US3130611A - Swaging machine - Google Patents

Swaging machine Download PDF

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Publication number
US3130611A
US3130611A US95414A US9541461A US3130611A US 3130611 A US3130611 A US 3130611A US 95414 A US95414 A US 95414A US 9541461 A US9541461 A US 9541461A US 3130611 A US3130611 A US 3130611A
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Prior art keywords
workpiece
portions
mandrel
forming
die
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Expired - Lifetime
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US95414A
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English (en)
Inventor
Otto A G Specht
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Milacron Inc
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Cincinnati Milling Machine Co
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Priority to GB923995D priority Critical patent/GB923995A/en
Application filed by Cincinnati Milling Machine Co filed Critical Cincinnati Milling Machine Co
Priority to US95414A priority patent/US3130611A/en
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    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21K—MAKING FORGED OR PRESSED METAL PRODUCTS, e.g. HORSE-SHOES, RIVETS, BOLTS OR WHEELS
    • B21K1/00—Making machine elements
    • B21K1/28—Making machine elements wheels; discs
    • B21K1/30—Making machine elements wheels; discs with gear-teeth
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21J—FORGING; HAMMERING; PRESSING METAL; RIVETING; FORGE FURNACES
    • B21J5/00—Methods for forging, hammering, or pressing; Special equipment or accessories therefor
    • B21J5/06—Methods for forging, hammering, or pressing; Special equipment or accessories therefor for performing particular operations
    • B21J5/12—Forming profiles on internal or external surfaces
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21J—FORGING; HAMMERING; PRESSING METAL; RIVETING; FORGE FURNACES
    • B21J7/00—Hammers; Forging machines with hammers or die jaws acting by impact
    • B21J7/02—Special design or construction
    • B21J7/14—Forging machines working with several hammers
    • B21J7/16—Forging machines working with several hammers in rotary arrangements

Definitions

  • Rotary swaging machines are capable of quickly forming many types of workpieces which would be difficult and time consuming to machine by other methods.
  • opposed, radially pulsating, forming dies impinge on a workpiece mounted on a mandrel and received therebetween. Under the impact of the dies the metal forms about the mandrel so that the internal conformation of the workpiece is determined by the mandrel while the external conformation is determined by the dies.
  • One type of complex workpiece which is diflicult to form in present rotary swaging machines is one having two tandem portions containing bores with conformations inclined with respect to each other.
  • Such a piece might, for example, have left hand helical grooves or ribs in one bore, and right hand helical grooves or ribs, or straight grooves or ribs, in the other bore.
  • the two portions of the workpiece are formed, in two separate operations, on different mandrels.
  • a complex workpiece having conformations inclined with respect to each other on tandem bores of different size can be formed on one mandrel in one continuous operation.
  • a mandrel having two relatively rotatable portions each of said portions having conformations to form the bore of one portion of the workpiece, is provided.
  • These mandrel portions which are spaced axially on the mandrel in accordance with the spacing of the bores in the workpiece, are received in the workpiece and the workpiece is formed thereon by the pulsating die members of the machine.
  • the mandrel can be removed therefrom by exerting an axial force between the workpiece and the mandrel.
  • This force will produce rotation of one or both mandrel portions, depending on the conformations impressed in the workpiece, in the required amount to permit separation of both mandrel portions in unison from the respective bores of the workpiece.
  • the relative ax al force is applied in a direction to move the smaller mandrel portion, after separation from the smaller bore, out through the larger bore. It is therefore one object of the present invention to provide mechanism for swaging in one continuous operation a workpiece having tandem bores of different size with conformations inclined relative to each other.
  • Another type of complex workpiece which has proved diflicult to form is one having two tandem portions of different radial span.
  • the workpiece is fed axially into the operating zone between pulsating dies having a flared forming face terminating at a trailing edge, the diameter of the trailing edge corresponding to the desired outer diameter of the workpiece.
  • the load on the machine begins to rise when the leading edge of the workpiece is initially contacted by the forming faces of the die and will reach maximum value when a maximum length (or axial span) of the workpiece is subjected to the forming action of the dies.
  • the load on the machine will begin to drop when the leading edge of the workpiece portion passes the ice trailing edge of the forming face of the die since the workpiece is formed to final outer diameter at the trailing edge of the forming face. If, on the other hand, the entire axial span of the workpiece portion to be formed is not being contacted by the forming faces of the pulsating dies at one time, the load will not begin to drop until the trailing edge of the workpiece passes that point of the die face which first contacts the workpiece, which point may be defined as the effective leading edge of the die face.
  • the load will be maximum when maximum contact occurs between the forming faces of the dies and the workpiece, and the load, which is a function of axial position of the workpiece relative to the die members, will begin to drop when the axial span of contact between the workpiece and the die diminishes.
  • a workpiece has two tandem portions of different radial span, there must be two die forming faces to engage the respective portions of the workpiece, each forming face portion having a trailing edge to bring the respective portions down to the different desired outer diameters.
  • To form the two portions of the workpiece simultaneously would increase the load on the machine and consequently each portion of such a workpiece is generally formed in a separate operation.
  • such a workpiece can be formed, without any significant increase in the maximum load, in a single operation. This is accomplished by spacing the forming faces of the die, in the axial direction, a different distance than the axial spacing between the respective portions of the workpiece.
  • the load resulting from operations on two tandem workpiece portions of different radial span can be satisfactorily distributed even though there is an intermediate axial position of the advancing workpiece when both portions thereof are operated on.
  • the mandrel supporting the workpiece is made in two portions, one for each portion of the workpiece, the slightest eccentricity between the mandrel portions will result in bending forces which can snap the mandrel if simultaneous operation occurs at any time on the two portions of the workpiece.
  • a similar result may ocur if there is any eccentricity between the forming faces of the die.
  • the mandrel Since the size of the mandrel is dictated by the desired bore in the finished workpiece, the mandrel cannot be enlarged to resist these forces. Under these conditions it is desirable to space the forming faces of the dies in the axial direction a distance sufficiently different from the axial spacing between the workpiece portions so that operation on one portion of the workpiece is finished before operation on the other portion is begun. With this spacing of the die faces, the mandrel is not subjected to bending forces which would occur if both portions of the workpiece were 3 being operated on at the same time. It is therefore another object of the present invention to provide a swaging machine which will complete formation of one portion of an advancing workpiece before operation on a second portion of the workpiece is begun.
  • FIG. 1 is a fragmentary view in elevation, with portions broken away, of a swaging machine constructed in accordance with the present invention
  • FIG. 2 is a view taken on line Z-2 of FIG. 1;
  • FIG. 3 is a perspective View of a workpiece formed in one continuous operation by the mechanism of the present invention
  • FIG. 4 is a View, partly in cross-section, of the mandrel of the machine of FIG. 1;
  • FIG. 5a is a view taken on line 5a5a of FIG. 4;
  • FIG. 5b is a view taken on the line 5b-5b of FIG. 4;
  • FIG. 6 is a View taken on line 66 of FIG. 1;
  • FIGS. 7a, 7b, and 7c are views of a workpiece being fed between the dies for forming and showing a workpiece when it is first contacted by the dies, at an intermediate position, and as it approaches its final position, respectively.
  • FIG. 7d is a chart showing the load on the machine resulting from operation on the two portions of the workpiece when the forming faces are spaced as shown in FIGS. 7a, 7b, and 70.
  • FIGS. 8a, 8b and 8c are views similar to FIGS. 7a, 7b, and 7c except that the die faces are spaced so that only one portion of a workpiece is operated on at one time;
  • FIG. 8d is a chart showing the load on the machine resulting from operation on the two portions of the workpiece when the forming faces are spaced as shown in FIGS. 8a, 8b, and 80.
  • FIG. 1 a rotary swaging machine having a base 16.
  • a head 11 mounted on the base 10 are a head 11, a feed carriage 12, and, between the head and the feed carriage, a loading and stripping mechanism 13.
  • a plurality of rollers 17 are rotatably supported between a pair of annular plates 18 and 1?.
  • Plate 18 has a plurality of spacer portions 20 extending between the rollers and plate 19 is secured to the end of the spacer portions, in spaced relation to plate 18, by bolts 21.
  • the ring of rollers 17 is carried between an outer race member 22 secured in the head, and a pair of inner race members 23a and 23b secured in hub 15 and spaced apart to receive the rams therebetween.
  • Each ram 1s has a head 14a, the inner side of which is engaged with resilient spacers 2.4 seated in the hub and the outer side of which is adapted to engage the rollers 17 between the races 23a and 2312.
  • the hub 16 is rotated the rams 14 are urged outwardly by centrifugal force and the resilient strips 24 but are periodically driven inwardly by contact with a roller.
  • the rotation of driven hub 16, and the inner race members ZZizrand 23b connected thereto, causes rotation of rollers 17 about their axes.
  • FIG. 3 A typical workpiece formed in one continuous operation by the mechanism of the present invention is shown in FIG. 3.
  • the formed workpiece 31 has two tandem portions 32 and 33 having outer cylindrical conformations, the portions having central bores 34 and 35, respectively.
  • the outer diameter of portion 32 is larger than the outer diameter of portion 33 and the diameter of bore 34 is larger than the diameter of bore 35.
  • Bore 34 has straight conformations, or grooves, 36 extending in the axial direction (parallel to the central longitudinal axis B of the workpiece) while bore 3d has helical ribs 37 which constitute conformations inclined relative to the straight conformations 36 in bore 34 (and inclined relative to axis B of the workpiece).
  • the feed carriage 12 is mounted on bed -16 for movement towards and away from the head 11 and has extending therefrom a mandrel 41 on the longitudinal axis A.
  • the mandrel 4-1 includes a rod 42 mounted in the carriage and, as shown in FIG. 4, the rod has a bore 43 at its outer end.
  • a bushing 44 is threadediy received in bore 43 and rotatably supports a shaft 45.
  • Shaft 45 has a mandrel portion 46 secured to its outer end which has helical grooves 47.
  • grooves correspond to the desired helical ribs 3 7 in the bore 35 of the finished workpiece portion 33 so that when the metal workpiece blank is pressed on the mandrel by the forming dies, the helical ribs on the mandrel will form the helical grooves in the workpiece.
  • Rotatably mounted on shaft 45 and abutting mandrel portion 4-6 is a second mandrel portion 43 having straight conformations, or ribs, 19 corresponding to the desired conformations, or grooves, 36 of the finished workpiece portion 32.
  • the shaft 45 has spacers 5d and 51 at each end of bushing 4 and, behind the spacer 51 in bore 43, the shaft has a sleeve 52 retained thereon by snap ring 53.
  • Sleeve 52 holds two locking shoes 54a, 54b in a groove 55 on shaft 45.
  • shaft 4-5 (and hence mandrel portion 46) is free to rotate on mandrel rod 42 and mandrel portion 4 8 is free to rotate relative to shaft 45 and mandrel portion 46.
  • mandrel portion 46 and mandrel portion 4-3 are held against axial movement relative to mandrel rod 42 and thus move axially therewith.
  • the mandrel 11 in its retracted position is behind the loading and stripping mechanism 13.
  • the mechanism 13 has an open ng 6% therethrough to permit advance and retraction of the mandrel.
  • the mechanism 13 has a loading chute 61 terminating at the opening and a seat 62 to hold a workpiece dropped from the chute with the central axis B of the workpiece on the longitudinal axis A.
  • a lever 63 has one end pivotally connected to the frame of mechanism 13 and has the opposite end connected to an actuating rod 64.
  • a pin 65 pivotaliy connected to lever 63 advances as the lever 63 is moved forward and slides between the piece on seat 62 and the piece thereabove to hold the pieces above seat 62 after the advancing mandrel has engaged the piece on the seat and moved it toward a the head.
  • the actuating rod 6- 5 extends through the frame of mechanism 13 and the lever 63 and rod 64 are biased toward the head by compressed spring 65 received on the rod between collar 67 thereon and the frame of mechanism 13.
  • the actuating rod 64- also slidably extends through bracket 68 on carriage '12 and is retracted, to retract lever 63 and pin as, when collar 69 is engaged by bracket 68 as carriage 12 approaches its fully retracted position. As pin d5 retracts the next piece falls onto seat 62.
  • the workpiece blank @111 like the finished workpiece, has two tandem cylindrical portions 32a and 36a, each portion having a central cylindrical bore.
  • the outer diameter of portion 32a is larger than the outer diameter of portion 33a and the bore in portion 32a is larger than the bore in portion 33a.
  • the loading chute has a slot 69 through which the workpiece blank extends, with the smaller portion thereof outside the chute and toward the head of the machine, and it is in this position that the workpiece is deposited on the seat 62.
  • the mandrel advances into the workpiece blank with mandrel portion 46 in the smaller portion of the workpiece and mandrel. portion 48 in the larger portion thereof, and a workpiece blank is carried toward the head.
  • a guide rod 70' extends through the head of the machine and between the dies thereof to engage the forward end of the workpiece and hold it on the mandrel with the mandrel portion 48 seated against the forward end of the bore in the larger portion 32a of the workpiece blank.
  • the guide rod 70 is yieldable and retracts as the mandrel advances into the head.
  • Each forming die 26 has, as shown in FIG. 7a, a first, or leading, die portion 75 adapted to form the portion 32a of the workpiece blank, and a second, or trailing, die portion 76 adapted to form the portion 33a of the blank.
  • Each die 26 thus forms a set of two die portions which together completely form the workpiece.
  • Each portion 75, 76 of each die has a flared forming face 77, 78 respectively, extending between an effective leading edge 79, '80 and a trailing edge 81, 82.
  • the effective leading edge of each die portion is that point on the pulsating die portion which first engages the advancing workpiece.
  • the distance of the effective leading edge 79 of die portion 75 from the longitudinal axis A when the die is closed equals the radius of portion 32a of the unformed workpiece blank 31a.
  • the distance of the effective leading edge 89 of die portion 76 from the longitudinal axis A when the die is closed equals the radius of unformed portion 33a of workpiece blank 31a.
  • the trailing edge 81 of die portion 75 is spaced from the axis A a distance equal to the outer diameter of the cylindrical finished workpiece portion 32 while trailing edge 8-2 of die portion 76 is spaced from i x's A a distance equal to the outer diameter of cylindrical finished workpiece portion 33.
  • workpiece portion 32 is operated on by forming face 77 as it advances and workpiece portion 33 is operated on by forming face 78 as it advances.
  • Other portions of the die perform no forming action on the workpiece.
  • the load on the machine in the formation of one portion of the workpiece will depend on the span (in the axial direction) of contact between the workpiece portion and the forming face of the die at any one time. After the workpiece portion engages the forming face the load from that portion will rise to a maximum value when maximum axial span of contact exists between the particular workpiece portion and the forming face.
  • the load resulting from formation of that particular portion decreases as the axial span of contact between the workpiece and forming face decreases.
  • the load resulting from formation of workpiece blank portion 32a is shown at 96 in FIG. 7d and the load resulting from formation of workpiece blank portion 33a is shown at 91.
  • the load 9% on the machine begins to increase.
  • the die portion 76 is spaced in the axial direction from die portion 75 a greater distance than the respective portions 32a, 33a of the workpiece blank so that the leading edge 86 of workpiece blank portion 33a does not yet contact the effective leading edge 80 of die portion 75, and portion 33a does not add to the load on the machine at this time.
  • Portion 32a which, in the workpiece shown for illustrative purposes, has an axial span C equal to the axial span of the forming face 77, establishes maximum forming contact with the forming face (and hence maximum load 9&3) when the leading edge 85 of the workpiece blank portion 32a is at the trailing edge 81 of the die portion 75, as shown in FIG. 711. At this time the leading edge 86 of workpiece portion 33a is at the effective leading edge 80 of die portion 76. As the workpiece advances the load 90 resulting from operation on portion 32a drops (since the axial span of contact between portion 32a and forming face 77 decreases) and the load 91 resulting from operation on portion 33a begins to rise.
  • forming face 78 operates on an increasing axial span of portion 33a
  • forming face 77 operates on a decreasing axial span of portion 32a.
  • the load 91 resulting from formation of this portion drops until the workpiece is formed to the desired extent.
  • the load on the machine is distributed. With this distribution of load a smaller machine can be used.
  • the workpiece blank 131 has two portions 132a, 133a.
  • Portion 132a has a leading edge 185 and a trailing edge 187
  • portion 133a has a leading edge 186.
  • the die 126 has two portions and 176, with forming faces 177, 178, respectively, and is constructed so that the trailing edge 181 of portion 175 is spaced from the effective leading edge of the second die portion 176 an equal or greater distance in the axial direction than the entire axial span of the workpiece (that is the distance from the leading edge 186 of workpiece portion 133a to the trailing edge 187 of workpiece portion 132a).
  • the portion 132a of the workpiece blank is formed, producing a load indicated at 190 in FIG.
  • the mechanism 13 in addition to supplying pieces one at a time for engagement by the advancing mandrel, serves to strip the pieces off the mandrel as the mandrel retracts.
  • FIG. 6 there is pivotally connected to the frame of mechanism 13, on each side of a workpiece resting on seat 62, a pair of parallel links 175, 176 of equal length pivotally connected to a floating link 177.
  • the link 177 is normally biased by spring 178 to a retracted position with its rear end 177a abutting against the frame of mechanism 13. In this position a projecting car 1771) on link 177 extends into the path of a workpiece blank 31a.
  • the links 177 in their retracted position, serve to support a workpiece blank received on seat 62 in a position to receive the advancing mandrel 41.
  • the floating links 177 are swung out of the path of the workpiece but swing back to the retracted position with end 177a abutting the frame as soon as the advancing workpiece clears the floating links.
  • the ends 1770 thereof are in the path of a retracting workpiece and define stop members therefor.
  • the mandrel After the blank has been compressed into a finished workpiece on the mandrel by the pulsating dies, the mandrel is retracted from the head. When the workpiece contacts ends 177c of the floating links, which are held against the frame by springs 178, the workpiece stops while the mandrel continues to retract. Helical ribs 37 have been formed in the helical grooves 47 of mandrel portion 46 so that shaft 45 (and hence mandrel portion 46) rotate by virtue of the relative axial force applied between the mandrel and the workpiece to unscrew mandrel portion 46 from the finished workpiece 31.
  • mandrel portion 43 form straight conformations in bore 34 and mandrel portion 48 cannot rotate as the mandrel is withdrawn from the workpiece.
  • shaft 45 and mandrel 46 can rotate relative to mandrel portion 43, the mandrel portion 48 can withdraw from bore 34 without rotation relative to the workpiece, while mandrel portion 46 rotates relative to the workpiece to unscrew therefrom.
  • leading and trailing when applied to the workpiece and die, derive their meaning from the relative axial movement between the die and the workpiece as the workpiece is advanced between the dies during the forming operation (as, for example, as the workpiece is advanced from the position shown in FIG. 7a or 8a to the position shown in FIG. 70 or 80).
  • leading edge of a workpiece portion is that edge first engaged by the die as the workpiece advances.
  • trailing edge of a forming face on a die portion is that edge of the forming face which last engages a portion of the advancing workpiece.
  • a mandrel mounted on said axis having two portions along its length adapted to be received within a workpiece blank, the portions of the mandrel formed to produce the desired conformations on the interior of a workpiece, one of said portions rotatable relative to the other to permit withdrawal of the respective portions of the mandrel simultaneously from a formed workpiece on relative movement in one direction between the mandrel and the workpiece.
  • a mandrel for forming the interior of two tandem portions of a workpiece having conformations inclined with respect to each other comprising a first portion having conformations for forming the interior of one of said portions of the workpiece, a second portion rota-table relative to the first portion and having conformations for forming the interior of the other of said portions, and means to mount said portions for longitudinal movement along said central axis spaced longitudinally in fixed axial relation in accordance with the spacing of the portions of the workpiece for insertion therein.
  • a swaging machine for forming a workpiece having two tandem portions with interior conformations inclined relative to each other, the machine having op posed forming dies mounted for radial pulsation about a.
  • a swaging machine for successive production of complex workpieces having two tandem portions with interior conformations inclined relative to each other comprising in combination opposed pulsating forming dies mounted about a central axis for radial impingement on a workpiece blank inserted therebetween, a mandrel rod, two mandrel portions mounted on the rod for relative rotation therebetween and spaced on the rod in fixed relation as said portions of the workpiece are spaced to receive a workpiece blank thereon, each of said mandrel portions having conformations inclined relative to the other portion to form the interior of said portions of the workpiece, a loading chute to deposit workpiece blanks one at a time on said central axis, means to reciprocate the mandrel rod along said central axis to move said mandrel portions between a retracted position behind the loading chute and an advanced position at an operating zone between the forming dies, and a stop member between the loading chute and operating zone movable into the path of a workpiece as the mandrel rod retracts to strip
  • a mandrel adapted to receive and move a workpiece along an axis, opposed rams mounted for radial pulsation about said axis, each of said rams having two die portions to operate respectively on said workpiece portions, said die portions spaced in the axial direction a different amount than said workpiece portions.
  • a mandrel having a longitudinal axis adapted to receive said workpiece in coaxial relation and advance said workpiece along said longitudinal axis, opposed sets for forming dies mounted for radial pulsation about said axis and having a leading die portion and a trailing die portion, said leading die portion spaced from the axis to pass the workpiece portion of smaller span Without contact therewith and to impinge on the workpiece portion of larger span for formation thereof, said trailing die portion spaced from the axis to impinge on the workpiece portion of smaller span for formation thereof, said die portions spaced in the axial direction a diiferent amount than said workpiece portions whereby one of said die portions commences formation of one of said workpiece portions before the other die portion commences formation of the other workpiece portion;
  • a swaging machine for forming a complex workpiece having a central axis and two tandem cylindrical portions of different radii, said workpiece portions having leading edges spaced a predetermined distance apart, said machine having a mandrel adapted to receive and advance a workpiece along a longitudinal axis coaxial with the central axis of the workpiece, the combination of opposed forming dies mounted for radial pulsation about said longitudinal axis, each comprising a first flared forming face terminating at a trailing edge spaced from the am's a distance equal to the desired radius of the larger workpiece portion and a second flared forming face terminating at a trailing edge spaced from the axis a distance equal to the desired radius of the smaller workpiece portion, said second forming face spaced in the direction of workpiece travel from the first forming face with the trailing edge of the second forming face spaced from the trailing edge of the first forming face a different distance than said predetermined distance.
  • a swaging machine for forming a complex workpiece having a central axis and two tandem cylindrical portions of different radii, said machine having a mandrel adapted to receive and advance a workpiece along a longitudinal axis coaxial with the central axis of the workpiece, opposed sets of forming dies mounted for radial pulsation about said longitudinal axis, each set having a first forming face adapted to form one of said workpiece portions and a second forming face adapted to form the other of said workpiece portions, said forming faces spaced in the axial direction a distance sufiiciently different from the spacing of the portions of the workpiece so that as the workpiece advances one portion of the Workpiece is completely formed when formation of the other portion of the workpiece begins.
  • a swaging machine for forming a complex workpiece having a central axis and first and second cylindrical portions of different radii, each of said portions having a leading edge and a trailing edge as the workpiece is advanced toward an operating zone
  • said machine having a mandrel adapted to receive and advance a workpiece toward the operating zone along a longitudinal axis coaxial with the central axis of the workpiece with said first portion leading said second portion, opposed forming dies mounted for radial pulsation about said longitudinal axis and each having a first forming face and a second forming face, said first and second forming faces each having a leading edge spaced from the axis when the dies are closed a distance equal to the radius of the first and second unformed portions, respectively, of the workpiece and the first and second forming faces each having a trailing edge spaced from the axis when the dies are closed a distance equal to the radius of the first and second formed portions, respectively, of the workpiece, the leading edge of the first
  • a mandrel having two relatively rotatable portions spaced in fixed relation in accordance with the portions of the workpiece and adapted for insertion into a workpiece blank to support the workpiece on an axis, one of said mandrel portions having external conformations to form the internal conformations on one portion of the workpiece and the other mandrel portion having external conformations to form the internal conformations on the other portion of the workpiece, means to move the mandrel to advance the workpiece along said axis, opposed forming dies mounted for radial pulsation about said axis, each of said forming dies having two portions to impinge on the respective portions of the workpiece and form the workpiece portions about the mandrel to desired radial span, said die portions spaced axially a different amount than said respective workpiece portions

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US95414A 1961-03-13 1961-03-13 Swaging machine Expired - Lifetime US3130611A (en)

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Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3352138A (en) * 1965-10-23 1967-11-14 Barber Colman Co Tool for forming toothed parts
US3374651A (en) * 1965-10-23 1968-03-26 Barber Colman Co Machine for forming gears
FR2608078A1 (fr) * 1986-12-15 1988-06-17 Hitachi Ltd Procede pour fabriquer une denture helicoidale interieure
EP0458100A1 (de) * 1990-05-02 1991-11-27 Gesellschaft für Innenhochdruckverfahren mbH & Co.KG Verfahren zur Herstellung von ineinandergreifenden Profilen

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8151436B2 (en) * 2003-12-22 2012-04-10 Honda Motor Co., Ltd. Method of forming member, valve guide and method of forming the same, and method of forming tubular member

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Publication number Priority date Publication date Assignee Title
US770072A (en) * 1904-03-02 1904-09-13 William N Jones Mandrel holding and operating machine.
US1696697A (en) * 1926-02-20 1928-12-25 William H Sommer Apparatus for pointing wires
US1944571A (en) * 1932-07-30 1934-01-23 Plastic Products Engineering C Molding machine
US1963942A (en) * 1933-07-20 1934-06-19 Allen Mfg Company Swaging machine
US2586943A (en) * 1947-04-25 1952-02-26 Haller John Machine for sizing bushings
US2759380A (en) * 1952-11-25 1956-08-21 Nat Lead Co Ejection mechanism for metal forming presses

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US770072A (en) * 1904-03-02 1904-09-13 William N Jones Mandrel holding and operating machine.
US1696697A (en) * 1926-02-20 1928-12-25 William H Sommer Apparatus for pointing wires
US1944571A (en) * 1932-07-30 1934-01-23 Plastic Products Engineering C Molding machine
US1963942A (en) * 1933-07-20 1934-06-19 Allen Mfg Company Swaging machine
US2586943A (en) * 1947-04-25 1952-02-26 Haller John Machine for sizing bushings
US2759380A (en) * 1952-11-25 1956-08-21 Nat Lead Co Ejection mechanism for metal forming presses

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3352138A (en) * 1965-10-23 1967-11-14 Barber Colman Co Tool for forming toothed parts
US3374651A (en) * 1965-10-23 1968-03-26 Barber Colman Co Machine for forming gears
FR2608078A1 (fr) * 1986-12-15 1988-06-17 Hitachi Ltd Procede pour fabriquer une denture helicoidale interieure
US4884427A (en) * 1986-12-15 1989-12-05 Hitachi, Ltd. Method of producing helical internal gear
EP0458100A1 (de) * 1990-05-02 1991-11-27 Gesellschaft für Innenhochdruckverfahren mbH & Co.KG Verfahren zur Herstellung von ineinandergreifenden Profilen

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