US3218156A - Process for vacuum deoxidation of alloys - Google Patents
Process for vacuum deoxidation of alloys Download PDFInfo
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- US3218156A US3218156A US316513A US31651363A US3218156A US 3218156 A US3218156 A US 3218156A US 316513 A US316513 A US 316513A US 31651363 A US31651363 A US 31651363A US 3218156 A US3218156 A US 3218156A
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- 229910045601 alloy Inorganic materials 0.000 title description 38
- 239000000956 alloy Substances 0.000 title description 38
- 238000000034 method Methods 0.000 title description 27
- 230000008569 process Effects 0.000 title description 5
- 239000000155 melt Substances 0.000 claims description 45
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 claims description 27
- 229910052760 oxygen Inorganic materials 0.000 claims description 27
- 239000001301 oxygen Substances 0.000 claims description 27
- 238000002844 melting Methods 0.000 claims description 17
- 230000008018 melting Effects 0.000 claims description 17
- 229910052761 rare earth metal Inorganic materials 0.000 claims description 13
- 150000002910 rare earth metals Chemical class 0.000 claims description 13
- 239000012535 impurity Substances 0.000 claims description 12
- 229910001404 rare earth metal oxide Inorganic materials 0.000 claims description 3
- 229910052684 Cerium Inorganic materials 0.000 description 45
- GWXLDORMOJMVQZ-UHFFFAOYSA-N cerium Chemical compound [Ce] GWXLDORMOJMVQZ-UHFFFAOYSA-N 0.000 description 45
- QSHDDOUJBYECFT-UHFFFAOYSA-N mercury Chemical compound [Hg] QSHDDOUJBYECFT-UHFFFAOYSA-N 0.000 description 23
- 229910052753 mercury Inorganic materials 0.000 description 23
- 239000000243 solution Substances 0.000 description 15
- 229910052751 metal Inorganic materials 0.000 description 12
- 239000002184 metal Substances 0.000 description 12
- 229910000420 cerium oxide Inorganic materials 0.000 description 11
- BMMGVYCKOGBVEV-UHFFFAOYSA-N oxo(oxoceriooxy)cerium Chemical compound [Ce]=O.O=[Ce]=O BMMGVYCKOGBVEV-UHFFFAOYSA-N 0.000 description 9
- 229910052727 yttrium Inorganic materials 0.000 description 9
- VWQVUPCCIRVNHF-UHFFFAOYSA-N yttrium atom Chemical compound [Y] VWQVUPCCIRVNHF-UHFFFAOYSA-N 0.000 description 9
- 238000007792 addition Methods 0.000 description 8
- 238000010494 dissociation reaction Methods 0.000 description 7
- 230000005593 dissociations Effects 0.000 description 7
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 6
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 6
- 238000007670 refining Methods 0.000 description 5
- 230000009467 reduction Effects 0.000 description 4
- 239000011261 inert gas Substances 0.000 description 3
- 229910052742 iron Inorganic materials 0.000 description 3
- 238000005272 metallurgy Methods 0.000 description 3
- 150000002739 metals Chemical class 0.000 description 3
- 238000007254 oxidation reaction Methods 0.000 description 3
- 238000005266 casting Methods 0.000 description 2
- DRVWBEJJZZTIGJ-UHFFFAOYSA-N cerium(3+);oxygen(2-) Chemical class [O-2].[O-2].[O-2].[Ce+3].[Ce+3] DRVWBEJJZZTIGJ-UHFFFAOYSA-N 0.000 description 2
- 238000006243 chemical reaction Methods 0.000 description 2
- 229910017052 cobalt Inorganic materials 0.000 description 2
- 239000010941 cobalt Substances 0.000 description 2
- GUTLYIVDDKVIGB-UHFFFAOYSA-N cobalt atom Chemical compound [Co] GUTLYIVDDKVIGB-UHFFFAOYSA-N 0.000 description 2
- 230000002939 deleterious effect Effects 0.000 description 2
- 230000001627 detrimental effect Effects 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 238000004519 manufacturing process Methods 0.000 description 2
- 229910052759 nickel Inorganic materials 0.000 description 2
- SIWVEOZUMHYXCS-UHFFFAOYSA-N oxo(oxoyttriooxy)yttrium Chemical compound O=[Y]O[Y]=O SIWVEOZUMHYXCS-UHFFFAOYSA-N 0.000 description 2
- 239000010936 titanium Substances 0.000 description 2
- 229910052719 titanium Inorganic materials 0.000 description 2
- 229910000636 Ce alloy Inorganic materials 0.000 description 1
- 229910052692 Dysprosium Inorganic materials 0.000 description 1
- 229910052691 Erbium Inorganic materials 0.000 description 1
- 229910052688 Gadolinium Inorganic materials 0.000 description 1
- 229910052689 Holmium Inorganic materials 0.000 description 1
- 229910001122 Mischmetal Inorganic materials 0.000 description 1
- 229910052779 Neodymium Inorganic materials 0.000 description 1
- 229910052777 Praseodymium Inorganic materials 0.000 description 1
- 229910052772 Samarium Inorganic materials 0.000 description 1
- 229910052771 Terbium Inorganic materials 0.000 description 1
- 229910052775 Thulium Inorganic materials 0.000 description 1
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 1
- 229910052769 Ytterbium Inorganic materials 0.000 description 1
- QCWXUUIWCKQGHC-UHFFFAOYSA-N Zirconium Chemical compound [Zr] QCWXUUIWCKQGHC-UHFFFAOYSA-N 0.000 description 1
- 229910052782 aluminium Inorganic materials 0.000 description 1
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 229910052799 carbon Inorganic materials 0.000 description 1
- 150000001768 cations Chemical class 0.000 description 1
- 150000001875 compounds Chemical class 0.000 description 1
- 239000000470 constituent Substances 0.000 description 1
- 230000000875 corresponding effect Effects 0.000 description 1
- 230000007797 corrosion Effects 0.000 description 1
- 238000005260 corrosion Methods 0.000 description 1
- 238000004090 dissolution Methods 0.000 description 1
- KBQHZAAAGSGFKK-UHFFFAOYSA-N dysprosium atom Chemical compound [Dy] KBQHZAAAGSGFKK-UHFFFAOYSA-N 0.000 description 1
- UYAHIZSMUZPPFV-UHFFFAOYSA-N erbium Chemical compound [Er] UYAHIZSMUZPPFV-UHFFFAOYSA-N 0.000 description 1
- UIWYJDYFSGRHKR-UHFFFAOYSA-N gadolinium atom Chemical compound [Gd] UIWYJDYFSGRHKR-UHFFFAOYSA-N 0.000 description 1
- KJZYNXUDTRRSPN-UHFFFAOYSA-N holmium atom Chemical compound [Ho] KJZYNXUDTRRSPN-UHFFFAOYSA-N 0.000 description 1
- -1 illinium Chemical compound 0.000 description 1
- 238000005495 investment casting Methods 0.000 description 1
- 229910052746 lanthanum Inorganic materials 0.000 description 1
- FZLIPJUXYLNCLC-UHFFFAOYSA-N lanthanum atom Chemical compound [La] FZLIPJUXYLNCLC-UHFFFAOYSA-N 0.000 description 1
- OHSVLFRHMCKCQY-UHFFFAOYSA-N lutetium atom Chemical compound [Lu] OHSVLFRHMCKCQY-UHFFFAOYSA-N 0.000 description 1
- 229910052748 manganese Inorganic materials 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 230000007246 mechanism Effects 0.000 description 1
- 229910001092 metal group alloy Inorganic materials 0.000 description 1
- 229910044991 metal oxide Inorganic materials 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- QEFYFXOXNSNQGX-UHFFFAOYSA-N neodymium atom Chemical compound [Nd] QEFYFXOXNSNQGX-UHFFFAOYSA-N 0.000 description 1
- 229910052758 niobium Inorganic materials 0.000 description 1
- 238000010943 off-gassing Methods 0.000 description 1
- 239000007800 oxidant agent Substances 0.000 description 1
- 230000003647 oxidation Effects 0.000 description 1
- 150000002927 oxygen compounds Chemical class 0.000 description 1
- PUDIUYLPXJFUGB-UHFFFAOYSA-N praseodymium atom Chemical compound [Pr] PUDIUYLPXJFUGB-UHFFFAOYSA-N 0.000 description 1
- 238000002360 preparation method Methods 0.000 description 1
- 238000000746 purification Methods 0.000 description 1
- KZUNJOHGWZRPMI-UHFFFAOYSA-N samarium atom Chemical compound [Sm] KZUNJOHGWZRPMI-UHFFFAOYSA-N 0.000 description 1
- 229910052706 scandium Inorganic materials 0.000 description 1
- SIXSYDAISGFNSX-UHFFFAOYSA-N scandium atom Chemical compound [Sc] SIXSYDAISGFNSX-UHFFFAOYSA-N 0.000 description 1
- 230000035939 shock Effects 0.000 description 1
- 239000006104 solid solution Substances 0.000 description 1
- 229910000601 superalloy Inorganic materials 0.000 description 1
- 229910052715 tantalum Inorganic materials 0.000 description 1
- GZCRRIHWUXGPOV-UHFFFAOYSA-N terbium atom Chemical compound [Tb] GZCRRIHWUXGPOV-UHFFFAOYSA-N 0.000 description 1
- NAWDYIZEMPQZHO-UHFFFAOYSA-N ytterbium Chemical compound [Yb] NAWDYIZEMPQZHO-UHFFFAOYSA-N 0.000 description 1
- 229910052726 zirconium Inorganic materials 0.000 description 1
Classifications
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21C—PROCESSING OF PIG-IRON, e.g. REFINING, MANUFACTURE OF WROUGHT-IRON OR STEEL; TREATMENT IN MOLTEN STATE OF FERROUS ALLOYS
- C21C7/00—Treating molten ferrous alloys, e.g. steel, not covered by groups C21C1/00 - C21C5/00
- C21C7/10—Handling in a vacuum
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C1/00—Making non-ferrous alloys
- C22C1/02—Making non-ferrous alloys by melting
Definitions
- This invention relates to a process for de-oxidizing metal alloys.
- the invention is particularly directed for use in the production of alloys which are prepared by means of vacuum melting techniques.
- the use of vacuum melting techniques has been effective to reduce oxygen levels whereby this time, and combination of the cerium with the oxygen is effected under these relatively high pressure conditions.
- the melt is subjected to a vacuum in the order of about 10 microns of mercury after the cerium has had an opportunity to go into solution and combine in the desired manner.
- Elements commonly used as de-oxidizing agents include aluminum, titanium and zirconium. These elements form an oxide which cerned, it will be appreciated that variations thereof are contemplated.
- the initial vacuum is preferably high enough to remove a substantial amount of impurities; however, a previously purified melt may not require any extensive initial period.
- the cerium is to be added while employing a relatively low vacuum since it is necessary to maintain conditions whereby the cerium will go into solution and combine with the oxygen.
- the final vacuum stage on the other hand, must be conducted at a sufficiently high vacuum whereby dissociation of the cerium and cerium oxide will be possible.
- the final vacuum of 10 v microns or less can then be effected in the same manner method whereby alloys having an extremely low oxygen 1 content can be produced in an economical and efiicient manner.
- the instant invention has particular application to the casting of large heats of vacuum cast metal which will subsequently be used as remelt stock in producing vacuum investment castings.
- the invention also has application with respect to other vacuum melting practices where a reduction of oxygen in solution and dissolution of oxides in solution is desirable to improve the alloy properties both with respect to castability and
- the method of this invention comprises a system for de-oxidizing alloys wherein the alloy is reduced to a molten state and subjected to a vacuum.
- this technique provides for removal of a substantial amount of the impurities within the metal.
- the present invention contemplates the addition "of a small percentage of cerium which is adapted to preferentially combine with the oxygen contained in the melt. After the addition of cerium, a relatively high vacuum is effected whereby the cerium oxide and excess cerium will vaporize and dissociate from the melt.
- the amount of cerium added is between 0.01 and 0.5 percent by weight of the melt while amounts between 0.1 and 0.3 percent COlTlIl'lOIl.
- alloys which can be effectively prepared in accordance with the techniques of this invention.
- the instant invention is particularly applicable to iron, nickel and cobalt base alloys which are used under conditions requiring high strength as Well as substantial resistance to heat and corrosive atmospheres. In order to achieve the desired properties in such alloys, removal of oxygen has been a prime requirement. It will be understood, however, that in addition to the following types of alloys,
- Example 1 Percent lNi 70 Mo 3.5 'Ti, Nb, Ta 2.5 .Fe Balance Example II Percent 35-.45 1.0 1.0
- a partial pressure of inert gas can then be introduced into the vacuum chamber to achieve a vacuum of about 200 microns or less.
- Cerium in amounts between 0.01 and 0.5 percent by weight of the melt and preferably in an amount between 0.1 and 0.3 percent is then added by introducing pure cerium or rare earth metal alloys into the melt. While maintaining the pressure at the last mentioned level, the cerium will go into solution and will combine with the oxygen whereby the cerium oxides are formed.
- a calculation regarding the amount of oxygen should be made whereby the quantity or" cerium introduced will be at least sufiicient to combine with this amount of oxygen. The time necessary for this reaction will usually be about 5 to 10 minutes.
- a pressure Well above microns is preferably maintained during the addition of cerium in order to insure that the cerium goes i't'n to solution and combines with the oxygen.
- a pressure in the order of about 10 microns of mercury is preferably maintained during the phase of the operation providing for dissociation of cerium oxide and excess cerium from the melt.
- the time necessary for the dissociation of the cerium oxide can only be estimated since this time will vary, depending on the particular melt practice and facilities available.
- the cerium content of the melt can be analyzed during the melt cycle and the values obtained can be compared with the oxygen content of the initially refined metal. Since cerium additions Will be controlled within the above ranges in accordance with the oxygen content of the initially refined metal, the progress of the formation of cerium oxide can be determined, and the time necessary for this phase of the operation can be, thus, accurately estimated.
- An average cycle on a 1000 pound melt will take from 25 minutes to two hours. The temperature of the melt will have a significant effect on the dissociation rate and the practice of the individual melt shop will, therefore, effect the exact time.
- the system of the instant invention has been found to provide significant improvements in the physical proper- ;ties of the alloys treated.
- the stress rupture life, impact pnoperties, tensile properties, thermal shock properties, and corrosion resistance are all positively efiected by the decxidation technique herein described.
- cerium in any conventional way, for example through the use of cerium alloys or other combinations.
- Misch metal is cited as a particular mechanism for providing the necessary amounts of metal capable of reacting in the desired fashion.
- Other equivalents of cerium are also obviously contemplated.
- cerium As used herein and in the aforementioned copending application, the term equivalents of cerium is meant to include the rare earth metals mainly, cerium, lanthanum, praseodymium, neodymium, illinium, Samarium, gadolinium, terbium, dysprosium, holmium, erbium, thulium, yttrium, ytterbium, scandium, lutecium. Excellent results are secured when yttrium is employed instead of cerium in the examples heretofore described and in correspond ing amounts. The others of the rare earth metals can also be substituted for cerium in equivalent amounts.
- L A method for tie-oxidizing an alloy comprising the steps of melting the alloy while maintained under a vacuum below 100 microns of mercury to thereby romove a substantial amount of the impurities therein, increasing the pressure over the melt above 100 microns of mercury, adding from about 0.01 to about 0.5 percent by weight rare earth metal to the melt. whereby the rare earth metal will go into solution and combine With the oxygen therein, and reinstituting a vaccum below 10 microns of mercury whereby rare earth metal oxide and excess rare earth metal will vaporize and dissociate from the melt.
- a method for de-oxidizing an alloy comprising the steps of melting the alloy While maintained under a vacuum below 100 microns of mercury to thereby romove a substantial amount of the impurities therein, increasing the pressure over the melt to about 200 microns of mercury, adding from about 0.01 to about 0.5 percent by weight rare earth metal to the melt whereby the rare earth metal will go into solution and combine with the oxygen therein, and reinstituting a vacuum in the order of about microns of mercury whereby rare earth metal oxide and excess rare earth metal will vaporize and dissociate from the melt.
- a method for de-oxidizing an alloy comprising the steps of melting the alloy while maintained under a vacuum below 100 microns of mercury to thereby romove a substantial amount of the impurities therein, increasing the pressure over the melt above 100 microns of mercury by introducing inert gas into the vacuum chamber, adding from about 0.01 to about 0.5 percent by weight yttrium to the melt whereby the yttrium will go into solution and combine with the oxygen therein, and reinstituting a vacuum below 10 microns of mercury whereby yttrium oxide and excess yttrium will vaporize and dissociate from the melt.
- a method for de-oxidizing an alloy comprising the steps of melting the alloy while maintained under a vacuum below 100 microns of mercury to thereby romove a substantial amount of the impurities therein, increasing the pressure over the melt to about 200 microns of mercury, adding from about 0.01 to about 0.5 percent by weight cerium to the melt whereby the cerium will go into solution and combine with the oxygen therein, and reinstituting a vacuum in the order of about 10 microns of mercury whereby cerium oxide and excess cerium will vaporize and dissociate from the melt.
- a method for de-oxidizing an alloy comprising the steps of melting the alloy while maintained under a vacuum below 100 microns of mercury to thereby romove a substantial amount of the impurities therein, increasing the pressure over the melt above 100 microns of mercury by introducing inert gas into the vacuum chamber, adding from about 0.01 to about 0.5 percent by weight cerium to the melt whereby the cerium will go into solution and combine with the oxygen therein, and reinstituting a vacuum below 10 microns of mercury whereby cerium oxide and excess cerium will vaporize and dissociate from the melt.
- a method for de-oxidizing an alloy comprising the steps of melting the alloy while maintained under a vacuum below 100 microns of mercury to thereby remove a substantial amount of the impurities therein, increasing the pressure over the melt to about 200 microns of mercury, adding from about 0.01 to about 0.5 percent by weight yttrium to the melt whereby the yttrium will go into solution and combine with the oxygen therein, and reinstituting a vacuum in the order of about 10 microns of mercury whereby yttrium oxide and excess yttrium will vaporize and dissociate from the melt.
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- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Mechanical Engineering (AREA)
- Manufacture And Refinement Of Metals (AREA)
Description
United States Patent C 3,218,156 PROCESS FOR VACUUM DEOXIDATION OF ALLOYS Jay L. Vander Sluis, Grand Haven, and Frank G. Vihtelic,
Whitehall, MiclL, assignors to Howe Sound Company,
New York, N.Y., a corporation of Delaware No Drawing. Filed Oct. 16, 1963, Ser. No. 316,513
8 Claims. (Cl. 75--49) This is a continuation-in-part of our copending appli cation Serial No. 296,078, filed July 18, 1963, and entitled De-Oxidation of Alloys, and now abandoned.
This invention relates to a process for de-oxidizing metal alloys. The invention is particularly directed for use in the production of alloys which are prepared by means of vacuum melting techniques.
It is well-known that certain impurities in metal tend to closely aliect the physical and mechanical properties of such metals. This is particularly true in the case of are preferred. The application of vacuum over the melt is controlled whereby the initial melting operation is undertaken with a vacuum of greater than 100 microns of mercury whereby dissociation of a substantial amount of the impurities in the melt can be efiectively undertaken. The cerium is added to the melt in the desired amounts after the pressure over the melt is increased to about 200 microns of mercury. The cerium is added at oxygen and many varied techniques have been devised for eifecting de-oxidation of alloys containing detrimental amounts of oxygen.
In many instances, the use of vacuum melting techniques has been effective to reduce oxygen levels whereby this time, and combination of the cerium with the oxygen is effected under these relatively high pressure conditions. Finally, the melt is subjected to a vacuum in the order of about 10 microns of mercury after the cerium has had an opportunity to go into solution and combine in the desired manner. By employing the low pressure above noted, the cerium oxide and excess cerium will dissociate from the melt to leave an extremely pure alloy.
With reference to the initial stages of the process, it is to be noted that the vacuum conditions prevailing can be maintained during the entire melting operation. On the other hand, it is contemplated that a melt be subjected to a vacuum for initial removal of impurities irrespective of the manner in which the initial molten state is achieved.
' Insofar as the other vacuum values above listed are conthe resulting alloys were suitable for certain applications.
the melt whereby oxygen compounds could be formed 1 which were less detrimental insofar as the properties of the resulting alloy were concerned. Elements commonly used as de-oxidizing agents include aluminum, titanium and zirconium. These elements form an oxide which cerned, it will be appreciated that variations thereof are contemplated. Thus, the initial vacuum is preferably high enough to remove a substantial amount of impurities; however, a previously purified melt may not require any extensive initial period. The cerium is to be added while employing a relatively low vacuum since it is necessary to maintain conditions whereby the cerium will go into solution and combine with the oxygen. The final vacuum stage, on the other hand, must be conducted at a sufficiently high vacuum whereby dissociation of the cerium and cerium oxide will be possible.
has greater stability than the compounds normally included in the melt, and they also have a lower solubility whereby removal of some of the oxides is facilitated.
Known techniques employing de-oxidizers in the manner described above have, however, been unsuitable since As noted, the cerium additions are undertaken at a pressure which permits the cerium to go into solution and combine with the oxygen. Introduction of an inert atmosphere is preferably effected to achieve an increase in in the case of vacuum melting, the oxides formed possess extremely low dissociation pressures. For this reason, a
significant amount of the oxides cannot be removed from the melt by any practical method.
It is an object of this invention to provide an improved pressure and the melt can be maintained under this atmosphere until after the cerium has gone into solution and the desired oxides formed. The final vacuum of 10 v microns or less can then be effected in the same manner method whereby alloys having an extremely low oxygen 1 content can be produced in an economical and efiicient manner.
It is a more specific object of this invention to provide an improved technique for the production of alloys substantially free of oxygen wherein the processing is carried out in combination with vacuum melting operations.
These and other objects of this invention will appear hereinafter and it will be understood that the specific examples set forth herein are provided solely for purposes of illustration and not by way of limitation.
as described above. Addition of the cerium as pure cerium, in the form of rare earth alloys, or any other conventional manner is contemplated.
The instant invention has particular application to the casting of large heats of vacuum cast metal which will subsequently be used as remelt stock in producing vacuum investment castings. However, the invention also has application with respect to other vacuum melting practices where a reduction of oxygen in solution and dissolution of oxides in solution is desirable to improve the alloy properties both with respect to castability and The method of this invention comprises a system for de-oxidizing alloys wherein the alloy is reduced to a molten state and subjected to a vacuum. As recognized by the prior art, this technique provides for removal of a substantial amount of the impurities within the metal. To provide for more effective purification of the melt, the present invention contemplates the addition "of a small percentage of cerium which is adapted to preferentially combine with the oxygen contained in the melt. After the addition of cerium, a relatively high vacuum is effected whereby the cerium oxide and excess cerium will vaporize and dissociate from the melt.
In accordance with this invention, the amount of cerium added is between 0.01 and 0.5 percent by weight of the melt while amounts between 0.1 and 0.3 percent COlTlIl'lOIl.
with respect to physical and mechanical properties in the as-cast state. In the preparation of certain alloys, for example the so-called iron, nickel and cobalt base super alloys, long vacuum refining cycles have heretofore been The present invention provides for substantial reductions in such cycles since the reduction of the oxygen level depends on the reaction of cerium and oxygen and not on the slow process of out gassing the melt.
The following comprise specific examples of alloys which can be effectively prepared in accordance with the techniques of this invention. As previously indicated, the instant invention is particularly applicable to iron, nickel and cobalt base alloys which are used under conditions requiring high strength as Well as substantial resistance to heat and corrosive atmospheres. In order to achieve the desired properties in such alloys, removal of oxygen has been a prime requirement. It will be understood, however, that in addition to the following types of alloys,
other alloys wherein oxygen presents a problem can be treated in accordance with the principles of this invention.
Example 1 Percent lNi 70 Mo 3.5 'Ti, Nb, Ta 2.5 .Fe Balance Example II Percent 35-.45 1.0 1.0
Nb 3.54.0 Fe Remainder i Example III Percent Si 1.25 Cr 14.0
Ni 16.0- W -c 3.5 .Fe Balance Example IV Percent Co 60.0 Cr 20.0
W 10.0 Nb 2.0 Ni 1.0 Fe, C, Mn, Si Balance In a typical procedure for treatment of any of'theabove alloys, the'constituents thereof can be first melted. down using standard melting techniques and standard. vacuum practices. The time necessary for initially refining the metal will vary with the individual melt practice, type of alloy, amount and nature of revert material used in the charge, condition of the melting plant, and on other obvious factors. The factors which are primarily considered when determining the length of the refining cycle are the vacuum pressure in the melting chamber and the melt temperature. Alloys are usually refined until a final vacuum pressure of about microms of mercury is achieved with a reasonably low leak rate. A typical 1000 to 2000 pound melt will have a melt-down and initial refining cycle in the range of seven to 12 hours. It will be understood, however, that the initial refining cycle does not constitute a novel aspect of this invention.
A partial pressure of inert gas can then be introduced into the vacuum chamber to achieve a vacuum of about 200 microns or less. Cerium in amounts between 0.01 and 0.5 percent by weight of the melt and preferably in an amount between 0.1 and 0.3 percent is then added by introducing pure cerium or rare earth metal alloys into the melt. While maintaining the pressure at the last mentioned level, the cerium will go into solution and will combine with the oxygen whereby the cerium oxides are formed. A calculation regarding the amount of oxygen should be made whereby the quantity or" cerium introduced will be at least sufiicient to combine with this amount of oxygen. The time necessary for this reaction will usually be about 5 to 10 minutes.
Since the vapor pressure of cerium at 2600 F. is about 100 microns, the additions of cerium must be undertaken .at a lower vacuum while the dissociation of cerium oxides and excess cerium must be conducted at a higher vacuum. As suggested by the above discussion, a pressure Well above microns is preferably maintained during the addition of cerium in order to insure that the cerium goes i't'n to solution and combines with the oxygen. On the other hand, a pressure in the order of about 10 microns of mercury is preferably maintained during the phase of the operation providing for dissociation of cerium oxide and excess cerium from the melt. When the desired removal of cerium oxide and cerium is completed, the metal will be ready for casting into ingot molds.
The time necessary for the dissociation of the cerium oxide can only be estimated since this time will vary, depending on the particular melt practice and facilities available. However, the cerium content of the melt can be analyzed during the melt cycle and the values obtained can be compared with the oxygen content of the initially refined metal. Since cerium additions Will be controlled within the above ranges in accordance with the oxygen content of the initially refined metal, the progress of the formation of cerium oxide can be determined, and the time necessary for this phase of the operation can be, thus, accurately estimated. An average cycle on a 1000 pound melt will take from 25 minutes to two hours. The temperature of the melt will have a significant effect on the dissociation rate and the practice of the individual melt shop will, therefore, effect the exact time.
The system of the instant invention has been found to provide significant improvements in the physical proper- ;ties of the alloys treated. The stress rupture life, impact pnoperties, tensile properties, thermal shock properties, and corrosion resistance are all positively efiected by the decxidation technique herein described.
The noted improvements are believed to result by reason of the reduction of deleterious oxides which has caused changes in the micro-structure of the treated alloys. By dissociating the metallic oxides from the melt in the manner described, the metal originally forming the deleterious oxides will go back into solution to serve its intended role as a solid solution strengthener, to enhance oxidation resistance, or for whatever other purpose it was added.
In the above description, reference has been made to the use of cerium; however, it will be understood that the addition of cerium can be eifected in any conventional way, for example through the use of cerium alloys or other combinations. The use of Misch metal is cited as a particular mechanism for providing the necessary amounts of metal capable of reacting in the desired fashion. Other equivalents of cerium are also obviously contemplated. As used herein and in the aforementioned copending application, the term equivalents of cerium is meant to include the rare earth metals mainly, cerium, lanthanum, praseodymium, neodymium, illinium, Samarium, gadolinium, terbium, dysprosium, holmium, erbium, thulium, yttrium, ytterbium, scandium, lutecium. Excellent results are secured when yttrium is employed instead of cerium in the examples heretofore described and in correspond ing amounts. The others of the rare earth metals can also be substituted for cerium in equivalent amounts.
It will be understood that various changes and modifications may be made in the above described procedures which provide the characteristics of this invention without departing from the spirit thereof particularly as defined in the following claims.
We claim:
L A method for tie-oxidizing an alloy comprising the steps of melting the alloy while maintained under a vacuum below 100 microns of mercury to thereby romove a substantial amount of the impurities therein, increasing the pressure over the melt above 100 microns of mercury, adding from about 0.01 to about 0.5 percent by weight rare earth metal to the melt. whereby the rare earth metal will go into solution and combine With the oxygen therein, and reinstituting a vaccum below 10 microns of mercury whereby rare earth metal oxide and excess rare earth metal will vaporize and dissociate from the melt.
2. A method for de-oxidizing an alloy comprising the steps of melting the alloy While maintained under a vacuum below 100 microns of mercury to thereby romove a substantial amount of the impurities therein, increasing the pressure over the melt to about 200 microns of mercury, adding from about 0.01 to about 0.5 percent by weight rare earth metal to the melt whereby the rare earth metal will go into solution and combine with the oxygen therein, and reinstituting a vacuum in the order of about microns of mercury whereby rare earth metal oxide and excess rare earth metal will vaporize and dissociate from the melt.
3. A method for de-oxidizing an alloy comprising the steps of melting the alloy while maintained under a vacuum below 100 microns of mercury to thereby romove a substantial amount of the impurities therein, increasing the pressure over the melt above 100 microns of mercury by introducing inert gas into the vacuum chamber, adding from about 0.01 to about 0.5 percent by weight yttrium to the melt whereby the yttrium will go into solution and combine with the oxygen therein, and reinstituting a vacuum below 10 microns of mercury whereby yttrium oxide and excess yttrium will vaporize and dissociate from the melt.
4. A method for de-oxidizing an alloy comprising the steps of melting the alloy while maintained under a vacuum below 100 microns of mercury to thereby romove a substantial amount of the impurities therein, increasing the pressure over the melt to about 200 microns of mercury, adding from about 0.01 to about 0.5 percent by weight cerium to the melt whereby the cerium will go into solution and combine with the oxygen therein, and reinstituting a vacuum in the order of about 10 microns of mercury whereby cerium oxide and excess cerium will vaporize and dissociate from the melt.
5. A method in accordance with claim 4 wherein the amount of cerium added is between 0.01 and 0.3 percent by weight of said melt.
6. A method for de-oxidizing an alloy comprising the steps of melting the alloy while maintained under a vacuum below 100 microns of mercury to thereby romove a substantial amount of the impurities therein, increasing the pressure over the melt above 100 microns of mercury by introducing inert gas into the vacuum chamber, adding from about 0.01 to about 0.5 percent by weight cerium to the melt whereby the cerium will go into solution and combine with the oxygen therein, and reinstituting a vacuum below 10 microns of mercury whereby cerium oxide and excess cerium will vaporize and dissociate from the melt.
7. A method for de-oxidizing an alloy comprising the steps of melting the alloy while maintained under a vacuum below 100 microns of mercury to thereby remove a substantial amount of the impurities therein, increasing the pressure over the melt to about 200 microns of mercury, adding from about 0.01 to about 0.5 percent by weight yttrium to the melt whereby the yttrium will go into solution and combine with the oxygen therein, and reinstituting a vacuum in the order of about 10 microns of mercury whereby yttrium oxide and excess yttrium will vaporize and dissociate from the melt.
8. A method in accordance with claim 7 wherein the amount of yttrium added is between 0.01 and 0.3 percent by weight of said melt.
References Cited by the Examiner UNITED STATES PATENTS 2,144,200 1/1939 Rohn 49 XR 2,360,717 10/1944 Phelps 7558 FOREIGN PATENTS 870,162 6/1961 Great Britain.
OTHER REFERENCES Vacuum Metallurgy, Papers presented at the Vacuum Metallurgy Symposium of the Electrothermics and Metallurgy Division of the Electrochemical Society, October 6 and 7, 1954, Boston, Massachusetts, pages -105.
ASM Metals Handbook, 8th edition, vol. 1, published by American Society for Metals, Novelty, Ohio, 1961, pages 1227, 1230 and 1231.
BENJAMIN HENKIN, Primary Examiner.
WINSTON A. DOUGLAS, Examiner.
Claims (1)
1. A METHOF FOR DE-OXIDIZING ANALLOY COMPRISING THE STEPS OF MELTING THE ALLOY WHILE MAINTAINED UNDER A VACUUM BELOW 100 MICRONS OF MERCURY TO THEREBY ROMOVE A SUBSTANTIAL AMOUNT OF THE IMPURITIES THEREIN, INCREASING THE PRESSURE OVE THE MELT ABOVE 100 MICRONS OF MERCURY, ADDING FROM ABOUT 0.01 TO ABOUT 0.5 PERCENT BY WEIGHT RARE EARTH METAL TO THE MELT WHEREBY THE RARE EARTH METAL WILL GO INTO SOLUTION AND COMBINE WITH THE OXYGEN THEREIN, AND REINSTITUTING A VACCUM BELOW 10 MICRONS OF MERCURY WHEREBY RARE EARTH METAL OXIDE AND EXCESS RARE EARTH METAL WILL VAPORIZE AND DISSOCIATE FROM THE MELT.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US316513A US3218156A (en) | 1963-10-16 | 1963-10-16 | Process for vacuum deoxidation of alloys |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US316513A US3218156A (en) | 1963-10-16 | 1963-10-16 | Process for vacuum deoxidation of alloys |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US3218156A true US3218156A (en) | 1965-11-16 |
Family
ID=23229367
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US316513A Expired - Lifetime US3218156A (en) | 1963-10-16 | 1963-10-16 | Process for vacuum deoxidation of alloys |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US3218156A (en) |
Cited By (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3816104A (en) * | 1970-09-25 | 1974-06-11 | Allegheny Ludlum Ind Inc | Deoxidizing nickel base and cobalt base alloys |
| US3853540A (en) * | 1973-04-11 | 1974-12-10 | Latrobe Steel Co | Desulfurization of vacuum-induction-furnace-melted alloys |
| US4042381A (en) * | 1976-07-06 | 1977-08-16 | Republic Steel Corporation | Control of inclusion morphology in steel |
| FR2438091A1 (en) * | 1978-10-04 | 1980-04-30 | Vasipari Kutato Intezet | METHOD AND APPARATUS FOR REDUCING THE INCLUSION CONTENT OF STEELS AND FOR REFINING THEIR STRUCTURE |
| US4826738A (en) * | 1987-07-07 | 1989-05-02 | United Technologies Corporation | Oxidation and corrosion resistant chromia forming coatings |
| US4895201A (en) * | 1987-07-07 | 1990-01-23 | United Technologies Corporation | Oxidation resistant superalloys containing low sulfur levels |
| RU2221067C1 (en) * | 2002-12-03 | 2004-01-10 | Федеральное государственное унитарное предприятие "Всероссийский научно-исследовательский институт авиационных материалов" | Method of production of carbon-free casting heat- resistant nickel-based alloys |
| RU2302473C2 (en) * | 2005-09-23 | 2007-07-10 | Общество с ограниченной ответственностью "ПЗЦМ-АВИА" | Method of processing high-temperature alloy wastes |
| RU2696625C1 (en) * | 2019-04-18 | 2019-08-06 | Федеральное государственное унитарное предприятие "Всероссийский научно-исследовательский институт авиационных материалов" (ФГУП "ВИАМ") | Production method of carbon-free foundry heat-resistant nickel-based alloys |
Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2144200A (en) * | 1936-06-27 | 1939-01-17 | Heraeus Vacuumschmelze Ag | Method of manufacturing siliconiron alloys |
| US2360717A (en) * | 1942-11-27 | 1944-10-17 | Cerium Corp | Method of eliminating aluminate and silicate inclusions |
| GB870162A (en) * | 1958-09-11 | 1961-06-14 | British Iron Steel Research | Improvements in or relating to the purification of metals |
-
1963
- 1963-10-16 US US316513A patent/US3218156A/en not_active Expired - Lifetime
Patent Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2144200A (en) * | 1936-06-27 | 1939-01-17 | Heraeus Vacuumschmelze Ag | Method of manufacturing siliconiron alloys |
| US2360717A (en) * | 1942-11-27 | 1944-10-17 | Cerium Corp | Method of eliminating aluminate and silicate inclusions |
| GB870162A (en) * | 1958-09-11 | 1961-06-14 | British Iron Steel Research | Improvements in or relating to the purification of metals |
Cited By (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3816104A (en) * | 1970-09-25 | 1974-06-11 | Allegheny Ludlum Ind Inc | Deoxidizing nickel base and cobalt base alloys |
| US3853540A (en) * | 1973-04-11 | 1974-12-10 | Latrobe Steel Co | Desulfurization of vacuum-induction-furnace-melted alloys |
| US4042381A (en) * | 1976-07-06 | 1977-08-16 | Republic Steel Corporation | Control of inclusion morphology in steel |
| FR2438091A1 (en) * | 1978-10-04 | 1980-04-30 | Vasipari Kutato Intezet | METHOD AND APPARATUS FOR REDUCING THE INCLUSION CONTENT OF STEELS AND FOR REFINING THEIR STRUCTURE |
| US4826738A (en) * | 1987-07-07 | 1989-05-02 | United Technologies Corporation | Oxidation and corrosion resistant chromia forming coatings |
| US4895201A (en) * | 1987-07-07 | 1990-01-23 | United Technologies Corporation | Oxidation resistant superalloys containing low sulfur levels |
| RU2221067C1 (en) * | 2002-12-03 | 2004-01-10 | Федеральное государственное унитарное предприятие "Всероссийский научно-исследовательский институт авиационных материалов" | Method of production of carbon-free casting heat- resistant nickel-based alloys |
| RU2302473C2 (en) * | 2005-09-23 | 2007-07-10 | Общество с ограниченной ответственностью "ПЗЦМ-АВИА" | Method of processing high-temperature alloy wastes |
| RU2696625C1 (en) * | 2019-04-18 | 2019-08-06 | Федеральное государственное унитарное предприятие "Всероссийский научно-исследовательский институт авиационных материалов" (ФГУП "ВИАМ") | Production method of carbon-free foundry heat-resistant nickel-based alloys |
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