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US3002614A - Vibratory squeeze-forming of metals in the solid state and apparatus therefor - Google Patents

Vibratory squeeze-forming of metals in the solid state and apparatus therefor
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US3002614A
US3002614AUS628126AUS62812656AUS3002614AUS 3002614 AUS3002614 AUS 3002614AUS 628126 AUS628126 AUS 628126AUS 62812656 AUS62812656 AUS 62812656AUS 3002614 AUS3002614 AUS 3002614A
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coupler
vibratory energy
squeeze
solid state
metals
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Jones James Byron
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Oct. 3, 1961 Fig. IA
J. B. JONES VIBRATORY SQUEEZEFORMING 0F METALS IN THE SOLID STATE AND APPARATUS THEREFOR Filed Dec. 13, 1956 2 1 ,6 7 L 9W 2 x Mia no 12 A 72 a 90 3 'Ql il'lllll as 56 501Q 98 I02 l as 82 so 42 4' iL M 2/ 54 '8 48 38 fi 310s 94 7 |4 Illlllk I I 1 Q V Fig. 2 U
k/uo l/l I I" VENTOR IN ames BYRON Jones ATTORNEY United States Patent assignments, to the United States of America as represented by the United States Atomic Energy Commission Filed Dec. 13, 1956, Ser. No. 628,126 6 Claims. (Cl. 207-2) The present invention relates to a process for vibratory squeeze-forming of metal in the solid state and to apparatus therefor.
In particular, the present invention is directed to a process in which a metal in the solid state is squeezeformed into a particular shape through the simultaneous application of pressure and vibratory energy. The present invention also comprises apparatus for squeeze-forming metals in the solid state into desired shapes, and comprises metal-shaping means comprising a housing, a die in communication with said housing, and means for squeezing the metal while in the solid state into the die, and means for applying vibratory energy to at least a portion of said metaleshaping means. By housing as used herein is meant to include the'guide means for the die and is not to be construed as limited to a closed vessel.
The squeeze-forming of metals in the solid state has in recent years assumed great industrial importance. A wide variety of commercial methods for squeeze-forming solid state metals have been developed and are in use. These methods include both hot and cold extrusion, forging, impact extrusion, drawing, cupping, etc. In most of these methods, the solid state metal is raised to anelevated temperature, so that it is softened during squeeze-forming. However, a number of methods and a variety of apparatus for squeeze-forming metals in the solid state at ambient temperatures have been developed, and are being used commercially.
Prior methods and apparatus for the squeeze-forming of metals in the solid state sufier'from a number of METALS IN i extrusion method.
This invention has as a further object the provision of serious handicaps, the minimization of which comprises a principal goal of the present invention. Thus, prior methods and apparatus for squeeze-forming metals in the solid state require the use of means for producing enormous pressures. For example, in commercial extrusion methods wherein large billets are shaped, it is frequently necessary to employ pressures of the order of many thousands of pounds per square inch, and in some cases pressures of hundreds of thousands of pounds per square inch are required. The cost of presses and other means for producing and transmitting such enormous pressures to the solid state metal undergoing forming frequently renders such methods and apparatus feasible only for the largest installations. Moreover, in many cases even where adequate squeeze-forming equipment is available, the production of the squeeze-formed articles is accomplished only at an undesirably low rate.
In addition to the foregoing, prior squeeze-forming methods and apparatus for producing shapes from metals in the solid state frequently yield articles having undesirable characteristics. For example, the surface finish of many extruded metals is apt to be unsatisfactory. With other metals, the resultant squeeze-formed articles may suffer from yet other inadequacies.
I have discovered that thesqueeze-forming of metals (and by metals as used herein is meant to include elemental metals, such as pure copper, and metallic alloys such'as mixtures of a plurality of elemental metals) in the, solid state, suchashot and cold extrusion, may be effected under relatively; low pressures, and/or may be etfected at a relatively-high rate when vibratory energy e In order to provide for the heating of the metal billet i Patented Oct. 3, 1961 ice is applied to at least a portion of the shaping means simultaneously with the application of pressure. Moreover, I have found that the resultant squeeze-formedmetal may possess superior. characteristics, when com pared with metals squeeze-formed in the solid state solely by the application of pressure.
I have invented a variety of means for introducing vibratory energy to the shaping means in the apparatus of the present invention; and may introduce axial and/or flexural vibratory energy to the housing, 'and/ or die, and/ or ram means for squeezing the metal into'the die, and/or radial vibratory energy to the housing. I have found that dilferent results may be secured depending upon the manner in which the vibratory energy is introduced, with certain constructional arrangements being superior to others. For the sake of completeness and clarity I am including herein a number of the various embodiments of the process and apparatus of my invention, although certain of these embodiments are preferable to other embodiments.
The process of the present invention may be accomplished both with the metal undergoing squeeze-forming maintained at ambient temperature, or with the metal raised to an elevated temperature below its melting point, as for example to a temperature at which the metal is appreciably softened. 1
This invention has as an object the provision of anovel novel extrusion apparatus.
For the purpose of illustrating the invention, there is shown in the'drawings a schematic illustration of an apparatus embodiment useful for the extrusion of a metal in the solid state.
FIGURES 1A and 1B comprise a longitudinal section through the illustrated apparatus embodiment. FIGURE 2 is a view taken from 2'2 of FIGURE 1A. Referring to the drawings, the extrusion apparatus schematically illustrated therein is designated generally by thenumeral 10, and includes a cylinder. 12, a die 14, .aram 16, and a press designated generally by the numeral Thepress 18 comprises ahydraulic cylinder 20 provided with apiston 22 of conventional design. It is, of course, to be understood that in place ofcylinder 20 andpiston 22, other means for exerting pressure maybe utilized. Thepress 18 may comprise a plurality of upright braces of conventional design (which for the sake of clarity are not shown in'the accompanyingdrawings) and across-head 26 for joining such upright braces together adjacent their upper ends. Y Y
Thecross-head 26 is provided with an aperture 28in its central portion within which the'cylinder 12 is'received. A'mountingplate 30, which embracescylinder 12, is secured by bolts'32 to cross-head 26, and is securedby means of welding or brazing 34 'to'cylinder 12. Anaperture 36 is provided inmounting plate 30, which mates with theaperture 28 incross-head 26.
to be squeeze-formed withinbore 38 of cylinder12 in those embodiments where the heating of the metal billet within cylinder -12 isnecessary or desirable, 'a plurality oflongitudinal chambers 42 maybe provided in the wall ofcylinder 12. Heating means, such aselectric filament cartridges 44, may be positioned within thechambers 42 to effect the heating of-billet 40. In place of theelectric filament cartridges 44 which depend for their heating action onthe resistance of a metal conductor to the flow of electricity, other means ,for effecting the heating of the metal billet may be provided, such as gas flames, etc. a a
Theram 16 comprises a rod of metal having fixedly as quartz crystals.
secured'to its innermost end a smoothfinished ram head- 46 of somewhat larger diameter than the diameter of theram 16 itself. Theoutermost end 48 of theram 16 may be flared outwardly to provide size adaptation and end-"to-end engagement with thecoupling member 108. Preferably, a fair degree of clearance should be provided between theram 16 and the cylinder wall ofbore 38.
For convenience, the uppermost end ofbore 38 may be enlarged to form the chamberStl. The die 14-comprises an inverted hollow generally conical diehousing 52 having the die opening 54 at its face:
The diehousing 52 is supported upon and fixedly secured tocylinder 12 bymeansof mount 56; Themount 56 is preferably a force-insensitive support as of the type disclosed in United States Letters Patent 2,891,- 180, issued June 16, 1959, in the name of'William C. Elmore.
Themount 56 comprises an approximatelycylindrical tube on'e-half wavelength long or unit multiples of onehalf wavelength long at the applied frequency of the vibratory energy delivered by themagnetostrictive transducers 76 and 78. Oneend 58 ofmount 56 is fixedly engaged as by threaded engagement or brazing to. the diehousing 52; theother end 60 ofmount 56 remains free. Anannular flange 62 is provided one-quarter wavelength from-thefree end 60 ofmount 56.
Theannular flange 62 ofmount 56 is received in oounterboredannular flange 64 and locked in place byannular flange 66; theflanges 64 and 66 being joined together bybolts 68. Counterbored annular flange 64 is fixed-1y secured as by brazing or welding to the end ofcylinder 12.
Afrustroconical coupler 70 is fixedly secured as by means of a brazed or soldered joint to the diehousing 52.Coupler 70 is slotted at its uppermost end to provide a pair ofhorns 72 and 74. Each of the horns is secured by means of silver soldering, brazing or soldering or the like to a magnetostrictive transducer. Thus, horn 72' carries m-agnetostrictive transducer 76 andhorn 74 carriesmagnetostrictive transducer 78.
Themagnetostrictive transducers 76 and 78 as well asthemagnetostrictive transducers 90, 96, 102, 110, 132, and 134 referred to below are formed from a magnetostrictive metal, such as nickel, the alloy 2-V Permendur (an iron-cobalt alloy), a nickel-iron alloy, or Alfenol (an aluminum-iron alloy), properly dimensioned to insure axial resonance with the frequency of the alternating current applied thereto, so as to cause it to decrease or increase in length according to its coeflicient of magnetostri'ction. Transducers of this type constitute a preferred embodiment for operation at frequencies of up to about 75,000 cycles per second. In place of metallic magnetostrictive materials, the transducer may comprise almost any material which has good physical properties and which changes its physical dimensions under the influence of an electric potential. Thus it may comprise a piezoelectric ceramic, such as barium titanate, or lead zirconate, or a natural piezoelectric material, such Such materials are preferably used at high frequency operations, as at frequencies above 75,000 cycles per second. The transducer may also consist of an electromagnetic device, such as that which actuates a radio loudspeaker.
Each of themagnetostrictive transducers 76 and 78 in the illustrated embodiment comprises a laminated core of nickel or other magnetostrictive metallic material, and has a rectangularly-shapedopening 80 in its center portion; For the sake of clarity only magnetost-rictive transducer 78 is" shown in two views (see FIG- URE 2), and will be described herein, but it is to be understood that the construction of magnetostrictive transducer" 76 and that ofmagnetostrictive transducers 90, 96, 102, 110, 132, and 134 are similar tomagnetost'rictivetransducer 78. The magnetostrictive transducer '78 includes apolarizing coil 82 and an.excitation coil 84 which are wound aboutsthe laminated nickel core through theopening 80. Upon variations of the magnetic field strength of theexcitation coil 84, there will be produced concomitant variations in the dimension of thetransducer 78, provided thepolarizing coil 82 is charged at a suitable level with DC current, with the frequency of the aforesaid variations, namely the. expansion and/ or contraction of themagnetostrictive transducer 78 being generally equal to the frequency of the alternating electric current flowing in theexcitation coil 84.
Inasmuch as each of the excitation coils 84 of themagnetostrictive transducers 76 and 78 may if necessary be connected to the same source of high frequency alternating current, and each of thetransducers 76 and 78 are dimensioned similarly, the transducers "l6 and 78 will deliver vibratory energy of the same frequency in phase to theirrespective horns 72 and 74 ofcoupler 70.
The dimensioning of thetransducer 76,coupler 70 and diehousing 52 should be regulated so that their total length is an even number of one-quarter wavelengths, and preferably these elements should be dimensioned as shown in the drawings, namely each of these elements should be dimensioned to equal one-half wavelength.
In place of themagnetostrictive transducers 76 and 78 shown in the drawings, other materials such as those heretofore mentioned may be used, such materials being cut to physical dimensions which minimize. electrical losses and insure axial resonance at the applied alternating frequency.
Acoupler 86 embracescoupler 70, as at a point midway between the ends ofcoupler 70. Thecoupler 86 includes an aperture Within which is secured by brazing or welding asplit ring 88, which in turn is secured by razing or welding tocoupler 70. Thesplit ring 88 is used to preclude the possibility of a sliding fit. Amagnetostrictive transducer 90 is secured in end-to-end contact withcoupler 86.Magnetostrictive transducer 90 is similar tomagnetostrictive transducers 76 and 78.
Acoupler 92 embraces cylinder 12'. Thecoupler 92 is brazed or welded to asplit ring 94 which is fixedly secured by brazing or welding to the outer wall ofcylinder 12. Amegnetostrictive transducer 96 is joined in end-to-end contact withcoupler 92. Themagnetostrlctive transducer 96 is preferably of the same construction as magnetostrictive transducers '76, '78 and 90.
Acoupler 98 embraces theram 16 adjacent the end thereof remote from ram head 46. Thecoupler 98 is provided with an aperture within which split ring 180 is secured as by brazing or soldering, thesplit rTng 100 being secured to ram 16 by brazing or soldering. Amagnetostrictive transducer 102 is permanently joined in end-to-end contact withcoupler 98.
Thecoupler 98 may be rest-supported and preferably not clamped upon the clevis oryoke 104 which is carried on the head ofpiston 22 so that thecoupler 98 travels upwardly with theram 16.
Thebase 48 ofram 16 is provided with a threaded stud 106. Thebase 48 is longitudinally engaged in end-to end engagement withcoupler 108, and is threadably joined therewith by means of stud 186.Coupler 108 is fixed secured, as by brazing or soldering or the like, in end-to-end contact withmagnetostrictive transducer 118.Magnetost'rictive transducer 110 is of similar design and construction asmagnetostrictive transducer 76, 78, 90, 96 or 102. Thus,magnetostrictive transducer 118 delivers vibratory energy of the same frequency as that delivered from the other magnetostrictive transducers to thecoupler 108.
Amount 112 is fixedly secured at itsend 114 tocoupler 108.' Themount 112 comprises a tube having a length equal to one-half wavelength, and includes an where the vibratory energy is applied axially.
annular flange 116 positioned one-quarter wavelength from the mountsfree end 118. V
Theflange 116 of mount 112'is fixedly secured as by soldering or the like within an annular groove on the uppermost end of ametal tube 120. The end portion oftube 120 which projects beyond the free end of magnetostrictive transducer. 110 is threaded and is provided with a matingly threadedcap 122. Thecap 122 rests on the upper surface of the head ofpiston 22, and receives the upward thrust of thepiston 22, and communicates itto thetube 120. a
Thelowermost end 124 ofcylinder 12 is joined in mitred end-to-end contact withcoupler 126 which generally resemblescoupler 70 and is provided with a pair ofhorns 128 and 130.
Magnetostrictive transducers 132 and 134 are joined in end-to-end contact withrespective horns 128 and 130. Each of themagnetostrictive transducers 132 and 134 are similar tomagnetostrictive transducers 76, 78, 90, 96, 102 and 110, and transmit vibratory energy to thecoupler 126.
Thecoupler 126 and its associatedmagnetostrictive transducers 132 and 134 are supported by means of tubularconical mount 136 which is joined at oneend 138 tocoupler 126. Themount 136 is one-half wavelength long or unit multiples of one-half wavelength long and includes aflange 140 positioned one-quarter wavelength from itsfree end 142.
Theflange 140 ofmount 136 is supported intermediate a face of supportingbrace 146 and clampingring 144 bybolts 152. Supportingbrace 146 is provided with anannular flange foot 148 which is connected to crosshead 26 by, means of "bolts 150. A plurality ofbolts 152 join clamping ring144to supporting brace 146 and provide for the engagement offlange 140 ofmount 136 therebetween. V p Thecoupler 70, diehousing 52;cylinder 12, and ram 16, and thecoupler 86 for the coupler 70 (which is fixedly secured to thedie housing 52), thecoupler 92 for thecylinder 12, andthecoupler 98forthe ram 16 should be properly dimensioned so as to resonate at their associated transducers operating frequency and should prefintroduced simultaneously. Axial vibratory energy may. I
erably be insensitive to applied forces, the same being accomplished by the use of the above-described mount Insensitivity to applied forces permits the transducers to operate efliciently under the force conditions existent in the illustrated extrusion apparatus. v
In the illustrated embodiment, the process of the present invention contemplates introducing vibratory energy axially to theram 16 frommagnetostrictive transducer 110 andcoupler 108; and/or axially to the die 14 throughmagnetostrictive transducers 76 and 78, andcoupler 70, and/or axially to thecylinder 12 throughmagnetostrictive transducers 132 and, 134 andcoupler 126. The
introduction of vibratory energy flexurally to the die 14 throughmagneto'strictive transducer 90 andcoupler 86;
and/or radially to thecylinder 12 through themagnetostrictive transducer 96 and coupler '92; and/or flexurally to theram 16 through themagnetostrictive transducer 102 andcoupler 98.
By axial vibratory energy (commonly called longitudinal vibration) is meant vibration wherein the mo tion ofthe particles of the medium being vibrated is along the direction of wave propagation or transmission, i.e,, in the direction of the length of the medium. By flexural vibratory energy (which is a type ofwhat is commonly called transverse vibration) is meant vibration wherein the motion of the particles of the meduim being vibrated is at right angles to the direction of wave propagation or transmission and in which the strain is extensional on one side of the axis of bending of the medium and compressional on the opposite side. By radial vibratory energy is meant vibration wherein the motion of the particles of the medium being vibrated is axially symmetrical and is in the direction of the radius vectors of the medium, which medium has-a cylindrical, annular,
or tube-like section, no nodes being involved, and the particle motion being of constant phase at any given radius. (See, for example, Warren P. Mason, Physical Acoustics and the Properties. of Solids (New York;
D. Van Nostrand Company, Inc., 1958, page 33, and:
Theodor F. Hueter and Richard H. Bolt, Sonics (New York: John Wiley & Sons, Inc., 1955), pages 146-147.
The process of the present invention contemplates the be introduced simultaneously to both the die and ram,
or flexural vibratory energy may be introduced simultaneously to both the die and ram, but both of these modes of vibratory energy should not be introduced simultaneously into the die and ram. Analogously, either axial vibratory energy or radial vibratory energy may be introduced into thecylinder 12 as alternatives, but both ofthese modes of vibratory energy should not be into a plurality of elements, such as to the ram and die, r
or to thecylinder, die and ram, etc. either in phase,
that iswith the vibratory energy being delivered to .the
billet undergoing squeeze-forming in the same manner from each location, namely simultaneously subjecting the billet to compression and simultaneously subjecting the billet to expansion from each of a plurality of elements.
delivering 'vibratory energy'to the billet; or the same mode of vibratory energy may be delivered to the billet undergoing squeeze-forming out of phase, namely sub jecting the billet to compression by vibratory energy from'one element and subjecting the billet toexpansion The aforementioned modes of application of vibratory energy to the billet produce different results, and are not to be regarded as equivalents and mere substitutes. However, all of the foregoing apparatus arrangements and processes are to be construed as included within the present inven-' tion.
The billet positionedwithin'bore 38 andchamber 50 in: the illustrated extrusion process is forced into and through die opening 54 at thebase of'die housing 52 due to. the pressure exerted bypiston 22 onram 16 throughcap 122,tube 120, andcoupler 108. Simultaneously, vibratory energy is introduced axially or flexurally or radially to the cylinder asaforesaid.
. I have found that due to unexplained forces, the effect of the vibratory energy may persist for a short time interval, the sameoccurring when the vibratory energy is interrupted or pulsed.
- The squeeze-forming process of the present invention may be effected over a wide range of frequencies. Generally, the application of frequencies within therange 59 to 300,000 cycles per second or somewhat more than 300,000 cycles per second is operative, although for 7 of the specific frequency of the applied vibratory energy. Thus, I have found that as a general rule the increase of the power level for the vibratory energy, other factors remaining constant, produces a greater reduction in necessary force and an increase in the rate of extrusion.
The process of the present invention comprehends the inclusion of the various techniques used by those skilled in the art of conventional squeeze-forming processes to facilitate squeeze-forming. For example, the process of the present invention comprehends the addition ofconventional lubricants and/or coatings to the billet and/or die.
Beneficial changes may be effected in the physical characteristics in metals processed in accordance with the process of the present invention. For example, the sur-' face finish characteristics of metals extruded in accordance with the process of the present invention appear to be markedly improved.
I do not believed that it is possible to satisfactorily explain the subject invention by existing theoretical physics. In'my opinion, and I do not wish to be bound hereby, it is my belief that the process of the present invention takes advantage of a plurality of phenomena whose nature is not as yet understood, namely changes in the interfacial contact areas of metals effected through the applicat on of vibratory energy (with such changes probably affecting both the billet undergoing forming and the juxtaposed surfaces of the apparatus of the present invention which engage such billet), a conversion of the vibratory energy into a form of energy useful for overcoming friction, the last-mentioned phenomenon being perhaps somewhat analogous to the fundamental physical maxim that dynamic friction is always lower than static friction; and to other eifects about which present-day physics furnishes no information. In particular, the apparent persistence of the effect of the vibratory energy for a short time after the introduction of such energy has been interrupted cannot be satisfactorily explained by present-day physics concepts.
The present invention permits the application of squeeze-forming techniques for metals in the solid state beyond the limits of all prior equipment. Moreover, the present invention permits the squeeze-forming of metals in the solid state at pressures appreciably below those necessitated by conventional techniques, or where conventional pressures are utilized, permits a marked improvement in the rate of squeeze-forming.
By wavelength as used in the annexed claims is meant the conventional definition for the term as used in the ultrasonic art, namely as the distance in the line of advance of a wave from any one point to the next point at which, at the same instant, there is the same phase. If N is the frequency of the waves and A their wavelength, their velocity of advance is the product Nx. The wavelengths of sound in common materials at commonly' used ultrasonic frequencies have been charted, see for example, Ultrasonic Engineering by Alan E. Crawford, 1955, Table III, atpage 10.
The present invention may be embodied in other specific forms without departing from the spirit or essential attributes thereof, and accordingly, reference should be made to the appended claims, rather than to the foregoing specification as indicating the scope of the invention.
Iclaim:
1. An extrusion process which comprises extruding a solid state metal rod through a die opening whose maximum dimension.is appreciably less than the minimum dimension of said solid state metal rod by simultaneously applying pressure to said solid state metal rod and vibratory energy to said solid state metal rod, said vibratory energy being applied by a plurality of vibrating devices at least two of which vibrate out of phase with one another, the amount of applied pressure being less than the requisite amount of pressure required to extrude said solid state metal rod through the die opening in the absence of the applied vibratory energy.
2. Extrusion apparatus including a housing having a cavity, a die having: an orifice of smaller cross-sectional area'than the cross-sectional area of the cavity ofthe housing in communication with the cavity of said housing, means for extruding a solid state metal from the cavity of said housing through said'die, means for applying vibratory energy to at least a portion of said extrusion apparatus, and support means for-supporting said means for applying vibratory energy including a member having a length equal to a unit multiple of one-half waveiength in the material of which the support means is made at the applied vibratory frequency, said'support means having one free end and including a flange positioned an odd unit multiple of one-quarter wavelength from the free end of the support means for securingsaid support means to the extrusion apparatus. Y
3. Extrusion apparatus including a housing having a cavity, a die having an orifice of smaller cross-sectional area than the cross-sectional area of the cavity of the housing in communication with the cavity of said housing, means for extruding a solid state metal from the cavity of said housing through said die, and means for applying vibratory energy to at least a portion of said extrusion apparatus, with said means including a substantially V-shaped vibration-transmitting coupler, and said means further including'two transducers, each capable of delivering 59 to about 300,000 cycles per second, each mounted on a respective arm of said coupler so that vibrations emanating from said transducers are transmitted down the respective arms of said'coupler to join at the coupler base to be transferred therefrom to said portion of said extrusion apparatus against said base is fixedly mounted.
4. Extrusion apparatus in accordance withclaim 2 in which the vibratory energy is introduced soas to axially vibrate a portion of the extrusion apparatus.
5. Extrusion apparatus in accordance withclaim 2 in which the vibratory energy is introduced so as to flexurally vibrate a portion of the extrusion apparatus.
6. Extrusion apparatus in accordance withclaim 2 in which the vibratory energy is introduced so as to radially vibrate the housing.
References Cited in the file of this patent UNITED STATES PATENTS 2,218,809 Calkins et a1 Oct. 22, 1940 2,382,045 Flowers Aug. 14, 1945 2,385,083 Kemerer Sept. 18, 1945 2,393,131 Vang Jan. 15, 1946 2,408,627 Green Oct; 1, 1946 2,550,771 Camp May 1, 1951 2,568,303 Rosenthal Sept. 18, 1951 2,632,858 Calosi Mar. 24, 1953 2,698,978 Welblund Jan. 11, 1955 2,723,386 Camp Nov. 8, 1955 2,775,008 Easton et al; Dec.' 25, 1956 2,799,065 Whitaker July 16, 1957 2,815,551 Hessenberg et a1. Dec. 10, 1957 FOREIGN- PATENTS 1,089,299 France Sept. 29, 1954 763,260 Great Britain Dec. 12, 1956
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US3148293A (en)*1961-06-051964-09-08Aeroprojects IncVibratory device for delivering vibratory energy at high power
US3166840A (en)*1961-06-281965-01-26Aeroprojects IncApparatus and method for introducing high levels of vibratory energy to a work area
US3194855A (en)*1961-10-021965-07-13Aeroprojects IncMethod of vibratorily extruding graphite
US3201967A (en)*1960-02-231965-08-24Cavitron Ultrasonics IncMetal forming
US3203215A (en)*1961-06-051965-08-31Aeroprojects IncUltrasonic extrusion apparatus
US3209574A (en)*1963-11-041965-10-05Aeroprojects IncApparatus and method applying vibratory energy
US3209572A (en)*1963-06-211965-10-05Aeroprojects IncVibratory energy method and apparatus
US3209573A (en)*1963-08-191965-10-05Aeroprojects IncMethod and apparatus using vibratory energy
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US3212312A (en)*1963-06-211965-10-19Aeroprojects IncApparatus utilizing vibratory energy
US3220199A (en)*1961-02-231965-11-30Siemens AgThermoelectric devices, and method and apparatus for producing thin thermocouple legs by extrusion
US3233012A (en)*1963-04-231966-02-01Jr Albert G BodineMethod and apparatus for forming plastic materials
US3268638A (en)*1963-02-191966-08-23Permawick CompanyMethod of extruding oil-impregnated fibers into bearing reservoirs
US3274812A (en)*1964-07-011966-09-27Babcock & Wilcox CoMethod and apparatus for vibratory squeeze-forming of metals
US3295349A (en)*1965-10-041967-01-03Aeroprojects IncMethod and apparatus applying vibratory energy
US3382692A (en)*1965-06-071968-05-14Albert G. BodineSonic method and apparatus for closed-die forging
US3422648A (en)*1961-10-021969-01-21Jerome H LemelsonExtrusion apparatus
US3456295A (en)*1963-01-161969-07-22Yasuo TorigaiMethod and apparatus for improving the coatability in the manufacture of coated welding rod or wire
US3535908A (en)*1967-07-141970-10-27IbmInjection molding of solid metal
DE1584297B1 (en)*1965-04-271971-03-25Aeroprojects Inc Mouthpiece holder for extrusion presses working with ultrasonic vibrations
US3585832A (en)*1968-06-141971-06-22Battelle Development CorpMetal working
US3657910A (en)*1969-09-161972-04-25Nippon Kokan KkMethod and apparatus for cold drawing metal tubes
US3874207A (en)*1957-10-221975-04-01Jerome H LemelsonExtrusion apparatus
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US3874207A (en)*1957-10-221975-04-01Jerome H LemelsonExtrusion apparatus
US3201967A (en)*1960-02-231965-08-24Cavitron Ultrasonics IncMetal forming
US3220199A (en)*1961-02-231965-11-30Siemens AgThermoelectric devices, and method and apparatus for producing thin thermocouple legs by extrusion
US3203215A (en)*1961-06-051965-08-31Aeroprojects IncUltrasonic extrusion apparatus
US3148293A (en)*1961-06-051964-09-08Aeroprojects IncVibratory device for delivering vibratory energy at high power
US3166840A (en)*1961-06-281965-01-26Aeroprojects IncApparatus and method for introducing high levels of vibratory energy to a work area
US3194855A (en)*1961-10-021965-07-13Aeroprojects IncMethod of vibratorily extruding graphite
US3422648A (en)*1961-10-021969-01-21Jerome H LemelsonExtrusion apparatus
US3456295A (en)*1963-01-161969-07-22Yasuo TorigaiMethod and apparatus for improving the coatability in the manufacture of coated welding rod or wire
US3268638A (en)*1963-02-191966-08-23Permawick CompanyMethod of extruding oil-impregnated fibers into bearing reservoirs
US3233012A (en)*1963-04-231966-02-01Jr Albert G BodineMethod and apparatus for forming plastic materials
US3209572A (en)*1963-06-211965-10-05Aeroprojects IncVibratory energy method and apparatus
US3212313A (en)*1963-06-211965-10-19Aeroprojects IncTube drawing apparatus employing vibratory energy
US3212312A (en)*1963-06-211965-10-19Aeroprojects IncApparatus utilizing vibratory energy
US3209573A (en)*1963-08-191965-10-05Aeroprojects IncMethod and apparatus using vibratory energy
US3209574A (en)*1963-11-041965-10-05Aeroprojects IncApparatus and method applying vibratory energy
US3274812A (en)*1964-07-011966-09-27Babcock & Wilcox CoMethod and apparatus for vibratory squeeze-forming of metals
DE1584297B1 (en)*1965-04-271971-03-25Aeroprojects Inc Mouthpiece holder for extrusion presses working with ultrasonic vibrations
US3382692A (en)*1965-06-071968-05-14Albert G. BodineSonic method and apparatus for closed-die forging
US3295349A (en)*1965-10-041967-01-03Aeroprojects IncMethod and apparatus applying vibratory energy
US3535908A (en)*1967-07-141970-10-27IbmInjection molding of solid metal
US3585832A (en)*1968-06-141971-06-22Battelle Development CorpMetal working
US3657910A (en)*1969-09-161972-04-25Nippon Kokan KkMethod and apparatus for cold drawing metal tubes
ES2694599A1 (en)*2017-06-212018-12-21Luis Saracho RotaecheVIBRATORY EXTRUSOR AND VIBRATORY EXTRUSION PROCEDURE FOR 3D PRINTER (Machine-translation by Google Translate, not legally binding)
US11666059B2 (en)2019-05-102023-06-06L & M Meats Ip Holdings Inc.Method of processing an intact animal carcass

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