US2408596A - Method of forming cylinder ends - Google Patents

Method of forming cylinder ends Download PDF

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Publication number
US2408596A
US2408596A US526253A US52625344A US2408596A US 2408596 A US2408596 A US 2408596A US 526253 A US526253 A US 526253A US 52625344 A US52625344 A US 52625344A US 2408596 A US2408596 A US 2408596A
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Prior art keywords
tool
workpiece
fissure
forming cylinder
point
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Expired - Lifetime
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US526253A
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Joseph J Bednar
Steven P Peck
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National Tube Co
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National Tube Co
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Priority to US526253A priority Critical patent/US2408596A/en
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Publication of US2408596A publication Critical patent/US2408596A/en
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    • 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
    • B21D41/00Application of procedures in order to alter the diameter of tube ends
    • B21D41/04Reducing; Closing
    • B21D41/045Closing

Definitions

  • This invention relates to an improved method of spinning integral ends oncylindersto adapt them for high-pressure service.
  • One object of the present invention is to provide a method for building up the thickness of an end section of a tube or cylinder which will adapt it for high-pressure service.
  • a further object isv to provide a method involving the building up of the end thickness of a cylinder by spinning and subsequently eliminat ing the fissure or feathers formed in the region of the original point of juncture of the end edges.
  • our improved method involves spinning integral closed ends on tubular metal workpieces to form a closure capable of withstanding a pressure of 2500 pounds per square inch or greater, the method.
  • Figure 7 illustrates a step in the method wherein the mid-portion of the built-up metal of increasedthickness is forced inwardly into engagement with a die member.
  • Figure 8 illustrates the step of removing feather-like portions resulting from the operation of Figure 7.
  • Figure 9 is a detail portion of an end of a cylinder made in accordance with the herein claimed method.
  • l0 represents a conventional form of chuck adapted to grip a tubular or cylindrical workpiece l2.
  • This chuck is rotatably supported by a suitable spindle M of conventional form Which is rotated by any suitable means such as a belt l6 connected to a power drive (not shown).
  • the chuck and its driving means are adapted to rotate the tubular workpiece I2 at a speed of approximately 1400 R. P. M. Mounted in juxtaposition with the extending from the periphery toward the longi- Y tudinal axis'of the workpiece, also moving the tool axially of the workpiece, to bring the end edges of said workpieceforcibly into abutment. in the region of the longitudinal'axis thereof,
  • Figure 1 is a plan view of conventional apparatus suitable for carrying out the present invention.
  • an initial step of the imchuck I 0 is a tool bed [8 having slidably mounted thereon a table 20 which canbe reciprocated back and forth by any suitable means in the direction lengthwise of the work.
  • a compound tool rest. 22 is pivoted at 24 at 1 a, point'ecccntri tothe longitudinal axis of the workpiece I2.
  • the tool rest carries a slide 26 which supports a tool holder 2,8 carrying a tool 30 which is preferably, although not necessarily, in the form of a roller pivotally mounted in a bearing 32, so that the tool can make a, rolling contact with the end portion of the tubular workpiece l2.
  • the end portion of the workpi ce will usually be locally heated, for example, by the impingement of flames from oxyacetylene torches such as indicated at 34 and 36.
  • the torches are eifective to maintain the end of the workpiece at the optimum spinning temperature of approximately 2000 to 2200 F.
  • the torch 36 is mounted adjacent the compound rest 22, and the torch 34 is mounted on any stationary portion of the apparatus.
  • the tool 30 is moved to the position of Figure 2, where the leading edge of the periphery of the tubular workpiece is engaged.
  • the tool rest 22 is swung about its pivot 24; for example, from the position of Figure 2 to the position of Figure i3, through the arcuate path indicated by the dotted arc a:.y, the tool'at this time swinging about a radius r struck from the center 24 which,
  • the tool 30 is moved back and forth along its arcuate path several times, with the result that metal from the outer normally cylindrical portion is flowed inwardly, thus thickening the end region of the tubefrom the normal gauge of the workpiecetothe thickened condition suggested in Figure 3.
  • Subsequent arcuate sweeps or the tool 3!] with an accompanying endwise movement of the tool toward the work gradually spins in the end of the tube'until it is substantially closed, as shown in r stroke of the tool 38 is then increased to the position such as suggested in Figure 5, thus completely closing the tube end and bringing the Figure 4.
  • the workpiece Upon completion of the operation represented in Figure 6, the workpiece is removed from the chuck l and the end thereof is entered into the cavity 38 of a die 4!). Thereupon another die 42 having a central recess 44 therein is forced inwardly, withthe result that featherlike portions 46 located in the longitudinal central axial region "of'the' workpiece and flanking the central fissure, are forced inwardly into, the recess 44 of the die 42'. moved and the work-piece is disengaged from the die '42.
  • the workpiece is then chucked in a suitable metal working tool such'as a lathe or the like, and a cutter bar 48 centered byaguide rest and carrying a spade or similar cutting tool 52 is brought into play, so as to machine Ifhedie 42 is then re solid section free from physical off the projecting feather-like portions which flank the fissure.
  • a suitable metal working tool such'as a lathe or the like
  • a cutter bar 48 centered byaguide rest and carrying a spade or similar cutting tool 52 is brought into play, so as to machine Ifhedie 42 is then re solid section free from physical off the projecting feather-like portions which flank the fissure.
  • the interior of the cylinder will have the finished face 54 and the exterior will have a dished cavity 56, as shown in Figure 9.
  • a method of spinning closed ends on tubular metal workpieces comprising rotating the workpiece and applying a work-engaging tool to the end portion thereof, moving said tool through arcs extending from the periphery toward'the longitudinal axis of the workpiece, moving said tool longitudinally of the axis of the workpiece to bring the end edges of said workpiece into abutment in the region of the longitudinal axis thereof, and thereafter continuing the movement of said tool in-arcs extending from the periphery tothe point beyond'the longitudinal axis of the workpiece to upset said end portion and build upmetal of substantial thickness without a fissure outside the original point or juncture of said edges, stopping rotation of the workpiece, then extrudingthe axial portion of said closed end inwardly'into an axial cavityin a die memher in the'region of the point of juncture of said edges," said extruding step causing featherlike portions to be forced axially into said die cavity, and finally removing said axially extru

Description

Def. *1, 1946. J; J. BEDNAR EI'AL ,40 6
METHOD'OF FORMING CYLINDER ENDS Filed March 13, 1944 '2 Sheets-Sheet l Oct. 1, 1946. J. J. BEDNAR EI'AL 2,408,596 METHOD OF FORMING CYLINDER ENDS- Filed March 13, 1944 2 Sheets-Sheet? 721545 Mal mi.
fizveizzarsx bals /7' J. 1950/1 46 m4 firm 5v PECK,
Patented Oct. 1, 1946 2,408,596 I METHOD OF FORMING CYLINDER ENDS Joseph J. Bedna and Steven P. Peck, McKeesport, 2a., assig'nors, to National Tube Company, a corpora ion of. New J ersey Application March 13, 1944, Serial No. 526,253
2, Claims, (Cl. 29-1482) This invention relates to an improved method of spinning integral ends oncylindersto adapt them for high-pressure service.
Heretofore the spinning of cylinder ends has been quite definitely restricted touse on small cylinders suited only for low-pressure work. One object of the present invention is to provide a method for building up the thickness of an end section of a tube or cylinder which will adapt it for high-pressure service.
A further object isv to provide a method involving the building up of the end thickness of a cylinder by spinning and subsequently eliminat ing the fissure or feathers formed in the region of the original point of juncture of the end edges.
As will appear more fully hereinafter, our improved method involves spinning integral closed ends on tubular metal workpieces to form a closure capable of withstanding a pressure of 2500 pounds per square inch or greater, the method.
being characterized by rotating the workpiece while. applying a work-engaging tool to the end portion thereof, moving said tool through arcs 2 dition of the tube orcylinder and the difierent stages in the operation of the method.
Figure 7 illustrates a step in the method wherein the mid-portion of the built-up metal of increasedthickness is forced inwardly into engagement with a die member.
Figure 8 illustrates the step of removing feather-like portions resulting from the operation of Figure 7.
Figure 9 is a detail portion of an end of a cylinder made in accordance with the herein claimed method.
Referring in detail to the drawings, l0 represents a conventional form of chuck adapted to grip a tubular or cylindrical workpiece l2. This chuck is rotatably supported by a suitable spindle M of conventional form Which is rotated by any suitable means such as a belt l6 connected to a power drive (not shown). The chuck and its driving means are adapted to rotate the tubular workpiece I2 at a speed of approximately 1400 R. P. M. Mounted in juxtaposition with the extending from the periphery toward the longi- Y tudinal axis'of the workpiece, also moving the tool axially of the workpiece, to bring the end edges of said workpieceforcibly into abutment. in the region of the longitudinal'axis thereof,
' cry to a point beyond the longitudinal axis of the workpiece, so as to upset said end portion and thereafter continuing the movement of said tocl in arcuate paths extending from the periphand build up metal of increased thickness without a fissure outside the original point of juncture of said edges, then stopping the rotating and thereafter pressing the mid-portion of the closed end inwardly into engagement with a die memher having an axial recess opposite the point of juncture of said edges, whereby feather-like portions in the axial region adjacent said point of juncture are pressed into said recess, and thereafter removing said feather-like portions.
For a full understanding of the invention, reference should be made to the following detailed disclosure, the accompanying drawings, and the appended claims.
In the drawings:
Figure 1 is a plan view of conventional apparatus suitable for carrying out the present invention.
an initial step of the imchuck I 0 is a tool bed [8 having slidably mounted thereon a table 20 which canbe reciprocated back and forth by any suitable means in the direction lengthwise of the work.
A compound tool rest. 22 is pivoted at 24 at 1 a, point'ecccntri tothe longitudinal axis of the workpiece I2. The tool rest carries a slide 26 which supports a tool holder 2,8 carrying a tool 30 which is preferably, although not necessarily, in the form of a roller pivotally mounted in a bearing 32, so that the tool can make a, rolling contact with the end portion of the tubular workpiece l2. Prior to the operations about to be described, the end portion of the workpi ce will usually be locally heated, for example, by the impingement of flames from oxyacetylene torches such as indicated at 34 and 36. The torches are eifective to maintain the end of the workpiece at the optimum spinning temperature of approximately 2000 to 2200 F. The torch 36 is mounted adjacent the compound rest 22, and the torch 34 is mounted on any stationary portion of the apparatus.
In starting the improved method, after the work is properly heated, the tool 30 is moved to the position of Figure 2, where the leading edge of the periphery of the tubular workpiece is engaged. After such engagement the tool rest 22 is swung about its pivot 24; for example, from the position of Figure 2 to the position of Figure i3, through the arcuate path indicated by the dotted arc a:.y, the tool'at this time swinging about a radius r struck from the center 24 which,
as shown, is in plan and is offset from the longitudinal central axis of the workpiece [2.
The tool 30 is moved back and forth along its arcuate path several times, with the result that metal from the outer normally cylindrical portion is flowed inwardly, thus thickening the end region of the tubefrom the normal gauge of the workpiecetothe thickened condition suggested in Figure 3. Subsequent arcuate sweeps or the tool 3!] with an accompanying endwise movement of the tool toward the work gradually spins in the end of the tube'until it is substantially closed, as shown in r stroke of the tool 38 is then increased to the position such as suggested in Figure 5, thus completely closing the tube end and bringing the Figure 4. Ihe arcuate end edges initially into abutment in the irri'mediate region of the longitudinal axis of the workpiece l2. At this stage of the methodfithere will be present a fissure f in the zone of initial abutment of the end edges of the tube. Thereafter the tool 30 is given a plurality of additional arcuate sweeps to the position indicated in Figure 6, where the working face of the tool crosses the longitudinal axis of the end of' the workpiece. This is for the purpose of building up worked metal of substantial thickness without 'a-fis'sure, beyond the original point of juncture of the end edges. This condition is illustrated in Figure 6, wherein it is noted that the fissure ends at the'point j, and the metal beyond that point is entirely devoid of a'fissure and is thus rendered more dense so that it is thereby made capable ofwithstanding' considerable pressure.
Upon completion of the operation represented in Figure 6, the workpiece is removed from the chuck l and the end thereof is entered into the cavity 38 of a die 4!). Thereupon another die 42 having a central recess 44 therein is forced inwardly, withthe result that featherlike portions 46 located in the longitudinal central axial region "of'the' workpiece and flanking the central fissure, are forced inwardly into, the recess 44 of the die 42'. moved and the work-piece is disengaged from the die '42. The workpiece is then chucked in a suitable metal working tool such'as a lathe or the like, and a cutter bar 48 centered byaguide rest and carrying a spade or similar cutting tool 52 is brought into play, so as to machine Ifhedie 42 is then re solid section free from physical off the projecting feather-like portions which flank the fissure. At the conclusion of this operation the interior of the cylinder will have the finished face 54 and the exterior will have a dished cavity 56, as shown in Figure 9.
It will be understood that in the machine operation of Figure 8, the feathers 46 flankin the fissure .willbe eliminated. .Thus the end closure or bottom of the cylinder is a dense homogeneous defects and sumcient to withstand high commercial test pressures of the order of 2500 to 3500 pounds per square inch.
While we have shown and described precise operating steps, it is to be understood that the drawings and descriptive matter are to be interpreted in an illustrative rather than a limiting sense, since various modifications may be made within the scope of the appended claims.
We claim: 7
l, A method of spinning closed ends on tubular metal workpieces, comprising rotating the workpiece and applying a work-engaging tool to the end portion thereof, moving said tool through arcs extending from the periphery toward'the longitudinal axis of the workpiece, moving said tool longitudinally of the axis of the workpiece to bring the end edges of said workpiece into abutment in the region of the longitudinal axis thereof, and thereafter continuing the movement of said tool in-arcs extending from the periphery tothe point beyond'the longitudinal axis of the workpiece to upset said end portion and build upmetal of substantial thickness without a fissure outside the original point or juncture of said edges, stopping rotation of the workpiece, then extrudingthe axial portion of said closed end inwardly'into an axial cavityin a die memher in the'region of the point of juncture of said edges," said extruding step causing featherlike portions to be forced axially into said die cavity, and finally removing said axially extruded feather-like portions; I i
' 2; The method of claim 1, further characterized-- by the step of facilitating the upsetting operation bydirecting heat locally against the end. portion of the workpiece while actuating said tool to upset the end portion of the work.
JOSEPH J. -BEDNAR. STEVEN P. PECK.
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Cited By (39)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2603177A (en) * 1950-04-05 1952-07-15 Ite Circuit Breaker Ltd Method of making metallic television tube bodies
US2653683A (en) * 1947-09-27 1953-09-29 Houdaille Hershey Corp Telescopic shock absorber
US2671348A (en) * 1951-08-31 1954-03-09 Adamson Stephens Mfg Co Live shaft idler pulley
US2699596A (en) * 1948-06-09 1955-01-18 Union Carbide & Carbon Corp Process of making gas pressure cylinders having walls with improved uniformity in thickness
US2789344A (en) * 1951-04-23 1957-04-23 American Radiator & Standard Method of cold shaping tubular steel articles and product
US2900712A (en) * 1956-07-20 1959-08-25 Keating Mfg Corp Method of making sealed metallic containers
US3098461A (en) * 1959-08-12 1963-07-23 Crescent Machine & Nipple Comp Tube shaping machine
US3104640A (en) * 1954-09-09 1963-09-24 Lodge & Shipley Co Metal working
US3196655A (en) * 1962-09-14 1965-07-27 Laystall Eng Co Ltd Liners or sleeves for engine cylinders and the like
US3348398A (en) * 1964-02-20 1967-10-24 Ohio Brass Co Manufacturing valve balls
US3496747A (en) * 1967-09-21 1970-02-24 Nordberg Manufacturing Co Numerically controlled spinning machine
US3685475A (en) * 1969-09-17 1972-08-22 Neill K Banks Jr Process for producing cup-shaped thin-walled metal wares
US3793863A (en) * 1971-07-09 1974-02-26 D Groppini Device for the manufacture of metal cylinders
US4032281A (en) * 1974-02-04 1977-06-28 Oscar Rakovsky Thermoplastic tubular container forming apparatus
US4361360A (en) * 1979-03-05 1982-11-30 Siegfried Kuether Tube end forging process
EP0081700A1 (en) * 1981-11-20 1983-06-22 Air Products And Chemicals, Inc. Spin forming
US4470281A (en) * 1980-06-26 1984-09-11 Kramotorsky Industrialny Institut Method of forming end face wall having concentric recess in tubular workpiece
US4627257A (en) * 1980-05-05 1986-12-09 Coilco, Inc. Tube spin close apparatus
US5069865A (en) * 1990-12-14 1991-12-03 Westinghouse Electric Corp. Method of forming a gripper cavity in a fuel rod end plug
US5085131A (en) * 1990-10-02 1992-02-04 Prime Tube, Inc. Hydraulic cylinder for automotive steering systems and the like
US5218849A (en) * 1990-05-18 1993-06-15 Zeppelin-Metallwerke Gmbh Process and device for metal spinning
US5235837A (en) * 1991-04-19 1993-08-17 Compression Technologies, Inc. Fabrication of pressure vessels
WO1996013347A1 (en) * 1994-10-26 1996-05-09 Tandem Systems, Inc. System for constricting a tube wall
EP0769337A1 (en) * 1995-10-18 1997-04-23 MAGNETI MARELLI CLIMATIZZAZIONE S.r.l. A method of closing an end of a metal pipe
WO2000062953A1 (en) * 1999-04-21 2000-10-26 Tandem Systems, Inc. Method for spin forming a tube
US6169268B1 (en) 1998-12-30 2001-01-02 Esterline & Sons, Inc. Method and apparatus for forming the ends of metallic tubes
FR2859654A1 (en) * 2003-09-11 2005-03-18 Ems Societe Metallic tube end sealing method, involves applying flat rotating tool at plane front side of work against preformed opening to drive material of tube towards center of opening and close it
US20070028915A1 (en) * 2005-08-03 2007-02-08 Alberto Bellomo Gas manifold for a cooking range, with a pipe closure
US20070093793A1 (en) * 2005-10-11 2007-04-26 Maurer Robert S Jr Microsurgical probe
FR2922128A1 (en) * 2007-10-11 2009-04-17 Peugeot Citroen Automobiles Sa Metallic fluid tube closing method for forming pressurized oil body of hydraulic shock absorber of automobile, involves locally deforming deposit channel of closed end of tube, where tube is not sealed to fluid
US20110089682A1 (en) * 2009-10-16 2011-04-21 Walter Bauer Method for manufacturing a wall connector
CN102921823A (en) * 2012-11-26 2013-02-13 宁波培源电器制造有限公司 Oil storing barrel sealing machine of motorcycle rear shock absorber
US20130247635A1 (en) * 2010-12-07 2013-09-26 Leifeld Metal Spinning Ag Method for forming a pipe section
JP2014188522A (en) * 2013-03-26 2014-10-06 Nippon Spindle Mfg Co Ltd Method for molding cylindrical material
US20150223979A1 (en) * 2012-08-28 2015-08-13 Mani, Inc. Vitreous body surgical probe and method of manufacturing same
US10105746B1 (en) * 2015-09-14 2018-10-23 Shoals Tubular Products, Inc. Tube end sealing method
US20190030973A1 (en) * 2016-03-30 2019-01-31 Nhk Spring Co., Ltd. Hollow coil spring and suspension device for vehicle
US11278946B2 (en) * 2018-09-27 2022-03-22 Inno-Spin LLC Multi-axis roll-forming methods, systems, and products
US11701943B2 (en) 2016-03-30 2023-07-18 Nhk Spring Co., Ltd Method of manufacturing a hollow spring member

Cited By (52)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2653683A (en) * 1947-09-27 1953-09-29 Houdaille Hershey Corp Telescopic shock absorber
US2699596A (en) * 1948-06-09 1955-01-18 Union Carbide & Carbon Corp Process of making gas pressure cylinders having walls with improved uniformity in thickness
US2603177A (en) * 1950-04-05 1952-07-15 Ite Circuit Breaker Ltd Method of making metallic television tube bodies
US2789344A (en) * 1951-04-23 1957-04-23 American Radiator & Standard Method of cold shaping tubular steel articles and product
US2671348A (en) * 1951-08-31 1954-03-09 Adamson Stephens Mfg Co Live shaft idler pulley
US3104640A (en) * 1954-09-09 1963-09-24 Lodge & Shipley Co Metal working
US2900712A (en) * 1956-07-20 1959-08-25 Keating Mfg Corp Method of making sealed metallic containers
US3098461A (en) * 1959-08-12 1963-07-23 Crescent Machine & Nipple Comp Tube shaping machine
US3196655A (en) * 1962-09-14 1965-07-27 Laystall Eng Co Ltd Liners or sleeves for engine cylinders and the like
US3348398A (en) * 1964-02-20 1967-10-24 Ohio Brass Co Manufacturing valve balls
US3496747A (en) * 1967-09-21 1970-02-24 Nordberg Manufacturing Co Numerically controlled spinning machine
US3685475A (en) * 1969-09-17 1972-08-22 Neill K Banks Jr Process for producing cup-shaped thin-walled metal wares
US3793863A (en) * 1971-07-09 1974-02-26 D Groppini Device for the manufacture of metal cylinders
US4032281A (en) * 1974-02-04 1977-06-28 Oscar Rakovsky Thermoplastic tubular container forming apparatus
US4361360A (en) * 1979-03-05 1982-11-30 Siegfried Kuether Tube end forging process
US4627257A (en) * 1980-05-05 1986-12-09 Coilco, Inc. Tube spin close apparatus
US4470281A (en) * 1980-06-26 1984-09-11 Kramotorsky Industrialny Institut Method of forming end face wall having concentric recess in tubular workpiece
EP0081700A1 (en) * 1981-11-20 1983-06-22 Air Products And Chemicals, Inc. Spin forming
US5218849A (en) * 1990-05-18 1993-06-15 Zeppelin-Metallwerke Gmbh Process and device for metal spinning
US5085131A (en) * 1990-10-02 1992-02-04 Prime Tube, Inc. Hydraulic cylinder for automotive steering systems and the like
US5069865A (en) * 1990-12-14 1991-12-03 Westinghouse Electric Corp. Method of forming a gripper cavity in a fuel rod end plug
US5235837A (en) * 1991-04-19 1993-08-17 Compression Technologies, Inc. Fabrication of pressure vessels
WO1996013347A1 (en) * 1994-10-26 1996-05-09 Tandem Systems, Inc. System for constricting a tube wall
US5598729A (en) * 1994-10-26 1997-02-04 Tandem Systems, Inc. System and method for constructing wall of a tube
US5845527A (en) * 1994-10-26 1998-12-08 Tandem Systems, Inc. System and method for constricting wall of a tube
CN1066987C (en) * 1994-10-26 2001-06-13 坦德姆系统公司 System for constricting tube wall
EP0769337A1 (en) * 1995-10-18 1997-04-23 MAGNETI MARELLI CLIMATIZZAZIONE S.r.l. A method of closing an end of a metal pipe
US6169268B1 (en) 1998-12-30 2001-01-02 Esterline & Sons, Inc. Method and apparatus for forming the ends of metallic tubes
US6212926B1 (en) 1999-04-21 2001-04-10 Tandem Systems, Inc. Method for spin forming a tube
WO2000062953A1 (en) * 1999-04-21 2000-10-26 Tandem Systems, Inc. Method for spin forming a tube
FR2859654A1 (en) * 2003-09-11 2005-03-18 Ems Societe Metallic tube end sealing method, involves applying flat rotating tool at plane front side of work against preformed opening to drive material of tube towards center of opening and close it
US20070028915A1 (en) * 2005-08-03 2007-02-08 Alberto Bellomo Gas manifold for a cooking range, with a pipe closure
ES2304269A1 (en) * 2005-08-03 2008-10-01 Alberto Bellomo Gas manifold for a cooking range, with a pipe closure
US7861706B2 (en) 2005-08-03 2011-01-04 Coprecitec, S.L. Gas manifold for a cooking range, with a pipe closure
EP1760405A3 (en) * 2005-08-03 2016-12-21 Coprecitec, S.L. Gas manifold for a cooking range, with a pipe closure
US20070093793A1 (en) * 2005-10-11 2007-04-26 Maurer Robert S Jr Microsurgical probe
US7600405B2 (en) * 2005-10-11 2009-10-13 Alcon, Inc. Microsurgical probe
FR2922128A1 (en) * 2007-10-11 2009-04-17 Peugeot Citroen Automobiles Sa Metallic fluid tube closing method for forming pressurized oil body of hydraulic shock absorber of automobile, involves locally deforming deposit channel of closed end of tube, where tube is not sealed to fluid
US8826714B2 (en) * 2009-10-16 2014-09-09 Ffg Werke Gmbh Method for manufacturing a wall connector
US20110089682A1 (en) * 2009-10-16 2011-04-21 Walter Bauer Method for manufacturing a wall connector
US20130247635A1 (en) * 2010-12-07 2013-09-26 Leifeld Metal Spinning Ag Method for forming a pipe section
US9233412B2 (en) * 2010-12-07 2016-01-12 Leifeld Metal Spinning Ag Method for forming a pipe section
US20150223979A1 (en) * 2012-08-28 2015-08-13 Mani, Inc. Vitreous body surgical probe and method of manufacturing same
CN102921823A (en) * 2012-11-26 2013-02-13 宁波培源电器制造有限公司 Oil storing barrel sealing machine of motorcycle rear shock absorber
JP2014188522A (en) * 2013-03-26 2014-10-06 Nippon Spindle Mfg Co Ltd Method for molding cylindrical material
US10105746B1 (en) * 2015-09-14 2018-10-23 Shoals Tubular Products, Inc. Tube end sealing method
US10596619B1 (en) * 2015-09-14 2020-03-24 Shoals Tubular Products, Inc. Tube end sealing method
US20190030973A1 (en) * 2016-03-30 2019-01-31 Nhk Spring Co., Ltd. Hollow coil spring and suspension device for vehicle
US11254177B2 (en) * 2016-03-30 2022-02-22 Nhk Spring Co., Ltd. Hollow coil spring and suspension device for vehicle
US11685211B2 (en) 2016-03-30 2023-06-27 Nhk Spring Co., Ltd Hollow coil spring and suspension device for vehicle
US11701943B2 (en) 2016-03-30 2023-07-18 Nhk Spring Co., Ltd Method of manufacturing a hollow spring member
US11278946B2 (en) * 2018-09-27 2022-03-22 Inno-Spin LLC Multi-axis roll-forming methods, systems, and products

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