5 glass fibers. BRIEF DESCRIPTION OF THE DRAWINGS Fig. 1 is a schematic side view of a belt press suitable for practicing the method of this 0 invention. Fig. 1A is a schematic side view of a batch mode operation. Fig. 2 is a schematic side view of a continuous mode operation. κ Fig. 3 is a schematic side view showing a honeycomb core and facings entering the nip of a belt press. Fig. 4 is a photomicrograph of a partial elevation view in cross section of a panel formed 0 with a honeycomb core of aramid paper. Fig. 5 is a schematic side view showing a foam core and facings entering the nip of a belt press. Figs. 6 and 7 are schematic illustrations of a partial elevation view in cross section of a panel formed with foam cores of thermoplastic and non-thermoplastic foam, respectively. Fig. 8 is a schematic illustration plan view of a panel having a form edge trim for a honeycomb core. Fig. 9 is a section of Fig. 8 taken along the line 9-9. DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENT In Fig. 1 the belt press has been designated generally by the numeral 10 and shown to include substantially identical upper and lower sections 12 and 14, respectively, that are aligned one above the other. Each section includes a pair of belt rolls 11, 13 on the upper and 15, 17 on the lower. The rolls are rotatably mounted to frame (not shown). Traveling around rolls 11, 13 is a metal alloy belt 18 and around rolls 15 and 17 an identical belt 20. Both belts coact to form a constant height nip section within the frame hereafter referred to as the heating and cooling zone 22. Each belt is supported on its back side in the zone 22 by a stationary antifriction bearing 24 sandwiched between the stationary zone and the moving belts. Belt tension rolls 28, 30 are mounted for rotatable and vertical movement as indicated by the direction arrows. The belts are driven in the direction of the arrows by conventional drive means (not shown). Each zone 22 is composed of heating sections 32, 34, and cooling sections 36 separated by thermal barriers 38. The zones are attached to the frame with mechanical shims 26, 26a_ in a fashion to allow vertical positioning for maintaining a constant spacing between the belts. There are nvmerous heating and cooling concepts practiced by commercial belt press suppliers. Heating systems use an electrical heat source to generate heat and then carry the heat to c the belt via pneumatic, hydraulic and regular conduction techniques. The source of cooling iε usually a water supply with the heat being carried from the belt by pneumatic, hydraulic and conductive sytems. In order to provide capability for the belt press to operate at temperatures above 540°F the static anti friction bearings 24 of woven screen must be permanently impregnated with either a dried graphite paste, a dried molylube 5 N(molybdenum) paste or a graphite sheeting, which are all high temperature and low volatility substrates which fill the voids in the screen. The bearing surface must then be coated periodically with a high temperature and low volatility 0 lubricant such as C5A (Fel Pro, Inc., Skokie, II), a copper based lubricant, Molylube-16 (Bel-Ray Co., Inc., Farmingdale, NJ) , a molybdenum based lubricant; or Krytox™ paste (Du Pont), a fluorinated lubricant. In a batch mode of operation shown in Fig. 1A, a layup consisting of a core member 50 and facings 50a_ comprised either of preimpregnated fiber reinforced sheets or sheets of thermoplastic resin and fabrics of high performance fibers 0 (glass, aramids or carbon) 50 is introduced from platform 49 i to the nip between the belts 18 and 20. If necessary, a release film 52 is unrolled from the supply roll 51 to cover belts 18 and 20. The facings are bonded to the core as the layup passes through zone 22 of Fig. 1 under a positive pressure created by the difference in the opening between the belts and the thickness of the core and its facings. Usually the bonding pressure is limited by the compressive strength of the core at the processing temperature. A stationary platen press of the type known to one skilled in the art o could also be used to heat and bond the facing 50a_ to the core 50. While Fig. 1A shows a system set up for a batch mode of operation, it is to be understood 0 that a (single step) continuous mode of operation could be obtained as disclosed in Fig. 2 wherein a continuous core 50' is fed to the nip of the belt press 10 from platform 49. Upper and lower facings 60, 62, respectively, are formed from a reinforcing 5 fabric 64, sandwiched between thermoplastic resin sheets 66, 68 (in the case of upper facing 60) and 64a_ sandwiched between thermoplastic resin sheets 65, 67 (in the case of lower facing 62) a release film 70 such as Kapton™ is fed between the upper 0 and lower facings and the belts of the belt press 10. Kapton™, aluminum or Teflon™ coated glass fabric are needed for a release agent with certain thermoplastic sheets but may not be required by others. The panels are formed in the belt press in 5 substantially the same manner as described above except the operation is continuous. Panels made according to the above procedure are then tested for damage tolerance via the climbing drum peel test (ASTM D781-76; 0 reapproved 1986). Panels exhibiting at least 10 pounds of peel per 3" sample have sufficient damage tolerance for use in aircraft interiors. If higher peel strengths are desired with honeycomb of Nomex™, crushed-core panels can be made. With the 5 above technology, peel strengths can be enhanced by as much as 3-4 times versus noncrushed core oanels. This is because the bonding surface area has been increased. More particularly, as shown in Fig. 3, a honeycomb core member 50'' is introduced into the nip between belts 18, 20 along with a fiber _ reinforced resin facing 51'. As they pass through the nip under positive pressure, the cell walls of the honeycomb structure are folded into hooklike configurations pointed generally in a direction opposite to the direction of movement of the core, 0 thus increasing the surface area of the honeycomb structure contacting the facings 52'. With the new thermoplastic facing technology, the core is heated above its softening point such that the cells are crushed much more uniformly than with conventional 5 thermoset crushed-core panels which have considerable cell damage after panel fabrication leading to a decrease in certain physical properties such as bending stiffness. An alternate embodiment using a foam core is shown in Fig. 5 wherein a foam core member 50''' is introduced into the nip between belts 18 and 20 along with a fiber reinforced resin facing 52'' . If- the foam is thermoplastic in nature, as shown in Fig. 6, a strong bond 54 is formed between D the foam and the facing resin as defined by peel strength exceeding 30 lbs./3" width. This strong bond results from fusion bonding (i.e. melting together of the facing resin and the melted foam surface) between the resin and the foam at the 0 interface. The heat from the belt press melts the surface of the foam as seen by thickening of the foam cell walls near the interface. The heat is not applied long enough to penetrate through the thickness of the foam, therefore, the foam interior remains intact. Examples of foams which will bond to thermoplastic PEKK resin in this manner are polymethacrylimide foams (Rohacell ") and polyetherimide foams (Airex™). If the foam is not thermoplastic in nature, as shown in Fig. 7, a strong bond 54' is formed between the foam and facing resin which results from flow of the PEKK polymer into the cells at the interface, resulting in a bond of increased surface area at the interface. The resin flows into and around the surface cell walls of the foam core. The strong bond is characterized by peel strength of greater than 25 lbs./3" width. Examples of foams which will bond to PEKK resin in this manner are polyurethanes and polyisocyanurateε (Last-A-Foam™ ) . In addition to being used as core materials, these foam materials have been demonstrated for use as an edge trim to honeycomb- cored sandwich panels as shown in Figs. 8 and 9. The foam edge trim member acts as a barrier to moisture for the honeycomb, as a location for fastener attachment, and also as a smooth edge finish for an aircraft part. The foam edge 50''' is held in- place around the honeycomb core member 50'' for processing by a variety of methods. In the preferred method a screw 56 is used to mechanically fasten the foam strips together at each splice point. Other types of fasteners at the splice point which have been demonstrated include Kapton™ tape or fast drying adhesives. Ultrasonic bonding of the face sheets to the core or a wooden frame around the edges of the panel have been demonstrated as techniques to hold the foam in place without fasteners. EXAMPLES ExamD —le 1 The components of the laminate were dried for at least 2 hours at 120°C and then laid up in the following manner. Three pieces of amorphous (60/40 T/I) PEKK film (1.5 mils thick, 150 melt index aε measured by ASTM 1238-79 procedures) were placed on the core bonding side of Kevlar™ 49 aramid fiber (by Du Pont) Style 285 fabric (5.1 10 oz./sq. yd., 9 mils thick) and one piece on the belt contact side to form the top facing. The bottom facing consisted of a balanced 2 pieces of film on each side of the Kevlar™ . The resin percentage by weight of the facings was 54%. The facings were placed on each side of a piece of honeycomb of Nomex™ aramid paper (by Du Pont) (3 lbs./cu. ft., 1/8" cell, 1/2" thick). The warp direction of the fabric was aligned with the ribbon direction of the core. The warp face of the fabric 20 was placed against the core. The facing layers were anchored to the core material with two 1" wide Kapton™ tape strips along the leading edge of the sample. The belt press (substantially as shown in Fig. 2) was set to a constant temperature of 650°F £ " J and a belt speed of 15" per min. (approximately 32 sec. residence time in the heat zone). The gap between the upper and lower belts was fixed to give a panel thickness of 0.518". A Kapton™ polyimide release sheet (by Du Pont) was placed over both 30 sides of the entire laminate. The front edge of the sample, perpendicular to the warp direction of the facing fabric and containing the Ke on™ tape anchors, was inserted into the belt press. Once consolidated, the Kapton release film and tape 5 anchors were removed from the sample. The panel was cut into three 3" x 12" samples (length perpendicular to the warp direction). Peeling the 3 ply PEKK/Kevlar™/1 ply PEKK facing from the core gave an average peel strength of 28.4 lbs./3" sample. Example 2 The components of the laminate were dried for at least 2 hours at 120°C and then laid up in the following manner. Two pieces of amorphous (60/40 T/I) PEKK film (1.5 mils thick, 150 melt index as measured by ASTM 1238-79 procedures) were placed on each side of Style 7781 glass (9 mils thick). The facesheet was consolidated at belt press conditions of 650°F and 15"/min. belt speed (about 32 sec. in the heating zone). The gap between upper and lower belts was adjuεted to give a sample thickness of 0.012". A second facesheet was consolidated in an identical fashion. The resin percentage by weight of the facings was 39%. The described facings were then placed on each side of a piece of honeycomb of Nomex™ (3 lbε./cu. ft., 1/8" cell, 1/2" thick). The facings were anchored to the core material with two 1" wide Kapton™ tape strips along the leading edge of the sample. The belt press was set to a constant temperature of 625°F and a belt speed of 15" per min. (residence time approximately 32 sec. in the heat zone) . The gap between the upper and lower belts was fixed to give a sample thickness of 0:516". A Kapton™ release sheet was placed over both sides of the entire laminate. The front edge of the sample, perpendicular to the warp direction of the facing fabric and containing the Kapton™ tape anchors, was inserted into the belt press. The belt press conditions were then adjusted to a constant 500°F and 3.5"/min. (residence time about 2.3 min. in the eat zone) belt speed and the panel was inserted as before. Once consolidated, the Kapton™ release film and tape anchors were removed from the sample. The panel was cut into three 3" by 8" samples (length parallel to the core ribbon 5 direction). The specimens gave an average short beam shear value of 100 psi. Example 3 The components of the laminate were dried 0 for at least 2 hours at 120°C and then laid up in the following manner. Two pieces of amorphous (60/40 T/I) PEKK film (1.5 mils thick, 180 melt index) were placed on each εide of a Kevlar™ Style 281 fabric, 5.1 oz./sq. yd., 10 mils thick, to form 5 the facing. To achieve a sample size of 14" x 17", 6.5" strips of the above mentioned amorphous PEKK film were concurrently placed over a 14" x 17" piece of core material being careful not to overlap film edges. Identical facings were placed on each 0 side of a piece of honeycomb of Nomex™ (3 lbs./cu. ft., 1/8" cell, 1/2" thick). The warp direction of the fabric was aligned with the ribbon direction of the core. • The facing layers were anchored to the core material with two 2" wide Kapton™ tape strips 5 along the leading edge of the sample. The belt press was set to a constant temperature of 650°F and a belt speed of 12" per min. (residence time approximately 48 sec. in the heat zone). The gap between the upper and lower belts was set to 0 achieve a total sample thickness of 0.36" (70% of the theoretical thickness). A Kapton™ release sheet was placed over both sides of the entire laminate according to the above described procedure. The front edge of the sample, ~ perpendicular to the warp direction cf the facing fabric and containing the Ka: on κ tape anchors, was inserted into the belt press. The Kapton™ release film and the tape anchors were removed from the sample. The average sample thickness, aε measured by a micrometer, was found to be 0.387". Three 3" x 12" samples (long direction perpendicular to the warp direction) were cut from the sample. The average peel strength was determined to be 56 lbε./3" sample. Example 4 The components of the laminate were dried for at least 2 hours at 120°C and then laid up in the following manner. Two pieces of polyethermide Ultem™ film were placed on each side of a Kevlar™ Style 281 fabric, 5.1 oz./sq. yd., 10 mils thick, to form the facing. Identical facings were placed on each side of a piece of honeycomb of Nomex™ (3 lbs./cu. ft., 1/8" cell, 1/2" thick). The warp direction of the facing fabric was aligned with the ribbon direction of the core. The facing layers were anchored to the core material with two 1" wide Kapton™ tape strips along the leading edge of the sample. The belt press was set to a constant temperature of 650°F and a belt speed of 15"/min. (residence time about 32 sec. in the heat zone). The gap between the upper and lower belts was set to achieve a total sample thickness of 0.44" (85% theoretical gap) . A Kapton™ release sheet was placed over both sides of the entire laminate according to the above described procedure. The front edge of the sample, perpendicular to the warp direction of the facing fabric and containing the Kapton™ tape anchors, was inserted to the belt press. The Kapton™ release film and the tape anchors were removed from the sample. A Climbing Drum Peel test was performed on three samples and had an average result of 11.0 lbs./3" εample. Exampl e 5 The components of the laminate were dried for at least 2 hours at 120 ' Z and then laid up - n the following manner. Two p ieces of 70/30 T/I, PEKK film were placed on the top side of a Kevlar™ 49 Style 281 fabric (5.1 oz./sq. yd., 10 mils thick) and two pieces of 60/40 T/I PEKK film (180 melt index as measured by ASTM 1238-79) on the bottom to form the facing. The percentage of r- sin by weight was about 49. Identical facings were placed on each side of a piece of honeycomb of Nσmex™ (3 lbs./cu. ft., 1/8" cell, 1/2" thick). The 60/40 T/I film was placed next to the honeycomb core on both sides. To achieve a sample size of 13" x 17", 6.5" strips of the above mentioned amorphous PEKK films were concurrently placed over a 14" x 17" piece of the core material being careful not to overlap film edges. The warp direction of the fabric was aligned with the ribbon direction of the core. The facing layers were anchored to the core material with two 1" wide Kapton™ tape strips along the lead i ng edge of the sample. The belt press was set to constant temperature of 650°F and a belt speed of 15"/min. (residence time approximately 32 sec. in the heat zone). The gap between the upper and lower belts was fixed to 0.360" (70% theoretical thickness;. A Kapton™ release sheet was placed over both sides of the entire laminate. The front edge of the sample, perpendicular to the warp direction of the facing fabric and containing the Kapton™ tape anchors, was inserted into the belt press. Once consolidated the Kapton™ release film and tape anchors were removed from the sample. The average sampl thickness, as measured by a micrometer, was found to be 0.365". Three 3" x 12" samples (length perpendicular to the warp direction) were cut from the sample. The peel strength was determined to be 27 lbs./3" sample. Example 6 The components of the panel were dried for at least 2 hours at 120°C and then laid up in the following manner. Three pieces of amorphous polyetheretherketone ■ (PEEK) film (Stabar K200-782), 1.06 oz./sq. yd., melt index 19 @ 360°C as measured by ASTM 1238-79 procedures, were laid over a piece of 1/2" thick No ex honeycomb core. Then a piece of 7781 glass fabric was placed atop the film layers with the warp direction of the fabric parallel to the core ribbon direction and the warp face towards the core. Three more layers of film were then placed on the fabric. This layup was intended to produce a resin content on the face sheets of approximately 41%. The film and fabric stacked layup was duplicated on the reverse side of the core. The layers of film and fabric were anchored to the core by ultrasonic welder along the leading edge of the panel. The belt press was set to a constant temperature of 680°F and a belt speed of 15" per min. (about 32 sec. residence time in the heat zone). The gap between the belts was adjusted to give a product thickness of .44", or 85% of the theoretical thickness expected. A Kapton™ release sheet was placed over both sides of the entire laminate. The laminate was placed into the belt preεε such that the ribbon direction of the core was parallel to the machine direction, with the edge that had been ultrasonic spot welded entering the belt press first. After consolidation, the release sheets were removed from the surfaces of the laminate. Three 3" x 12" sampleε were cut from the panel, length perpendicular to the core ribbon direction. The average peel εtrength of the three samples was found to be 15 lbs./3" sample. Example 7 The components of the laminate were dried for at least 2 hours at 120°C and then laid up in the following manner. Two pieces of amorphous (60/40 T/I) PEKK film (130 melt index as measured by ASTM 1238-79 procedures) were placed on each side of a Kevlar™ 49 Style 281 fabric, 5.1 oz./sq. yd., 10 mils thick, to form the facing. The percentage of resin by weight was calculated to be 51%. Identical facingε were placed on each side of a piece of honeycomb of aluminum (3 lbε./cu. ft., 1/8" cell, 1/2" thick). To achieve a sample size of 13" x 17", 6.5" strips of the above mentioned amorphous PEKK film were concurrently placed over a 14" x 17" piece of the core material being careful not to overlap film edges. The warp direction of the fabric was aligned with the ribbon direction of the core. The facing layers were anchored to the core material with two 1" wide Kapton™ tape εtrips along the leading edge of the εample . The belt press was set to a constant temperature of 650°F and a belt speed of 15"/min. (residence time approximately 32 sec. in the heat zone). The gap between the upper and lower belts was fixed to give a sample thickness of 0.516". A Kapton™ release sheet was placed over both sides of the entire laminate. The front edge of the sample, perpendicular to the warp direction of the facing fabric and containing the Kapton™ tape anchors, was inserted into the belt press. Once consolidated the Kapton r' release film and tape anchors were removed from the sample. The average sample thickness, as measured by a micrometer, was found to be 0.523" . Three 3" x 12" εamples (length perpendicular to the warp direction) were cut from the sample. The peel strength waε determined to be 11.9 lbs./3" sample. Example 8 The components of the laminate were drid for at least 2 hours -at 120°C and then laid up in the following manner. Two pieceε of amorphouε (60/40 T/I) PEKK film (150 melt index) were placed on either side of a Kevlar™ Style 281 fabric, 5.1 oz./sq. yd., 10 mils thick, to form the panel facings. One inch wide strips of 1/2" thick foam (Last-A-Foam™ FR-10118 polyisocyanurate by General Plastics Mfg. Co., Tacoma, WA) were cut from a sheet of foam and assembled into a frame with outer dimensions measuring 12" x 16". The strips of foam were held together using a rigid wooden frame with inner dimensions of 12" x 16". A piece of Nomex™ honeycomb core cut exactly to 10" x 14" was fitted into the center of the frame. The identical facings described above were then placed on each side of the foam-framed Nomex™ honeycomb εuch that the warp direction of the fabric ran in the ribbon direction of the honeycomb core. One inch wide εtrips of Kapton™ tape were used to anchor the facings to the frame along the leading edge of the sample. The belt press was set to a constant temperature of 650°F with a belt speed of 15"/min. (residence time approximately 32 εecε. in the heat zone). The gap between the upper and lower beltε waε εet to produce a finiεhed εample thickneεε of 0.516" or 100% of the theoretical thickneεs. The front edge of the εample with the Kapton™ tape anchors) was inserted into the belt press. This sample was covered with Kapton™ film aε a releaεe agent to prevent the sample from sticking to the belts. Once consolidated the Kapton™ release film and tape anchors were removed from the sample. The m. finished panel edges were trimmed, leaving 1/2" width of foam around the panel. The average thickness of the foam trimmed portion of the panel, as measured by a micrometer, was 0.507" and the average thickness of- the honeycomb cored portion of 0 the sample was measured to be 0.494". Example 9 The components of the laminate were dried for at least 2 hours at 120°C and then laid up in the following manner. Identical panel facings as 5 described in Example 8 were laid up. 1.5" εtrips of 1/2" thick foam (Rohacell™ 200 WF polymethacrylimide by Rohm Tech, Inc., Maiden, MA) • re cut from a foam sheet and assembled into a ϋame with outer dimensions measuring 12" x 12". 0 The strips of foam were anchored together using T M T M Kapton tape. A piece of Nomex honeycomb core cut exactly to 9" x 9" dimensions waε fitted into the center of the frame. The identical facingε were placed on either side of the foam-framed ^ Nomex™ honeycomb with the warp direction of the fabric parallel to the ribbon direction of the honeycomb core. The Kapton™ tape waε used to anchor the facings in place along the leading edge of the sample. The belt press was set to a 0 constant temperature of 650°F with a belt speed of 15"/min. (residence time about 32 sec. in the heat zone). The gap between the upper and lower beltε was set to produce a finished sample thickneεs of 0.516". The panel waε then consolidated in the Ξ belt press using Kapton™ release film. After processing, the Kapton™ film and tape were removed. This sample was then reprocessed to apply a decorative laminate to one side of the panel. The belt press was set to a constant temperature of 250°F and 6"/min. ( reεidence time about 80 sec. in the heat zone). The panel waε consolidated using Kapton release film which was removed after processing. The finished average thickness of the foam was measured to be 0.521" and the honeycomb core thickness was 0;516". Example 10 The components of the laminate were dried for at least 2 hourε at 120°C and then laid up in the following manner. Two pieces of amorphous (60/40 T/I) PEKK film (150 melt index) were placed on either side of a Kevlar™ Style 281 fabric, 5.1 oz./sq. yd., 10 mils thick, to form the panel facings. Dimensions of the fabric and film measured 16" x 25". A piece of foam core (Rohacell™ 200 WF polymethacrylimide ) was cut to these same dimensionε. The facingε were placed on either side of the foam and anchored in place uεing two 1" wide Kapton™ tape anchorε along the leading edge of the sample. The warp direction of the fabric was aligned along the length (25") direction of the panel. The belt presε waε set to a constant temperature of 650°F with a belt speed of 15"/min. (residence time about 32 sec. in the heat zone). The gap between the upper and lower beltε was set to produce a finished sample thickness of 0.516" or 100% of the theoretical thicknesε. The leading edge of the sample waε inεerted into the belt preεε. A Kapton™ releaεe film waε uεed when processing the εample. After conεolidation the release film and tape anchorε were removed. The average sample thickness, as measured by the micrometer, waε 0.540". This panel was cut into five 3" x 24" strips for long beam flex evaluation as described in test Boeing Mil. Spec. 256, page 29. The average flex strength waε determined to be 14.7 kεi at maximum machine deflection. An identical sample was manufactured but with the warp direction of the fabric perpendicular to the length of the foam cored panel. This sample was cut into 3" x 12" samples for climbing .drum peel evaluation. The average peel strength waε determined to be 33 lbε. per 3" sample. Example 11 The components of the laminate were dried for at least 2 hours at 120°C and then le i up in the following manner. Identical facingε aε described in Example 9were placed on each side of a piece of foam (Last-A-Foam™ FR 3718 polyurethane) measuring 16" x 25" with the warp direction of the fabric parallel to the length of the panel. Two Kapton™ tape strips were used to anchor the facings to the core along the leading edge of the panel. The panel was consolidated using a constant belt press temperature of 600°F and a constant belt speed of 12"/min. (residence time about 48 sec. in the heat zone). Kapton™ release film was used during consolidation. After consolidation the release film and tape anchors were removed. The average panel thickness was measured to be 0.541". This panel was cut into samples for long beam flex evaluation. The average flex strength was determined to be 13 kεi at maximum machine deflection. An identical sample was manufactured with the warp direction perpendicular to the length of the panel for climbing drum peel evaluation. Manufacturing conditions for this sample were 650°F belt tempe.rature and 15"/min. belt speed (residence me a ou sec. n e ea zone . e average peel strength was determined to be 27 lbs./3" sample . Example 12 The components of the laminate were dried for at least 2 hours at 120°C and then laid up in the following manner. Identical facings of amorphous (60/40) PEKK film and Kevlar™ fabric Style 281 were placed on either side of a foam (Laεt-A-Foam™ FR 10118 polyiεocyanurate ) core. Two 1" wide strips of Kapton™ were used to anchor the facings in place along the leading edge of the sample. All parts of the lay-up were cut to dimensions of 12" x 16". The warp direction of the fabric was laid parallel to the length of the panel. The panel was consolidated uεing a conεtant belt press temperature of 650°F and a constant belt speed of 12"/min. (residence time about 48 sec. in the heat zone). The gap between the upper and lower beltε waε set to achieve a finished panel thickness of 0.516", The Kapton™ release film waε used during panel procesεing. After conεolidation the Kapton™ film and tape were removed. The panel was cut into four 3" x 12" sampleε with the warp direction of the fabric parallel to the 3" dimension. The average peel strength of this panel by the climbing drum peel strength test method waε determined to be 27 lbs./3" sample. Example 13 The components of the laminate were dried for at least 2 hours at 120°C and then laid up in the following manner. One piece of amorphous nylon film (0.008" thick) was placed on each side of a flat woven 5 x 5 harness satin fabric (15 oz./sq. yd. code, T5674-34) made from E-glaεε/amorphouε nylon impregnated tow (Binnersley and Krueger U.S. Patent No. 4,640,861) to form the facing. Identical facingε were placed on each side of a piece of honeycomb of Nomex™ (3 lbε./sq. ft., 1/8" cell, 1/2" thick). The warp direction of the facinα fabric was aligned with the ribbon direction of the core and the predominently warp faced side of the fabric placed closest to the core. The facing layers were anchored to the core with (3) 1" wide Kapton™ tape εtrips along the leading edge of the sample. The belt press was set to a constant temperature of 650°F and a belt speed of 15"/min. (residence time about 32 sec. in the heat zone). The gap between the upper and lower belts was set to achieve a total sample thickness of 0.504". A Kapton™ release sheet was placed over both sideε of the entire laminate according to the above described procedure. The front edge of the sample, perpendicular to the warp direction of the facing fabric and containing the Kapton™ tape anchors, was inserted into the belt press. The Kapton™ release sheet and the tape anchorε were removed from the sample. The average εample thickness, as measured by micrometer, was found to be .507". A Climbing Drum Peel test was performed on three samples (in the fabric warp direction) and had an average result of 19.1 lbs./3" sample. Example 14 The components of this panel were dried for at least 2 hours at 120°C- and then laid up in the following manner. A piece of amorphous PEKK (60/40) film (Melt index 150) was laid over a piece of 1/2" Nomex™ honeycomb core. A piece of PEEK/AS4 uni tape (ICI Fibεrite APC-2/AS-4 12" uni tape, batch No. N89-0038, roll No. 11) was then placed upon the core with the fibers in the tape running perpendicular to the ribbon direction of the core. Another piece of the same tape was then placed on the stack, but with the AS-4 fibers running parallel to the ribbon direction of the core. The tape layup waε repeated in the same fashion for the opposite side of the core, including the layer of PEKK film. The facing layers were fastened to the core material with Kapton™ tape along the leading edge of the sample for insertion into the belt press (an edge perpendicular to the ribbon direction of the core). The belt press was set up for a constant temperature of 680°F and a belt speed of 15"/min. (reεidence time about 32 sees, in the heat zone) . The gap between the upper and lower belts waε fixed to a final εample thickneεs of 0.516". A Kapton™ release sheet was placed over both sides of the entire laminate. The leading edge of the layup was inserted into the belt press. Once consolidated, the Kapton™ release film and the Kapton™ 1 tape were removed from the sample. The average sample thickness as measured by micrometer was found to be 0.512". The completed panel waε then cut into three 3" x 24" εpeci enε (length parallel to the ribbon direction of the core) and teεted for flexural strength and modulus according to method BMS-256. Test results: Long Beam Flex Modulus - Average 174 Strength - 27754 psi Another sample was fabricated in the above manner except that the facing ply orientation of the uni graphite tape was reversed to give maximum peel srength. Therefore, the 0° axiε of the fibers waε placed parallel to the ribbon direction cf the honeycomb core and the outer ply waε placed perpendicular to the core riboon direction. Peel strength εampleε were then cut in a perpendicular orientation to the core ribbon direction. The meaεured peel value waε determined to be 13.6 lbs./3" sample. Example 15 The components of the laminate were laid up in the following manner. Two εtrips of foam measuring 17.5" x 2" and two stripε measuring 8" x 2" were cut from a sheet of Rohacell™ 200WF foam. These foam strips were assembled into a frame 17.5" long and 12" wide held together with 2.5" regular screws inserted into the side approximately 1/2" from the panel edge. A piece of honeycomb waε cut to fit tightly into the center of the frame. Identical panel facingε compoεed of two pieces of amorphous (60/40 T/I) PEKK film (150 melt index) on either side of a Kevlar™ Style 285 fabric were assembled and placed on either side of the honeycomb core/foam frame assembly. One inch wide εtrips of Kapton™ tape were uεed to anchor the panel facingε in place along the leading edge of the sample. The belt presε waε εet to a conεtant temperature of 650°F with a belt speed of 15"/min. Sample residence time in the heat zone waε approximately 32 sees. The gap between the upper and lower beltε waε set to produce a finiεhed sample thicknesε of 0.516" or 100% of the theoretical thickness. The εample was inserted into the belt process with Kapton™ film as the release agent. After consolidation, the releεe film and tape anchorε were removed. Visual inspection of the panel suface indicates that minimal space exists at the foam/honeycomb interface. The finiεhed average thicknesε cf the foam trimmed portion of the panel, as measured ' by a micrometer, waε 0.539", and the average thickneεε of the honeycomb-cored portion of the εample waε meaεured aε 0.536".

Claims: What is claimed is: 1. A panel compriεing: a core member and a fiber reinforced thermoplastic resin εheet material bonded to at least one side of said core member to form a facing therefor, the thermoplaεtic resin being between 30 to about 65 weight percent of said facing, the peel strength of the panel being greater than 10 lbε./3" εample. 2. The panel of Claim 1, said core member being in the form of a honeycomb structure of aramid paper. 3. The panel of Claim 2, said honeycomb structure being a plurality of adjoining cells formed of continuous upstanding walls, εaid wallε being folded at each end in the εame direction in a hook-like configuration to increase the surface area of said honeycomb structure contacting said facing. 4. The panel of Claim 1, said thermoplastic resin εheet material being reinforced with aramid fiber. 5. The panel of Claim 1, εaid thermoplaεtic resin sheet material being reinforced with glass fiber. 6. The panel of Claim 1, said thermoplastic resin sheet material being reinforced with carbon fibers. 7. The panel of Claims 1, 2, 3, 4, 5 or 6 in which said thermoplaεtic reεin εheet material iε polyetherketoneketone . 8. The panel of Claimε 1, 2, 3, 4, 5 or 6 wherein εaid thermoplaεtic reεin material iε polyetherimide . 9. The panel of Claimε 1, 2, 3, 4, 5 or 6 wherein said thermoplaεtic reεin material iε polyetheretherketone . 10. The panel of Claim 1 wherein said thermoplastic resin material comprises a plurality of different thermoplastic resins. 11. The panel of Claim 1, said core member being foam. 12. The panel of Claim 1, said core member being a honeycomb structure edge trimmed with foam. 13. A method for bonding a fiber- reinforced sheet of thermoplastic resin material to at least one side of a core member to form a bonded structure comprising: heating said core and said thermoplastic sheet material to a temperature of from about 480°F to about 710°F under positive pressure for a time less than 2.3 min.; and cooling said core and said sheet material while maintaining said positive pressure. 14. The method of Claim .13 wherein said positive pressure is from about 4 psi to about 300 psi. 15. The method of Claim 13 wherein said thin sheet of thermoplastic reεin material is reinforced with fiber. 16. The method of Claim 13 wherein said core member is in the form of a honeycomb structure. 17. The method of Claim 16 wherein said honeycomb structure is made of aramid paper, said thermoplastic resin material being polyetherketoneketone. 18. The method of Claim 13 wherein said core member is a foam material. 19. The method of Claim 18 wherein said foam material is selected from the group consisting of polyetherimide, polymethacrylimide, polyurethane and polyisocyanurate foams. 20. The method of Claim 13 wherein said core is in the form of a honeycomb structure edge trimmed with foam. 21. A method for bonding a thin sheet of _ thermoplastic resin material to at least one side of a core member to form a bonded structure comprising passing the core and said thermoplastic sheet material in mating surface contact through a belt press for a residence time period of less than 0 2.3 minutes; heating said core and said thermoplastic sheet material to a temperature of from about 480°F to about 710°F in said belt press; and cooling said core and said sheet material in said belt press while maintaining said positive 5 pressure. 22. The method of Claim 21 wherein said positive pressure is from about 4 psi to about 300 psi. 23. The method of Claim 21 wherein said 0 thin sheet of thermoplastic resin material is reinforced with fiber. 24. The method of Claim 21 wherein said core member is in the form of a honeycomb structure. 25. The method of Claim 24 wherein said honeycomb structure is made of aramid paper, said thermoplastic resin material being polyetherketoneketone. 26. The method of Claim 21 wherein said core member is a foam material. 27. The method of Claim 26 wherein said foam material is selected from the group consisting of polyetherimide, polymethacrylimide, polyurethane and polyisocyanurate foams. 28. The method of Claim 21 wherein said core is in the form of a hone y comb structure edge. 29. The method of Claim 21 wherein said thermoplastic resin material is polyetherimide. 30. The method of Claim 21 wherein said thermoplastic resin is polyetheretherketone.

Inventors: KAUFMANN CHRISTINE MARIE, MURSCHELL DALE LESTER, NOLLEN DENNIS ARTHUR, SARACINO ANTHONY RONALD, TRENTACOSTA JOSEPH DANIEL, KAUFMANN, CHRISTINE, MARIE, MURSCHELL, DALE, LESTER, NOLLEN, DENNIS, ARTHUR, SARACINO, ANTHONY, RONALD, TRENTACOSTA, JOSEPH, DANIEL
Applicants: DU PONT, E.I. DU PONT DE NEMOURS AND COMPANY
Application year: 1991
Main classification: B32B3
IPC codes: B32B3, B32B5, B32B27, E04C2