US2300353A - Method of making seamless tubing - Google Patents
Method of making seamless tubing Download PDFInfo
- Publication number
- US2300353A US2300353A US396025A US39602541A US2300353A US 2300353 A US2300353 A US 2300353A US 396025 A US396025 A US 396025A US 39602541 A US39602541 A US 39602541A US 2300353 A US2300353 A US 2300353A
- Authority
- US
- United States
- Prior art keywords
- core
- tubing
- molybdenum
- steel
- tube
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
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Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21C—MANUFACTURE OF METAL SHEETS, WIRE, RODS, TUBES, PROFILES OR LIKE SEMI-MANUFACTURED PRODUCTS OTHERWISE THAN BY ROLLING; AUXILIARY OPERATIONS USED IN CONNECTION WITH METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL
- B21C1/00—Manufacture of metal sheets, wire, rods, tubes or like semi-manufactured products by drawing
- B21C1/16—Metal drawing by machines or apparatus in which the drawing action is effected by means other than drums, e.g. by a longitudinally-moved carriage pulling or pushing the work or stock for making metal sheets, rods or tubes
- B21C1/22—Metal drawing by machines or apparatus in which the drawing action is effected by means other than drums, e.g. by a longitudinally-moved carriage pulling or pushing the work or stock for making metal sheets, rods or tubes specially adapted for making tubular articles
- B21C1/24—Metal drawing by machines or apparatus in which the drawing action is effected by means other than drums, e.g. by a longitudinally-moved carriage pulling or pushing the work or stock for making metal sheets, rods or tubes specially adapted for making tubular articles by means of mandrels
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/4981—Utilizing transitory attached element or associated separate material
Definitions
- My invention relates to a process for the manufacture of seamless tubing, and particularly to a process for the manufacture of seamless tubing of molybdenum or tungsten.
- Molybdenum is a silver-white, very hard, brittle metal in its pure condition, with the extremely high melting point of 4748 F. (2620 CJ.
- ferro-molybdenum, calcium molybdate or -molyte its chief use up to the presenthas been as an alloying element in the manufacture of steel.
- ferro-molybdenum, calcium molybdate or -molyte its chief use up to the presenthas been as an alloying element in the manufacture of steel.
- Another object of my invention is a process of manufacturing seamless molybdenum tubing.
- Still another object of my invention is a process of manufacturing tubing of refractory metals for purposes requiring high resistance to heat.
- Figure 1 of the drawing is ⁇ a side elevation of a portion of a. molybdenum bar which is to be made into tubing;
- Fig. 2 shows a longitudinal hole being drilled in the bar concentric with the outer surface to form a tubular blank
- Fig. 3 is a sectional view showing swaging dies and core mandrel
- Fig. 4 is a fragmentary cross-sectional view showing mandrel and drawing dies in operation
- Fig. 5 is a side elevation, partly in section, showing the method of removing the corefrom the finished tube.
- Fig. 6 is a side elevation showing the method of forming tubing by rolling.
- a tubular blank l of suitable dimensions is prepared either by molding a molybdenum ingot with a longitudinal central hole or by boring such a hole through a solid round
- the ratio of inside to outside diameter of theV tubular blank preferably should be the same as is desired in the nished tube, although it may be larger.
- An appropriate tubular blank for example, may be 0.75 inch outside diameter by 0.438 inch inside diameter by 12 inches long.
- Within the tubular blank is placed as a core a work-hardenable l ground steel bar 5 preferably coated with dry slaked lime or the like to facilitate withdrawal of the bar after working.
- a limecoated core of drill steel stock .425 inch diameter is suitable, and it should be slightly shorter than the tubular blank to prevent cracking of the blank at the ends.
- the grain structure and chemical composition ofthe steel are very important factors, and austenitic alloy steels have proven to be. best adapted for this use.
- Austenite in steel is a solid solution of carbon or of carbon and other elements in gamima iron, and austenitic steels, particularly of coarse grain structure, show a higher resistance to creep at temperatures above 850 F. than other and nner-grained steels.
- the tubular blank and core are heated in a high-temperature gas or electric furnace, and are then swaged and/or drawn to the desired outside diameter.
- the tube will be swaged to a suitablevdiameter and finished by drawing.
- the temperature must be carefullycontrolled so as to be high enough to. render the molybdenum workable yet not so high as to unduly soften the steel core; and (2) the surface of the tube must. be kept smooth and the diametervmust be kept uniform at all stages so as to avoid irregularities in the diameter of the steel core. If at anytime the outer surface of the tube becomes irregular, these irregularities are carried into the steel core and cannot -be removed by subsequent treatment. That is, every swaging pass must be the equivalent of a finishing pass.
- the swaged tube, coated with graphite or other suitable refractory lubricant is preferably drawn through suitable dies 1 to the desired diameter.
- the 0.24 inch diameter mentioned above is not to be taken as necessarily indicative of the-proper Apoint at which to start drawing. In general, it is best to start drawing at as large a diameter as is convenient for the purpose.
- the temperature used in dra-wing is related to the reduction made in each pass; it must be high enough to avoid4 splitting of the tube yet not so high as to reduce its tensile: strength to the -point where it breaks. Again, this temperature is critical since allof the tension in drawing must be supported by the tube, the steel core having negligible strength in smaller diameters when hot. ⁇
- molybdenum tubing may also be reduced by rolling between suitable rolls 8, which must, however, be of great strength and v ery rigidly mounted.
- the steel core is removed from the finished tube 9 by nicking and breaking an end of the tube to expose the end of the core, then stretching the cuted to permit ready removal by pincers or gripping tongs IIJ.
- the method of making seamless molybdenum tubing which comprises forming a hollow tubular blank of the metal, inserting a core of a coarse-grained austenitic alloy steel containing substantially 10 to 14 per cent of manganese and coated with lime therein, heating said blank and core to a temperature approximately 2300 to 2500 F., hot-swaging with long-bearing finishing dies through a plurality of passes to improve the crystalline structure of the blank and workharden the core while reducing the diameter of both the core and the blank, and during swaging allowing the temperature to reduce to 2000 to 2200 F. for the nal swaging passes.
- the method of making seamless molybdenum tubing which comprises forming a hollow tubular blank of the metal, inserting therein a shorter steel core of coarse-grained austenitic steel containing substantially 10 to 14 per cent manganese and 3 to 5 per cent nickel, heating said blank and core to a temperature approximately 2300 to 2500 F., hot-swaging with longy core until its diameter has been sufliciently retesting machine in removing the cores from the bearing nishing dies through a plurality of passes to improve the crystalline structure of the blank and work-harden the core while reducing the diametervof both the blank and the core, to a temperature approximately 2000 to 2200? F., then coating the exterior of the blank with a refractory lubricant, and further reducing by drawing through dies at gradually diminishing temperatures between 1700 and 1100 F.
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Metal Extraction Processes (AREA)
- Forging (AREA)
Description
` Oct.l27, 1942.. .J. E. EBERHARDT p 2,300,353
' METHOD OF MAKING SYEAMLESSTUBING Filed May 51,' 1941 "#7 1 l lj I ca/WEZ Patented Oct. 27, 1942 METHOD oF MAKING snAMmss TUBING- John E. Eberhardt, Bethlehem, Pa., assigner to Bethlehem 'Steel Company, a corporation of Pennsylvania Application May 31, 1941,- Serial No. 396,025
3 Claims.
My invention relates to a process for the manufacture of seamless tubing, and particularly to a process for the manufacture of seamless tubing of molybdenum or tungsten.
Molybdenum is a silver-white, very hard, brittle metal in its pure condition, with the extremely high melting point of 4748 F. (2620 CJ. As ferro-molybdenum, calcium molybdate or -molyte, its chief use up to the presenthas been as an alloying element in the manufacture of steel. Despite obvious advantages, its independent use as a metal has been greatly retarded by the lack Another object of my invention is a process of manufacturing seamless molybdenum tubing.
Still another object of my invention is a process of manufacturing tubing of refractory metals for purposes requiring high resistance to heat.
Having thus briefly stated the advantages and objectsgof my invention, I shall now, in order to make the same more clear, give a detailed description thereof, referring for illustration 'to the annexed sheet of drawings showing the steps in 1 my invention.
Figure 1 of the drawing is` a side elevation of a portion of a. molybdenum bar which is to be made into tubing;
Fig. 2 shows a longitudinal hole being drilled in the bar concentric with the outer surface to form a tubular blank;
Fig. 3 is a sectional view showing swaging dies and core mandrel;
Fig. 4 is a fragmentary cross-sectional view showing mandrel and drawing dies in operation;
Fig. 5 is a side elevation, partly in section, showing the method of removing the corefrom the finished tube; and
Fig. 6 is a side elevation showing the method of forming tubing by rolling.
In my process a tubular blank l of suitable dimensions is prepared either by molding a molybdenum ingot with a longitudinal central hole or by boring such a hole through a solid round The ratio of inside to outside diameter of theV tubular blank preferably should be the same as is desired in the nished tube, although it may be larger. An appropriate tubular blank, for example, may be 0.75 inch outside diameter by 0.438 inch inside diameter by 12 inches long. Within the tubular blank is placed as a core a work-hardenable l ground steel bar 5 preferably coated with dry slaked lime or the like to facilitate withdrawal of the bar after working. For the size of tubular blank given above, a limecoated core of drill steel stock .425 inch diameter is suitable, and it should be slightly shorter than the tubular blank to prevent cracking of the blank at the ends.
A high resistance to creep, or plastic flow, under the great stressand high temperatures to which it will be subjected, is the Amost necesasry property of the steel core. In this regard the grain structure and chemical composition ofthe steel are very important factors, and austenitic alloy steels have proven to be. best adapted for this use. Austenite in steel is a solid solution of carbon or of carbon and other elements in gamima iron, and austenitic steels, particularly of coarse grain structure, show a higher resistance to creep at temperatures above 850 F. than other and nner-grained steels. Alloy steels containing 10 to 14 percent manganese, with which 3 to 5 percent of nickel may form either an addition or a substitute for part of the manganese, have the useful property of rapid work-hardening, so that when slightly deformed initially the tensile ,strength and hardness at once are multiplied at the point of deformation and necking down is obviated.'N
The tubular blank and core are heated in a high-temperature gas or electric furnace, and are then swaged and/or drawn to the desired outside diameter. Usually the tube will be swaged to a suitablevdiameter and finished by drawing. In the swaging operation two things are of paramount importance: (1) the temperature must be carefullycontrolled so as to be high enough to. render the molybdenum workable yet not so high as to unduly soften the steel core; and (2) the surface of the tube must. be kept smooth and the diametervmust be kept uniform at all stages so as to avoid irregularities in the diameter of the steel core. If at anytime the outer surface of the tube becomes irregular, these irregularities are carried into the steel core and cannot -be removed by subsequent treatment. That is, every swaging pass must be the equivalent of a finishing pass.
bar 2, held in a, grippping device 3, by a, drin 4, In swaging the tubes described above, I reduced the outside diameter from 0.7 5 inch to 0.24 inch in fifteen passes, using long bearing lnishing dies f v6 of tool steel or the like for each pass.
temperature was held at 2300 to 2500 F. for the first passes and, as the working reflned the crystal structure of the molybdenum, the temperature was reduced to 2000 to 2200 for the last (0.24 inch) pass.
It was found that in these sizes at lower temperatures the molybdenum` split badly, and at higher temperatures the steel core showed severe distortion. The die's should also be heated through to prevent their cracking when they initially come into contact with the hot work.
Improvement in grain structure of the molybdenum with continued working permits a reduction in working temperatures as the tube and core become smaller.
For making very small diameter tubing, however, the swaged tube, coated with graphite or other suitable refractory lubricant, is preferably drawn through suitable dies 1 to the desired diameter. The 0.24 inch diameter mentioned above is not to be taken as necessarily indicative of the-proper Apoint at which to start drawing. In general, it is best to start drawing at as large a diameter as is convenient for the purpose. The temperature used in dra-wing is related to the reduction made in each pass; it must be high enough to avoid4 splitting of the tube yet not so high as to reduce its tensile: strength to the -point where it breaks. Again, this temperature is critical since allof the tension in drawing must be supported by the tube, the steel core having negligible strength in smaller diameters when hot.`
In drawingthetubes mentioned above, I reduced the outside diameter lfrom 0.24 inch to 0.093 inch in seven passes. yThe temperature was held at l400 to 1700" F. for the first passes and was` reduced for subsequent passes until for the last (0.093 inch). pass it was held at approximately 1100" to 1200 F.. Higher temperatures caused the tube to break and lower ones caused it to split. These dies, of course, should also be heated to the proper working temperatures.
Within the temperatures stated, molybdenum tubing may also be reduced by rolling between suitable rolls 8, which must, however, be of great strength and v ery rigidly mounted.
The steel core is removed from the finished tube 9 by nicking and breaking an end of the tube to expose the end of the core, then stretching the duced to permit ready removal by pincers or gripping tongs IIJ. Depending on the size, it may be necessary to anneal the core by heating the tube and the core a number` of times. I used a tensile The 0.093 inch tubes, and found that one auueai after a preliminary stretch was usually sufficient.
As used in the following claims, the word molybdenum shalll be construed to includetungsten and all other metals of like known properties unless I specifically indicate otherwise. In other respects, also although I have described my invention in considerable detail, I do not wish to be limited strictly to theexact and specific steps and details described, but may use such substitutions, modifications or equivalents thereof as are embraced within the scope of the invention or as are pointed out in the claims.
Having thus described my invention, what I claim as new and useful and desire to secure by Letters Patent is:
1. The method of making seamless molybdenum tubing which comprises forming a hollow tubular blank of the metal, inserting a core of a coarse-grained austenitic alloy steel containing substantially 10 to 14 per cent of manganese and coated with lime therein, heating said blank and core to a temperature approximately 2300 to 2500 F., hot-swaging with long-bearing finishing dies through a plurality of passes to improve the crystalline structure of the blank and workharden the core while reducing the diameter of both the core and the blank, and during swaging allowing the temperature to reduce to 2000 to 2200 F. for the nal swaging passes.
2. The method of making seamless molybdenum tubing which comprises forming a hollow tubular blank of the metal, inserting therein a shorter steel core of coarse-grained austenitic steel containing substantially 10 to 14 per cent manganese and 3 to 5 per cent nickel, heating said blank and core to a temperature approximately 2300 to 2500 F., hot-swaging with longy core until its diameter has been sufliciently retesting machine in removing the cores from the bearing nishing dies through a plurality of passes to improve the crystalline structure of the blank and work-harden the core while reducing the diametervof both the blank and the core, to a temperature approximately 2000 to 2200? F., then coating the exterior of the blank with a refractory lubricant, and further reducing by drawing through dies at gradually diminishing temperatures between 1700 and 1100 F.
3. The method of treating seamless molybdenum tubing which consists in heating the same on a lime-coated austenitic manganese steel core to a proper working temperature, then reducing the diameter of the tubing and core and improving the crystalline structure of the tubing and work-hardening the core by a plurality of swaging passes between long-bearing nishing dies heated to an appropriate temperature, and subse- JOHN E. EBERHARDT.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US396025A US2300353A (en) | 1941-05-31 | 1941-05-31 | Method of making seamless tubing |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US396025A US2300353A (en) | 1941-05-31 | 1941-05-31 | Method of making seamless tubing |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US2300353A true US2300353A (en) | 1942-10-27 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US396025A Expired - Lifetime US2300353A (en) | 1941-05-31 | 1941-05-31 | Method of making seamless tubing |
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| Country | Link |
|---|---|
| US (1) | US2300353A (en) |
Cited By (17)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2454172A (en) * | 1941-02-27 | 1948-11-16 | Bishop & Co Platinum Works J | Method of making seamless platinum ruthenium alloy cannulae |
| US2611475A (en) * | 1948-10-07 | 1952-09-23 | Remington Arms Co Inc | Cup drawing apparatus |
| US2628516A (en) * | 1949-07-09 | 1953-02-17 | Westinghouse Electric Corp | Tube making process |
| US2628926A (en) * | 1949-06-21 | 1953-02-17 | Westinghouse Electric Corp | Manufacture of machinable molybdenum |
| US2733503A (en) * | 1956-02-07 | Method of mfiking a shock strut | ||
| US2768430A (en) * | 1952-10-10 | 1956-10-30 | Hellefors Bruks Aktiebolag | Method of producing hollow rock drill steel |
| US2836884A (en) * | 1954-04-29 | 1958-06-03 | Int Nickel Co | Production of hollow metal articles |
| US2891307A (en) * | 1954-05-26 | 1959-06-23 | Int Nickel Co | Method of hot working heat-resistant metal articles |
| US2948957A (en) * | 1956-03-26 | 1960-08-16 | Vanadium Alloys Steel Co | Manufacture of metal stock having internal holes |
| US2960763A (en) * | 1955-10-11 | 1960-11-22 | Reymond M Reichl | Method of forging with thin webs |
| US2965959A (en) * | 1956-12-04 | 1960-12-27 | Int Nickel Co | Method of locating the blind terminals of filled holes in a deformed metal object |
| US2972179A (en) * | 1952-07-29 | 1961-02-21 | Stuart V Cuthbert | Method for producing molybdenum or molybdenum alloy gun liner |
| US3162943A (en) * | 1961-07-27 | 1964-12-29 | Wah Chang Corp | Method of making wire of superconductive materials |
| US3212178A (en) * | 1960-12-16 | 1965-10-19 | Atomic Energy Authority Uk | Process of assembling a temperature measuring device within an aperture of a fuel element |
| US3314143A (en) * | 1964-11-03 | 1967-04-18 | Robert E Mcdonald | Method for producing tube shells |
| US3316626A (en) * | 1964-10-26 | 1967-05-02 | J F Fredericks Tool Company In | Method of making an airfoil shaped electrode |
| US3349468A (en) * | 1963-05-06 | 1967-10-31 | Schloemann Ag Fa | Method for arresting a mandrel and tube discharged from a rolling mill |
-
1941
- 1941-05-31 US US396025A patent/US2300353A/en not_active Expired - Lifetime
Cited By (17)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2733503A (en) * | 1956-02-07 | Method of mfiking a shock strut | ||
| US2454172A (en) * | 1941-02-27 | 1948-11-16 | Bishop & Co Platinum Works J | Method of making seamless platinum ruthenium alloy cannulae |
| US2611475A (en) * | 1948-10-07 | 1952-09-23 | Remington Arms Co Inc | Cup drawing apparatus |
| US2628926A (en) * | 1949-06-21 | 1953-02-17 | Westinghouse Electric Corp | Manufacture of machinable molybdenum |
| US2628516A (en) * | 1949-07-09 | 1953-02-17 | Westinghouse Electric Corp | Tube making process |
| US2972179A (en) * | 1952-07-29 | 1961-02-21 | Stuart V Cuthbert | Method for producing molybdenum or molybdenum alloy gun liner |
| US2768430A (en) * | 1952-10-10 | 1956-10-30 | Hellefors Bruks Aktiebolag | Method of producing hollow rock drill steel |
| US2836884A (en) * | 1954-04-29 | 1958-06-03 | Int Nickel Co | Production of hollow metal articles |
| US2891307A (en) * | 1954-05-26 | 1959-06-23 | Int Nickel Co | Method of hot working heat-resistant metal articles |
| US2960763A (en) * | 1955-10-11 | 1960-11-22 | Reymond M Reichl | Method of forging with thin webs |
| US2948957A (en) * | 1956-03-26 | 1960-08-16 | Vanadium Alloys Steel Co | Manufacture of metal stock having internal holes |
| US2965959A (en) * | 1956-12-04 | 1960-12-27 | Int Nickel Co | Method of locating the blind terminals of filled holes in a deformed metal object |
| US3212178A (en) * | 1960-12-16 | 1965-10-19 | Atomic Energy Authority Uk | Process of assembling a temperature measuring device within an aperture of a fuel element |
| US3162943A (en) * | 1961-07-27 | 1964-12-29 | Wah Chang Corp | Method of making wire of superconductive materials |
| US3349468A (en) * | 1963-05-06 | 1967-10-31 | Schloemann Ag Fa | Method for arresting a mandrel and tube discharged from a rolling mill |
| US3316626A (en) * | 1964-10-26 | 1967-05-02 | J F Fredericks Tool Company In | Method of making an airfoil shaped electrode |
| US3314143A (en) * | 1964-11-03 | 1967-04-18 | Robert E Mcdonald | Method for producing tube shells |
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