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US3063835A - Corrosion-resistant alloys - Google Patents

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US3063835A
US3063835A US821134A US82113459A US3063835A US 3063835 A US3063835 A US 3063835A US 821134 A US821134 A US 821134A US 82113459 A US82113459 A US 82113459A US 3063835 A US3063835 A US 3063835A
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Stern Milton
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    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C14/00Alloys based on titanium
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C27/00Alloys based on rhenium or a refractory metal not mentioned in groups C22C14/00 or C22C16/00
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C27/00Alloys based on rhenium or a refractory metal not mentioned in groups C22C14/00 or C22C16/00
    • C22C27/06Alloys based on chromium

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  • This invention relates to corrosion-resistant alloys and, particularly, to corrosion resistant alloys in which titanium or chromium is the predominant metal.
  • Titanium and many of its alloys, as well as chromium and many of its alloys are noted for excellent resistance to oxidizing corrosive media.
  • non-oxidizing corrosive media such as hydrochloric and sulfuric acid solutions
  • these metals and alloys exhibit little or no resistance. It would be most desirable to have available alloys capable of withstanding corrosive environments ranging from strongly oxidizing to weakly oxidizing or non-oxidizing.
  • An alloy of this type would have the widest utility. For example, such an alloy would be invaluable in chemical plant equipment.
  • Hydrochloric and sulfuric acids are prime examples of non-oxidizing corrosive media. These acids enter into many important commercial processes. They require storing and handling equipment which combine the desirable properties cited above. If a titanium alloy, for example, were to possess resistance to non-oxidizing acid solutions, in addition to its natural endowments of lightness, strength, and resistance to oxidizing acid solutions, it would be extremely useful in such applications.
  • titanium alloys specifically to resist attack by a strong non-oxidizing acid.
  • the corrosion resistance is derived in great measure from the molybdenum which is itself resistant to these acids, but the eitectiveness of the molybdenum does not become especially significant until amounts up to 20 percent are added.
  • One disadvantage of this alloy is that the tendency toward brittleness increases along with molybdenum content so that by the time 40 percent is reached, the alloy has become excessively brittle and difiicult to fabricate.
  • resistance to non-oxidizing acids is gained, the resistance to oxidizing acids is lost.
  • One widely used method for preventing corrosion is to add passivating inhibitors to the environment which, it is believed, operate by producing local action current to anodically polarize a metal into the passive potential region. It is not always desirable, however, to alter the composition of a solution to prevent corrosion of the equipment in which it is contained, particularly when the composition of the solution is critical or specific to some process. Such a means of preventing corrosion is limited to the particular case where the composition of the contained solution is not critical.
  • corosion resistance can be achieved in non-oxidizing environments by artificially anodically polarizing the base metal by applying an external current (which might be termed anodic protection as opposed to cathodic protection).
  • anodic protection as opposed to cathodic protection
  • the primary object of this invention to provide alloys of titanium and alloys of chromium which are resistant to the attack of oxidizing and non-oxidizing corrosive media.
  • a corrosion resistant alloy consisting essentially of from 0.005 to 5 percent by weight in the aggregate of at least one metal selected from the group consisting of ruthenium, rhodium, palladium, osmium, iridium, platinum, gold, rhenium, and alloys thereof, and the balance a metal selected from the group consisting of titanium, chromium, and alloys thereof wherein said selected metal is present in predominant amounts.
  • alloys of the invention have been prepared and tested. Dramatic improvements in corrosion rates were obtained and are set forth in the following table in comparison with pure titanium and various titanium alloys. In these tests, the samples were degreased, pickled, dried, and weighed. They were then immersed in boiling acid of composition and concentration as set forth, for one period of 24 hours duration, removed, washed, and weighed again. The corrosion rate was calculated and reported as mils penetration per year.
  • Table I indicates the results of noble metal additions to substantially pure titanium.
  • Table II provides the same information as to noble metal additions to binary and tertiary titanium base alloys. The percentages given in each case are percentages by weight of the total alloy.
  • FIGS. 1 and 2 demonstrate the eifectiveness of platinum and palladium in decreasing the rate of corrosion of titanium in hydrochloric and sulfuric acid, respectively.
  • the addition of 0.035 percent palladium is effective in reducing the corrosion rate of titaniumrexposed to 10.0 percent boiling HCl to the level of approximately 100 mils penetration per year, only 0.005 percent is necessary to reduce the rate to the same level when titanium is exposed to 3.0 percent boiling HCl.
  • the additive is used in amounts of 0.1 to 0.5 percent. With amounts below 0.1 percent noble metal addition, the desired improvement in corrosion resistance may not be needs. As cited previously, as little as.005 percent of noble metal addition to titanium may sufiice for low concentrations of acids. With amounts substantially in excess of about 2.0 per- 4 cent, no marked degree of improvement results.
  • the noble metals may be present in the alloy either singly or in any combination with each other.
  • the titanium-base alloys shown in Table II also exhibit improved corrosion resistance in non-oxidizing media when alloyed with one of the noble metals listed. It is seen from Table II that alloys containing at least about 80 percent by weight titanium are benefitted. Of especial significance is the titanium-molybdenum-noble metal alloy shown in Table II.
  • Some alloys of titanium and molybdenum are known to possess resistance to corrosive non-oxidizing media because of the resistance to such media naturally possessed by molybdenum.
  • the resistance to non-oxidizing media of a titanium-40 percent molybdenum alloy is much greater than the resistance of pure titanium in such media.
  • the increased resistance to non-oxidizing media poossessed by this alloy is acquired at the expense of the resistance to oxidizing media normally possessed by titanium.
  • With amounts of less than 40 percent molybdenum in titanium the resistance to non-oxidizing media is not as great. Below 15 percent molybdenum, a titanium molybdenum alloy shows little of this resistance to non-oxidizing media.
  • titanium-molybdenum alloys of one of the noble metals selected from the group ruthenium, rhodium, palladium, osmium, iridium, platinium, gold and rhenium a corrosion resistance alloy is obtained that is suitable for use in both oxidizing and non-oxidizing media.
  • the titaniumbase alloy should contain from about 8 percent to 20 percent by weight molybdenum, and may contain up to 5 percent by weight of one or more of the noble metals.
  • a preferred range of composition is from 8 to 20 percent molybdenum, from 0.05 to 2 percent palladium, and the balance titanium and incidental impurities. Any noble metal from the group listed above may beused; but because of economic considerations, it is preferred to use palladium.
  • an alloy may be prepared that consists of from 12 to 14 percent molybdenum, about 0.2 percent palladium, and the balance titanium and incidental impurities.
  • the alloys shown in Table V II include some high-molybdenum titanium-base alloys which show greatly improved resistance to non-oxidizing media, but do not exhibit the re'sistance'to oxidizing'media found in the alloys of this invention.
  • Table -III indicates the results of noble metal additions to substantially pure chromium.
  • Table IV provides the same information as to noble metal additions to binary and tertiary chromium-base alloys. The percentages given in each case are percentages by weight of the total alloy.
  • the 0.5 osmium addition while it decreases the rate drastically, is not as elfective as an equal amount of platinum. It will further be observed that, in general, additions of noble metal reduce the rate of corrosion of chromium in boiling non-oxidizing acids of concentrations as high as 60%.
  • the proportion of noble metal addition may be varied according to the anticipated use. Where contact with a more rigorous environment is anticipated, such as strong concentrations of acid, more noble metal is required. For best results in conditions where exposure to strong solutions is encountered, the additive is used in amounts of between 0.05 and 0.5%. With amounts below 0.05% noble metal addition, the desired improvement in corrosion resistance may not be suflicient to meet the particular needs. As little as 0.005% of noble metal addition may suflice for low concentration of acid, however. With amounts substantially in excess of about 5%, no marked degree of improvement results.
  • the noble metals may be present either singly or in combination with each other.
  • the alloys of the present invention may be prepared according to current metallurgical practice, although the invention is not limited by the method of preparation.
  • the ingredients may be in any commercially pure form since the invention is not limited to the degree of its constituents.
  • a corrosion-resistant alloy consisting essentially of from about 0.005 to about 5 percent by weight in the aggregate of at least one metal selected from the group consisting of ruthenium, rhodium, palladium, osmium, iridium, platinum, and rhenium, and the balance titanium and incidental impurities.
  • a corrosion-resistant alloy consisting essentially of from about 0.05 to about 2 percent by weight in the aggregate of at least one metal selected from the group consisting of ruthenium, rhodium, palladium, osmium, iridium, platinum, and rhenium, and the balance titanium and incidental impurities.
  • a corrosion-resistant alloy consisting essentially of about 0.05 percent by weight palladium, and the balance titanium and incidental impurities.
  • a corrosion-resistant alloy consisting essentially of about 0.05 percent by weight platinum, and the balance titanium and incidental impurities.
  • a corrosion resistant alloy consisting essentially of from about 8 to about 20 percent by weight molybdenum, from about 0.05 to about 2 percent by weight in the aggregate of at least one metal selected from the group consisting of ruthenium, rhodium, palladium, osmium, iridium, platinum, and rhenium, and the balance titanium and incidental impurities.
  • a corrosion-resistant alloy consisting essentially of from about 8 to about 20 percent by weight molybdenum, from about 0.05 to about 2 percent by weight palladium, and the balance titanium and incidental impurities.
  • a corrosion-resistant alloy consisting essentially of from about 12 to 14 percent by weight molybdenum, about 0.2 palladium, and the balance titanium and incidental impurities.
  • a corrosion resistant alloy consisting essentially of about 0.2 percent by weight palladium, and the balance titanium and incidental impurities.
  • a corrosion-resistant alloy consisting essentially of from about 0.005 to about 5 percent by weight in the aggregate of at least one metal selected from the group consisting of ruthenium, rhodium, palladium, osmium, iriditun, platinum, and rhenium, and the balance substantially all a metallic material selected from the group consisting of titanium and alloys of titanium with at least one element selected from the group consisting of aluminum, vanadium, manganese, molybdenum, and carbon containing :at least about percent by weight titanium.
  • a corrosion-resistant alloy consisting essentially of from about 0.05 to about 2 percent by weight in the aggregate of at least one metal selected from the group consisting of ruthenium, rhodium, palladium, osmium, iridium, platinum, and rhenium, and the balance substantially all a metallic material selected from the group consisting of titanium and alloys of titanium with at alloy containing consisting of 40 and the balance may also be made 7 7 least one element selected from the group consisting of FOREIGN PATIENTS aluminum, vanadinm, manganese, molybdenum, and car- 18 212 Great Britain July 9, 1914 bon containing at least about 80 per-gent by weight ti- M1913 +11; V tanium. 1

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Description

Nov. 13, 1962 M. STERN CORROSION-RESISTANT ALLOYS Filed June 18, 1959 2 Sheets-Sheet 2 l I U! I 40,000 Ol/. H2504 I os'/. H2504 I 43-40244 s0 4,000 2 4 4| H :4,000 400 407. BOILING H2504 a H M 2 0 U I 400 g s 4 I E I I o E o 5/. BOILING H2804 I, I E n: i m 2 g i 4 o 40 77 8 0 g F: g 8 Q 0 2 O 8 E 47. BOILING H2504 I l J LO 4 E I 4 4 4 444; 0 0.4 0.2 0.3 0.4 0.5 0?! .20
PER CENT PLATINUM INVENTOR. MILTON STERN BY fimfi z) A T TORNEV United States Patent Ofitice 3,063,835 Patented Nov. 13, 1962 3,063,835 CORROSION-RESISTANT ALLOYS Milton Stern, Tonawanda, N.Y., assignor to Union Carbide Corporation, a corporation of New York Filed June 18, 1959, Ser. No. 821,134 Claims. (Cl. 75175.5)
This invention relates to corrosion-resistant alloys and, particularly, to corrosion resistant alloys in which titanium or chromium is the predominant metal.
Titanium and many of its alloys, as well as chromium and many of its alloys are noted for excellent resistance to oxidizing corrosive media. In non-oxidizing corrosive media, such as hydrochloric and sulfuric acid solutions, these metals and alloys exhibit little or no resistance. It would be most desirable to have available alloys capable of withstanding corrosive environments ranging from strongly oxidizing to weakly oxidizing or non-oxidizing. An alloy of this type would have the widest utility. For example, such an alloy would be invaluable in chemical plant equipment.
Hydrochloric and sulfuric acids are prime examples of non-oxidizing corrosive media. These acids enter into many important commercial processes. They require storing and handling equipment which combine the desirable properties cited above. If a titanium alloy, for example, were to possess resistance to non-oxidizing acid solutions, in addition to its natural endowments of lightness, strength, and resistance to oxidizing acid solutions, it would be extremely useful in such applications.
There have been attempts to design titanium alloys specifically to resist attack by a strong non-oxidizing acid. Most typical among these are compositions of 30 to 40 percent molybdenum, balance substantially all titanium. The corrosion resistance is derived in great measure from the molybdenum which is itself resistant to these acids, but the eitectiveness of the molybdenum does not become especially significant until amounts up to 20 percent are added. One disadvantage of this alloy is that the tendency toward brittleness increases along with molybdenum content so that by the time 40 percent is reached, the alloy has become excessively brittle and difiicult to fabricate. Moreover, as resistance to non-oxidizing acids is gained, the resistance to oxidizing acids is lost.
One widely used method for preventing corrosion is to add passivating inhibitors to the environment which, it is believed, operate by producing local action current to anodically polarize a metal into the passive potential region. It is not always desirable, however, to alter the composition of a solution to prevent corrosion of the equipment in which it is contained, particularly when the composition of the solution is critical or specific to some process. Such a means of preventing corrosion is limited to the particular case where the composition of the contained solution is not critical.
According to scientific theory, corosion resistance can be achieved in non-oxidizing environments by artificially anodically polarizing the base metal by applying an external current (which might be termed anodic protection as opposed to cathodic protection). This method, for obvious reasons, would be extremely difiicult to accomplish in chemical plant equipment.
It is, therefore, the primary object of this invention to provide alloys of titanium and alloys of chromium which are resistant to the attack of oxidizing and non-oxidizing corrosive media.
It is also an object of this invention to provide a method for increasing the resistance to non-oxidizing corrosive media of the metals titianum, chromium, and their alloys.
Other aims and advantages of this invention will be apparent from the following description and the appended claims.
In accordance with these objects a corrosion resistant alloy is provided consisting essentially of from 0.005 to 5 percent by weight in the aggregate of at least one metal selected from the group consisting of ruthenium, rhodium, palladium, osmium, iridium, platinum, gold, rhenium, and alloys thereof, and the balance a metal selected from the group consisting of titanium, chromium, and alloys thereof wherein said selected metal is present in predominant amounts.
It is believed that the important factor in obtaining the desired improvement, and the principle upon which the in-- vention operates, lies in the production of suflicient local action current to anodically polarize the alloy into the passive region. High local action currents are created by high potential differences between the electrodes of the galvanic couple and by shallow polarization curve slopes. The current required to change the potential of either cathode or anode a given amount by polarization is proportional to the cathode and anode areas which, in turn, are determined by the noble metal content of the alloy.
Specific embodiments of alloys of the invention have been prepared and tested. Dramatic improvements in corrosion rates were obtained and are set forth in the following table in comparison with pure titanium and various titanium alloys. In these tests, the samples were degreased, pickled, dried, and weighed. They were then immersed in boiling acid of composition and concentration as set forth, for one period of 24 hours duration, removed, washed, and weighed again. The corrosion rate was calculated and reported as mils penetration per year.
Table I indicates the results of noble metal additions to substantially pure titanium. Table II provides the same information as to noble metal additions to binary and tertiary titanium base alloys. The percentages given in each case are percentages by weight of the total alloy.
TABLE I Effect of Noble Metal Additions ion Corrosion Rate of Titanium Corrosion rate (mils/year) Composition, percent noble metal Boiling H28 04 Boiling H01 Ti 455 3 2, 952 6 241. 8 4, 479. 7 Ti+0.01 Pt- 9. 0 1, 411. 8 Ti+0.37 Pt- 1. 3 39. 0 1. 0 71. 2 Ti+2.00 Pt 1. 0 36. 0 Ti+5.00 Pt 89. 6 Ti+0.005 Pd 56.1 3,125. 4 Ti+0.44 Pd--- 1. 3 0. 6 67. 3 Ti-HL48 AIL--- 3. 2 206. 4 8. 7 145. 5 Ti+0.60 Ir Nil 44. 8 2. 6 87. 6 Ti+0.48 Os. 1. 0 81. 5 2. 6 207. 7 ii+0.36 Re- 8.7 29.0 Ti+0.5 Rh.. 2.6 48. 0 1. 6 55.1 TH-0.5 Run"- 1.6 48.0 2. 3 112. 7
7 sufficient to meet the particular I 3 TABLE n Effect of Noble Metal Additions on Corrosion Rate of Titanium Base Alloys Corrosion rate (mils/year) Composition, percent additive BoilingHzs O4 Boiling H01 .5 Al+15 V+ .Mn-l-fli 8 Mu+Ti+0.1 Pd 5 Mo+Ti Corrosion rate (mils/year) boiling H 04, 10%
' Dissolved In the tables above, the corrosion rate of titanium, without any addition, is given first to serve as a comparison. It will be observed that all the noble metals tested were extremely effective in reducing the corrosion rate of both titanium and its alloys. It will be observed that as little as'0.005 percent by weight palladium produces a fourfold decrease in the corrosion rate of titanium in boiling 3.0 percent HCl. It will further be observed that, in general, additions of noble metals reduce the rate of corrosion of titanium and its alloys at least an order of magnitude, even in boiling non-oxidizing acids of concentrations as high as 55.0 percent.
The proportion of the noble metal addition may be varied according to the anticipated use. Where contact with more rigorous environments is anticipated, such as strong concentrations of acid, more noble metal is required. FIGS. 1 and 2 demonstrate the eifectiveness of platinum and palladium in decreasing the rate of corrosion of titanium in hydrochloric and sulfuric acid, respectively. Referring to FIG. 1, whereas the addition of 0.035 percent palladium is effective in reducing the corrosion rate of titaniumrexposed to 10.0 percent boiling HCl to the level of approximately 100 mils penetration per year, only 0.005 percent is necessary to reduce the rate to the same level when titanium is exposed to 3.0 percent boiling HCl. Referring to FIG. 2 whereas the addition of 0.2 percent platinum is effective in reducing the corrosion rate of titanium exposed to 10 percent boiling H 80 to the level of approximately 50 mils penetration per year, only 0.015 percent is necessary to reduce the rate to the same level when titanium is exposed to 1 percent boiling H 50 For best results, in conditions where exposure to strong solutions is encountered, the additive is used in amounts of 0.1 to 0.5 percent. With amounts below 0.1 percent noble metal addition, the desired improvement in corrosion resistance may not be needs. As cited previously, as little as.005 percent of noble metal addition to titanium may sufiice for low concentrations of acids. With amounts substantially in excess of about 2.0 per- 4 cent, no marked degree of improvement results. The noble metals may be present in the alloy either singly or in any combination with each other.
The titanium-base alloys shown in Table II also exhibit improved corrosion resistance in non-oxidizing media when alloyed with one of the noble metals listed. It is seen from Table II that alloys containing at least about 80 percent by weight titanium are benefitted. Of especial significance is the titanium-molybdenum-noble metal alloy shown in Table II.
Some alloys of titanium and molybdenum are known to possess resistance to corrosive non-oxidizing media because of the resistance to such media naturally possessed by molybdenum. The resistance to non-oxidizing media of a titanium-40 percent molybdenum alloy is much greater than the resistance of pure titanium in such media. However, the increased resistance to non-oxidizing media poossessed by this alloy is acquired at the expense of the resistance to oxidizing media normally possessed by titanium. With amounts of less than 40 percent molybdenum in titanium, the resistance to non-oxidizing media is not as great. Below 15 percent molybdenum, a titanium molybdenum alloy shows little of this resistance to non-oxidizing media. However, by the addition to titanium-molybdenum alloys of one of the noble metals selected from the group ruthenium, rhodium, palladium, osmium, iridium, platinium, gold and rhenium, a corrosion resistance alloy is obtained that is suitable for use in both oxidizing and non-oxidizing media. The titaniumbase alloy should contain from about 8 percent to 20 percent by weight molybdenum, and may contain up to 5 percent by weight of one or more of the noble metals. A preferred range of composition is from 8 to 20 percent molybdenum, from 0.05 to 2 percent palladium, and the balance titanium and incidental impurities. Any noble metal from the group listed above may beused; but because of economic considerations, it is preferred to use palladium.
For satisfactory commercial use :an alloy may be prepared that consists of from 12 to 14 percent molybdenum, about 0.2 percent palladium, and the balance titanium and incidental impurities. The alloys shown in Table V II include some high-molybdenum titanium-base alloys which show greatly improved resistance to non-oxidizing media, but do not exhibit the re'sistance'to oxidizing'media found in the alloys of this invention. For example, an alloy consisting of about 10 percent molybdenum, about 0.2 percent palladium, and the balance titanium'willfshow about the same corrosion resistance in boiling 5 percent hydrochloricacid as titanium-20 percent molybdenum alloy; however, the low-molybdenum alloy of this invention has ten times greater resistance to an oxidizing environment, such as boiling percent nitric acid, than the 20 percent molybdenum alloy.
TABLE III Effect of Noble Metal Additions on Corrison Rate of Chromium Table -III indicates the results of noble metal additions to substantially pure chromium. Table IV provides the same information as to noble metal additions to binary and tertiary chromium-base alloys. The percentages given in each case are percentages by weight of the total alloy.
TABLE IV Efiect of Noble Metal Additions on Corrosion Rate of Chromium-Base Alloys 1 Dissolved.
In Table III, the corrosion resistance of chromium without any addition is given first to serve as a comparison. Pure chromium, it will be noted, dissolves in both boiling sulfuric acid and boiling hydrochloric acid in the concentrations indicated. It will be observed that all the noble metals tested were extremely effective in reducing the corrosion rate of chromium. The degree of efiFectiveness varies with the quantity of noble metal added. It will be observed that as little as 0.1% by weight platinum renders chromium practically insoluble in 20% boiling sulfuric acid. Although the corrosion rate appears to increase with increasing amounts of platinum up to 5%, it will be understood that no significant difference actually exists between the various rates except for the 0.5 osmium rate. The 0.5 osmium addition, while it decreases the rate drastically, is not as elfective as an equal amount of platinum. It will further be observed that, in general, additions of noble metal reduce the rate of corrosion of chromium in boiling non-oxidizing acids of concentrations as high as 60%. The proportion of noble metal addition may be varied according to the anticipated use. Where contact with a more rigorous environment is anticipated, such as strong concentrations of acid, more noble metal is required. For best results in conditions where exposure to strong solutions is encountered, the additive is used in amounts of between 0.05 and 0.5%. With amounts below 0.05% noble metal addition, the desired improvement in corrosion resistance may not be suflicient to meet the particular needs. As little as 0.005% of noble metal addition may suflice for low concentration of acid, however. With amounts substantially in excess of about 5%, no marked degree of improvement results. The noble metals may be present either singly or in combination with each other.
In Table IV, the corrosion rate of several chromiumbase alloys, together with the rate of the same alloy with the platinum addition, is given for comparison. It will be seen that the base alloy readily dissolves in moderate to strong concentration of either sulfuric or hydrochloric acid. Although a chromium base alloy containing 40 percent iron and percent molybdenum is able to withstand the lower concentrations higher than 20%. However, when only 0.5% platinum is added to the base alloy, a very marked decrease in the rate of corrosion results. The elfectiveness of the noble metal addition, as before, depends on the strength of the corrosive medium and on the amount of noble metal added. Moreover, some alloys are more efliectively protected by the same amount of noble metal addition than others. An 0.5% addition of platinum, for instance, while it decreases the rate of corrosion of a chromium-base alloy containing 2 percent Cu in 40 percent boiling sulfuric acid, is not as effective with this alloy as with a chromium-base 10 percent molybdenum, or an alloy percent iron, 10 percent molybdenum chromium. Additions of noble metals to chromium electrodeposit.
The alloys of the present invention may be prepared according to current metallurgical practice, although the invention is not limited by the method of preparation. The ingredients may be in any commercially pure form since the invention is not limited to the degree of its constituents.
The description of the invention above has been in terms of its specific embodiments. Modifications and equivalents will be apparent to those skilled in the art and this disclosure is intended to be illustrative of, but not necessarily to constitute a limitation upon, the scope of the invention.
This application is a continuation in part of my copending application Serial No. 732,793, filed May 5, 1958, now abandoned.
What is claimed is:
1. A corrosion-resistant alloy consisting essentially of from about 0.005 to about 5 percent by weight in the aggregate of at least one metal selected from the group consisting of ruthenium, rhodium, palladium, osmium, iridium, platinum, and rhenium, and the balance titanium and incidental impurities.
2. A corrosion-resistant alloy consisting essentially of from about 0.05 to about 2 percent by weight in the aggregate of at least one metal selected from the group consisting of ruthenium, rhodium, palladium, osmium, iridium, platinum, and rhenium, and the balance titanium and incidental impurities.
3. A corrosion-resistant alloy consisting essentially of about 0.05 percent by weight palladium, and the balance titanium and incidental impurities.
4. A corrosion-resistant alloy consisting essentially of about 0.05 percent by weight platinum, and the balance titanium and incidental impurities.
5. A corrosion resistant alloy consisting essentially of from about 8 to about 20 percent by weight molybdenum, from about 0.05 to about 2 percent by weight in the aggregate of at least one metal selected from the group consisting of ruthenium, rhodium, palladium, osmium, iridium, platinum, and rhenium, and the balance titanium and incidental impurities.
6. A corrosion-resistant alloy consisting essentially of from about 8 to about 20 percent by weight molybdenum, from about 0.05 to about 2 percent by weight palladium, and the balance titanium and incidental impurities.
7. A corrosion-resistant alloy consisting essentially of from about 12 to 14 percent by weight molybdenum, about 0.2 palladium, and the balance titanium and incidental impurities.
8. A corrosion resistant alloy consisting essentially of about 0.2 percent by weight palladium, and the balance titanium and incidental impurities.
9. A corrosion-resistant alloy consisting essentially of from about 0.005 to about 5 percent by weight in the aggregate of at least one metal selected from the group consisting of ruthenium, rhodium, palladium, osmium, iriditun, platinum, and rhenium, and the balance substantially all a metallic material selected from the group consisting of titanium and alloys of titanium with at least one element selected from the group consisting of aluminum, vanadium, manganese, molybdenum, and carbon containing :at least about percent by weight titanium.
10. A corrosion-resistant alloy consisting essentially of from about 0.05 to about 2 percent by weight in the aggregate of at least one metal selected from the group consisting of ruthenium, rhodium, palladium, osmium, iridium, platinum, and rhenium, and the balance substantially all a metallic material selected from the group consisting of titanium and alloys of titanium with at alloy containing consisting of 40 and the balance may also be made 7 7 least one element selected from the group consisting of FOREIGN PATIENTS aluminum, vanadinm, manganese, molybdenum, and car- 18 212 Great Britain July 9, 1914 bon containing at least about 80 per-gent by weight ti- M1913 +11; V tanium. 1
5 OTHER EEXEsR N E R n e Ci d in h fi eo i PM? Pietrokowsky et a1.: Journal of Metals, v01. 8, August UNITED STATES PATENTS 1956, pages 930-935. Published by the A.1.M.E., New
7 York, N.Y. 2247755 Hansel et July 1941 ASM Metals Handbook, 1948 edition, page 22, pub- 29659669 M NW1?! 1953 10 lished by the ASM, cleveilnnd, 01110.-

Claims (1)

1. A CORROSION-RESISTANT ALLOY CONSISTING ESSENTIALY OF FROM ABOUT 0.005 TO ABOUT 5 PERCENT BY WEIGHT IN THE AGGREGATE OF AT LEAST ONE METAL SELECTED FROM THE GROUP CONSISTING OF RUTHENIUM, RHODIUM, PALLADIUM, OSMIUM, IRIDIUM, PLATINUM, AND RHENIUM, AND THE BALANCE TITANIUM AND INCIDENTAL IMPURITIES.
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US821134A US3063835A (en) 1959-06-18 1959-06-18 Corrosion-resistant alloys
GB21160/60A GB903679A (en) 1959-06-18 1960-06-16 Improvements in and relating to chromium base alloys
LU38827D LU38827A1 (en) 1959-06-18 1960-06-16

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US3111406A (en) * 1961-09-13 1963-11-19 Gen Dynamics Corp High temperature resistant titanium base alloys
US3131059A (en) * 1961-09-13 1964-04-28 Gen Dynamics Corp Chromium-titanium base alloys resistant to high temperatures
US3479161A (en) * 1966-02-01 1969-11-18 Gen Electric Co Ltd Oxidation resistant tungsten and molybdenum alloy bodies
US3713901A (en) * 1970-04-20 1973-01-30 Trw Inc Oxidation resistant refractory alloys
FR2213986A1 (en) * 1973-01-16 1974-08-09 Glazunov Sergei Titanium alloy for gas and steam turbine blades - contg. rhenium, aluminium, zirconium, tin, molybdenum, tungsten, silicon and chromium
US3880655A (en) * 1972-11-17 1975-04-29 Sergei Georgievich Glazunov Titanium base alloy
US4011075A (en) * 1971-07-16 1977-03-08 The Furukawa Electric Co., Ltd. Materials for tamping battery mix
FR2333050A1 (en) * 1975-11-27 1977-06-24 Johnson Matthey Co Ltd PERFECTED TITANIUM ALLOY
DE3541223A1 (en) * 1984-11-22 1986-05-28 Nippon Mining Co., Ltd., Tokio/Tokyo CORROSION-RESISTANT TITANIUM BASED ALLOY
JPS63114931A (en) * 1986-10-31 1988-05-19 Sumitomo Metal Ind Ltd Improving method for corrosion resistance of titanium alloy for oil-well environment
US5238647A (en) * 1990-12-26 1993-08-24 Nippon Mining And Metals Company Limited Titanium alloys with excellent corrosion resistance
US5316722A (en) * 1992-07-09 1994-05-31 Kabushiki Kaisha Kobe Seiko Sho Corrosion resistant Ti-Cr-Ni alloy containing a platinum group metal
US6334913B1 (en) 1998-12-28 2002-01-01 Kobe Steel, Ltd. Corrosion-resistant titanium alloy
WO2002042506A2 (en) * 2000-11-06 2002-05-30 Rmi Titanium Company Process for melting and casting ruthenium-containing or iridium-containing titanium alloys
US6607846B1 (en) 2002-09-25 2003-08-19 Titanium Metals Corporation Titanium article having improved corrosion resistance
US20040058190A1 (en) * 2002-09-25 2004-03-25 Grauman James S. Fabricated titanium article having improved corrosion resistance
US20050021129A1 (en) * 2000-12-28 2005-01-27 Pelton Brian Lee Thermoelastic and superelastic Ni-Ti-W alloy
US20070212251A1 (en) * 2004-04-09 2007-09-13 Hiroaki Otsuka High Strength AlphaType Titanuim Alloy
EP1909348A1 (en) * 2005-07-28 2008-04-09 Kabushiki Kaisha Kobe Seiko Sho Titanium electrode material
RU2451771C2 (en) * 2010-08-27 2012-05-27 Федеральное Государственное Унитарное Предприятие "Центральный Научно-Исследовательский Институт Конструкционных Материалов "Прометей" Фгуп "Цнии Км "Прометей" Method for corrosion-resistant covering application to titanium alloy hardware
RU2619535C1 (en) * 2016-07-12 2017-05-16 Юлия Алексеевна Щепочкина Titanium-based alloy

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US3111406A (en) * 1961-09-13 1963-11-19 Gen Dynamics Corp High temperature resistant titanium base alloys
US3131059A (en) * 1961-09-13 1964-04-28 Gen Dynamics Corp Chromium-titanium base alloys resistant to high temperatures
US3479161A (en) * 1966-02-01 1969-11-18 Gen Electric Co Ltd Oxidation resistant tungsten and molybdenum alloy bodies
US3713901A (en) * 1970-04-20 1973-01-30 Trw Inc Oxidation resistant refractory alloys
US4011075A (en) * 1971-07-16 1977-03-08 The Furukawa Electric Co., Ltd. Materials for tamping battery mix
US3880655A (en) * 1972-11-17 1975-04-29 Sergei Georgievich Glazunov Titanium base alloy
FR2213986A1 (en) * 1973-01-16 1974-08-09 Glazunov Sergei Titanium alloy for gas and steam turbine blades - contg. rhenium, aluminium, zirconium, tin, molybdenum, tungsten, silicon and chromium
US4139373A (en) * 1975-11-27 1979-02-13 Johnson, Matthey & Co., Limited Alloys of titanium
FR2333050A1 (en) * 1975-11-27 1977-06-24 Johnson Matthey Co Ltd PERFECTED TITANIUM ALLOY
DE3541223A1 (en) * 1984-11-22 1986-05-28 Nippon Mining Co., Ltd., Tokio/Tokyo CORROSION-RESISTANT TITANIUM BASED ALLOY
US4666666A (en) * 1984-11-22 1987-05-19 Nippon Mining Co., Ltd. Corrosion-resistant titanium-base alloy
JPS63114931A (en) * 1986-10-31 1988-05-19 Sumitomo Metal Ind Ltd Improving method for corrosion resistance of titanium alloy for oil-well environment
GB2198144A (en) * 1986-10-31 1988-06-08 Sumitomo Metal Ind Method of improving the resistance of ti-based alloys to corrosion
US4859415A (en) * 1986-10-31 1989-08-22 Sumitomo Metal Industries, Ltd. Method of improving the resistance of Ti-based alloys to corrosion in deep-well environments
GB2198144B (en) * 1986-10-31 1991-06-26 Sumitomo Metal Ind Method of improving the resistance of ti-based alloys to corrosion
US5238647A (en) * 1990-12-26 1993-08-24 Nippon Mining And Metals Company Limited Titanium alloys with excellent corrosion resistance
US5316722A (en) * 1992-07-09 1994-05-31 Kabushiki Kaisha Kobe Seiko Sho Corrosion resistant Ti-Cr-Ni alloy containing a platinum group metal
US6334913B1 (en) 1998-12-28 2002-01-01 Kobe Steel, Ltd. Corrosion-resistant titanium alloy
DE19962585C2 (en) * 1998-12-28 2003-06-26 Kobe Steel Ltd Corrosion-resistant titanium alloy and components made from it
WO2002042506A3 (en) * 2000-11-06 2003-03-13 Rmi Titanium Co Process for melting and casting ruthenium-containing or iridium-containing titanium alloys
US6409792B1 (en) 2000-11-06 2002-06-25 Rmi Titanium Company Process for melting and casting ruthenium-containing or iridium-containing titanium alloys
WO2002042506A2 (en) * 2000-11-06 2002-05-30 Rmi Titanium Company Process for melting and casting ruthenium-containing or iridium-containing titanium alloys
US8974517B2 (en) 2000-12-28 2015-03-10 Abbott Cardiovascular Systems Inc. Thermoelastic and superelastic NI-TI-W alloy
US8702790B2 (en) 2000-12-28 2014-04-22 Abbott Cardiovascular Systems Inc. Thermoelastic and superelastic Ni—Ti—W alloy
US8382819B2 (en) 2000-12-28 2013-02-26 Abbot Cardiovascular Systems Inc. Thermoelastic and superelastic Ni-Ti-W alloy
US7658760B2 (en) 2000-12-28 2010-02-09 Abbott Cardiovascular Systems Inc. Thermoelastic and superelastic Ni-Ti-W alloy
US20050021129A1 (en) * 2000-12-28 2005-01-27 Pelton Brian Lee Thermoelastic and superelastic Ni-Ti-W alloy
KR100721107B1 (en) 2002-09-25 2007-05-22 티타늄 메탈스 코포레이션 Titanium article having corrosion resistance
EP1403399A2 (en) * 2002-09-25 2004-03-31 Titanium Metals Corporation Titanium article having improved corrosion resistance
EP1734153A3 (en) * 2002-09-25 2007-04-11 Titanium Metals Corporation Titanium article having improved corrosion resistance
US6849344B2 (en) * 2002-09-25 2005-02-01 Titanium Metals Corp. Fabricated titanium article having improved corrosion resistance
EP1734153A2 (en) * 2002-09-25 2006-12-20 Titanium Metals Corporation Titanium article having improved corrosion resistance
US6607846B1 (en) 2002-09-25 2003-08-19 Titanium Metals Corporation Titanium article having improved corrosion resistance
US20040058190A1 (en) * 2002-09-25 2004-03-25 Grauman James S. Fabricated titanium article having improved corrosion resistance
EP1403399A3 (en) * 2002-09-25 2004-04-07 Titanium Metals Corporation Titanium article having improved corrosion resistance
US20070212251A1 (en) * 2004-04-09 2007-09-13 Hiroaki Otsuka High Strength AlphaType Titanuim Alloy
US8562763B2 (en) * 2004-04-09 2013-10-22 Nippon Steel & Sumitomo Metal Corporation High strength α+β type titanuim alloy
US8137866B2 (en) 2005-07-28 2012-03-20 Kobe Steel, Ltd. Titanium material for fuel cell separator having low contact resistance
US20100119882A1 (en) * 2005-07-28 2010-05-13 Kabushiki Kaisha Kobe Seiko Sho (Kobe Steel, Ltd.) Titanium electrode material
EP1909348A4 (en) * 2005-07-28 2008-09-24 Kobe Steel Ltd Titanium electrode material
EP1909348A1 (en) * 2005-07-28 2008-04-09 Kabushiki Kaisha Kobe Seiko Sho Titanium electrode material
RU2451771C2 (en) * 2010-08-27 2012-05-27 Федеральное Государственное Унитарное Предприятие "Центральный Научно-Исследовательский Институт Конструкционных Материалов "Прометей" Фгуп "Цнии Км "Прометей" Method for corrosion-resistant covering application to titanium alloy hardware
RU2619535C1 (en) * 2016-07-12 2017-05-16 Юлия Алексеевна Щепочкина Titanium-based alloy

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