| 序号 | 专利名 | 申请号 | 申请日 | 公开（公告）号 | 公开（公告）日 | 发明人 |
|---|---|---|---|---|---|---|
| 101 | Matrize zum Kaltverformen von Gegenständen | EP97109465.1 | 1997-06-11 | EP0812637A1 | 1997-12-17 | Stiebitz, Günter, c/o SWG Schraubenwerk |
Eine Matrize zum Kaltverformen von Gegenständen, insbesondere Befestigungselementen, enthält eine Fassung (1) mit einer schwach kegelförmigen Innenöffnung (3). In der Innenöffnung (3) werden durch eine leicht kegelförmige geschlitzte Büchse (5) Kernelemente (8,9,10) verpreßt, die vorzugsweise aus Hartmetall bestehen. Aufgrund des Einpressens durch eine geschlitzte Büchse (5) entsteht einerseits eine Vorspannung für die Kerne, andererseits können diese durch Herauspressen der Büchse (5) auch wieder ausgetauscht werden. |
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| 102 | A METHOD AND AN APPARATUS FOR MAKING SCREWS, RIVETS OR SIMILAR OBJECTS | EP93906461.4 | 1993-03-03 | EP0630302B1 | 1996-10-23 | NIELSEN, Ove |
| In a method of making screws, rivets or similar objects from a metal wire (6) the wire (6) is moved through a stationary cropping bushing (14) forwardly to a movable cropping bushing (24) present in a receiving position, following which the movable cropping bushing (24) is moved away from the receiving position substantially transversely to the axial direction of the wire to release a blank from the wire (6). The movable cropping bushing (24, 25) is then moved together with the released blank (26) further on to a discharge position, in which a punch (27) is adapted to move the blank (26) partly into a die (16) and to compress the blank (26) sufficiently to pre-upset it by cold flowing in the region between the die (16) and the movable cropping bushing (25). In an apparatus of making screws, rivets or similar objects the movable cropping bushing (24, 25) is secured to a transport device (15), by means of which it can be moved from a receiving position opposite the stationary bushing (14) to a discharge position opposite a die (16) between said die and a punch (27), which is adapted to move the blank (26) partly into the die (16) and to compress the blank (26) sufficiently to pre-upset it by cold flowing in the region between the die (16) and the movable cropping bushing (25). | ||||||
| 103 | Procédé et outillage de fabrication de rivets matricés | EP89400023.1 | 1989-01-04 | EP0323931A1 | 1989-07-12 | Colin, Bernard Albert Marie; Cortey, Michel Antoine Claudius |
Dans ce procédé, dans lequel on utilise une matrice (5') ayant une empreinte (4'), un poinçon (6') et un éjecteur (7'), on dispose l'extrémité de l'ébauche en appui contre une surface creuse (12) de forme complémentaire formée à une extrémité d'un organe formant éjecteur (7') monté coulissant et réglable dans ladite empreinte (4'), on exerce une pression de matriçage sur l'extrémité opposée du rivet et on éjecte le rivet au moyen dudit éjecteur (7'). |
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| 104 | METHOD OF MANUFACTURING SELF-PIERCE RIVETS | US15573412 | 2016-05-13 | US20180117666A1 | 2018-05-03 | Russell John Trinick |
| A method of manufacturing self-pierce rivets from a length of wire comprises separating the length of wire to form a plurality of slugs, each slug defining a head end and a tail end. The method further comprises forging a plurality of rivets from the slugs, each rivet having a head formed from the head end of a slug and a tip formed from the tail end of that slug, the head and the tip of the rivet being separated by a shank which defines a longitudinal axis, the rivet having a bore which runs substantially longitudinally through the tip and at least part way along the shank. For each of the plurality of rivets, the method comprises performing a machining operation on the tip the rivet or on the tail end of the slug from which the rivet was forged. | ||||||
| 105 | METHOD OF FORMING A HIGHLY-DEFORMABLE TITANIUM OR TITANIUM-ALLOY ONE-PIECE FASTENER | US15479848 | 2017-04-05 | US20170203356A1 | 2017-07-20 | Steven G. Keener |
| A method of forming a fastener includes inserting a blank precursor into a bore of a forming die having an enlarged bore portion, applying a first axial compression force to the blank precursor, and forming a cold-worked head section and an enlarged shank portion on the blank precursor corresponding to the enlarged bore portion. The enlarged shank portion has a nominal shank portion extending therefrom. The method additionally includes inserting the nominal shank portion into a bore of a final reduction die, applying a second axial compression force to the enlarged shank portion, and urging the enlarged shank portion into the bore of the final reduction die. The method includes reducing a cross-sectional area of the enlarged shank portion by approximately 2 to 5 percent to form a cold-worked shank section. | ||||||
| 106 | Connecting element and method for manufacturing a connecting element | US13558658 | 2012-07-26 | US09062702B2 | 2015-06-23 | Roland Wendt; Michael Badent; Wolfgang Pfeiffer; Ewald Wennehorst; Karlheinz Munz |
| A connecting element for forming a punch-riveted connection of at least two component sections is provided, wherein a foot section has at its free end a foot base with a basic shape which is cylindrical or at least approximated to the cylindrical shape. According to the invention, an annular circumferential elevated portion is formed in the foot section between the foot base and the shaft section. | ||||||
| 107 | Self-attaching fastener manufacturing apparatus and method | US13815996 | 2013-03-21 | US20140287842A1 | 2014-09-25 | Mark J. GOTTSCHALL; James A. NICODEMUS; Frederick J. RATERMANN |
| The present invention is an assembly line for continuously manufacturing self-attaching fasteners from a metal rod having a predetermined profile. The self-attaching fasteners are joined together with wires and reeled onto spools for use at a secondary installation site. More importantly the invention is an improved streamline method and apparatus which produces burr-free self-attaching fasteners, without deformation, and joins the self-attaching fasteners and wires together within a die press. | ||||||
| 108 | Hybrid fastening system | US12206283 | 2008-09-08 | US07654909B2 | 2010-02-02 | Steven G. Keener; Cesare Peralta |
| A hybrid fastening system comprising a female fastener component, i.e., swage collar, fabricated from a titanium or titanium-alloy material, preferably Ti-3Al-2.5V, and a mating titanium or titanium-alloy material male fastener component, i.e., threaded pin, each preferably pre-coated with an organic coating material comprising an organic, phenolic resin. The threaded pin component is installed through two or more structural components to be joined. The swage collar component is then deformed or swaged onto the threads of the pre-coated threaded pin component to achieve the same, if not improved, fastener/joint performance characteristics of existing lockbolt systems using aluminum-alloy material swage collar components. | ||||||
| 109 | Method of preparing ultra-fine grain metallic articles and metallic articles prepared thereby | US11114457 | 2005-04-26 | US07077755B2 | 2006-07-18 | Steven G. Keener; Max R. Runyan |
| An apparatus and method are provided for angularly extruding a workpiece through a die to form blanks and articles having refined grain structure. The die is also used to form the workpiece to a desired shape, such as a cylinder. The angular extrusion method can be used in place of some heat treatments, thereby lowering the cost and time for manufacturing articles. The method is compatible with materials with high strength-to-weight ratios such as aluminum, titanium, and alloys thereof. The blanks can be used to form articles having favorable mechanical properties such as strength, toughness, formability, and resistance to fatigue, corrosion, and thermal stresses. | ||||||
| 110 | Method of preparing ultra-fine grain metallic articles and metallic articles prepared thereby | US10331672 | 2002-12-30 | US06912885B2 | 2005-07-05 | Steven G. Keener; Max R. Runyan |
| An apparatus and method are provided for angularly extruding a workpiece through a die to form blanks and articles having refined grain structure. The die is also used to form the workpiece to a desired shape, such as a cylinder. The angular extrusion method can be used in place of some heat treatments, thereby lowering the cost and time for manufacturing articles. The method is compatible with materials with high strength-to-weight ratios such as aluminum, titanium, and alloys thereof. The blanks can be used to form articles having favorable mechanical properties such as strength, toughness, formability, and resistance to fatigue, corrosion, and thermal stresses. | ||||||
| 111 | Rivets and methods for their production and use | US10204816 | 2002-08-23 | US20030177626A1 | 2003-09-25 | Cedric Berkeley Paynter |
| There is provided self piercing rivet comprising a substantially planar metal body portion (160) having deformable tabs (161) symmetrically disposed about a slit (162) as per the first embodiment. The upper portion of the body portion (160) is provided with a V-shaped recess (163) diverging from a point (164) adjacent the centreline of the body portion (160) and terminating at the upper edge (165) of the body portion (160). The V-shaped recess (163) divides the upper portion of the body portion (160) into head tabs (166) disposed to each side of the body portion (160). The upper remaining edges of the head tabs (166) enable the rivet to be partially driven and then set by deformation of the deformable tabs (161) and the head tabs (166) against respective sides of the riveted workpiece. Methods of producing the rivets and tools for their use are also provided. | ||||||
| 112 | Method for preparing ultra-fine grain titanium and titanium-alloy articles and articles prepared thereby | US10022882 | 2001-12-18 | US20030111147A1 | 2003-06-19 | Steven G. Keener; Edward Litwinski |
| A method for preparing ultra-fine grain titanium or titanium-alloy articles used for adjoining or assembling of detail components. Coarse-grained titanium or titanium-alloy materials typically are heated and forced under constant pressure through a friction stir processing tooling device containing a stirring chamber and a stirring rod. As the material is passed through the stirring chamber, the stirring rod solutionizes the titanium or titanium-alloy material and stirs the material to obtain a homogeneous or uniform material condition. As the processed material exits the stirring chamber of the friction stir process tooling device, it reconsolidates as an extremely homogeneous structure possessing ultra-fine grain structure. Titanium or titanium-alloy materials having been processed to achieve such ultra-fine grain material structure may then be manufactured into aerospace structural articles or components such as fasteners or articles that do not require a subsequent thermal or heat-treatment steps. The resulting fasteners, articles or components have improved material performance characteristics associated with this ultra-fine grain material structure. | ||||||
| 113 | Method for preparing pre-coated aluminum alloy articles and articles prepared thereby | US09570651 | 2000-05-15 | US06403230B1 | 2002-06-11 | Steven G. Keener |
| An aluminum-alloy article such as a fastener is prepared by providing an aluminum-alloy article precursor that is not in its final heat-treated state, and in one form is in its solution treated/annealed state. A curable organic coating material is also provided. The method includes anodizing the article precursor, preferably in chromic acid solution and without chemical sealing during anodizing, applying the organic coating material to the aluminum-alloy article precursor, and precipitation heat-treating the coated aluminum article precursor to its final heat-treated state, thereby simultaneously curing the organic coating. If the aluminum alloy temper is of the naturally aging type, it is optionally lightly deformed prior to precipitation treatment aging. The approach may also be applied to articles that are not solution treated/annealed and aged, by first overly deforming the article precursor so that the curing treatment of the coating also partially anneals the article precursor to the final desired deformation state. | ||||||
| 114 | Fatigue resistant, fluid tight rivet assembly | US09915245 | 2001-07-25 | US20010052178A1 | 2001-12-20 | Ralph Luhm |
| The present invention comprises aluminum solid rivets and methods of manufacturing aluminum solid rivets for aircraft and other demanding applications to provide rivets with high strength and excellent driveabiltity while improving the rivets' resistance to fatigue and stress corrosion cracking. In accordance with the method, an aluminum rivet blank approximately the same diameter as the head of the finished rivet is used. This rivet blank is forced into a die to extrude the tapered region and the shank of the finished rivet. The fabrication process provides more uniform cold working at the junction of the shank and the tapered region of the rivet, and better orients the flow lines in this region. The process also can provide a superior surface finish, and may be suitable for use in wet wing fabrication without further processing for improved surface finish. Alternate embodiments are disclosed. | ||||||
| 115 | Method for preparing pre-coated aluminum alloy articles and articles prepared thereby | US634748 | 1996-04-26 | US5858133A | 1999-01-12 | Steven G. Keener |
| An aluminum-alloy article such as a fastener is prepared by providing an aluminum-alloy article precursor that is not in its final heat-treated state, and in one form is in its solution treated/annealed state. A curable organic coating material is also provided. The method includes anodizing the article precursor, preferably in chromic acid solution and without chemical sealing during anodizing, applying the organic coating material to the aluminum-alloy article precursor, and precipitation heat-treating the coated aluminum article precursor to its final heat-treated state, thereby simultaneously curing the organic coating. If the aluminum alloy temper is of the naturally aging type, it is optionally lightly deformed prior to precipitation treatment aging. The approach may also be applied to articles that are not solution treated/annealed and aged, by first overly deforming the article precursor so that the curing treatment of the coating also partially anneals the article precursor to the final desired deformation state. | ||||||
| 116 | Method of forming a rivet of titanium-columbium alloy | US590693 | 1975-06-26 | US3975786A | 1976-08-24 | Roland Howard Gapp; Rahmatollah Fakhri Toosky; Ira Bill Lee York |
| A high strength buckable rivet made of an alloy consisting of titanium and columbium, the optimum proportion being about 55% titanium and about 45% columbium. The method of making this rivet includes the steps of cold forming a cylindrical blank so as to form a head and shank of the rivet and cold working the head and a portion of a shank of the rivet so as to leave a ductile tail portion capable to form a buck tail, the optimum length of the ductile portion being about 0.8 times the diameter of the rivet shank. | ||||||
| 117 | Method of manufacturing a fastener such as a bolt, rivet, or the like | US14009371 | 1971-05-04 | US3828382A | 1974-08-13 | NAKAMURA Y |
| A method of manufacturing a fastener such as bolt, rivet and the like having an integrated flange on the head. The flange may be made of any metal and in any form, but must have a central flat part where it is integrated with the head. The head is two stage cold headed. After a first flowing cold heading, the head is inserted into an opening in the central flat part of the flange and finishing cold headed simultaneously with the integration of the flange on the head so that flow of structure of the head partly surrounds the part of the flange received in the head.
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| 118 | Manufacture of composite materials | US3634934D | 1968-12-26 | US3634934A | 1972-01-18 | FITZGERALD WILLIAM M B |
| A welded composite formed by cutting and heating continuous lengths of wire and immediately transferring the lengths to a die where the lengths are joined by pressing at high pressure and the joined lengths are then forced at least a portion of the way out of the die where heading operations are performed.
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| 119 | Die,and method of manufacturing calibrated rivets | US3570031D | 1967-05-25 | US3570031A | 1971-03-16 | AURIOL ELOI |
| A GUN-SHAPED DIE FOR MANUFACTURING RIVETS MADE OF AN ELASTIC ETAL HAVING AT ONE END A SLIGHTLY INWARDLY TAPER ING FLANGE MEMBER AND AT THE OTHER END A FLANGE MEMBER APPROXIMATELY TWICE AS GREAT OR GREATER IN DIAMETER THAN THE INWARDLY TAPERING FLANGE MEMBER. THE PORTION OF THE GUN-SHAPED DIE BOUNDED BETWEEN THE TWO FLANGE MEMBERS HAS A THICKNESS SUFFICIENT TO WITHSTAND ELASTIC DEFORMATIONS AND GENERALLY THE THICKNESS OF THIS PORTION WILL BE APPROXIMATELY EQUAL TO THE BORE OF THE DIE.
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| 120 | Method and apparatus for forming composite electrical contacts | US48236365 | 1965-08-25 | US3397454A | 1968-08-20 | GWYN JR CHILDRESS B |
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