US1719975A - Annealed thorium and method of making the same - Google Patents
Annealed thorium and method of making the same Download PDFInfo
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- US1719975A US1719975A US91354A US9135426A US1719975A US 1719975 A US1719975 A US 1719975A US 91354 A US91354 A US 91354A US 9135426 A US9135426 A US 9135426A US 1719975 A US1719975 A US 1719975A
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- US
- United States
- Prior art keywords
- thorium
- annealing
- bomb
- metal
- annealed
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- ZSLUVFAKFWKJRC-IGMARMGPSA-N 232Th Chemical compound [232Th] ZSLUVFAKFWKJRC-IGMARMGPSA-N 0.000 title description 26
- 229910052776 Thorium Inorganic materials 0.000 title description 26
- 238000004519 manufacturing process Methods 0.000 title description 3
- 229910052751 metal Inorganic materials 0.000 description 31
- 239000002184 metal Substances 0.000 description 31
- 238000000137 annealing Methods 0.000 description 28
- 238000000034 method Methods 0.000 description 17
- 239000007789 gas Substances 0.000 description 13
- 239000000843 powder Substances 0.000 description 10
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 description 8
- 238000010438 heat treatment Methods 0.000 description 8
- 150000002739 metals Chemical class 0.000 description 7
- 150000001875 compounds Chemical class 0.000 description 6
- 239000000463 material Substances 0.000 description 6
- 239000012298 atmosphere Substances 0.000 description 4
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 4
- 239000012535 impurity Substances 0.000 description 4
- 229910052757 nitrogen Inorganic materials 0.000 description 4
- 239000001301 oxygen Substances 0.000 description 4
- 229910052760 oxygen Inorganic materials 0.000 description 4
- OYPRJOBELJOOCE-UHFFFAOYSA-N Calcium Chemical compound [Ca] OYPRJOBELJOOCE-UHFFFAOYSA-N 0.000 description 3
- 229910052791 calcium Inorganic materials 0.000 description 3
- 239000011575 calcium Substances 0.000 description 3
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 2
- HCBIBCJNVBAKAB-UHFFFAOYSA-N Procaine hydrochloride Chemical compound Cl.CCN(CC)CCOC(=O)C1=CC=C(N)C=C1 HCBIBCJNVBAKAB-UHFFFAOYSA-N 0.000 description 2
- QCWXUUIWCKQGHC-UHFFFAOYSA-N Zirconium Chemical compound [Zr] QCWXUUIWCKQGHC-UHFFFAOYSA-N 0.000 description 2
- 239000011261 inert gas Substances 0.000 description 2
- 239000003870 refractory metal Substances 0.000 description 2
- 238000012360 testing method Methods 0.000 description 2
- WFKWXMTUELFFGS-UHFFFAOYSA-N tungsten Chemical compound [W] WFKWXMTUELFFGS-UHFFFAOYSA-N 0.000 description 2
- 229910052721 tungsten Inorganic materials 0.000 description 2
- 239000010937 tungsten Substances 0.000 description 2
- 229910052726 zirconium Inorganic materials 0.000 description 2
- 241000465531 Annea Species 0.000 description 1
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 1
- 229910052770 Uranium Inorganic materials 0.000 description 1
- 239000011149 active material Substances 0.000 description 1
- 239000003795 chemical substances by application Substances 0.000 description 1
- 238000011109 contamination Methods 0.000 description 1
- 229910002804 graphite Inorganic materials 0.000 description 1
- 239000010439 graphite Substances 0.000 description 1
- 229910052742 iron Inorganic materials 0.000 description 1
- 238000002844 melting Methods 0.000 description 1
- 230000008018 melting Effects 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000007789 sealing Methods 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
- 229910052715 tantalum Inorganic materials 0.000 description 1
- GUVRBAGPIYLISA-UHFFFAOYSA-N tantalum atom Chemical compound [Ta] GUVRBAGPIYLISA-UHFFFAOYSA-N 0.000 description 1
- -1 thorium Chemical class 0.000 description 1
- DNYWZCXLKNTFFI-UHFFFAOYSA-N uranium Chemical compound [U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U] DNYWZCXLKNTFFI-UHFFFAOYSA-N 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
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Classifications
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22F—CHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
- C22F1/00—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
- C22F1/16—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of other metals or alloys based thereon
- C22F1/18—High-melting or refractory metals or alloys based thereon
Definitions
- This invention relates to a process of annealing metals and more particularly to a process and Iapparatus suitable t'or annealing readily oxidizable metals, such as thorium,
- the metal thorium will be referred to hereinafter, however it is to be understood that the present process is useful in connection with the annealing of other lo metals, especially those which readily combine with nitrogen, oxygen and the like upon exposure thereto, particularly when in the heated condition.
- the present invention offers a simple and inexpensive process for accomplishing the annealing of such active metals as thorium.
- This process stated generally, comprises heating the metal to the desired temperature While surrounded by active materials whichl readily combine with impurities such as nitrogen, oxygen, and the like and which materials do not combine with the metal being annealed.
- the process comprisessur-l rounding the metal product by the pow-der of an active metal and encasing the same in a bomb and then surrounding the bomb with another active metal powder and enclosing the same in another and larger bomb.
- the bombs may then be brought to the desired temperature to eeet the annealing of the metal product without any combination taking place between the metal product and the gases in the surrounding atmosphere.
- Another object of the invention is to provide a suitable apparatus for annealing such metals as thorium, tantalum, uranium, zirconium, and the like.
- a thorium metal product lA comprising a swaged rod of thorium which has been worked cold, is placed centrally within a cylindrical iron bomb 2 and surrounded by metal powder 3, preferably thorium.
- the end of the bomb may then be sealed bymetal plug 4 threaded into the end of the bomb, it being preferable to first place a mixture 'of graphite and water on the threads in order to provide a hermetic seal.
- This small bomb may then be placed in a larger bomb 5 and the latter packed with well-reduced tungsten metal powder 6.
- the bomb 5 is then sealed in a manner similar to the first bomb.
- the bombs thus prepared are placed in a gas or other furnace and heated to about 1000o C. and held at that temperature for approximately 45 minutes. When cold, the bombs are opened andthe metal product removed. i'
- the purpose of surrounding the metal product with thorium powder is to prevent contamination of the product since the thorium powder will combine with oxygen and the like to form stable'compounds which do not dissociate at the annealing temperature. Furthermore, it is desirable to employ a metal powder or clean-up material which will combine with the impurities at a temperature below that at which the thorium metal product becomes heated sufficiently to combine with such impurities. It will be seen, therefore, that the object which I desire and do attain, is to provide an atmosphere surrounding the thorium metal product which does not contain any contaminating gases at the time the heating of the thorium is affected. It is also a factor to select the proper clean-up material, that is one which forms with the gaseons impurities a stable compound which does not dissociate at the temperature to which the thorium product is heated during annealing.
- the purpose of surrounding the inner bomb with tungsten is to prevent the air from passing into the inner bomb in the event the plug 4 should not remain perfectly tight. Obviously, if the plug is properly designed and litted in the end of the inner bomb, the external bomb need not be employed.
- a small quantity of calcium may be placed with the thorium metal powder in the inner bomb for the purpose of combining 'with and removing any nitrogen which might be present or enter the bomb during the annealing process.
- the bombs may be provided with a conduit 7, for the purpose of introducing an inert gas such as ar on within the inner bomb.
- the method of annealing worked bodies of highly reactive rare refractory metals ywhich comprisesI heating the same to the annealing temperature in an inert environment, hermetlcally sealed wlth respect to the atmos phere, while surrounding the metal body withv finely divided chemically reactive materials inert with respect to the refractory metal bc ing annealed but capable ofcombining with the residual atmospheric gases of the inert environment to form stable compounds at the temperature of annealing.
- the method of annealing mechanically worked thorium which comprises embedding the metal body in a container with a chemically reactive substance inert with respect to the thorium metal but reactive with and forming stable non-dissociable compounds with residual atmospheric gases therein, hermctically sealing the container,
- the method 'of annealing mechanically worked thorium which comprises embedding the metal body in a container with a chemically reactive material, inert with respect to thel thorium met-al but reactive with respect to residual gases contained therein to form compounds therewith stable at the temperature of annealing, displacing the atmospheric gases in the container with an inert gas, and thereafter heating the container to the annealing temperature for the desired length of time.
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- Chemical & Material Sciences (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Crystallography & Structural Chemistry (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Physical Or Chemical Processes And Apparatus (AREA)
Description
July 9, 1929. w. B. GERo ANNEALED THORIUM AND METHOD OF MAKING THE SAME INVENTOR ///LL//QM B. GERO ATTORNEY ARGO/v Gas Patented July 9, 1929.
UNITED STATES 1,719,975 PATENT OFFICE..
WILLIAM BENJAMIN GERO, OF BLOOMFIELD, NEW JERSEY, ASSIGNOR TO WESTING- HOUSE LAMP COMPANY, A CORPORATION F PENNSYLVANIA.
ANNEALED THORIUM AND METHOD OF MAKING THE SAME.
Application led March 1, 1926. Serial No. 91,354.
This invention relates to a process of annealing metals and more particularly to a process and Iapparatus suitable t'or annealing readily oxidizable metals, such as thorium,
uranimn, tantalnm, zirconium and the like.
As a specific example, the metal thorium will be referred to hereinafter, however it is to be understood that the present process is useful in connection with the annealing of other lo metals, especially those which readily combine with nitrogen, oxygen and the like upon exposure thereto, particularly when in the heated condition.
The ordinary processes of annealing are not suitable for metals such as thorium for the reason, it a metal of this character is heatc ed in an atmosphere of nitrogen or oxygen,
it either combines with or absorbs such gases to such an extent that the metal loses the properties upon which workability depends.
The present invention offers a simple and inexpensive process for accomplishing the annealing of such active metals as thorium. This process stated generally, comprises heating the metal to the desired temperature While surrounded by active materials whichl readily combine with impurities such as nitrogen, oxygen, and the like and which materials do not combine with the metal being annealed.
More specifically the process comprisessur-l rounding the metal product by the pow-der of an active metal and encasing the same in a bomb and then surrounding the bomb with another active metal powder and enclosing the same in another and larger bomb. The bombs may then be brought to the desired temperature to eeet the annealing of the metal product without any combination taking place between the metal product and the gases in the surrounding atmosphere.
Therefore, it is an object of the invention to provide a process for annealing metals of the class which readily become contaminated or lose the property upon which workability depends when exposed to the air when in a heated state.
Another object of the invention is to provide a suitable apparatus for annealing such metals as thorium, tantalum, uranium, zirconium, and the like.
Other objects of the invention will become apparent as the following description is read when taken in connection with the accompanying drawing in which the single figure is a longitudinal sectional view of the apparatus in which the annealing process may be practiced.
Referring to the drawing, a thorium metal product lA comprising a swaged rod of thorium which has been worked cold, is placed centrally within a cylindrical iron bomb 2 and surrounded by metal powder 3, preferably thorium. The end of the bomb may then be sealed bymetal plug 4 threaded into the end of the bomb, it being preferable to first place a mixture 'of graphite and water on the threads in order to provide a hermetic seal.
This small bomb may then be placed in a larger bomb 5 and the latter packed with well-reduced tungsten metal powder 6. The bomb 5 is then sealed in a manner similar to the first bomb.
The bombs thus prepared are placed in a gas or other furnace and heated to about 1000o C. and held at that temperature for approximately 45 minutes. When cold, the bombs are opened andthe metal product removed. i'
The purpose of surrounding the metal product with thorium powder is to prevent contamination of the product since the thorium powder will combine with oxygen and the like to form stable'compounds which do not dissociate at the annealing temperature. Furthermore, it is desirable to employ a metal powder or clean-up material which will combine with the impurities at a temperature below that at which the thorium metal product becomes heated sufficiently to combine with such impurities. It will be seen, therefore, that the object which I desire and do attain, is to provide an atmosphere surrounding the thorium metal product which does not contain any contaminating gases at the time the heating of the thorium is affected. It is also a factor to select the proper clean-up material, that is one which forms with the gaseons impurities a stable compound which does not dissociate at the temperature to which the thorium product is heated during annealing.
The purpose of surrounding the inner bomb with tungsten is to prevent the air from passing into the inner bomb in the event the plug 4 should not remain perfectly tight. Obviously, if the plug is properly designed and litted in the end of the inner bomb, the external bomb need not be employed. A
The following tests on a Rockwell testing machine made on certain specimens show the tentsi desird hardness before annealing and after annealy v invention.
If desired, a small quantity of calcium may be placed with the thorium metal powder in the inner bomb for the purpose of combining 'with and removing any nitrogen which might be present or enter the bomb during the annealing process. In case calcium or similar low melting point clean-up materials are employed, it is desirable to arrange the same within the inner bomb so that it does not come into contact with metal product.
Although I have given a specific example of the temperature and duration of heating, it 'is obvious that variations may be made therein, depending u on the hardness of the initial product, the istory of its previous islaat treatment, size of the'sample, and the As indicated in the drawings, the bombs may be provided with a conduit 7, for the purpose of introducing an inert gas such as ar on within the inner bomb.`
odications of the process may occur to those skilled in the art, however, such modifications are contemplated by me as come within the scope of the invention as defined inthe appended claims.
What is claimed is:
1. The method of annealing worked bodies.
non-contaminating and inert with respect to tl t lb d b l l f 1eme a o y emg annea ed but capab e 0 the annealing temperature for the desired combining with residual atmospheric gases within the container to form stable compounds at the temperature of annealing, and thereafter heating the container and conto the annealing temperature for the interval of time.
2. The method of annealing worked bodies of highly reactive rare refractory metals ywhich comprisesI heating the same to the annealing temperature in an inert environment, hermetlcally sealed wlth respect to the atmos phere, while surrounding the metal body withv finely divided chemically reactive materials inert with respect to the refractory metal bc ing annealed but capable ofcombining with the residual atmospheric gases of the inert environment to form stable compounds at the temperature of annealing.
3. The method of annealing mechanically worked thorium which comprises embedding the metal body in a container with a chemically reactive substance inert with respect to the thorium metal but reactive with and forming stable non-dissociable compounds with residual atmospheric gases therein, hermctically sealing the container,
and heating the mass to the annealing temperature for the desired length of time.
4. The method 'of annealing mechanically worked thorium which comprises embedding the metal body in a container with a chemically reactive material, inert with respect to thel thorium met-al but reactive with respect to residual gases contained therein to form compounds therewith stable at the temperature of annealing, displacing the atmospheric gases in the container with an inert gas, and thereafter heating the container to the annealing temperature for the desired length of time.
5. The process of annealing mechanically worked thorium which comprises embedding the worked article in thorium powder containing a proportion of a suitable gas cleanthe annealing temperaturefor the `desired length vof time.
6. The process of annealing mechanically worked thorium which comprises embedding the worked article in a sealedcontainer with thorium powder containing a proportion of a suitable gas clean-up agent such as calcium, displacing the atmospheric gases with' an inert environment, and thereafter heating to WILLLAM'BENJAMIN cano.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US91354A US1719975A (en) | 1926-03-01 | 1926-03-01 | Annealed thorium and method of making the same |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US91354A US1719975A (en) | 1926-03-01 | 1926-03-01 | Annealed thorium and method of making the same |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US1719975A true US1719975A (en) | 1929-07-09 |
Family
ID=22227338
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US91354A Expired - Lifetime US1719975A (en) | 1926-03-01 | 1926-03-01 | Annealed thorium and method of making the same |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US1719975A (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2546320A (en) * | 1948-11-04 | 1951-03-27 | Dominion Magnesium Ltd | Method of sintering titanium and like metals |
| US2898252A (en) * | 1951-07-03 | 1959-08-04 | Sylvester T Zegler | Method of heat-treating uranium-silicon alloys |
| US3068093A (en) * | 1959-03-03 | 1962-12-11 | Alfred J Darnell | Method of purifying thorium |
| US3490958A (en) * | 1966-04-13 | 1970-01-20 | Du Pont | Halocarbon-metal oxide combinations in heat treatment of metals |
-
1926
- 1926-03-01 US US91354A patent/US1719975A/en not_active Expired - Lifetime
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2546320A (en) * | 1948-11-04 | 1951-03-27 | Dominion Magnesium Ltd | Method of sintering titanium and like metals |
| US2898252A (en) * | 1951-07-03 | 1959-08-04 | Sylvester T Zegler | Method of heat-treating uranium-silicon alloys |
| US3068093A (en) * | 1959-03-03 | 1962-12-11 | Alfred J Darnell | Method of purifying thorium |
| US3490958A (en) * | 1966-04-13 | 1970-01-20 | Du Pont | Halocarbon-metal oxide combinations in heat treatment of metals |
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