US3670555A - Method of fabricating structural members - Google Patents

Method of fabricating structural members Download PDF

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US3670555A
US3670555A US49221A US3670555DA US3670555A US 3670555 A US3670555 A US 3670555A US 49221 A US49221 A US 49221A US 3670555D A US3670555D A US 3670555DA US 3670555 A US3670555 A US 3670555A
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recess
mandrels
loop
mandrel
structural member
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US49221A
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Carl K Fredericks
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Corlite Corp
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Corlite Corp
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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29DPRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCES IN A PLASTIC STATE
    • B29D99/00Subject matter not provided for in other groups of this subclass
    • B29D99/0003Producing profiled members, e.g. beams
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B21MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21DWORKING OR PROCESSING OF SHEET METAL OR METAL TUBES, RODS OR PROFILES WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21D47/00Making rigid structural elements or units, e.g. honeycomb structures
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B21MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21DWORKING OR PROCESSING OF SHEET METAL OR METAL TUBES, RODS OR PROFILES WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21D5/00Bending sheet metal along straight lines, e.g. to form simple curves
    • B21D5/01Bending sheet metal along straight lines, e.g. to form simple curves between rams and anvils or abutments
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C53/00Shaping by bending, folding, twisting, straightening or flattening; Apparatus therefor
    • B29C53/02Bending or folding
    • B29C53/04Bending or folding of plates or sheets
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C53/00Shaping by bending, folding, twisting, straightening or flattening; Apparatus therefor
    • B29C53/02Bending or folding
    • B29C53/08Bending or folding of tubes or other profiled members
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C67/00Shaping techniques not covered by groups B29C39/00 - B29C65/00, B29C70/00 or B29C73/00
    • B29C67/0011Shaping techniques not covered by groups B29C39/00 - B29C65/00, B29C70/00 or B29C73/00 for shaping plates or sheets
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C67/00Shaping techniques not covered by groups B29C39/00 - B29C65/00, B29C70/00 or B29C73/00
    • B29C67/0014Shaping techniques not covered by groups B29C39/00 - B29C65/00, B29C70/00 or B29C73/00 for shaping tubes or blown tubular films
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29DPRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCES IN A PLASTIC STATE
    • B29D24/00Producing articles with hollow walls
    • B29D24/002Producing articles with hollow walls formed with structures, e.g. cores placed between two plates or sheets, e.g. partially filled
    • B29D24/008Producing articles with hollow walls formed with structures, e.g. cores placed between two plates or sheets, e.g. partially filled the structure having hollow ridges, ribs or cores
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29KINDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
    • B29K2105/00Condition, form or state of moulded material or of the material to be shaped
    • B29K2105/06Condition, form or state of moulded material or of the material to be shaped containing reinforcements, fillers or inserts
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29LINDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
    • B29L2024/00Articles with hollow walls
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29LINDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
    • B29L2031/00Other particular articles
    • B29L2031/001Profiled members, e.g. beams, sections
    • B29L2031/003Profiled members, e.g. beams, sections having a profiled transverse cross-section
    • 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
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/49616Structural member making
    • Y10T29/49623Static structure, e.g., a building component
    • Y10T29/49634Beam or girder

Definitions

  • the method may also include the step of pivoting certain of the mandrels to bring them into contiguity with the ram or rams to thereby form structural members of still different configurations.
  • the mandrels can be removed from the structural member, or made of lightweight material and left in place for insulation, structural stifi'ening, and the like.
  • the formable material is preferably in the form of a continuous loop or band arranged about the mandrel or mandrels so that urging of the material into the recess or recesses places the loop under tension, confomiing it to the shape of the mandrel and the recess.
  • FIGJI 6474l 4470 (2 I Ir FIG.
  • the present invention relates to a method of fabricating a structural member.
  • a method of fabricating a structural member which comprises the steps of arranging a length of material adjacent a mandrel or mandrels with a portion of the material length being made formable and located in overlying relation to a recess defined by or between the mandrel or mandrels, as the case may be.
  • the method includes the step of urging the deformable portion of the material into the recess until the length of formable material is placed under tension.
  • a pair of triangular mandrels may be spaced apart, a loop or band of formable material loosely disposed about the mandrels, and a triangular shaped ram urged against the exterior of the formable band to deform the band into the space or recess between the two mandrels, whereby the band is placed under tension so that it conforms to the triangular shapes of the mandrels and the ram. If the two rams are then pivoted toward one another and against the adjacent ram, a truss-like configuration is formed.
  • the su'uctural member will retain its deformed state, and a number of such elements can be nested and fastened together to form a composite beam characterized by internal cell walls, providing a,
  • the band is made of reinforced plastics material, such material can be polymerized or cured, so that the band retains its deformed state.
  • the method of the present invention makes possible economical fabrication of relatively long beams and structures such as lightweight power and telephone poles which can be made of reinforced plastics material for air dropping in remote, treeless areas.
  • relatively long beams and structures such as lightweight power and telephone poles which can be made of reinforced plastics material for air dropping in remote, treeless areas.
  • the present invention provides a method which enables reduction of both the weight of the resulting structure and also the labor and tooling costs, and also frequently is the only feasible method for fabricating the structure.
  • the present invention provides a method which can be automated to fabricate long beams of such materials and characterized by relatively complex crosssections or flat sides, a structure heretofore imposible without use of expensive hand lay-up procedures.
  • the present method also makes possible inexpensive fabrication of cylinders, tubes, ducts, and other cylindrical objects out of reinforced plastics, and without resort to the hand labor common in the prior art for ironing or otherwise making the reinforced plastics material lie tightly against the forming mandrel prior to curing.
  • a band of formable material is placed under sufficient tension during formation of the structural member that the material is tightly fitted against the associated forming mandrels without any necessity for hand fitting and ironing.
  • FIG. 1 is a perspective view of apparatus for practicing the present method and including an internal mandrel having a cavity or recess, a loop or band of formable material disposed about the mandrel, and a single ram thrusting a portion of the loop into the mandrel recess;
  • FIG. 2 is an end elevational view of the apparatus of FIG. 1, on a reduced scale, and schematically showing the disposition of the components prior to movement of the ram into the mandrel recess;
  • FIG. 3 is a view similar to FIG. 2, but illustrating the disposition of the components after movement of the ram into the mandrel recess;
  • FIG. 4 is an end elevational view of apparatus for forming a structural member of I-shape
  • FIG. 5 is an end elevational view of an apparatus in which a structural member of square cross-section is formed, the embodiment being noteworthy in that the ram is located interiorly of the band of formable material, the mandrel being located exteriorly of the band;
  • FIG. 6 is a view similar to FIG. 5 but illustrating the ram in its extended position
  • FIG. 7 is yet another embodiment of apparatus utilizing the present invention, this embodiment being characterized by'a mandrel adapted to press a band of formable material within a dovetail recess in the mandrel;
  • FIGS. 8, 9 and 10 are end elevational views illustrating steps in the formation of a structural member characterized by a truss-like cross-section, and utilizing triangularly shaped mandrels and a triangularly shaped ram;
  • FIG. 11 is another apparatus for practicing the method of the present invention, the apparatus in this case utilizing mandrels efi'ective to provide a structural member of circular cross-section;
  • FIG. 12 is an end elevational view of the structural member formed by the apparatus of FIG. 1 1;
  • FIG. 13 is another apparatus for practicing the present in vention, utilizing a pair of triangular mandrels and a relatively thin ram member which remains as part of the formed structural member;
  • FIG. 14 is an end elevational view of the structural member formed by the apparatus of FIG. 13;
  • FIG. 15 is an end elevational view of an apparatus utilizing three mandrels and one ram to form a structural member having a cross-section characterized by four triangular cells;
  • FIG. 16 is an end elevational view of a structural member formed by the apparatus of FIG.
  • FIG. 17 is another apparatus for practicing thepresent invention, and utilizing two circular mandrels and a circular ram;
  • FIG. 18 is an end elevational view of a structural member formed by the apparatus of FIG. 17.
  • FIG. 19 is a perspective view, partially cut away, and illustrating a composite structure formed by utilizing a plurality of the elements of FIG. 10 to form a structural sandwich.
  • FIGS. 1 through 3 there is illustrated an apparatus for practicing the present method of fabricating a structural member, the structural member in this case being generally indicated at 10 in FIGS. 1 and 3.
  • the structural member in this case comprises a sheath, sleeve, band, or loop 12 which is disposed about and completely encompasses a mandrel means or composite mandrel 14.
  • loop is intended to comprehend a variety of configurations ranging from a thin wire to a ribbon to a belt or to a long sleeve, so that the fabricated structural members may range from discs to long beams, for example.
  • mandrel is also intended to comprehend more than a solid pieceof tooling, including for example a telescopable or collapsible member, a foam material solid member, or decorative insert left in place as part of the fabricated su'uctural member, a truss similarly left in place, a previously fabricated part which is to receive another ply of material, or such a fabricated part which is to become part of a larger assembly.
  • the loop 12 is made of reinforced plastics material such as glass fiber fabric impregnated with a suitable resin adapted to be polymerized, as is well know to those skilled in the art.
  • the particular mandrel 14 of the apparatus of FIG. 1 is a composite or two part mandrel maintained in its extended state by the introduction of fluid under pressure therein through a manifold 16.
  • the mandrel 14 is retracted or collapsed by venting the pressurized fluid from between the relatively movable parts of the mandrel whereby the mandrel 14 can be separated from the loop 12 once the loop has been cured to form the structural member 10.
  • the structurally continuous loop 12 is arranged adjacent the mandrel 14 with a portion thereof located in overlying location to a space or recess 18 located in the upper, exterior surface of the mandrel 14.
  • a ram means in this case a single ram 20 having an exterior surface shaped to complementally fit within the recess 18, is disposed above the recess 18 and is moved by any suitable means (not shown) against the portion of the loop 12 located over the recess 18. Downward pressure is exerted upon the ram 20 until the loop portion is forced within the recess 18, as best viewed in FIG. 3, to place the loop under tension.
  • the dimensions of the band will necessarily depend upon the materials being used, the shape to be imparted to it, and other factors obvious to those skilled in the art.
  • the present invention is not limited to the use of a continuous loop 12.
  • a material different from the material of the parent loop 12 can be disposed between the points A-A and BB; which are diagrammatically indicated in FIG. 2, and stitched or otherwise secured to the parent loop.
  • the material used to couple the points A-A and B--B of the modified loop 12 it can be made detachable for re-use as part of the tooling for the next part.
  • An extension of this concept is to provide any suitable means, not shown, to secure against movement the upper run of the loop 12 at point A-A, with similar clamping means or anchorages being provided for the lower run of the loop 12 at the points B-B.
  • two separate lengths of forrnable material can be independently clamped to provide the same result as would occur if a structurally continuous loop were used.
  • mandrel 22 which is I- shaped.
  • the opposite channels 24 each constitute a separate recess and a pair of confronting rams 26 are moved toward each other to sequentially press a first loop 28 into the recesses 24, and next a loop 30 into the recesses 24 in overlying relation to the loop 28.
  • both plies or loops 28 and 30 could be formed simultaneously by the rams 26.
  • the outer loop 30 must be made slightly larger in dimension than the first loop 28 in order to provide the necessary tensioning effect as the loops achieve intimate contact with the mandrel 22, or the loop 28 as the case may be.
  • Su'uctural elements such as channels, angles, T-sections or the like are difi'icult to fabricate out of reinforced plastics unless resort is made to prior art hand lay-up procedures, or expensive male-female matched molds, or close-tolerance dies and punches, and the like.
  • the method of the present invention greatly simplifies the fabrication of such I defined by the interior surfaces of an internal cavity of an exterior mandrel 40.
  • FIG. 6 shows the ram portions 34 urging the loop 36 intothe recesses of the mandrel 40, demonstrating that the present method is not limited to an arrangement in which the mandrel is located interiorly of the band or loop 36.
  • FIG. 7 illustrates a structural member which would be difficult if not impossible to produce by any method of the prior art.
  • the structural member is formed by utilizing an internal mandrel 42 having a dovetail shaped recess 44, with a continuous band or loop of forrnable material 46 being disposed about the mandrel 42.
  • a ram 48 is provided having extensible fingers or ram portions 50 for urging the adjacent portions of the loops 46 into the recess 44.
  • band or loop of any of the various embodiments of this disclosure can be tapered, that is, reduced in cross-sectional dimension throughout its length, whereby it is suited for association with similarly tapered mandrels and rams to provide a structural member having a corresponding tapered shape.
  • mandrels and rams which can be utilized with the present method has been omitted for brevity inasmuch as such variations are well known to those skilled in the art.
  • mandrels can be left in place to provide strength, structural rigidity, insulation or the like, meltable or dissolvable mandrels may also be used to enable their easy removal.
  • meltable or dissolvable mandrels may also be used to enable their easy removal.
  • many types of removable mandrel are presently available and in the interest of brevity will be omitted from the present discussion.
  • FIGS. 8 through 10 there is illustrated a structural member 52 which is truss-like in crosssectional configuration.
  • the member 52 is fabricated by utilizing a pair of triangularly shaped mandrels 54 disposed within a structurally continuous loop or band 56 of fonnable material such as resin reinforced glass fiber fabric material.
  • a triangularly shaped ram 58 is disposed, in FIG. 8, above a space, opening or recess 60 which is defined by the spaced apart mandrels 54, which rest upon a work table 61.
  • the ram 58 is termed a Ram, it will be apparent that it functions in a manner similar to the mandrels once the loop 56 is deformed.
  • FIG. 9 illustrates depression of the ram 58 into the space 60 to deform the loop 56, and also illustrates the upward and inward pivotable movement of the mandrels 54 toward one another and into contiguity with the sloping adjacent surfaces of the ram 58.
  • the ram 58 is now performing a function like that of the mandrels 54, as will be apparent.
  • a loop of formable material is positioned adjacent a pair of mandrels, the loop is tightened to firmly enclose the mandrels by pushing in on a portion of the loop with a ram, and the internal mandrels are pivoted around hinge points created in the loop to form a cross-section of cellular configuration.
  • the mandrels may be removed or left in place, as desired.
  • mandrels 64 can be used, as seen in FIGS. 11 and 12, a pair of mandrels 64 being illustrated which are characterized by a curvilinear exterior surface.
  • the ram 66 utilized is also similarly configured.
  • the mandrels 64 rest within complemental depressions formed in the work table 68, and a structurally continuous band or loop 70 is disposed about the pair of mandrels 64, a portion of the loop 70 lies within a central depression or recess 72 formed in the work table 68.
  • the ram 66 is brought down upon the loop 70 to deform it into the recess 72, the ram 66 is left in place and an insert 74 is placed in overlying relation to the inplace ram 66.
  • the mandrels 64 are pivoted toward one another and into abutment with the insert 74 to form the structural member 76 shown in FIG. 12.
  • the mandrels 64 and rams 66 can be made of lightweight foam material, for example, and left in place in the final structural member 76. This enables use of the assembly as a packing container for an elongated fragile member (not shown) disposed within the hollow central portion of the structural member 76.
  • FIGS. 13 and 14 also illustrate this feature, the ram in this case being a pane of glass 78, or the like, sandwiched between foam material mandrels 80 which are pivoted towards one another from the positions of FIG. 13 to those of FIG. 14. This orients the continuous loop 82 into a generally square cross-section, with the fragile glass pane 78 cushioned by the mandrels 80.
  • FIG. 15 illustrates another apparatus using the present method, and comprising three mandrels 84 and a single ram 86, all of triangular shape.
  • the lowermost mandrel 84 fits within a triangular trough provided in the work table 88, and the continuous band or loop 90 is disposed around all three mandrels 84, as illustrated, with pivotal movement of the outermost mandrels 84 producing the structural member 92 iilustrated in FIG. 16.
  • FIGS. 17 and 18, and apparatus which utilizes a pair of spaced apart mandrels 94 of circular cross-section.
  • a continuous band or loop 96 or formable material is disposed about the mandrels 94, and is made of resin reinforced glass fiber or the like so that it becomes rigid upon curing.
  • the formable material can be flexible, non-rigid material such as corrugated packing board or the like so that the structural member 98 illustrated in FIG. 18 is then useful as a carrier for transporting fragile items.
  • the mandrels 94 and the ram 100 would constitute the fragile items to be shipped.
  • a tie member 102 is adhesively bonded to the pivoted-together components to maintain them in their assembled relation, as will be apparent.
  • FIG. 19 a plurality of the structural members 52 of FIG. are arranged in nested, side-by-side, parallel relation. Facing skins 104 are bonded or otherwise attached to the structural members 52 to form a strong, lightweight, structural sandwich characterized by a truss-like cross-section defined by the assembled members 52.
  • a variety of structural or decorative end uses for this and similarly fabricated structures will immediately suggest themselves to those skilled in the art. Many of these complex shapes and structures could not readily be fabricated in the prior art, being producible only by utilization of the method of the present invention.
  • the work table support for the mandrels of the various embodiments is largely schematic. In actual practice the mandrels would most likely be supported at their ends so as to permit the lengths or loop of formable material to move relative to the mandrels during the tensioning operation. Such relative movement will also be facilitated by providing lubrication, vibration, or the like of the mandrels and the rams.
  • the loop of formable material may also take the form of a vacuum tight bag to completely enclose a part, such as the I- beam, of FIG. 4. Utilizing the present method to tension the bag on the I-beam would facilitate a desirable intimate contact between the bag and the part, which is valuable for autoclave curing of certain reinforced plastic parts.

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Abstract

A method of fabricating a structural member by arranging a length of formable material in overlying relation to one or more recesses defined by a mandrel or mandrels. One or more rams are utilized to urge the formable material into such recess to place the formable material under tension. Various configurations of mandrels and rams are utilized to form structural members of various configurations. The method may also include the step of pivoting certain of the mandrels to bring them into contiguity with the ram or rams to thereby form structural members of still different configurations. The mandrels can be removed from the structural member, or made of lightweight material and left in place for insulation, structural stiffening, and the like. The formable material is preferably in the form of a continuous loop or band arranged about the mandrel or mandrels so that urging of the material into the recess or recesses places the loop under tension, conforming it to the shape of the mandrel and the recess. Many variations of the concept are disclosed.

Description

United States Patent Fredericks [451 June 20, 1972 [54] METHOD OF FABRICATING STRUCTURAL MEMBERS [72] Inventor: Carl K. Fredericks, San Diego, Calif. [73] Assignee: Corlite Corporation, San Diego, Calif.
[22] Filed: June 24, 1970 [21] Appl. No.: 49,221
580,238 7/1958 Italy ..29/155 Primary Examiner-Lowell A. Larson Attorney-Fulwider, Patton, Rieber, Lee & Utecht ABSTRACT A method of fabricating a structural member by arranging a length of formable material in overlying relation to one or more recesses defined by a mandrel or mandrels. One or more rams are utilized to urge the formable material into such recess to place the formable material under tension. Various configurations of mandrels and rams are utilized to form structural members of various configurations. The method may also include the step of pivoting certain of the mandrels to bring them into contiguity with the ram or rams to thereby form structural members of still different configurations. The mandrels can be removed from the structural member, or made of lightweight material and left in place for insulation, structural stifi'ening, and the like.
The formable material is preferably in the form of a continuous loop or band arranged about the mandrel or mandrels so that urging of the material into the recess or recesses places the loop under tension, confomiing it to the shape of the mandrel and the recess. Many variations of the concept are disclosed.
1 1 Claims, 19 Drawing Figures PATENTEnJum m2 3, 570.555
INVENTOR. 64% I11 fi'eepae/c/vs Array/v5):
P'A'TE'N'TEDmzo m2 sum 2 or z FIG.I2
FIGJI 6474l 4470 (2 I Ir FIG.|3
INVENTOR. 6/9/2L If. FEEDER/6K5 J i Anne/vars METHOD OF FABRICATING STRUCTURAL MEMBERS BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a method of fabricating a structural member.
2. Description of the Prior Art Certain structures and decorative items have heretofore been diflicult or impossible to produce incertain shapes and from certain materials. For example, one of the most difficult fabrication tasks in the reinforced plastics industry is making long beams with cross-sections other than circular or uniformly convexly curved. Circular beams or tubes can presently be made by production techniques which include filament winding, tape winding, template wrapping and the like. Square tubes are roughly analogous and can also be made in the same fashion, although their manufacture is complicated by the necessity of using forming mandrels having flat faces. However, it is not possible to make a beam with a hexagonal cell wall diagonal array without utilizing expensive and time consuming hand lay-up procedures, which involves individually wrapping mandrels and subsequently nesting them together into the required configuration.
In the paper and cardboard field it has heretofore been possible to fold such material into various configurations not possible in the reinforced plastics industry. However, very long paper or cardboard structures require equipment with long creasing capacity, which is expensive and not always readily available.
The prior art systems for fabricating metal beams and pipes, such as heating ducts, are also quite limited with respect to the configurations which can be formed by known metal rolling and folding techniques.
In summary, there are many relatively complex cross-sections which cannot now be economically provided in elongated members such as beams, or which cannot be provided at all.
SUMMARY According to the present invention, there is provided a method of fabricating a structural member which comprises the steps of arranging a length of material adjacent a mandrel or mandrels with a portion of the material length being made formable and located in overlying relation to a recess defined by or between the mandrel or mandrels, as the case may be. The method includes the step of urging the deformable portion of the material into the recess until the length of formable material is placed under tension. With this technique it is possible to make beams of complex, truss-like cross-section quickly and easily. For example, a pair of triangular mandrels may be spaced apart, a loop or band of formable material loosely disposed about the mandrels, and a triangular shaped ram urged against the exterior of the formable band to deform the band into the space or recess between the two mandrels, whereby the band is placed under tension so that it conforms to the triangular shapes of the mandrels and the ram. If the two rams are then pivoted toward one another and against the adjacent ram, a truss-like configuration is formed. Ifthe band is made of a non-resilient metal, for example, the su'uctural member will retain its deformed state, and a number of such elements can be nested and fastened together to form a composite beam characterized by internal cell walls, providing a,
high strength-to-weight ratio. If the band is made of reinforced plastics material, such material can be polymerized or cured, so that the band retains its deformed state.
The method of the present invention makes possible economical fabrication of relatively long beams and structures such as lightweight power and telephone poles which can be made of reinforced plastics material for air dropping in remote, treeless areas. Heretofore, it was economically feasible in the reinforced plastics industry to produce only a tapered cylinder, and the labor and the heavy walls of such a cylinder made its use as a pole prohibitive. In contrast, the present invention provides a method which enables reduction of both the weight of the resulting structure and also the labor and tooling costs, and also frequently is the only feasible method for fabricating the structure.
Recent development of boron and graphite high modulus fibers, and epoxy composites using these fibers, has made possible the production of primary structures which are stifi', strong, and light in weight. The present invention provides a method which can be automated to fabricate long beams of such materials and characterized by relatively complex crosssections or flat sides, a structure heretofore imposible without use of expensive hand lay-up procedures.
The present method also makes possible inexpensive fabrication of cylinders, tubes, ducts, and other cylindrical objects out of reinforced plastics, and without resort to the hand labor common in the prior art for ironing or otherwise making the reinforced plastics material lie tightly against the forming mandrel prior to curing. According to the present invention, a band of formable material is placed under sufficient tension during formation of the structural member that the material is tightly fitted against the associated forming mandrels without any necessity for hand fitting and ironing.
Other objects and features of the invention will become apparent from a consideration of the following detailed description when taken in conjunction with the accompanying drawings.
BRIEF DESCRIPTION OF THE DRAWINGS FIG. 1 is a perspective view of apparatus for practicing the present method and including an internal mandrel having a cavity or recess, a loop or band of formable material disposed about the mandrel, and a single ram thrusting a portion of the loop into the mandrel recess;
FIG. 2 is an end elevational view of the apparatus of FIG. 1, on a reduced scale, and schematically showing the disposition of the components prior to movement of the ram into the mandrel recess;
FIG. 3 is a view similar to FIG. 2, but illustrating the disposition of the components after movement of the ram into the mandrel recess;
FIG. 4 is an end elevational view of apparatus for forming a structural member of I-shape;
FIG. 5 is an end elevational view of an apparatus in which a structural member of square cross-section is formed, the embodiment being noteworthy in that the ram is located interiorly of the band of formable material, the mandrel being located exteriorly of the band;
FIG. 6 is a view similar to FIG. 5 but illustrating the ram in its extended position;
FIG. 7 is yet another embodiment of apparatus utilizing the present invention, this embodiment being characterized by'a mandrel adapted to press a band of formable material within a dovetail recess in the mandrel;
FIGS. 8, 9 and 10 are end elevational views illustrating steps in the formation of a structural member characterized by a truss-like cross-section, and utilizing triangularly shaped mandrels and a triangularly shaped ram;
FIG. 11 is another apparatus for practicing the method of the present invention, the apparatus in this case utilizing mandrels efi'ective to provide a structural member of circular cross-section;
FIG. 12 is an end elevational view of the structural member formed by the apparatus of FIG. 1 1;
FIG. 13 is another apparatus for practicing the present in vention, utilizing a pair of triangular mandrels and a relatively thin ram member which remains as part of the formed structural member;
FIG. 14 is an end elevational view of the structural member formed by the apparatus of FIG. 13;
FIG. 15 is an end elevational view of an apparatus utilizing three mandrels and one ram to form a structural member having a cross-section characterized by four triangular cells;
FIG. 16 is an end elevational view of a structural member formed by the apparatus of FIG.
FIG. 17 is another apparatus for practicing thepresent invention, and utilizing two circular mandrels and a circular ram;
FIG. 18 is an end elevational view of a structural member formed by the apparatus of FIG. 17; and
FIG. 19 is a perspective view, partially cut away, and illustrating a composite structure formed by utilizing a plurality of the elements of FIG. 10 to form a structural sandwich.
DESCRIPTION OF THE PREFERRED EMBODIMENTS Referring now to the drawings, and particularly to FIGS. 1 through 3, there is illustrated an apparatus for practicing the present method of fabricating a structural member, the structural member in this case being generally indicated at 10 in FIGS. 1 and 3. The structural member in this case comprises a sheath, sleeve, band, or loop 12 which is disposed about and completely encompasses a mandrel means or composite mandrel 14.
The term loop is intended to comprehend a variety of configurations ranging from a thin wire to a ribbon to a belt or to a long sleeve, so that the fabricated structural members may range from discs to long beams, for example. Moreover, the term mandrel is also intended to comprehend more than a solid pieceof tooling, including for example a telescopable or collapsible member, a foam material solid member, or decorative insert left in place as part of the fabricated su'uctural member, a truss similarly left in place, a previously fabricated part which is to receive another ply of material, or such a fabricated part which is to become part of a larger assembly.
In the present embodiment, the loop 12 is made of reinforced plastics material such as glass fiber fabric impregnated with a suitable resin adapted to be polymerized, as is well know to those skilled in the art.
The particular mandrel 14 of the apparatus of FIG. 1 is a composite or two part mandrel maintained in its extended state by the introduction of fluid under pressure therein through a manifold 16. The mandrel 14 is retracted or collapsed by venting the pressurized fluid from between the relatively movable parts of the mandrel whereby the mandrel 14 can be separated from the loop 12 once the loop has been cured to form the structural member 10.
The structurally continuous loop 12 is arranged adjacent the mandrel 14 with a portion thereof located in overlying location to a space or recess 18 located in the upper, exterior surface of the mandrel 14.
A ram means, in this case a single ram 20 having an exterior surface shaped to complementally fit within the recess 18, is disposed above the recess 18 and is moved by any suitable means (not shown) against the portion of the loop 12 located over the recess 18. Downward pressure is exerted upon the ram 20 until the loop portion is forced within the recess 18, as best viewed in FIG. 3, to place the loop under tension. This causes the inside periphery of the loop 12 to closely fit against the outside periphery of the mandrel 14, the loop 12 being made of such a dimension that it is placed under tension just prior to or at the point of final deformation to the shape of the recess 18. The dimensions of the band will necessarily depend upon the materials being used, the shape to be imparted to it, and other factors obvious to those skilled in the art.
This method lends itself to automation in that the loop 12 is adapted to be loosely positioned about the mandrel 14 and yet the continuous nature of the loop 12 enables tension to be developed in it by the ram 20 to an extent suflicient that the loop 12 closely hugs the contour of the mandrel 14 without any necessity for hand fitting or auxiliary rams. However, the present invention is not limited to the use of a continuous loop 12. For example, a material different from the material of the parent loop 12 can be disposed between the points A-A and BB; which are diagrammatically indicated in FIG. 2, and stitched or otherwise secured to the parent loop. Whatever the material used to couple the points A-A and B--B of the modified loop 12, it can be made detachable for re-use as part of the tooling for the next part.
An extension of this concept, which is also within the scope of the present invention, is to provide any suitable means, not shown, to secure against movement the upper run of the loop 12 at point A-A, with similar clamping means or anchorages being provided for the lower run of the loop 12 at the points B-B. Thus, two separate lengths of forrnable material can be independently clamped to provide the same result as would occur if a structurally continuous loop were used.
It will be apparent that various configurations of mandrel can be used in the practice of the present method, including mandrels of circular cross-section or cruciform cross-section. Referring now to FIG. 4, a mandrel 22 is illustrated which is I- shaped. The opposite channels 24 each constitute a separate recess and a pair of confronting rams 26 are moved toward each other to sequentially press a first loop 28 into the recesses 24, and next a loop 30 into the recesses 24 in overlying relation to the loop 28. This forms a two-ply structural member. Alternatively, both plies or loops 28 and 30 could be formed simultaneously by the rams 26. Of course, the outer loop 30 must be made slightly larger in dimension than the first loop 28 in order to provide the necessary tensioning effect as the loops achieve intimate contact with the mandrel 22, or the loop 28 as the case may be.
Su'uctural elements, such as channels, angles, T-sections or the like are difi'icult to fabricate out of reinforced plastics unless resort is made to prior art hand lay-up procedures, or expensive male-female matched molds, or close-tolerance dies and punches, and the like. However, the method of the present invention greatly simplifies the fabrication of such I defined by the interior surfaces of an internal cavity of an exterior mandrel 40. FIG. 6 shows the ram portions 34 urging the loop 36 intothe recesses of the mandrel 40, demonstrating that the present method is not limited to an arrangement in which the mandrel is located interiorly of the band or loop 36.
FIG. 7 illustrates a structural member which would be difficult if not impossible to produce by any method of the prior art. The structural member is formed by utilizing an internal mandrel 42 having a dovetail shaped recess 44, with a continuous band or loop of forrnable material 46 being disposed about the mandrel 42. In this case, a ram 48 is provided having extensible fingers or ram portions 50 for urging the adjacent portions of the loops 46 into the recess 44.
Although not shown, it will be apparent that the band or loop of any of the various embodiments of this disclosure can be tapered, that is, reduced in cross-sectional dimension throughout its length, whereby it is suited for association with similarly tapered mandrels and rams to provide a structural member having a corresponding tapered shape.
A detailed description of all of the various types and shapes of mandrels and rams which can be utilized with the present method has been omitted for brevity inasmuch as such variations are well known to those skilled in the art. Although the mandrels can be left in place to provide strength, structural rigidity, insulation or the like, meltable or dissolvable mandrels may also be used to enable their easy removal. Here again, many types of removable mandrel are presently available and in the interest of brevity will be omitted from the present discussion.
The present method also contemplates the use of more than one mandrel. Referring now to FIGS. 8 through 10, there is illustrated a structural member 52 which is truss-like in crosssectional configuration. The member 52 is fabricated by utilizing a pair of triangularly shaped mandrels 54 disposed within a structurally continuous loop or band 56 of fonnable material such as resin reinforced glass fiber fabric material. A triangularly shaped ram 58 is disposed, in FIG. 8, above a space, opening or recess 60 which is defined by the spaced apart mandrels 54, which rest upon a work table 61. Although the ram 58 is termed a Ram, it will be apparent that it functions in a manner similar to the mandrels once the loop 56 is deformed.
FIG. 9 illustrates depression of the ram 58 into the space 60 to deform the loop 56, and also illustrates the upward and inward pivotable movement of the mandrels 54 toward one another and into contiguity with the sloping adjacent surfaces of the ram 58. The ram 58 is now performing a function like that of the mandrels 54, as will be apparent.
The new arrangement of the mandrels and ram-mandrel produces a truss-like configuration of the structural member 52 illustrated in FIG. 10. Once the material of the loop 56 is cured and hardened, the loop 56 normally will adequately retain its deformed shape, but adhesive can be applied at the line of abutment indicated at 62 to insure shape retention and structural integrity.
Summarizing the steps in the method of FIGS. 8 through 10, a loop of formable material is positioned adjacent a pair of mandrels, the loop is tightened to firmly enclose the mandrels by pushing in on a portion of the loop with a ram, and the internal mandrels are pivoted around hinge points created in the loop to form a cross-section of cellular configuration. The mandrels may be removed or left in place, as desired.
Other shapes of mandrels can be used, as seen in FIGS. 11 and 12, a pair of mandrels 64 being illustrated which are characterized by a curvilinear exterior surface. The ram 66 utilized is also similarly configured. For convenience, the mandrels 64 rest within complemental depressions formed in the work table 68, and a structurally continuous band or loop 70 is disposed about the pair of mandrels 64, a portion of the loop 70 lies within a central depression or recess 72 formed in the work table 68. After the ram 66 is brought down upon the loop 70 to deform it into the recess 72, the ram 66 is left in place and an insert 74 is placed in overlying relation to the inplace ram 66. Next, the mandrels 64 are pivoted toward one another and into abutment with the insert 74 to form the structural member 76 shown in FIG. 12. If desired, the mandrels 64 and rams 66 can be made of lightweight foam material, for example, and left in place in the final structural member 76. This enables use of the assembly as a packing container for an elongated fragile member (not shown) disposed within the hollow central portion of the structural member 76. FIGS. 13 and 14 also illustrate this feature, the ram in this case being a pane of glass 78, or the like, sandwiched between foam material mandrels 80 which are pivoted towards one another from the positions of FIG. 13 to those of FIG. 14. This orients the continuous loop 82 into a generally square cross-section, with the fragile glass pane 78 cushioned by the mandrels 80.
FIG. 15 illustrates another apparatus using the present method, and comprising three mandrels 84 and a single ram 86, all of triangular shape. The lowermost mandrel 84 fits within a triangular trough provided in the work table 88, and the continuous band or loop 90 is disposed around all three mandrels 84, as illustrated, with pivotal movement of the outermost mandrels 84 producing the structural member 92 iilustrated in FIG. 16.
Referring now to FIGS. 17 and 18, and apparatus is illustrated which utilizes a pair of spaced apart mandrels 94 of circular cross-section. A continuous band or loop 96 or formable material is disposed about the mandrels 94, and is made of resin reinforced glass fiber or the like so that it becomes rigid upon curing. However, the formable material can be flexible, non-rigid material such as corrugated packing board or the like so that the structural member 98 illustrated in FIG. 18 is then useful as a carrier for transporting fragile items. In such a case the mandrels 94 and the ram 100 would constitute the fragile items to be shipped. A tie member 102 is adhesively bonded to the pivoted-together components to maintain them in their assembled relation, as will be apparent.
The foregoing illustrates the considerable variety of shapes and configurations which can be provided for the mandrels and rams to produce structural members of various configurations. In addition, a plurality of such structural members can 5 be joined together to form still more complex structures. Thus, in FIG. 19 a plurality of the structural members 52 of FIG. are arranged in nested, side-by-side, parallel relation. Facing skins 104 are bonded or otherwise attached to the structural members 52 to form a strong, lightweight, structural sandwich characterized by a truss-like cross-section defined by the assembled members 52. A variety of structural or decorative end uses for this and similarly fabricated structures will immediately suggest themselves to those skilled in the art. Many of these complex shapes and structures could not readily be fabricated in the prior art, being producible only by utilization of the method of the present invention.
The work table support for the mandrels of the various embodiments is largely schematic. In actual practice the mandrels would most likely be supported at their ends so as to permit the lengths or loop of formable material to move relative to the mandrels during the tensioning operation. Such relative movement will also be facilitated by providing lubrication, vibration, or the like of the mandrels and the rams.
The loop of formable material may also take the form of a vacuum tight bag to completely enclose a part, such as the I- beam, of FIG. 4. Utilizing the present method to tension the bag on the I-beam would facilitate a desirable intimate contact between the bag and the part, which is valuable for autoclave curing of certain reinforced plastic parts.
Various modifications and changes may be made with regard to the foregoing detailed description without departing from the spirit of the invention.
I claim:
1. The method of fabricating a structural member comprising the steps of:
arranging structurally continuous loop means about the exterior surfaces of a mandrel means comprising at least a pair of mandrels spaced apart to define a recess, with a portion of said loop means being formable and located in overlying relation to said recess;
moving rarn means against said portion of said loop means and into said recess to urge said portion into said recess and place said loop means under tension; and
pivoting said pair of mandrels toward one another and upon said ram means in said recess.
2. The method of fabricating a structural member comprising the steps of:
arranging structurally continuous loop means adjacent a mandrel means having a forming surface including a recess, at least a portion of said loop means being formable and located in adjacent relation to said recess, said loop means having a peripheral dimension less than the peripheral dimension of said forming surface; and
moving ram means against said portion of said loop means to urge said portion into said recess and place said loop means under sufficient tension throughout the length thereof that the remainder of said loop means is tightly urged against the periphery of said mandrel means.
3. The method according to claim 2 wherein said loop means are arranged about the exterior surfaces of said mandrel means and said exterior surfaces comprise said forming surface.
4. The method according to claim 3 wherein said mandrel means are left in place as an integral part of the structural member.
5. The method according to claim 3 including the additional step of removing said mandrel means to render the structural member hollow.
6. The method according to claim 3 wherein said mandrel means is I-shaped and the opposite channels thereof each constitute a separate said recess; wherein said ram means comprise a pair of confronting rams; and moving said rams toward each other to form said loop means against said mandrel means into a tensioned I-shape structural member.
10. The method according to claim 1 wherein said pair of mandrels and said rarn means are each characterized by a cireular cross section whereby they may be transported using said structural member as a carrier.
11. The method according to claim 8 and including the additional steps of arranging a plurality of said structural membeta in nested, side-by-side and parallel relation; and affixing I facing skins to said structural members to fonn a structural sandwich.

Claims (11)

1. The method of fabricating a structural member comprising the steps of: arranging structurally continuous loop means about the exterior surfaces of a mandrel means comprising at least a pair of mandrels spaced apart to define a recess, with a portion of said loop means being formable and located in overlying relation to said recess; moving ram means against said portion of said loop means and into said recess to urge said portion into said recess and place said loop means under tension; and pivoting said pair of mandrels toward one another and upon said ram means in said recess.
2. The method of fabricating a structural member comprising the steps of: arranging structurally continuous loop means adjacent a mandrel means having a forming surface including a recess, at least a portion of said loop means being formable and located in adjacent relation to said recess, said loop means having a peripheral dimension less than the peripheral dimension of said forming surface; and moving ram means against said portion of said loop means to urge said portion into said recess and place said loop means under sufficient tension throughout the length thereof that the remainder of said loop means is tightly urged against the periphery of said mandrel means.
3. The method according to claim 2 wherein said loop means are arranged about the exterior surfaces of said mandrel means and said exterior surfaces comprise said forming surface.
4. The method according to claim 3 wherein said mandrel means are left in place as an integral part of the structural member.
5. The method according to claim 3 including the additional step of removing said mandrel means to render the structural member hollow.
6. The method according to claim 3 wherein said mandrel means is I-shaped and the opposite channels thereof each constitute a separate said recess; wherein said ram means comprise a pair of confronting rams; and moving said rams toward each other to form said loop means against said mandrel means into a tensioned I-shape structural member.
7. The method according to claim 2 wherein said loop means are arranged adjacent interior surfaces of said mandrel means and said recess is defined by said interior surfaces.
8. The method according to claim 1 wherein said pair of mandrels and said ram means are each triangular in cross-section whereby said structural member is truss-like in construction.
9. The method according to claim 1 wherein said pair of mandrels and said ram means are each characterized by a curved exterior surface whereby said structural member may be formed circular in cross section.
10. The method according to claim 1 wherein said pair of mandrels and said ram means are each characterized by a circular cross section whereby they may be transported using said structural member as a carrier.
11. The method according to claim 8 and including the additional steps of arranging a plurality of said structural members in nested, side-by-side and parallel relation; and affixing facing skins to said structural members to form a structural sandwich.
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Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4238878A (en) * 1979-03-09 1980-12-16 Brooks & Perkins, Incorporated Method and apparatus for forming shroud
US5118531A (en) * 1987-12-18 1992-06-02 Uniroyal Chemical Company, Inc. Pumpability sealant composition
US6131362A (en) * 1998-02-04 2000-10-17 Buecker Machine & Iron Works, Inc. Sheet metal beam
US6289710B1 (en) * 1999-01-11 2001-09-18 Trw Automotive Japan Co., Ltd. Method of manufacturing a hollow rack bar
US6317979B1 (en) 1999-01-11 2001-11-20 Trw Automotive Japan Co. Ltd Method of manufacturing a hollow rack bar
US20130174396A1 (en) * 2012-01-10 2013-07-11 Manuel Torres Martinez Installation for manufacturing fibre stringers for aerospace structures
EP2743066A1 (en) * 2012-12-14 2014-06-18 AIRBUS HELICOPTERS DEUTSCHLAND GmbH Grid type element of open polygonal cells

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB191327121A (en) * 1913-11-25 1914-11-25 Harry Joyce Improvements in or relating to Stay or Frame Members suitable for use in the Construction of Cycles, Motor Cycles, Aeroplanes or the like.
US1173470A (en) * 1915-03-04 1916-02-29 Charles A Wiant Machine for making roofing-strip.
US1344105A (en) * 1915-06-12 1920-06-22 Durand Steel Locker Company Art of forming tubes
US1963057A (en) * 1930-10-03 1934-06-12 American Fork & Hoe Co Method of forming tubular structural elements
US2998339A (en) * 1955-12-23 1961-08-29 Foil Process Corp Production of tubes and structural shapes from metal foils
FR1306721A (en) * 1961-09-07 1962-10-19 Carnaud & Forges Manufacturing process of pallets for the transport of light goods and resulting pallets
US3298218A (en) * 1963-08-20 1967-01-17 Kelsey Hayes Co Method and apparatus for forming wheel rims and the like

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB191327121A (en) * 1913-11-25 1914-11-25 Harry Joyce Improvements in or relating to Stay or Frame Members suitable for use in the Construction of Cycles, Motor Cycles, Aeroplanes or the like.
US1173470A (en) * 1915-03-04 1916-02-29 Charles A Wiant Machine for making roofing-strip.
US1344105A (en) * 1915-06-12 1920-06-22 Durand Steel Locker Company Art of forming tubes
US1963057A (en) * 1930-10-03 1934-06-12 American Fork & Hoe Co Method of forming tubular structural elements
US2998339A (en) * 1955-12-23 1961-08-29 Foil Process Corp Production of tubes and structural shapes from metal foils
FR1306721A (en) * 1961-09-07 1962-10-19 Carnaud & Forges Manufacturing process of pallets for the transport of light goods and resulting pallets
US3298218A (en) * 1963-08-20 1967-01-17 Kelsey Hayes Co Method and apparatus for forming wheel rims and the like

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4238878A (en) * 1979-03-09 1980-12-16 Brooks & Perkins, Incorporated Method and apparatus for forming shroud
US5118531A (en) * 1987-12-18 1992-06-02 Uniroyal Chemical Company, Inc. Pumpability sealant composition
US6131362A (en) * 1998-02-04 2000-10-17 Buecker Machine & Iron Works, Inc. Sheet metal beam
US6289710B1 (en) * 1999-01-11 2001-09-18 Trw Automotive Japan Co., Ltd. Method of manufacturing a hollow rack bar
US6317979B1 (en) 1999-01-11 2001-11-20 Trw Automotive Japan Co. Ltd Method of manufacturing a hollow rack bar
US20130174396A1 (en) * 2012-01-10 2013-07-11 Manuel Torres Martinez Installation for manufacturing fibre stringers for aerospace structures
US8555945B2 (en) * 2012-01-10 2013-10-15 Manuel Torres Martinez Installation for manufacturing fibre stringers for aerospace structures
EP2743066A1 (en) * 2012-12-14 2014-06-18 AIRBUS HELICOPTERS DEUTSCHLAND GmbH Grid type element of open polygonal cells
KR101473977B1 (en) 2012-12-14 2014-12-17 에어버스 헬리콥터스 도이칠란트 게엠베하 Grid Type Fibre Composite Structure of Open Polygonal Cells
US9266304B2 (en) 2012-12-14 2016-02-23 Airbus Helicopters Deutschland GmbH Grid type element of open polygonal cells

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