US3627608A - Method of forming a panel having a compound curvature - Google Patents

Method of forming a panel having a compound curvature Download PDF

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US3627608A
US3627608A US833480A US3627608DA US3627608A US 3627608 A US3627608 A US 3627608A US 833480 A US833480 A US 833480A US 3627608D A US3627608D A US 3627608DA US 3627608 A US3627608 A US 3627608A
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Prior art keywords
forming
sheet
panel
automotive headliner
areas
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US833480A
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Francis J Steiner
Robert M Paulsen
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Woodall Industries Inc
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Woodall Industries Inc
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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B27WORKING OR PRESERVING WOOD OR SIMILAR MATERIAL; NAILING OR STAPLING MACHINES IN GENERAL
    • B27DWORKING VENEER OR PLYWOOD
    • B27D1/00Joining wood veneer with any material; Forming articles thereby; Preparatory processing of surfaces to be joined, e.g. scoring
    • B27D1/04Joining wood veneer with any material; Forming articles thereby; Preparatory processing of surfaces to be joined, e.g. scoring to produce plywood or articles made therefrom; Plywood sheets
    • B27D1/08Manufacture of shaped articles; Presses specially designed therefor
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T156/00Adhesive bonding and miscellaneous chemical manufacture
    • Y10T156/10Methods of surface bonding and/or assembly therefor
    • Y10T156/1002Methods of surface bonding and/or assembly therefor with permanent bending or reshaping or surface deformation of self sustaining lamina
    • Y10T156/1026Methods of surface bonding and/or assembly therefor with permanent bending or reshaping or surface deformation of self sustaining lamina with slitting or removal of material at reshaping area prior to reshaping
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T156/00Adhesive bonding and miscellaneous chemical manufacture
    • Y10T156/10Methods of surface bonding and/or assembly therefor
    • Y10T156/1002Methods of surface bonding and/or assembly therefor with permanent bending or reshaping or surface deformation of self sustaining lamina
    • Y10T156/1028Methods of surface bonding and/or assembly therefor with permanent bending or reshaping or surface deformation of self sustaining lamina by bending, drawing or stretch forming sheet to assume shape of configured lamina while in contact therewith
    • Y10T156/1031Methods of surface bonding and/or assembly therefor with permanent bending or reshaping or surface deformation of self sustaining lamina by bending, drawing or stretch forming sheet to assume shape of configured lamina while in contact therewith with preshaping of lamina

Definitions

  • Montone Attorney-Harness, Dickey & Pierce ABSTRACT A method of forming a flexible, self-supporting sheetlike structure having a compound curvature, including the steps of perforating a sheet of woodlike fibrous material, such as fiberboard, wetting the sheet, applying steam, and forming the compound curvature in a press.
  • the method of forming an integral single piece automotive headliner includes forming the sheet into a flexible dish-shaped structure and finishing the inner concave surface by painting, or applying a fabric cushioning material.
  • Fiberboard or hardboard panels provide a relatively inexpensive building material, however such panels have a substantial resistance to bending and tend to return to their original shape when deformed into a curved structure. Further, fiberboard panels will tear when shaped, and the panels will crumble, if soaked. It is therefore an object os this invention to provide a method of forming fiberboard panels into self-supporting compound curvatures without crumbling or tearing the panel.
  • the prior art teaches two principal methods of forming flat fiberboard panels, however, these methods require the utilization of a means to retain the compound curvature after forming.
  • One method suggested by the prior art for forming automotive headliners includes cutting V-shaped slots at the areas of curvature, and thereafter deforming the panel and securing the contour with box fasteners in the slots.
  • the resultant panel structure is not self-supporting, and the stresses remain in the headliner, which may result in loosening of the fasteners.
  • the method is relatively expensive, substantially reducing the advantage of utilizing an inexpensive fiberboard panel.
  • the second method includes filling holes in the fiberboard panel with a liquid resin of the type which sets under heat and pressure.
  • the panel is then deformed in a press which sets the resin, and the resin retains the deformed contour of the sheet.
  • the sheet is not reformed," because the thermosetting binder used in commercial fiberboard is merely held in its stressed condition. It will be understood however that single automotive headliners have been formed from other materials, including various plastics.
  • the method of this invention is adapted to reform fiberboard or hardboard panels into flexible self-supporting structures, without fasteners or other means to retain the finished contour.
  • This method is particularly, although not exclusively adapted to forming single piece automotive headliners which have a compound curvature at the comers, and which are generally dish-shaped.
  • the method of this invention includes perforating a sheet of woodlike fibrous material or panel with numerous holes at the areas to be formed, wetting the sheet, applying steam to the sheet for a period of time sufiicient to make the sheet ductile enough to pen-nit forming without tearing or crumbling, and forming the compound curvature in a die under pressure.
  • Fiberboard or hardboard panels generally include a thermosetting resin binder which retains the wood or woodlike fibers in suspension. The fiberboard panels therefore have a substantial resistance to bending, and will tear when deformed into compound curvatures, unless slotted. Further, the fiberboard panels tend to return to their original flat shape, unless the fibers are actually shifted and the panel reformed.”
  • the perforations in the panel not only weaken the structural integrity of the panel, to permit forming, but also provide voids into which the fibers may be shifted at the areas of compound curvature.
  • the apertures also provide a means for escapement of the steam vapors, which is important to the process.
  • the wetting solution preferably includes a wetting agent which lubricates the fibers and prevents soaking.
  • the steam reduces the rigidity of the thermosetting binders and conducts moisture into the internal structure of the fibrous material without soaking the panel, which would cause crumbling. It has also been found advantageous to heat the panel, prior to wetting, to expand the fibers and reduce the time required to reach the critical forming condition. The problem is to conduct moisture into the internal structure of the fiberboard panel without soaking the structure of the fiberboard panel without soaking the structure, and yet make the panel sufficiently ductile to permit forming without tearing.
  • the panel is preferably fonned between heated dies, under pressure, wherein the spacing between the dies is quite important.
  • the pressure is preferably sufficient to actually cause material flow of the fibers toward the areas of greatest curvature, reducing buckling or tearing at these areas.
  • the apertures therefore provide a space which receives the material flow, and the resultant structure has smaller apertures at the areas of greatest curvature, although the apertures initially were of the identical size. It will also be understood that a greater number of perforations per square inch may be provided at the areas of greatest curvature, or the diameter of the perforations may initially be greater at such areas. It has been found by experimentation that the preferred diameter of the perforations are from 0.080 to 0. inches.
  • the fiberboard panel is first cut to the desired shape, and thereafter the sheet is formed by wetting, applying steam and reforming the sheet in a heated press.
  • the apertures may be formed prior to or subsequent to cutting.
  • the final step is to finish the inner or concave surface of the sheet, which may be accomplished by painting or applying a fabric material.
  • a fabric cushioning material is applied to the concave surface by draping the fabric over a male mold, which may be heated, applying an adhesive to the inner concave surface of the sheet, and pressing the adhesive coated side of the formed sheet on the fabric. It has been found that this method provides a smooth fabric liner, substantially free of wrinkles or other defects.
  • FIG. 1 is a partial side view of an automotive body showing a headliner
  • FIG. 2 is a top perspective view of a fiberboard panel
  • FIG. 3 is a top perspective view of the panel shown in FIG. 2 after cutting;
  • FIG. 4 is a top perspective view of a fabric liner for the headliner, cut to shape
  • FIG. 5 is a top view of a portion of the fiberboard panel after perforation
  • FIG. 6 is a schematic illustration of the heating step of this invention.
  • FIG. 7 is a schematic illustration of the wetting step of this invention.
  • FIG. 8 is a schematic illustration of the application of steam in the method of this invention.
  • FIG. 9 is a schematic illustration of the press utilized in the method of this invention.
  • FIG. 10 is a schematic illustration of the shaped panel drying on a cradle
  • FIG. 11 is a schematic illustration of a convex mold being heated to receive the fabric linear; liner;
  • FIG. 12 is a schematic illustration of the convex mold shown in FIG. 1 1 after receipt of the fabric liner;
  • FIG. 13 is an enlarged partial view of the embodiment shown in FIG. 12;
  • FIG. 14 is a schematic illustration of the application of adhesive to the concave surface of the formed headliner panel
  • FIG. 15 is a schematic illustration of the application of the formed headliner panel to the fabric material
  • FIG. 16 is a cross-sectional view of the finished automotive headliner
  • FIG. 17 is a partial cross-sectional view of the headliner shown in FIG. 16.
  • FIG. 18 is a perspective view of the finished headliner, prior to receipt in the automotive body shown in FIG. I.
  • the method of this invention is particularly adapted to reform relatively flat fiberboard or hardboard panels into selfsupporting curved structures, including structures having a compound curvature such as automotive headliners.
  • the disclosed embodiment is an automotive headliner, and the method of this invention has been described in regard to such embodiment to simplify the disclosure, however it will be understood that the method is not limited to such embodiments.
  • the embodiment of the automotive body shown in FIG. 1 includes a roof panel 2%, usually formed of metal, a front windshield 22 and a rear window 24.
  • the headliner 26 is secured to the inner or concave surface of the roof panel 20 and conforms to the compound curvature. Where a single piece or integral headliner is to be utilized, it is important that the headliner be sufficiently resilient to permit receipt through one of the window openings, which is narrower than the width of the roof panel, as shown, and that the headliner be self-supporting to prevent buckling or sagging. Further, in the preferred embodiment of the headliner, the width and length is slightly greater than the inner surface of the roof panel, and the headliner is bowed slightly to snap in position between the supporting channels, now shown. The headliner must therefore be sufficiently resilient to permit such installation, and retain its tensioned engagement.
  • the method of this invention is adapted to utilize relatively flat panels or sheets of commercial fiberboard or hardboard, which are relatively inexpensive, and provide a strong resilient structure.
  • Fiberboard panels of the type preferred herein are commercially available from various sources, including the Masonite Corporation under the trade names Masonite and Presdwood.
  • the fiberboard is however formed from steam exploded wood fibers in a thermosetting resin binder, making the panels difficult to form into complex or compound curvatures, and the therrnosetting resin binder causes the panel to return to its original flat shape, when formed. Further, the panel will crumble when soaked, or tear when deformed without wetting.
  • the method of this invention is adapted to provide sufficient moisture to permit forming without tearing or crumbling.
  • FIG. 2 illustrates a commercial fiberboard panel 28 of the type described hereinabove
  • FIG. 3 shows the panel after it has been cut to the desired shape.
  • the panel may be cut by hand or in a die, and the shape will depend upon the particular application of the structure.
  • the longitudinal edges 30 have been bowed slightly outwardly adjacent the midportion and the ends 32 are bowed inwardly to provide substantially flat or straight edges in the dishshaped headliner, and compensate for changes during forming.
  • the panel is then perforated, as shown in FIG. 5. It will be understood that the panel may however be perforated prior to cutting, or simultaneously therewith.
  • the perforations 34 weaken the resistance of the panel to bending, and provide other advantages peculiar to the method of this invention, as described hereinbelow. It will be understood that it may not be necessary to perforate the entire panel in certain applications, as where only a portion of the panel is to be formed, and larger diameter apertures may be provided at the areas of maximum curvature; the density of the apertures may also be increased at such areas.
  • a panel having a thickness of 0.095 to 0.105 inches has been found suitable with perforations of approximately three thirty-seconds of an inch diameter on one-fourth inch diagonal centers. Panels having a greater thickness may require a greater density of apertures, because such panels would have a greater resistance to bendmg.
  • the perforated panel may then be preheated as shown in FIG. 6, wherein a bank of heating elements 36 are directed on the panel 28.
  • the panel is preheated to ap proximately 180 degrees by a bank of lights 36 over a load of stocks, or the panels are placed in an oven.
  • the wetting solution includes a wetting agent such as the commercially available silicone wetting agents.
  • a suitable wetting agent is ls-76 Silicone" available from Union Carbide Company.
  • the wetting solution is this embodiment includes approximately 8 grams of a silicone wetting agent per 10 pounds of water. The wetting agent conducts the moisture into the fibers of the fiberboard panel to lubricate the fibers, without soaking, and reduces the time required to dry the panel after forming.
  • the apertures also serve to conduct the wetting agent into intimate contact with the fibers.
  • the panel is then subjected to steam, as shown in FIG. 8, which conducts the moisture into the internal structure of the fibrous material, without soaking the panel, and reduces the rigidity of the thermosetting binders in the panel, to permit forming without tearing.
  • the steam and the wetting agent are adapted to speed the wetting of the wood fibers to permit forming prior to soaking, because soaking and heat tend to break down the thermosetting resin, causing the panel to crumble.
  • the steam is also preferably superheated to further speed the process.
  • a "pants press" type steam applicator 42 is utilized, which applies the steam under pressure. In this embodiment, the steam is applied for 15 seconds maximum with I00 pounds per square inch dry steam.
  • An electrical heating element is provided which superheats the steam to 400 to 500 Fahrenheit. It is important to note that the apertures in the panel not only aid in conducting the steam into the internal fibrous structure, but also provide a means of escapement for the steam vapors. The apertures therefore prevent soaking of the panel during steaming.
  • the perforated panel 28 may then be reformed in a press 44, as shown in FIG. 9, without tearing the panel.
  • This embodiment of the method of this invention utilizes a heated press, wherein the pressure is sufficient to cause material flow of the fibers toward the areas of greatest curvature.
  • the fibers are thus redistributed into the corner areas of compound curvature, and into the cove areas of the headliner, making the structure self-supporting.
  • the apertures or perforations in these areas take-up" the redistributed fibers, causing the perforations to be smaller at the areas of greatest curvature.
  • a conventional size automotive headliner may be formed in a 550 to 600 ton press, in approximately 30 seconds at 375 Fahrenheit.
  • the formed panel may then be placed on a cradle 48, as shown in FIG. 10, where it is permitted to dry.
  • the apertures in the panel and the wetting agent reduce the drying time.
  • the formed panel may now be finished, by painting for example, and installed in the car body as shown in FIG. I.
  • the panel is finished by securing a sound and heat absorbent fabric liner to the inner or concave surface of the panel.
  • the fabric liner 50 is first cut to size as shown in FIG. 4.
  • the fabric liner in this embodiment is cut to the approximate same size and shape as the unforrned panel shown in FIG. 3, allowing for waste.
  • the fabric preferably has a twoway" stretch so that it will accurately conform to the configuration of the panel, including the curved areas.
  • the fabric may be provided with a foam backing to aid in the sound and heat absorption.
  • a suitable material for the fabric liner is a Guilford knap knit nylon commercially available from Guilford Mills, Inc. having a three thirty-seconds inch polyurethane foam backing.
  • the fabric liner 50' is then placed over a convex mold 52, as shown in FIG. 12, which has been preheated by a bank of heating elements 54 or the like as shown in FIG. ii.
  • the mold may alternatively be internally heated.
  • the convex external surface of the mold is curved to conform to the internal or concave surface of the formed panel, and the fabric is held in place by suitable fasteners, such as pin frame or individual Velcro grips 56, as shown in FIG. 13.
  • the fabric is slightly stretched over the convex mold to accurately conform to the curved areas, with the foam layer opposite the mold.
  • a bonding agent such as the commercially available synthetic resin adhesives is then applied to the internal surface of the formed panel, as shown in FIG. 14, wherein the panel 28 is supported on a table 58 and the adhesive is sprayed on to the concave surface by spray nozzles 60.
  • a suitable synthetic resin adhesive is commercially available from the H. B. Fuller Company under the number -3990. Five to 6 grams of adhesive per square foot of panel has been found suitable for this adhesive.
  • the panel is then transferred quickly to the convex mold 52 and placed with the concave adhesive coated surface over the fabric, as shown in FIG. 15. Full contact between the panel and the fabric is then established by hand pressure or a pressure pad, and held for approximately 60 seconds. A pressure of approximately 2 to 5 pounds per square inch has been found satisfactory.
  • the excess fabric 62 is then trimmed from the panel, as shown in FIG. 16, and the finished headliner 26, shown in H68. 17 and 18, is ready for installation.
  • the headliner formed by the method of this invention thus includes the resilient self-supporting fiberboard panel 28, the foam backing 6e, and the finish fabric lamination 50.
  • a method of forming a flexible self-supporting sheetlike structure having a compound curvature including the steps of:
  • a method of forming a single piece, relatively flexible, self-supporting automotive headliner having a compound curvature including the steps of:

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  • Engineering & Computer Science (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Manufacturing & Machinery (AREA)
  • Mechanical Engineering (AREA)
  • Wood Science & Technology (AREA)
  • Forests & Forestry (AREA)
  • Vehicle Interior And Exterior Ornaments, Soundproofing, And Insulation (AREA)
  • Laminated Bodies (AREA)

Abstract

A method of forming a flexible, self-supporting sheetlike structure having a compound curvature, including the steps of perforating a sheet of woodlike fibrous material, such as fiberboard, wetting the sheet, applying steam, and forming the compound curvature in a press. The method of forming an integral single piece automotive headliner includes forming the sheet into a flexible dish-shaped structure and finishing the inner concave surface by painting, or applying a fabric cushioning material.

Description

METHOD OF FORMlNG A PANEL HAVING A COMPOUND CURVATURE 22 Claims, 18 Drawing Figs.
U.S.Cl 156/211, 156/214,156/245, 264/156, 264/322 Int. Cl G29c 3/00, B29c 17/08 Field of Search 156/21 1,
[56] References Cited UNITED STATES PATENTS 1,561,763 11/1925 Atwood 156/77 X 3,466,354 9/1969 Donner 264/156 X 1,471,906 10/1923 Longren 1. 264/322 2,338,685 1/1944 Dee 1. 264/322 2,934,790 5/1960 Shwayder 144/309 X 3,265,530 9/1966 Marzocchi et a1. 296/137 X Primary Examiner-Benjamin A. Borchelt Assistant Examiner-G. E. Montone Attorney-Harness, Dickey & Pierce ABSTRACT: A method of forming a flexible, self-supporting sheetlike structure having a compound curvature, including the steps of perforating a sheet of woodlike fibrous material, such as fiberboard, wetting the sheet, applying steam, and forming the compound curvature in a press. The method of forming an integral single piece automotive headliner includes forming the sheet into a flexible dish-shaped structure and finishing the inner concave surface by painting, or applying a fabric cushioning material.
METHOD OF FOG A PANEL HAVING A COMPOUND CURVA SUMMARY OF THE PRIOR ART Fiberboard or hardboard panels provide a relatively inexpensive building material, however such panels have a substantial resistance to bending and tend to return to their original shape when deformed into a curved structure. Further, fiberboard panels will tear when shaped, and the panels will crumble, if soaked. It is therefore an object os this invention to provide a method of forming fiberboard panels into self-supporting compound curvatures without crumbling or tearing the panel.
The prior art teaches two principal methods of forming flat fiberboard panels, however, these methods require the utilization of a means to retain the compound curvature after forming. One method suggested by the prior art for forming automotive headliners includes cutting V-shaped slots at the areas of curvature, and thereafter deforming the panel and securing the contour with box fasteners in the slots. The resultant panel structure is not self-supporting, and the stresses remain in the headliner, which may result in loosening of the fasteners. Further, the method is relatively expensive, substantially reducing the advantage of utilizing an inexpensive fiberboard panel. The second method includes filling holes in the fiberboard panel with a liquid resin of the type which sets under heat and pressure. The panel is then deformed in a press which sets the resin, and the resin retains the deformed contour of the sheet. In either method therefore, the sheet is not reformed," because the thermosetting binder used in commercial fiberboard is merely held in its stressed condition. It will be understood however that single automotive headliners have been formed from other materials, including various plastics.
SUMMARY OF THE INVENTION The method of this invention is adapted to reform fiberboard or hardboard panels into flexible self-supporting structures, without fasteners or other means to retain the finished contour. This method is particularly, although not exclusively adapted to forming single piece automotive headliners which have a compound curvature at the comers, and which are generally dish-shaped.
The method of this invention includes perforating a sheet of woodlike fibrous material or panel with numerous holes at the areas to be formed, wetting the sheet, applying steam to the sheet for a period of time sufiicient to make the sheet ductile enough to pen-nit forming without tearing or crumbling, and forming the compound curvature in a die under pressure. Fiberboard or hardboard panels generally include a thermosetting resin binder which retains the wood or woodlike fibers in suspension. The fiberboard panels therefore have a substantial resistance to bending, and will tear when deformed into compound curvatures, unless slotted. Further, the fiberboard panels tend to return to their original flat shape, unless the fibers are actually shifted and the panel reformed."
The perforations in the panel not only weaken the structural integrity of the panel, to permit forming, but also provide voids into which the fibers may be shifted at the areas of compound curvature. In the method of this invention, the apertures also provide a means for escapement of the steam vapors, which is important to the process. The wetting solution preferably includes a wetting agent which lubricates the fibers and prevents soaking. The steam reduces the rigidity of the thermosetting binders and conducts moisture into the internal structure of the fibrous material without soaking the panel, which would cause crumbling. It has also been found advantageous to heat the panel, prior to wetting, to expand the fibers and reduce the time required to reach the critical forming condition. The problem is to conduct moisture into the internal structure of the fiberboard panel without soaking the structure of the fiberboard panel without soaking the structure, and yet make the panel sufficiently ductile to permit forming without tearing.
The panel is preferably fonned between heated dies, under pressure, wherein the spacing between the dies is quite important. The pressure is preferably sufficient to actually cause material flow of the fibers toward the areas of greatest curvature, reducing buckling or tearing at these areas. The apertures therefore provide a space which receives the material flow, and the resultant structure has smaller apertures at the areas of greatest curvature, although the apertures initially were of the identical size. It will also be understood that a greater number of perforations per square inch may be provided at the areas of greatest curvature, or the diameter of the perforations may initially be greater at such areas. It has been found by experimentation that the preferred diameter of the perforations are from 0.080 to 0. inches.
In the preferred embodiment of forming an automotive headliner, the fiberboard panel is first cut to the desired shape, and thereafter the sheet is formed by wetting, applying steam and reforming the sheet in a heated press. The apertures may be formed prior to or subsequent to cutting. The final step is to finish the inner or concave surface of the sheet, which may be accomplished by painting or applying a fabric material. In the preferred embodiment of the method, a fabric cushioning material is applied to the concave surface by draping the fabric over a male mold, which may be heated, applying an adhesive to the inner concave surface of the sheet, and pressing the adhesive coated side of the formed sheet on the fabric. It has been found that this method provides a smooth fabric liner, substantially free of wrinkles or other defects.
Other advantages and meritorious features will more fully appear from the following description, claims, and accompanying drawings, wherein:
BRIEF DESCRIPTION OF THE DRAWINGS FIG. 1 is a partial side view of an automotive body showing a headliner;
FIG. 2 is a top perspective view of a fiberboard panel;
FIG. 3 is a top perspective view of the panel shown in FIG. 2 after cutting;
FIG. 4 is a top perspective view of a fabric liner for the headliner, cut to shape;
FIG. 5 is a top view of a portion of the fiberboard panel after perforation;
FIG. 6 is a schematic illustration of the heating step of this invention;
FIG. 7 is a schematic illustration of the wetting step of this invention;
FIG. 8 is a schematic illustration of the application of steam in the method of this invention;
FIG. 9 is a schematic illustration of the press utilized in the method of this invention;
FIG. 10 is a schematic illustration of the shaped panel drying on a cradle;
FIG. 11 is a schematic illustration of a convex mold being heated to receive the fabric linear; liner;
FIG. 12 is a schematic illustration of the convex mold shown in FIG. 1 1 after receipt of the fabric liner;
FIG. 13 is an enlarged partial view of the embodiment shown in FIG. 12;
FIG. 14 is a schematic illustration of the application of adhesive to the concave surface of the formed headliner panel;
FIG. 15 is a schematic illustration of the application of the formed headliner panel to the fabric material;
FIG. 16 is a cross-sectional view of the finished automotive headliner;
FIG. 17 is a partial cross-sectional view of the headliner shown in FIG. 16; and
FIG. 18 is a perspective view of the finished headliner, prior to receipt in the automotive body shown in FIG. I.
DESCRIPTION OF THE DRAWINGS AND PREFERRED METHOD OF THIS INVENTION The method of this invention is particularly adapted to reform relatively flat fiberboard or hardboard panels into selfsupporting curved structures, including structures having a compound curvature such as automotive headliners. The disclosed embodiment is an automotive headliner, and the method of this invention has been described in regard to such embodiment to simplify the disclosure, however it will be understood that the method is not limited to such embodiments. The embodiment of the automotive body shown in FIG. 1 includes a roof panel 2%, usually formed of metal, a front windshield 22 and a rear window 24.
The headliner 26 is secured to the inner or concave surface of the roof panel 20 and conforms to the compound curvature. Where a single piece or integral headliner is to be utilized, it is important that the headliner be sufficiently resilient to permit receipt through one of the window openings, which is narrower than the width of the roof panel, as shown, and that the headliner be self-supporting to prevent buckling or sagging. Further, in the preferred embodiment of the headliner, the width and length is slightly greater than the inner surface of the roof panel, and the headliner is bowed slightly to snap in position between the supporting channels, now shown. The headliner must therefore be sufficiently resilient to permit such installation, and retain its tensioned engagement. The method of this invention is adapted to utilize relatively flat panels or sheets of commercial fiberboard or hardboard, which are relatively inexpensive, and provide a strong resilient structure. Fiberboard panels of the type preferred herein are commercially available from various sources, including the Masonite Corporation under the trade names Masonite and Presdwood. The fiberboard is however formed from steam exploded wood fibers in a thermosetting resin binder, making the panels difficult to form into complex or compound curvatures, and the therrnosetting resin binder causes the panel to return to its original flat shape, when formed. Further, the panel will crumble when soaked, or tear when deformed without wetting. The method of this invention is adapted to provide sufficient moisture to permit forming without tearing or crumbling.
FIG. 2 illustrates a commercial fiberboard panel 28 of the type described hereinabove, and FIG. 3 shows the panel after it has been cut to the desired shape. The panel may be cut by hand or in a die, and the shape will depend upon the particular application of the structure. In this embodiment, the longitudinal edges 30 have been bowed slightly outwardly adjacent the midportion and the ends 32 are bowed inwardly to provide substantially flat or straight edges in the dishshaped headliner, and compensate for changes during forming.
The panel is then perforated, as shown in FIG. 5. It will be understood that the panel may however be perforated prior to cutting, or simultaneously therewith. The perforations 34 weaken the resistance of the panel to bending, and provide other advantages peculiar to the method of this invention, as described hereinbelow. It will be understood that it may not be necessary to perforate the entire panel in certain applications, as where only a portion of the panel is to be formed, and larger diameter apertures may be provided at the areas of maximum curvature; the density of the apertures may also be increased at such areas. In this embodiment, a panel having a thickness of 0.095 to 0.105 inches has been found suitable with perforations of approximately three thirty-seconds of an inch diameter on one-fourth inch diagonal centers. Panels having a greater thickness may require a greater density of apertures, because such panels would have a greater resistance to bendmg.
The perforated panel may then be preheated as shown in FIG. 6, wherein a bank of heating elements 36 are directed on the panel 28. In this embodiment, the panel is preheated to ap proximately 180 degrees by a bank of lights 36 over a load of stocks, or the panels are placed in an oven.
The panel is then wetted as shown in FIG. 7, wherein a series of spray nozzles 40 direct the wetting solution on to the panel. The panel may also be wetted by hand. In the preferred embodiment of this method, the wetting solution includes a wetting agent such as the commercially available silicone wetting agents. A suitable wetting agent is ls-76 Silicone" available from Union Carbide Company. The wetting solution is this embodiment includes approximately 8 grams of a silicone wetting agent per 10 pounds of water. The wetting agent conducts the moisture into the fibers of the fiberboard panel to lubricate the fibers, without soaking, and reduces the time required to dry the panel after forming. The apertures also serve to conduct the wetting agent into intimate contact with the fibers.
The panel is then subjected to steam, as shown in FIG. 8, which conducts the moisture into the internal structure of the fibrous material, without soaking the panel, and reduces the rigidity of the thermosetting binders in the panel, to permit forming without tearing. The steam and the wetting agent are adapted to speed the wetting of the wood fibers to permit forming prior to soaking, because soaking and heat tend to break down the thermosetting resin, causing the panel to crumble. The steam is also preferably superheated to further speed the process. In the disclosed embodiment of the method of this invention, a "pants press" type steam applicator 42 is utilized, which applies the steam under pressure. In this embodiment, the steam is applied for 15 seconds maximum with I00 pounds per square inch dry steam. An electrical heating element is provided which superheats the steam to 400 to 500 Fahrenheit. It is important to note that the apertures in the panel not only aid in conducting the steam into the internal fibrous structure, but also provide a means of escapement for the steam vapors. The apertures therefore prevent soaking of the panel during steaming.
The perforated panel 28 may then be reformed in a press 44, as shown in FIG. 9, without tearing the panel. This embodiment of the method of this invention utilizes a heated press, wherein the pressure is sufficient to cause material flow of the fibers toward the areas of greatest curvature. The fibers are thus redistributed into the corner areas of compound curvature, and into the cove areas of the headliner, making the structure self-supporting. The apertures or perforations in these areas take-up" the redistributed fibers, causing the perforations to be smaller at the areas of greatest curvature. A conventional size automotive headliner may be formed in a 550 to 600 ton press, in approximately 30 seconds at 375 Fahrenheit. The formed panel may then be placed on a cradle 48, as shown in FIG. 10, where it is permitted to dry. The apertures in the panel and the wetting agent reduce the drying time.
The formed panel may now be finished, by painting for example, and installed in the car body as shown in FIG. I. In this embodiment however the panel is finished by securing a sound and heat absorbent fabric liner to the inner or concave surface of the panel. The fabric liner 50 is first cut to size as shown in FIG. 4. The fabric liner in this embodiment is cut to the approximate same size and shape as the unforrned panel shown in FIG. 3, allowing for waste. The fabric preferably has a twoway" stretch so that it will accurately conform to the configuration of the panel, including the curved areas. Further, the fabric may be provided with a foam backing to aid in the sound and heat absorption. A suitable material for the fabric liner is a Guilford knap knit nylon commercially available from Guilford Mills, Inc. having a three thirty-seconds inch polyurethane foam backing.
The fabric liner 50' is then placed over a convex mold 52, as shown in FIG. 12, which has been preheated by a bank of heating elements 54 or the like as shown in FIG. ii. The mold may alternatively be internally heated. The convex external surface of the mold is curved to conform to the internal or concave surface of the formed panel, and the fabric is held in place by suitable fasteners, such as pin frame or individual Velcro grips 56, as shown in FIG. 13. The fabric is slightly stretched over the convex mold to accurately conform to the curved areas, with the foam layer opposite the mold.
A bonding agent, such as the commercially available synthetic resin adhesives is then applied to the internal surface of the formed panel, as shown in FIG. 14, wherein the panel 28 is supported on a table 58 and the adhesive is sprayed on to the concave surface by spray nozzles 60. A suitable synthetic resin adhesive is commercially available from the H. B. Fuller Company under the number -3990. Five to 6 grams of adhesive per square foot of panel has been found suitable for this adhesive.
The panel is then transferred quickly to the convex mold 52 and placed with the concave adhesive coated surface over the fabric, as shown in FIG. 15. Full contact between the panel and the fabric is then established by hand pressure or a pressure pad, and held for approximately 60 seconds. A pressure of approximately 2 to 5 pounds per square inch has been found satisfactory. The excess fabric 62 is then trimmed from the panel, as shown in FIG. 16, and the finished headliner 26, shown in H68. 17 and 18, is ready for installation. The headliner formed by the method of this invention thus includes the resilient self-supporting fiberboard panel 28, the foam backing 6e, and the finish fabric lamination 50.
What is claimed is:
1. A method of forming a flexible self-supporting sheetlike structure having a compound curvature, including the steps of:
a. perforating a sheet of woodlike fibrous material, having a substantial resistance to bending, with numerous holes in the areas to be formed,
b. applying a controlled amount of steam to the areas of the sheet to be formed for a period of time sufficient to make the sheet sufficiently ductile to permit forming without tearing or crumbling, and
c. placing the sheet with its open perforations between a pair of heated dies and fonning a compound curvature in the sheet by the application of heat and pressure to the opposite sides of said sheet with said dies, the heat transmitted to said sheet by said dies being effective to drive moisture from said sheet into the perforations thereof.
2. The method of forming a structure defined in claim 1, wherein the number of perforations per square inch is greater at the areas of greatest curvature.
3. The method of forming the structure defined in claim 1, wherein the diameter of the perforations are greater at the areas of greatest curvature.
4. The method of forming the structure defined in claim 1, wherein the diameter of the perforations are from 0.080 to 0.120 inches.
5. The method of forming the structure defined in claim 1, wherein the surface of the sheet is wetted.
6. The method of forming the structure defined in claim 5, wherein the surface of the sheet is wetted with a solution including a wetting agent.
7. The method of forming the structure defined in claim 6 wherein the wetting agent lubricates the fibers.
8. The method of forming the structure defined in claim 1, wherein the steam is applied under pressure to the sheet.
9. The method of forming the structure defined in claim 8, wherein the steam is superheated prior to application of the steam to the sheet.
10. The method of forming the structure defined in claim ll,
wherein the sheet is heated prior to wetting.
11. The method of forming the structure defined in claim 1, wherein the pressure of the die is suficient to cause material flow toward the areas of greatest curvature, reducing buckling at such areas.
2. The method of fonning the structure defined in claim 1, wherein the sheet is formed into a generally rectangular automotive headliner having areas of greatest curvature at the comers.
13. The method of forming the structure defined in claim l2, wherein a sound absorbent fabric layer is secured within the automotive headliner.
M. A method of forming a single piece, relatively flexible, self-supporting automotive headliner having a compound curvature, including the steps of:
a. perforating a generally flat rectangular sheet of woodlike fibrous material, having a thermosetting bonding agent and substantial resistance to bending, with numerous holes,
b. wetting the surface of the sheet with a wetting solution,
c. applying steam to the sheet for a period of time sufficient to make the sheet sufficiently ductile to permit fonning without tearing or crumbling,
d. forming the compound curvature of an automotive headliner by placing the sheet with its perforations in an unfilled condition in a heated press and applying suffcient pressure to reform the sheet into the contour of an automotive headliner and to drive moisture from said sheet into the perforations thereof, and
e. finishing the inner surface of the sheet.
15. The method of forming an automotive headliner defined in claim 14, wherein the sheet is finished by painting the inner concave surface.
16. The method of forming an automotive headliner defined in claim 14, wherein the inner surface is finished by bonding a fabric material to the inner concave surface of the sheet.
17. The method of forming an automotive headliner defined in claim 16, wherein the fabric material is bonded to the sheet by draping the fabric over a male mold, applying adhesive to the inner concave surface of the sheet, and placing the adhesive coated side of the fonned sheet on the fabric.
18. The method of forming an automotive headliner defined in claim 17, wherein the fabric material includes a foam cushioning material, and the fabric is draped over the male mold with the foam cushioning material opposite the mold.
19. The method of forming an automotive headliner defined in claim 18, wherein the male mold is heated, prior to receipt of the fabric material.
20. The method of forming an automotive headliner defined in claim 14, wherein the wetting solution includes a lubricating wetting agent.
21. The method of forming an automotive headliner defined in claim 14, wherein superheated steam is applied under pressure to the sheet.
22. The method of forming an automotive headliner defined in claim 14, wherein the areas of greatest curvature are adjacent the corners of the rectangular sheet, and the pressure of the die is sufficient to cause the material to flow toward the areas of greatest curvature, reducing buckling at the comers.

Claims (21)

  1. 2. The method of forming a structure defined in claim 1, wherein the number of perforations per square inch is greater at the areas of greatest curvature.
  2. 3. The method of forming the structure defined in claim 1, wherein the diameter of the perforations are greater at the areas of greatest curvature.
  3. 4. The method of forming the structure defined in claim 1, wherein the diameter of the perforations are from 0.080 to 0.120 inches.
  4. 5. The method of forming the structure defined in claim 1, wherein the surface of the sheet is wetted.
  5. 6. The method of forming the structure defined in claim 5, wherein the surface of the sheet is wetted with a solution including a wetting agent.
  6. 7. The method of forming the structure defined in claim 6, wherein the wetting agent lubricates the fibers.
  7. 8. The method of forming the structure defined in claim 1, wherein the steam is applied under pressure to the sheet.
  8. 9. The method of forming the structure defined in claim 8, wherein the steam is superheated prior to application of the steam to the sheet.
  9. 10. The method of forming the structure defined in claim 1, wherein the sheet is heated prior to wetting.
  10. 11. The method of forming the structure defined in claim 1, wherein the pressure of the die is sufficient to cause material flow toward the areas of greatest curvature, reducing buckling at such areas.
  11. 12. The method of forming the structure defined in claim 1, wherein the sheet is formed into a generally rectangular automotive headliner having areas of greatest curvature at the corners.
  12. 13. The method of forming the structure defined in claim 12, wherein a sound absorbent fabric layer is secured within the automotive headliner.
  13. 14. A method of forming a single piece, relatively flexible, self-supporting automotive headliner having a compound curvature, including the steps of: a. perforating a generally flat rectangular sheet of woodlike fibrous material, having a thermosetting bonding agent and substantial resistance to bending, with numerous holes, b. wetting the surface of the sheet with a wetting solution, c. applying steam to the sheet for a period of time sufficient to make the sheet sufficiently ductile to permit forming without tearing or crumbling, d. forming the compound curvature of an automotive headliner by placing the sheet with its perforations in an unfilled condition in a heated press and applying sufficient pressure to reform the sheet into the contour of an automotive headliner and to drive moisture from said sheet into the perforations thereof, and e. finishing the inner surface of the sheet.
  14. 15. The method of forming an automotive headliner defined in claim 14, wherein the sheet is finished by painting the inner concave surface.
  15. 16. The method of forming an automotive headliner defined in claim 14, wherein the inner surface is finished by bonding a fabric material to the inner concave surface of the sheet.
  16. 17. The method of forming an automotive headliner defined in claim 16, wherein the fabric material is bonded to the sheet by draping the fabric over a male mold, applying adhesive to the inner concave surface of the sheet, and placing the adhesive coated side of the formed sheet on the fabric.
  17. 18. The method of forming an automotive headliner defined in claim 17, wherein the fabric material includes a foam cushioning material, and the fabric is draped over the male mold with the foam cushioning material opposite the mold.
  18. 19. The method of forming an automotive headliner defined in claim 18, wherein the male mold is heated, prior to receipt of the fabric material.
  19. 20. The method of forming an automotive headliner defined in claim 14, wherein the wetting solution includes a lubricating wetting agent.
  20. 21. The method of forming an automotive headliner defined in claim 14, wherein superheated steam is applied under pressure to the sheet.
  21. 22. The method of forming an automotive headliner defined in claim 14, wherein the areas of greatest curvature are adjacent the corners of the rectangular sheet, and the pressure of the die is sufficient to cause the material to flow toward the areas of greatest curvature, reducing buckling at the corners.
US833480A 1969-06-16 1969-06-16 Method of forming a panel having a compound curvature Expired - Lifetime US3627608A (en)

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US3935353A (en) * 1970-05-22 1976-01-27 Detroit Gasket & Manufacturing Co. Heat shrinkable decorative covering material for vehicle panels
US3948708A (en) * 1973-03-26 1976-04-06 Van Dresser Corporation Method of forming a panel
US4119451A (en) * 1976-07-15 1978-10-10 Nissan Motor Company, Ltd. Method of press-forming corrugated paperboard as substrate of curved trim board
US4783298A (en) * 1986-01-08 1988-11-08 Mazda Motor Corporation In-mold coating method and apparatus
WO1998057797A1 (en) * 1997-06-19 1998-12-23 Masonite Corporation Post-press molding of fiberboard door skins
US5902434A (en) * 1996-03-25 1999-05-11 Lear Corporation Method for bonding a cover material to a foam cushion
US6103180A (en) * 1993-10-06 2000-08-15 Matec Holding Ag Method for producing a low odor, sound- and heat-insulation shaped element
US20040036197A1 (en) * 2002-08-21 2004-02-26 Janiga Eugene R. Methods of forming molded, coated wood composites
WO2004024435A1 (en) * 2002-08-26 2004-03-25 Trocellen Gmbh Planar structure for trimming partial areas of a motor vehicle interior
US20060059811A1 (en) * 1997-04-14 2006-03-23 Timmerman Timothy L Lateral force resisting system
US20070056344A1 (en) * 2002-07-19 2007-03-15 Minoru Ishihara Metal sheet pressing method
US20070175144A1 (en) * 2006-01-11 2007-08-02 Valinge Innovation Ab V-groove
US20080000417A1 (en) * 2004-10-05 2008-01-03 Valinge Innovation Ab Appliance and method for surface treatment of a board shaped material and floorboard
US20080034701A1 (en) * 2005-02-15 2008-02-14 Valinge Innovation Ab Building panel with compressed edges and method of making same
US20080120938A1 (en) * 2006-09-15 2008-05-29 Jan Jacobsson Device and method for compressing an edge of a building panel and a building panel with compressed edges
US20110146188A1 (en) * 2009-12-17 2011-06-23 Valinge Innovation Ab Methods and arrangements relating to surface forming of building panels
DE102010029116A1 (en) * 2010-05-19 2011-11-24 Bayerische Motoren Werke Aktiengesellschaft Producing thick calibrated adhesive sample, comprises e.g. covering at least two mold plates with high heat applied non-adhesive coating, inserting adhesive composition in between the coated mold surfaces and compressing together
US8683698B2 (en) 2002-03-20 2014-04-01 Valinge Innovation Ab Method for making floorboards with decorative grooves
US20220041082A1 (en) * 2018-09-27 2022-02-10 Bayerische Motoren Werke Aktiengesellschaft Method for Producing a Seat Cover for a Vehicle Seat Made of a Form-Fit Knit Part
US20220134966A1 (en) * 2020-10-30 2022-05-05 Harman International Industries, Incorporated Methods for forming a hidden audio assembly

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US1561763A (en) * 1923-08-23 1925-11-17 Rubwood Inc Composite laminated structure and method of making same
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Cited By (40)

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Publication number Priority date Publication date Assignee Title
US3935353A (en) * 1970-05-22 1976-01-27 Detroit Gasket & Manufacturing Co. Heat shrinkable decorative covering material for vehicle panels
US3948708A (en) * 1973-03-26 1976-04-06 Van Dresser Corporation Method of forming a panel
US4119451A (en) * 1976-07-15 1978-10-10 Nissan Motor Company, Ltd. Method of press-forming corrugated paperboard as substrate of curved trim board
US4783298A (en) * 1986-01-08 1988-11-08 Mazda Motor Corporation In-mold coating method and apparatus
US6103180A (en) * 1993-10-06 2000-08-15 Matec Holding Ag Method for producing a low odor, sound- and heat-insulation shaped element
US5902434A (en) * 1996-03-25 1999-05-11 Lear Corporation Method for bonding a cover material to a foam cushion
US5942081A (en) * 1996-03-25 1999-08-24 Lear Corporation Apparatus for bonding a cover material to foam
US20060059811A1 (en) * 1997-04-14 2006-03-23 Timmerman Timothy L Lateral force resisting system
US7797907B2 (en) * 1997-04-14 2010-09-21 Timmerman Timothy L Lateral force resisting system
WO1998057797A1 (en) * 1997-06-19 1998-12-23 Masonite Corporation Post-press molding of fiberboard door skins
US8683698B2 (en) 2002-03-20 2014-04-01 Valinge Innovation Ab Method for making floorboards with decorative grooves
US10471678B2 (en) 2002-03-20 2019-11-12 Valinge Innovation Ab Floorboards with decorative grooves
US11498305B2 (en) 2002-03-20 2022-11-15 Valinge Innovation Ab Floorboards with decorative grooves
US20070056344A1 (en) * 2002-07-19 2007-03-15 Minoru Ishihara Metal sheet pressing method
US20100218584A1 (en) * 2002-07-19 2010-09-02 Minoru Ishihara Metal sheet pressing method
US20090078021A1 (en) * 2002-07-19 2009-03-26 Minoru Ishihara Metal sheet pressing method
US20040036197A1 (en) * 2002-08-21 2004-02-26 Janiga Eugene R. Methods of forming molded, coated wood composites
WO2004024435A1 (en) * 2002-08-26 2004-03-25 Trocellen Gmbh Planar structure for trimming partial areas of a motor vehicle interior
US20080000417A1 (en) * 2004-10-05 2008-01-03 Valinge Innovation Ab Appliance and method for surface treatment of a board shaped material and floorboard
US8042484B2 (en) 2004-10-05 2011-10-25 Valinge Innovation Ab Appliance and method for surface treatment of a board shaped material and floorboard
US9623433B2 (en) 2004-10-05 2017-04-18 Valinge Innovation Ab Appliance and method for surface treatment of a board shaped material and floorboard
US20080034701A1 (en) * 2005-02-15 2008-02-14 Valinge Innovation Ab Building panel with compressed edges and method of making same
US8215078B2 (en) 2005-02-15 2012-07-10 Välinge Innovation Belgium BVBA Building panel with compressed edges and method of making same
US8429872B2 (en) 2005-02-15 2013-04-30 Valinge Innovation Belgium Bvba Building panel with compressed edges and method of making same
US8261504B2 (en) 2006-01-11 2012-09-11 Valinge Innovation Ab V-groove
US20080000190A1 (en) * 2006-01-11 2008-01-03 Valinge Innovation Ab V-groove
US20070175144A1 (en) * 2006-01-11 2007-08-02 Valinge Innovation Ab V-groove
US20080120938A1 (en) * 2006-09-15 2008-05-29 Jan Jacobsson Device and method for compressing an edge of a building panel and a building panel with compressed edges
US8323016B2 (en) * 2006-09-15 2012-12-04 Valinge Innovation Belgium Bvba Device and method for compressing an edge of a building panel and a building panel with compressed edges
US8940216B2 (en) 2006-09-15 2015-01-27 Valinge Innovation Ab Device and method for compressing an edge of a building panel and a building panel with compressed edges
US20110146188A1 (en) * 2009-12-17 2011-06-23 Valinge Innovation Ab Methods and arrangements relating to surface forming of building panels
US9447587B2 (en) 2009-12-17 2016-09-20 Valinge Innovation Ab Methods and arrangements relating to surface forming of building panels
US9169654B2 (en) 2009-12-17 2015-10-27 Valinge Innovation Ab Methods and arrangements relating to surface forming of building panels
US8591691B2 (en) 2009-12-17 2013-11-26 Valinge Innovation Ab Methods and arrangements relating to surface forming of building panels
DE102010029116B4 (en) 2010-05-19 2021-10-14 Bayerische Motoren Werke Aktiengesellschaft Method and mold for making an adhesive sample
DE102010029116A1 (en) * 2010-05-19 2011-11-24 Bayerische Motoren Werke Aktiengesellschaft Producing thick calibrated adhesive sample, comprises e.g. covering at least two mold plates with high heat applied non-adhesive coating, inserting adhesive composition in between the coated mold surfaces and compressing together
US20220041082A1 (en) * 2018-09-27 2022-02-10 Bayerische Motoren Werke Aktiengesellschaft Method for Producing a Seat Cover for a Vehicle Seat Made of a Form-Fit Knit Part
US11850983B2 (en) * 2018-09-27 2023-12-26 Bayerische Motoren Werke Aktiengesellschaft Method for producing a seat cover for a vehicle seat made of a form-fit knit part
US20220134966A1 (en) * 2020-10-30 2022-05-05 Harman International Industries, Incorporated Methods for forming a hidden audio assembly
US11827162B2 (en) * 2020-10-30 2023-11-28 Harman International Industries, Incorporated Methods for forming a hidden audio assembly

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DE2027086A1 (en) 1971-01-07

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