US2899054A - Refractory dde for extruding uranium - Google Patents
Refractory dde for extruding uranium Download PDFInfo
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- US2899054A US2899054A US2899054DA US2899054A US 2899054 A US2899054 A US 2899054A US 2899054D A US2899054D A US 2899054DA US 2899054 A US2899054 A US 2899054A
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- United States
- Prior art keywords
- die
- extrusion
- extruding
- metals
- uranium
- Prior art date
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- 229910052770 Uranium Inorganic materials 0.000 title description 22
- JFALSRSLKYAFGM-UHFFFAOYSA-N uranium(0) Chemical compound [U] JFALSRSLKYAFGM-UHFFFAOYSA-N 0.000 title description 22
- 238000004553 extrusion of metal Methods 0.000 claims description 20
- PWHULOQIROXLJO-UHFFFAOYSA-N manganese Chemical compound [Mn] PWHULOQIROXLJO-UHFFFAOYSA-N 0.000 claims description 14
- 229910052748 manganese Inorganic materials 0.000 claims description 14
- 239000011572 manganese Substances 0.000 claims description 14
- 229910052782 aluminium Inorganic materials 0.000 claims description 12
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminum Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims description 12
- 239000011651 chromium Substances 0.000 claims description 10
- VYZAMTAEIAYCRO-UHFFFAOYSA-N chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 claims description 8
- 229910052804 chromium Inorganic materials 0.000 claims description 8
- VTLYFUHAOXGGBS-UHFFFAOYSA-N fe3+ Chemical compound [Fe+3] VTLYFUHAOXGGBS-UHFFFAOYSA-N 0.000 claims description 8
- XEEYBQQBJWHFJM-UHFFFAOYSA-N iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 claims description 8
- JEIPFZHSYJVQDO-UHFFFAOYSA-N iron(III) oxide Inorganic materials O=[Fe]O[Fe]=O JEIPFZHSYJVQDO-UHFFFAOYSA-N 0.000 claims description 8
- FYYHWMGAXLPEAU-UHFFFAOYSA-N magnesium Chemical compound [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 claims description 8
- 229910052749 magnesium Inorganic materials 0.000 claims description 8
- 239000011777 magnesium Substances 0.000 claims description 8
- 239000000203 mixture Substances 0.000 claims description 6
- HCHKCACWOHOZIP-UHFFFAOYSA-N zinc Chemical compound [Zn] HCHKCACWOHOZIP-UHFFFAOYSA-N 0.000 claims description 6
- 239000011701 zinc Substances 0.000 claims description 6
- 229910052725 zinc Inorganic materials 0.000 claims description 6
- 229910052742 iron Inorganic materials 0.000 claims description 4
- 229910052751 metal Inorganic materials 0.000 description 60
- 239000002184 metal Substances 0.000 description 60
- 238000001125 extrusion Methods 0.000 description 42
- 150000002739 metals Chemical class 0.000 description 18
- VPBIQXABTCDMAU-UHFFFAOYSA-N magnesium;oxido(oxo)alumane Chemical group [Mg+2].[O-][Al]=O.[O-][Al]=O VPBIQXABTCDMAU-UHFFFAOYSA-N 0.000 description 12
- 210000003800 Pharynx Anatomy 0.000 description 10
- 229910052790 beryllium Inorganic materials 0.000 description 10
- ATBAMAFKBVZNFJ-UHFFFAOYSA-N beryllium(0) Chemical compound [Be] ATBAMAFKBVZNFJ-UHFFFAOYSA-N 0.000 description 10
- SZVJSHCCFOBDDC-UHFFFAOYSA-N Iron(II,III) oxide Chemical compound O=[Fe]O[Fe]O[Fe]=O SZVJSHCCFOBDDC-UHFFFAOYSA-N 0.000 description 8
- CPLXHLVBOLITMK-UHFFFAOYSA-N magnesium oxide Chemical compound [Mg]=O CPLXHLVBOLITMK-UHFFFAOYSA-N 0.000 description 8
- 239000011819 refractory material Substances 0.000 description 8
- QCWXUUIWCKQGHC-UHFFFAOYSA-N zirconium Chemical compound [Zr] QCWXUUIWCKQGHC-UHFFFAOYSA-N 0.000 description 8
- 229910052726 zirconium Inorganic materials 0.000 description 8
- -1 metals alloy Chemical class 0.000 description 6
- 229910052566 spinel group Inorganic materials 0.000 description 6
- 229910052776 Thorium Inorganic materials 0.000 description 4
- 238000005275 alloying Methods 0.000 description 4
- XKRFYHLGVUSROY-UHFFFAOYSA-N argon Chemical compound [Ar] XKRFYHLGVUSROY-UHFFFAOYSA-N 0.000 description 4
- CWYNVVGOOAEACU-UHFFFAOYSA-N fe2+ Chemical compound [Fe+2] CWYNVVGOOAEACU-UHFFFAOYSA-N 0.000 description 4
- 238000007710 freezing Methods 0.000 description 4
- 238000010438 heat treatment Methods 0.000 description 4
- UQSXHKLRYXJYBZ-UHFFFAOYSA-N iron oxide Chemical compound [Fe]=O UQSXHKLRYXJYBZ-UHFFFAOYSA-N 0.000 description 4
- 239000000463 material Substances 0.000 description 4
- 230000035939 shock Effects 0.000 description 4
- LIVNPJMFVYWSIS-UHFFFAOYSA-N silicon monoxide Inorganic materials [Si-]#[O+] LIVNPJMFVYWSIS-UHFFFAOYSA-N 0.000 description 4
- 229910052596 spinel Inorganic materials 0.000 description 4
- 239000011029 spinel Substances 0.000 description 4
- ZSLUVFAKFWKJRC-UHFFFAOYSA-N thorium Chemical compound [Th] ZSLUVFAKFWKJRC-UHFFFAOYSA-N 0.000 description 4
- 238000004804 winding Methods 0.000 description 4
- 239000000956 alloy Substances 0.000 description 2
- 229910045601 alloy Inorganic materials 0.000 description 2
- 229910052786 argon Inorganic materials 0.000 description 2
- 230000002542 deteriorative Effects 0.000 description 2
- 229910052500 inorganic mineral Inorganic materials 0.000 description 2
- 239000011707 mineral Substances 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 238000006011 modification reaction Methods 0.000 description 2
- 239000003345 natural gas Substances 0.000 description 2
- 230000003647 oxidation Effects 0.000 description 2
- 238000007254 oxidation reaction Methods 0.000 description 2
- 230000001590 oxidative Effects 0.000 description 2
- 239000000126 substance Substances 0.000 description 2
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21C—MANUFACTURE OF METAL SHEETS, WIRE, RODS, TUBES OR PROFILES, OTHERWISE THAN BY ROLLING; AUXILIARY OPERATIONS USED IN CONNECTION WITH METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL
- B21C25/00—Profiling tools for metal extruding
- B21C25/02—Dies
- B21C25/025—Selection of materials therefor
Definitions
- Refractory materials will not alloyand do not deteriorate at high temperatures but in the extrusion 'of metals through refractories these materials generally are brittle undershock.
- a further object of my invention is to provide an extrusion die of refractory material that is useful for the extrusion of metals at high temperatures such as above 900 C.
- Fig. l is a cross-sectional View of an extruding press, die and plunger
- Fig. 2 is a view in front elevation of a piercing member suitable for use in the apparatus of Fig. 1.
- uranium has three crystallographic phases which are referred to generally as the alpha, beta and gamma phases, the beta and gamma phases being formed in succession as metal in the low temperature alpha phase is increased in temperature.
- the extrusion of uranium is preferably carried on at a temperature within the gamma phase because of the greater ductility of the uranium metal in this phase over that of the alpha and beta phases.
- the transition temperature at which uranium is altered from the beta phase to the gamma phase is atabout 780 C., the greatest plasticity of the uranium being reached at temperatures above 870 C. Therefore extrusion of uranium is preferably carried on at temperatures between about 900 C. and 1000 C. or even somewhat higher.
- refractory complex or double oxides having the general, formulaM O R p where M is a metal of the group consisting of magnesium, zinc, divalent manganese and ferrous iron, R is aluminum, chromium, ferric iron, manganic manganese'orjsilicon, and m, n, x and y are small whole numbers.
- M is a metal of the group consisting of magnesium, zinc, divalent manganese and ferrous iron
- R is aluminum, chromium, ferric iron, manganic manganese'orjsilicon, and m, n, x and y are small whole numbers.
- Particularly satisfactory dies may be constructed of fosterite or the spinel-group double oxides.
- the spinel group of refractories is a series of minerals crystallizing in a regular.
- MO.R O metal-organic iron
- R 0 aluminum, chromium ferric iron or manganic manganese.
- Typicalrnembers, of this group are spinel MgO.Al O magnetite; FeQ.Fe O magnesioferrite M gQ.l?e O v chromite; FeO.Cr O and franklinite (EeZnMn Fe Q Eosterite, has theformula 2MgO. SiO contains about 5 7 .3; pertzentbfMgO. and 42.:7. percent of SiO and possesses excellent stability and strength at high temperatures.
- the apparatus or extrusion press comprises a die block 1 with a central chamber 2 of circular cross-section terminating in an extruding die 3 having a channel 4 of circular or other cross-section, through which the metal is extruded and formed into an elongated shape such as a wire, rod, tube, etc.
- the die block 1 is provided with a resistance winding 5 or other heating means to heat the apparatus.
- a movable plunger 6 having a slightly smaller diameter than that of the chamber 2 is provided within the chamber so that it may slide freely and force a billet 7 of the metal being extruded through the die channel 4.
- the die 3 is preferably coextensive in area with the plunger 6 and is of the funnel type being characterized by sides 8 sloping towards the die channel 4 at an angle of approximately 30 with the horizontal. Starting at a narrow throat portion 11 the walls of die channel 4flare away from the center of the channel at a slight angle so that the metal after being formed by the throat 11 does not adhere to the die 4.
- the die 3, which shapes the extruded metal and determines the outside diameter of the rod or tube that is formed, is composed of a refractory complex or double oxide of great hardness such as magnesium aluminate or other oxide heretofore illustrated.
- a piercing member 9 shown in Fig.
- the piercing member 9 forms the interior surface of the extruded tubing and should be of sufficient length to lie within the throat 11 of the die 3 at the start of extrusion.
- the recess. 10 should. be filledby screw plug 12 as shown in Fig. 1..
- the apparatus is heated by the resistance winding 5 at about 870 C. for a suflicient period to raise the temperature of the die to over 700 C.
- the billet 7 is preheated separately from the apparatus in a non-oxidizing atmosphere and preferably in a naturalgas atmosphere or in an atmosphere of argon.
- the billet 7 is placed in the central chamber 2 of the die block 1 in an air atmosphere, and a few minutes are allowed for the apparatus and billet 7 to attain the same temperature.
- the extruding pressure is then applied to the plunger 6 and thereby against the billet 7 forcing it in turn against the funnelled sides 8 and through the throat 11 and into the die channel 4, thereby forming the extruded metal in the shape of a rod.
- screw plug 12 is removed from the threaded recess and the piercing member 9 is fitted into the recess 10.
- the piercing member 9 precedes the plunger 6, pierces the billet, and extends into the throat 11 of the die 3 at the start of the extrusion.
- the plunger 6 extrudes the billet through the die channel 4
- the piercing member 9 moves into the die channel 4 creating a hollow center in the extruded metal.
- a die for extrusion of metals said die being formed of refractory magnesium aluminate.
- a die for extrusion of metals said die being formed of chromite.
- a die for extrusion of metals said die being formed of franklinite.
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Extrusion Of Metal (AREA)
Description
g- 19.59 E. c. CREUTZ 2,899,054
REFRACTORYDIE FOR EXTRUDING URANIUM Filed Oct. 50, 1944 fit @zz for: Edward C. (We a 5 United States Patent Edward C. Creutz, Chicago, 111., assignor to the United States of America as represented by the United States Atomic Energy Commission Application October 30, 1944, Serial No. 561,006 7 Claims. (cram-17 My invention relates toa press for extruding metals at elevated temperatures and more particularly to extrusion dies suitable for this purpose.
The extrusion of such metals as uranium, beryllium, Zirconium and thoriumis preferablyconducted at an elevated temperature because of the greater ductility of the metals obtained in the higher temperature ranges. This greater ductility makes extrusion easier and in some cases the extrusion can only be obtained at temperatures above 900 C. To insure the maintenance of the metalin a high-temperature range during extrusion the press and die through which a billet of th e metal is being extruded is heated to a temperature approximating the temperature of the billet. Thus a die used for extruding metals such as uranium, beryllium, zirconium; and thorium, must withstand contact with a metal heated to above 900 C. without alloying with it and withstand being heated to a high temperature without deteriorating. Refractory materials will not alloyand do not deteriorate at high temperatures but in the extrusion 'of metals through refractories these materials generally are brittle undershock.
It is an object of my invention to provide a die for metal extrusion that will withstand high temperatures without deterioration. p A
A further object of my invention is to provide an extrusion die of refractory material that is useful for the extrusion of metals at high temperatures such as above 900 C.
These and other objects, features and advantages of my invention will be apparent from the following detailed description of a preferred embodiment taken with the accompanying drawings in which:
Fig. l is a cross-sectional View of an extruding press, die and plunger; and
Fig. 2 is a view in front elevation of a piercing member suitable for use in the apparatus of Fig. 1.
In the extrusion of metals, it is frequently found advantageous to conduct the extrusion at high temperature, for example, 800 C. and above. For example, it has been found that uranium has three crystallographic phases which are referred to generally as the alpha, beta and gamma phases, the beta and gamma phases being formed in succession as metal in the low temperature alpha phase is increased in temperature. The extrusion of uranium is preferably carried on at a temperature within the gamma phase because of the greater ductility of the uranium metal in this phase over that of the alpha and beta phases. The transition temperature at which uranium is altered from the beta phase to the gamma phase is atabout 780 C., the greatest plasticity of the uranium being reached at temperatures above 870 C. Therefore extrusion of uranium is preferably carried on at temperatures between about 900 C. and 1000 C. or even somewhat higher.
Beryllium is brittle at low temperatures but becomes ductile at red heat; therefore it is preferable to extrude beryllium at elevated temperatures, for example, in the 2,899,054 1 Patented Aug. 11, 1959 range of 900' C. to'135 0 C. Other metals that are preferably extruded at elevated temperatures include zirconium, aluminum and thorium.
The extruding 'press used at these elevated temperatures' is heated to nearthe temperature of the billet to be extruded so that the billet will not be appreciably cooled during the extrusion. Thus when extruding metals at elevated temperatures the extruding die is also raised to a high temperature, generally in excess of 700 C., not only by the heating 'of the extrusion press but also by contact with the preheated billet of the extruded metal. At these temperatures ordinary die metals alloy with the extruded metal causinga freezing of the billet to the die which prevents extrusion. This freezing between the extruded metal and the die continues despite substantial increases in pressure in attempts to force the extrusion metal through the die to which it is alloyed. The metal of the die is subjected also to oxidation when exposed to the atmosphere at these extruding temperatures, and the resultant oxide film is objectionable for some purposes. I have found in accordance with my invention that refractory complex or double oxides having the general, formulaM O R p where M is a metal of the group consisting of magnesium, zinc, divalent manganese and ferrous iron, R is aluminum, chromium, ferric iron, manganic manganese'orjsilicon, and m, n, x and y are small whole numbers. Particularly satisfactory dies may be constructed of fosterite or the spinel-group double oxides. The spinel group of refractories is a series of minerals crystallizing in a regular. --crystallographic system and having the generalformula, MO.R O where M is usually magnesium, zinc manganese or ferrous iron, and R 0 maybe aluminum, chromium ferric iron or manganic manganese. Typicalrnembers, of this group are spinel MgO.Al O magnetite; FeQ.Fe O magnesioferrite M gQ.l?e O v chromite; FeO.Cr O and franklinite (EeZnMn Fe Q Eosterite, has theformula 2MgO. SiO contains about 5 7 .3; pertzentbfMgO. and 42.:7. percent of SiO and possesses excellent stability and strength at high temperatures. The hardness of these materials and their resistance to mechanical and thermal shock are particularly advantageous in their use for an extrusion die, since they will resist wear and retain their shape for several operations or for continued operation for a substantial period of time, and since they resist mechanical and thermal shock. In addition their chemical inertness and refractory nature is such that the temperatures in volved in extruding uranium, beryllium, zirconium, thoriurn, aluminum and similar metals at temperatures above 800-900 C. are withstood readily and alloying or combination with the metal undergoing extrusion is substantially avoided. Magnesium aluminate, MgO.Al O is particularly advantageous and is found to be the most suitable refractory for this purpose.
In the preferred embodiment of apparatus incorporating my invention shown in Fig. l the apparatus or extrusion press comprises a die block 1 with a central chamber 2 of circular cross-section terminating in an extruding die 3 having a channel 4 of circular or other cross-section, through which the metal is extruded and formed into an elongated shape such as a wire, rod, tube, etc. The die block 1 is provided with a resistance winding 5 or other heating means to heat the apparatus. A movable plunger 6 having a slightly smaller diameter than that of the chamber 2 is provided within the chamber so that it may slide freely and force a billet 7 of the metal being extruded through the die channel 4. The die 3 is preferably coextensive in area with the plunger 6 and is of the funnel type being characterized by sides 8 sloping towards the die channel 4 at an angle of approximately 30 with the horizontal. Starting at a narrow throat portion 11 the walls of die channel 4flare away from the center of the channel at a slight angle so that the metal after being formed by the throat 11 does not adhere to the die 4. The die 3, which shapes the extruded metal and determines the outside diameter of the rod or tube that is formed, is composed of a refractory complex or double oxide of great hardness such as magnesium aluminate or other oxide heretofore illustrated. For extruding tubing I prefer to provide a piercing member 9 shown in Fig. 2 afiixed centrally of the plunger 6 in a threaded recess 10 provided in the plunger 6. The piercing member 9 forms the interior surface of the extruded tubing and should be of sufficient length to lie within the throat 11 of the die 3 at the start of extrusion. When using plunger 6 for rod extrusion the recess. 10 should. be filledby screw plug 12 as shown in Fig. 1..
The preferred mode of operation for extruding a rod will now be explained. The apparatus is heated by the resistance winding 5 at about 870 C. for a suflicient period to raise the temperature of the die to over 700 C. The billet 7 is preheated separately from the apparatus in a non-oxidizing atmosphere and preferably in a naturalgas atmosphere or in an atmosphere of argon. When the apparatus and billet 7 have received requisite preheating, the billet 7 is placed in the central chamber 2 of the die block 1 in an air atmosphere, and a few minutes are allowed for the apparatus and billet 7 to attain the same temperature. The extruding pressure is then applied to the plunger 6 and thereby against the billet 7 forcing it in turn against the funnelled sides 8 and through the throat 11 and into the die channel 4, thereby forming the extruded metal in the shape of a rod.
When it is desired toproduce a tube rather than a rod, screw plug 12 is removed from the threaded recess and the piercing member 9 is fitted into the recess 10. Thus when extruding a metal billet, the piercing member 9 precedes the plunger 6, pierces the billet, and extends into the throat 11 of the die 3 at the start of the extrusion. As the plunger 6 extrudes the billet through the die channel 4, the piercing member 9 moves into the die channel 4 creating a hollow center in the extruded metal.
It will be apparentv to those skilled in the art that var- 4 ious modifications may be made without departing from the principles of the invention as disclosed herein, and for that reason it is not intended that the invention should be limited other than by the scope of the appended claims.
I claim:
1. A die for extrusion of metals, said die being formed of a refractory complex oxide having the composition M O R O where M is a divalent metal of the group consisting of magnesium, zinc, manganese and iron, R is a member of the group consisting of aluminum, chromic chromium, ferric iron, and manganic manganese, and m, n, x and y are whole numbers.
2. A die for extrusion of metals, said die being formed of a refractory spinel.
3. A die for extrusion of metals, said die being formed of refractory magnesium aluminate.
4. A die for extrusion of metals, said die being formed of magnetite.
5. A die for extrusion of metals, said die being formed of magnesioferrite.
6. A die for extrusion of metals, said die being formed of chromite.
7. A die for extrusion of metals, said die being formed of franklinite.
References Cited in the file of this patent UNITED STATES PATENTS 1,082,933 Coolidge Dec. 30, 1913 1,827,446 Westberg Oct. 13, 1931 1,840,472 Singer Jan. 12, 1932 2,150,734 Unckel Mar. 14, 1939 2,164,750 Nadler July 4, 1939 2,219,442 Chesler et al Oct. 29, 1940 2,331,232 Ross Oct. 5, 1943 OTHER REFERENCES A Study of a Group of Typical Spinels, University of Illinois Engineering Experiment Station Bulletin No. 248, June 1932, 56 pages.
Metals Handbook, page 770, 1948 edition.
Dictionary of Applied Chemistry, published by Longmans, Green & Co., 1928,
Claims (1)
1. A DIE FOR EXTRUSION OF METALS, SAID DIE BEING FORMED OF A REFRACTORY COMPLEX OXIDE HAVING THE COMPOSITION MNOMRIOY WHERE M IS A DIVALENT METAL OF THE GROUP CONSISTING OF MAGNESIUM, ZINC, MANGANESE AND IRON, R IS A MEMBER OF THE GROUP CONSISTING OF ALUMINUM, CHROMIC CHROMIUM, FERRIC IRON, AND MANGANESE, AND M, N, X AND Y ARE WHOLE NUMBERS.
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US2899054A true US2899054A (en) | 1959-08-11 |
Family
ID=3447888
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US2899054D Expired - Lifetime US2899054A (en) | Refractory dde for extruding uranium |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US2899054A (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3190107A (en) * | 1962-12-13 | 1965-06-22 | Extrusion Dies Inc | Extrusion die |
| US3247547A (en) * | 1963-04-03 | 1966-04-26 | Heany Ind Ceramic Corp | Wire guide for extruding machines |
| US3428717A (en) * | 1964-07-17 | 1969-02-18 | Commissariat Energie Atomique | Method of extruding metallic carbides and in particular uranium monocarbide |
| US3788522A (en) * | 1971-08-26 | 1974-01-29 | Mcdowell Wellman Eng Co | Nozzle structure for injection molding machine |
Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US1082933A (en) * | 1912-06-19 | 1913-12-30 | Gen Electric | Tungsten and method of making the same for use as filaments of incandescent electric lamps and for other purposes. |
| US1827446A (en) * | 1928-04-26 | 1931-10-13 | Westberg Sigurd | Process of making refractory linings |
| US1840472A (en) * | 1928-03-24 | 1932-01-12 | Singer Fritz | Matrix die for extruding solid and hollow articles |
| US2150734A (en) * | 1937-09-08 | 1939-03-14 | Unckel Herman | Drawing disk |
| US2164750A (en) * | 1937-08-21 | 1939-07-04 | Jr Joseph G Nadler | Drawing and extrusion die |
| US2219442A (en) * | 1936-07-01 | 1940-10-29 | Eagle Pencil Co | Synthetic tool die and the method of manufacture thereof |
| US2331232A (en) * | 1940-07-13 | 1943-10-05 | Donald W Ross | Method of making refractories |
-
0
- US US2899054D patent/US2899054A/en not_active Expired - Lifetime
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US1082933A (en) * | 1912-06-19 | 1913-12-30 | Gen Electric | Tungsten and method of making the same for use as filaments of incandescent electric lamps and for other purposes. |
| US1840472A (en) * | 1928-03-24 | 1932-01-12 | Singer Fritz | Matrix die for extruding solid and hollow articles |
| US1827446A (en) * | 1928-04-26 | 1931-10-13 | Westberg Sigurd | Process of making refractory linings |
| US2219442A (en) * | 1936-07-01 | 1940-10-29 | Eagle Pencil Co | Synthetic tool die and the method of manufacture thereof |
| US2164750A (en) * | 1937-08-21 | 1939-07-04 | Jr Joseph G Nadler | Drawing and extrusion die |
| US2150734A (en) * | 1937-09-08 | 1939-03-14 | Unckel Herman | Drawing disk |
| US2331232A (en) * | 1940-07-13 | 1943-10-05 | Donald W Ross | Method of making refractories |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3190107A (en) * | 1962-12-13 | 1965-06-22 | Extrusion Dies Inc | Extrusion die |
| US3247547A (en) * | 1963-04-03 | 1966-04-26 | Heany Ind Ceramic Corp | Wire guide for extruding machines |
| US3428717A (en) * | 1964-07-17 | 1969-02-18 | Commissariat Energie Atomique | Method of extruding metallic carbides and in particular uranium monocarbide |
| US3788522A (en) * | 1971-08-26 | 1974-01-29 | Mcdowell Wellman Eng Co | Nozzle structure for injection molding machine |
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