Corrosion-resistant titanium-base alloy

Information

  • Patent Grant
  • 4666666
  • Patent Number
    4,666,666
  • Date Filed
    Tuesday, November 12, 1985
    38 years ago
  • Date Issued
    Tuesday, May 19, 1987
    37 years ago
Abstract
An excellently corrosion-resistant titanium-base alloy comprises, all by weight, either from 0.005% to less than 0.2% ruthenium or from 0.005% to 2.0% palladium or both, at least one of from 0.01% to 2.0% nickel, from 0.005% to 0.5% tungsten, and from 0.01% to 1.0% molybdenum, and the remainder titanium and unavoidable impurities.
Description

BACKGROUND OF THE INVENTION
This invention rleates to an excellently corrosion-resistant titanium-base alloy.
Titanium has come into extensive use as an industrial material, replacing conventional corrosion-resistant materials by dint of its greater corrosion resistance. It is particularly resistant to corrosive attacks of oxidizing environments such as of nitric acid, chromic acid, chloric acid, chlorine dioxide, and chlorate. Also, it is inert to sea water and other chloride-containing corrosive environments. In a non-oxidizing acid such as hydrochloric or sulfuric acid, however, titanium fails to prove as anticorrosive as in above said environments. Efforts to overcome this disadvantage have led to the introduction of its alloys, typically Ti-Pd, Ti-Ni, and Ti-Ni-Mo alloys, in some sectors of industry. The Ti-Pd alloy is high-priced because it uses expensive palladium, whereas the Ti-Ni and Ti-Ni-Mo alloys have a common drawback of poor workability. These drawbacks have hampered widespread use of the titanium alloys.
Thus, much remains to be settled before successful employment of titanium in severely corrosive environments despite the excellent corrosion resistance inherent to the metal element. Titanium alloys developed to attain partial improvements in this respect have not proved satisfactory either, with many shortcomings yet to be corrected.
SUMMARY OF THE INVENTION
The present invention has now been perfected with the foregoing in view. It is directed to a titanium-base alloy which exhibits a profound anticorrosive effect in rigorously corrosive environments not only of oxidizing acids such as nitric acid but also, and in particular, of non-oxidizing acids. The alloy is, moreover, resistant outstandingly to the crevice corrosion that frequently occurs in solutions wherein chlorine ions are present.
The alloy is a titanium-base alloy of a composition containing one or two of
from 0.005% to less than 0.2% by weight ruthenium and
from 0.005% to 2.0% by weight palladium
and one or more of
from 0.01% to 2.0% by weight nickel,
from 0.01% to 1.0% by weight molybdenum, and
from 0.005% to 0.5% by weight tungsten.





DETAILED DESCRIPTION
In the composition according to the present invention, the ruthenium content has the lower limit fixed at 0.005 wt% because a smaller ruthenium proportion brings a too slight improvement in corrosion resistance for practical purposes. More then 0.005 wt%, preferably more than 0.01 wt%, is required. The upper limit of less than 0.2 wt% is set because a larger addition is uneconomical in that the anticorrosive effect is saturated and the ruthenium cost increases non-negligibly.
The minimum amount of palladium is specified to be 0.005 wt% because a less amount of the element is of little practical significance in improving the corrosion resistance. An amount of at least 0.005 wt%, preferably at least 0.01 wt%, is needed. The maximum palladium amount is specified to be 2.0 wt%. Saturation of the anticorrosive effect and the high palladium cost make a larger addition economically unjustified.
Nickel should be used in an amount of at least 0.01 wt%. When added in a smaller amount, it will not improve the corrosion resistance to a practically beneficial degree. Preferably, at least 0.1 wt% nickel is added. On the other hand, the nickel amount should not exceed 2.0 wt%. A greater nickel proportion adds little to the anticorrosive effect but renders the resulting alloy difficult to work and fabricate. A nickel amount of 1.0 wt% or less is preferred.
The lower limit of the molybdenum content is 0.01 wt%. The addition below this limit is impractical, with a negligible improvement in corrosion resistance. The upper limit of 1.0 wt% is placed because more molybdenum no longer produces an appreciable improvement but rather reduces the workability of the alloy, making it difficult to fabricate.
For tungsten the lower limit of 0.005 wt% is fixed since the addition below this limit is little contributory to the corrosion resistance and is impractical. A preferred amount is 0.01 wt% or more. The upper limit of 0.5 wt% is set on the grounds that a larger percentage of tungsten creates little more favorable effect but decreases the workability and presents difficulty of fabrication.
Next, the effectiveness of the titanium alloy according to the present invention will be explained below in comparison with conventional corrosion-resistant titanium alloys.
The corrosive environments used for tests were, for general corrosion tests,
1. 1% H.sub.2 SO.sub.4, boiling, and
2. 5% HCl, boiling, and for crevice corrosion tests,
3. 10% NaCl, pH=6.1, boiling.
Table 1 summarizes the results of the tests carried out using 1% H.sub.2 SO.sub.4.
Among the materials tested, pure titanium and conventional corrosion-resistant titanium alloys are designated by Nos. 1 to 7. Ternary alloys prepared in accordance with the invention are represented by Nos. 8 through 51 and quaternary and further multicomponent alloys of the invention by Nos. 52 through 62.
Test material Nos. 8 to 13 are (Ti-Ru-Ni) alloys embodying the invention in which the Ni proportion was varied. A Ni content as small as 0.01 wt% (No. 8) proved effective, and the corrosion rate was sharply lowered with 0.1 wt% or more. The favorable effect of Ni addition is readily distinguishable by comparison with No. 3.
TABLE 1______________________________________Results of general corrosion tests(1% H.sub.2 SO.sub.4, boiling) Corrosion rateNo. Composition (wt %) (mm/y)______________________________________ 1 Pure titanium 10.4 2 Ti--0.15Pd 0.278 3 Ti--0.04Ru 0.280 4 Ti--0.6Ni 6.55 5 Ti--0.8Ni--0.3Mo 1.69 6 Ti--0.02W 9.74 7 Ti--0.1Mo 9.42 8 Ti--0.03Ru--0.01Ni 0.271 9 Ti--0.03Ru--0.06Ni 0.15610 Ti--0.03Ru--0.12Ni 0.07811 Ti--0.03Ru--0.6Ni 0.06012 Ti--0.03Ru--1.0Ni 0.05913 Ti--0.03Ru--2.0Ni 0.05414 Ti--0.01Ru--0.6Ni 0.08515 Ti--0.04Ru--0.6Ni 0.07616 Ti--0.07Ru--0.6Ni 0.07517 Ti--0.11Ru--0.6Ni 0.06918 Ti--0.20Ru--0.6Ni 0.05819 Ti--0.04Ru--0.01W 0.24120 Ti--0.04Ru--0.05W 0.14421 Ti--0.04Ru--0.1W 0.10822 Ti--0.04Ru--0.5W 0.08923 Ti--0.01Ru--0.02W 0.27124 Ti--0.1Ru--0.02W 0.07325 Ti--0.2Ru--0.02W 0.06626 Ti--0.04Ru--0.01Mo 0.23127 Ti--0.04Ru--0.3Mo 0.17728 Ti--0.04Ru--1.0Mo 0.19229 Ti--0.01Ru--0.1Mo 0.27530 Ti--0.1Ru--0.1Mo 0.17731 Ti--0.2Ru--0.1Mo 0.10032 Ti--0.05Pd--0.01Ni 0.26633 Ti--0.05Pd-- 0.1Ni 0.09334 Ti--0.05Pd--1.0Ni 0.07135 Ti--0.05Pd--2.0Ni 0.06936 Ti--0.01Pd--0.6Ni 0.27537 Ti--0.1Pd--0.6Ni 0.06238 Ti--1.1Pd--0.6Ni 0.03339 Ti--2.0Pd--0.6Ni 0.02940 Ti--0.07Pd--0.005W 0.25341 Ti--0.07Pd--0.09W 0.19442 Ti--0.07Pd--0.5W 0.18843 Ti--0.01Pd--0.05W 0.27144 Ti--0.15Pd--0.05W 0.14345 Ti--2.0Pd--0.05W 0.03346 Ti--0.05Pd--0.01Mo 0.19947 Ti--0.05Pd--0.3Mo 0.18848 Ti--0.05Pd--1.0Mo 0.17649 Ti--0.01Pd--0.1Mo 0.27250 Ti--0.15Pd--0.1Mo 0.23151 Ti--2.0Pd--0.1Mo 0.08452 Ti--0.05Ru--0.5Ni--0.02W 0.04953 Ti--0.05Ru--0.5Ni--0.1Mo 0.04554 Ti--0.04Ru--0.02W--0.1Mo 0.11355 Ti--0.05Pd--0.5Ni--0.02W 0.07756 Ti--0.05Pd--0.5Ni--0.1Mo 0.07357 Ti--0.04Pd--0.02W--0.1Mo 0.09458 Ti--0.05Pd--0.05Ru--0.5Ni 0.04359 Ti--0.05Pd--0.05Ru--0.5Mo 0.10160 Ti--0.05Pd--0.05Ru--0.5W 0.10861 Ti--0.05Ru--0.02W--0.1Mo--0.5Ni 0.07362 Ti--0.05Pd--0.02W--0.1Mo--0.5Ni 0.084______________________________________
It should be clear from these why the lower limit was fixed at 0.01 wt%. The upper limit of 2.0 wt% is placed because a larger addition of Ni does not produce a correspondingly favorable effect but affects the workability of the alloy seriously.
Nos. 14 to 18 are (Ti-Ru-Ni) alloys embodying the invention with varied Ru proportions. A Ru content of only 0.01 wt% (No. 14) exhibited its beneficial effect. The effectiveness of Ru addition is obvious in contrast with No. 4. Thus, it will be appreciated that the lower limit is 0.005 wt%. The upper limit of 0.2 wt% for Ru addition is required since a higher percentage addition is little contributive to rise the anticorrosive effect for the added amount of unduly raises the Ru cost.
Nos. 19 to 22 represent (Ti-Ru-W) alloys according to the invention with varied W contents. The corrosion rate was noticeably retarded by the addition of 0.005 wt% (No. 19), demonstrating the advantage derived from the W addition over No. 3. Hence, the lower limit of 0.005 wt% for W addition. The upper limit of 0.5 wt% is chosen because more W seriously affects the workability of the alloy.
In Nos. 23 to 25, (Ti-Ru-W) alloys of the invention, the Ru content was varied. With 0.01 wt% Ru (No. 23) the favorable effect is evident, as contrasted with No. 6. Thus, the lower limit is 0.005 wt%. The upper limit of 0.2 wt% is necessary because more Ru does not give a marked effect but raise the Ru cost to excess.
Nos. 26 to 28 are (Ti-Ru-Mo) alloys embodying the invention with varied Mo contents. The corrosion rate began to slow down with 0.01 wt% Mo (No. 26), indicating the merit of Mo addition in contrast with No. 3. For this reason the lower limit of 0.01 wt% is put to Mo addition. The upper limit of 1.0 wt% is placed to avoid a larger Mo percentage which will reduce the workability of the resulting alloy.
In (Ti-Ru-Mo) alloys of the invention, only the Ru content was varied in Nos. 29 to 31. Ru addition evidently took its effect with only 0.01 wt% (No. 29), and its favorable effect makes a sharp contrast to No. 7. In view of this, the lower limit of Ru addition is set at 0.005 wt%. The upper limit is 0.2 wt% because a larger Ru content does not add an accordingly desirable effect but merely boosts the Ru cost.
Nos. 32 through 51 represent Ti-Pd alloys with the addition of Ni, Mo, or W in accordance with the invention. The data suggest practically the same tendency as observed with the Ru-containing alloys already described. In brief, the addition of Ni, Mo, or W remarkably improves the corrosion resistance of the Ti-Pd alloys.
Nos. 52 through 62 represent the alloys of four or more components embodying the invention. It must be understood that all are superior to conventional corrosion-resistant titanium alloys.
Table 2 shows the results of tests conducted using 5% HCl, boiling.
TABLE 2______________________________________Results of general corrosion tests(5% HCl, boiling) Corrosion rateNo. Composition (wt %) (mm/y)______________________________________ 1 Pure titanium 29.7 2 Ti--0.11Pd 6.20 3 Ti--0.02Ru 9.51 4 Ti--0.6Ni 83.3 5 Ti--0.8Ni--0.3Mo 71.7 6 Ti--0.02W 33.1 7 Ti--0.1Mo 44.6 8 Ti--0.03Ru--0.01Ni 5.39 9 Ti--0.03Ru--0.06Ni 2.2010 Ti--0.03Ru--0.12Ni 0.68511 Ti--0.03Ru--0.6Ni 0.57912 Ti--0.03Ru--1.0Ni 0.50413 Ti--0.03Ru--2.0Ni 0.49814 Ti--0.01Ru--0.6Ni 0.47915 Ti--0.04Ru--0.6Ni 0.39016 Ti--0.07Ru--0.6Ni 0.33117 Ti--0.11Ru--0.6Ni 0.36018 Ti--0.20Ru--0.6Ni 0.29919 Ti--0.04Ru--0.01W 0.35220 Ti--0.04Ru--0.05W 0.29121 Ti--0.04Ru--0.1W 0.20322 Ti--0.04Ru--0.5W 0.19423 Ti--0.01Ru--0.02W 5.8824 Ti--0.1Ru--0.02W 0.93325 Ti--0.2Ru--0.02W 0.42826 Ti--0.04Ru--0.01Mo 1.9827 Ti--0.04Ru--0.3Mo 1.0328 Ti--0.04Ru--1.0Mo 1.4129 Ti--0.01Ru--0.1Mo 6.0730 Ti--0.1Ru--0.1Mo 1.3231 Ti--0.2Ru--0.1Mo 0.7532 Ti--0.05Pd--0.01Ni 5.0133 Ti--0.05Pd--0.13Ni 0.54334 Ti--0.05Pd-- 1.0Ni 0.49535 Ti--0.05Pd--2.0Ni 0.42636 Ti--0.01Pd--0.6Ni 3.4737 Ti--0.1Pd--0.6Ni 0.37838 Ti--1.1Pd--0.6Ni 0.14139 Ti--2.0Pd--0.6Ni 0.09340 Ti--0.07Pd--0.005W 2.8841 Ti--0.07Pd--0.09W 1.3142 Ti--0.07Pd--0.5W 1.0743 Ti--0.01Pd--0.05W 6.3444 Ti--0.15Pd--0.05W 0.88345 Ti--2.0Pd--0.05W 0.69146 Ti--0.05Pd--0.01Mo 7.0347 Ti--0.05Pd--0.3Mo 5.3248 Ti--0.05Pd--1.0Mo 4.3749 Ti--0.01Pd--0.1Mo 6.4350 Ti--0.15Pd--0.1Mo 1.0351 Ti--2.0Pd--0.1Mo 0.74552 Ti--0.05Ru--0.5Ni--0.02W 1.9453 Ti--0.05Ru--0.5Ni--0.1Mo 1.8854 Ti--0.04Ru--0.02W--0.1Mo 1.9155 Ti--0.05Pd--0.5Ni--0.02W 2.0056 Ti--0.05Pd--0.5Ni--0.1Mo 2.0357 Ti--0.04Pd--0.02W--0.1Mo 2.2158 Ti--0.05Pd--0.05Ru--0.5Ni 0.35559 Ti--0.05Pd--0.05Ru--0.5Mo 0.70360 Ti--0.05Pd--0.05Ru--0.5W 0.81761 Ti--0.05Ru--0.02W--0.1Mo--0.5Ni 0.22162 Ti--0.05Pd--0.02W--0.1Mo--0.5Ni 0.296______________________________________
The corrosive environment was more rigorous than with 1% H.sub.2 SO.sub.4 and the corrosion rates were generally higher. However, the alloys embodying the invention all remained superior to the ordinary corrosion-resistant titanium alloys.
Crevice corrosion tests were conducted and the results as in Table 3 were obtained.
As the corrosive conditions, an aqueous solution of 10% sodium chloride was used, with pH=6.1 in a boiling state.
Crevice corrosion occurred in pure titanium and a Ti-0.15Pd alloy before the lapse of one full day. A Ti-0.8Ni-0.3Mo alloy corroded in two days. The alloys embodying the invention, by contrast, were all more resistant to crevice corrosion. It will be seen from the table that the alloys according to the invention are superior in resistance to crevice corrosion as well as to general corrosion.
Aside from the resistance to the afore-described corrosive attacks, the alloys according to the invention have excellent resistance to hydrogen absorption. Table 4 gives the results of tests on this subject.
The data were obtained from tests performed using platinum as the counter electrode and a bath voltage of 6 V and then allowing the test material to absorb hydrogen from hydrogen bubbles formed and directed to the alloy surface. The table clearly indicates that the alloys of the invention absorbed less hydrogen than pure titanium does.
TABLE 3______________________________________Results of crevice corrosion tests(NaCl = 10%, pH = 6.1, boiling)No. Composition (wt %) 1 2 3 4 (day)______________________________________Comparative alloy 1 Pure titanium X X X X 2 Ti--0.15Pd X X X X 3 Ti--0.05Ru .DELTA. X X X 4 Ti--0.8Ni--0.3Mo O .DELTA. X X 5 Ti--0.02W X X X X 6 Ti--0.1Mo X X X X 7 Ti--0.6Ni O X X X 8 Ti--0.05Ru--0.5Ni O O O O 9 Ti--0.05Ru--0.05W O O .DELTA. X10 Ti--0.05Ru--0.1Mo O O X X11 Ti--0.05Pd--0.5Ni O O O O12 Ti--0.05Pd--0.05W O O .DELTA. X13 Ti--0.05Pd--0.1Mo O O .DELTA. X14 Ti--0.05Ru--0.5Ni--0.02W O O O O15 Ti--0.05Ru--0.5Ni--0.1Mo O O O O16 Ti--0.05Ru--0.02W--0.1Mo O O O .DELTA.17 Ti--0.05Pd--0.5Ni--0.02W O O O O18 Ti--0.05Pd-- 0.5Ni--0.1Mo O O O O19 Ti--0.05Pd--0.02W--0.1Mo O O O X20 Ti--0.05Ru--0.02W--0.1Mo--0.5Ni O O O O21 Ti--0.05Pd--0.02W--0.1Mo--0.5Ni O O O O______________________________________ O: No change .DELTA.: Color change X: Crevice corrosion
TABLE 4______________________________________Results of hydrogen absorption tests Item H.sub.2 conc. increasedCondition Test material by H.sub.2 abspn. (wt %)______________________________________6 v .times. 3 hours Pure titanium 0.0040(25.degree. C.) Ti--0.05Ru--0.5Ni 0.0001 Ti--0.05Ru--0.01W 0.0007 Ti--0.05Ru--0.05Mo 0.0013 Ti--0.05Pd--0.5Ni 0.0001 Ti--0.05Pd--0.01W 0.0009 Ti--0.05Pd--0.05Mo 0.00066 v .times. 24 hours Pure titanium 0.0059(15.degree. C.) Ti--0.05Ru--0.5Ni 0.0004 Ti--0.05Ru--0.01W 0.0013 Ti--0.05Ru--0.05Mo 0.0030 Ti--0.05Pd--0.5Ni 0.0005 Ti--0.05Pd--0.01W 0.0017 Ti--0.05Pd--0.05Mo 0.0036______________________________________
As has been described hereinbefore, the alloy according to this invention is strongly resistant to such highly corrosive non-oxidizing acids as sulfuric acid. It also possesses excellent resistance to crevice corrosion and hydrogen absorption. The proportions of the alloying elements added are small enough for the alloy to be worked almost as easily as pure titanium and made at low cost. It will be understood from these that the alloy of the invention is a novel titanium alloy that eliminates the disadvantages of the existing corrosion-resistant titanium alloys and exhibits greater corrosion resistance.
Claims
  • 1. An excellently corrosion-resistant titanium-base alloy consisting essentially of, all by weight, either from 0.005% to less than 0.2% ruthenium or from 0.005% to 2.0% palladium or both, at least one of from 0.01% to 2.0% nickel, from 0.005% to 0.5% tungsten, and from 0.01% to 1.0% molybdenum, and the remainder titanium and unavoidable impurities.
Priority Claims (4)
Number Date Country Kind
59-246317 Nov 1984 JPX
59-246318 Nov 1984 JPX
60-31504 Feb 1985 JPX
60-31505 Feb 1985 JPX
US Referenced Citations (1)
Number Name Date Kind
3063835 Stern Nov 1962
Foreign Referenced Citations (6)
Number Date Country
653938 Apr 1965 BEX
657872 Feb 1963 CAX
1289992 Feb 1969 DEX
37513 Apr 1978 JPX
161746 Sep 1983 JPX
406929 Nov 1973 SUX