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Publication numberUS3128178 A
Publication typeGrant
Publication dateApr 7, 1964
Filing dateFeb 28, 1961
Priority dateFeb 28, 1961
Publication numberUS 3128178 A, US 3128178A, US-A-3128178, US3128178 A, US3128178A
InventorsDuffek Jr Edward F
Original AssigneeCalifornia Research Corp
Export CitationBiBTeX, EndNote, RefMan
External Links: USPTO, USPTO Assignment, Espacenet
Tantalum-titanium base alloy
US 3128178 A
Abstract  available in
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Claims  available in
Description  (OCR text may contain errors)

United States Patent 3,128,178 TANTALUM-TTTANIUM BASE ALLQY Edward F. Dutieir, in, Mountain View, Qalit, assignor to California Research florporation, an Francisco, Calif.,

a corporation of Delaware No Drawing. Filed Feb. 28, 1961, Ser. No. 92,151 2 Claims. (=Cl. 75--174) This invention relates to tantalum-titanium base metal alloys, particularly to such alloys which contain alloying metals of vanadium and nickel as essential components, which make the resulting alloys ductile and resistant to corrosion by hot oxidizing and hot non-oxidizing acids.

Alloys with the above properties are most useful for lining chemical reaction vessels, auxiliary equipment and connecting lines, which are exposed to hot phosphoric acid and hot sulfuric acid. Liquid phosphoric acid is recognized as an efficient catalyst for certain organic chemical reactions, including alkylation and isomerization and the polymerization of normally gaseous olefins. Corrosive attack appears to be the greatest with aqueous solutions of about 85% phosphoric acid. While considerable progress has been made in controlling corrosion in the presence of liquid phosphoric acid (see, for example, Kemp and Zeh Patent 2,65 3,177 and Piehl Patent 2,854,- 497), there is need for further improvement and particularly for alloys which are also resistant to corrosion in the presence of hot oxidizing acids such as sulfuric acid. Sulfonations, cleavage and hydrolysis reactions often employ hot sulfuric acid. The most corrosive concentration for hot aqueous solutions of sulfuric acid appears to be about 55 sulfuric acid.

Prior art alloys are poor in corrosion resistance in the presence of either or both hot phosphoric acid and hot sulfuric acid. Usually resistance to sulfuric acid corrosion is readily attained, but the characteristic of resistance to corrosion by hot phospohric acid is difiicult to add. Even more diflicult is to retain these corrosion resistant characteristics in an alloy that is ductile and can be worked sufficiently so that it can be used without sole reliance upon casting as the method of shaping.

The metal alloy of this invention has the above desirable characteristics. It is a tantalum base alloy comprised by Weight of about 10 to 30% titanium, 3 to 10% vanadium and 0.25 to 3% nickel. Preferably, for good workability and ductility, the alloy contains 20 to 25% titanium and 5 to 7.5% vanadium. Without vanadium, a tantalum-titanium-nickel alloy was extremely difficult to work, either in cold rolling or hot rolling with protective cladding. *For use with the most corrosive hot phosphoric acid concentrations, i.e., about 85%, the alloy should contain at least 0.5%, and preferably about 1%, of nickel. Optionally, columbium and tungsten can be added. Up to 15%, and sometimes up to 25%, of columbium can be used where lighter weight is an important factor. Tungsten in amounts to serves to increase further the resistance to hydrogen embrittlement as well as to stabilize and to add strength to the alloy. However, the alloy shoud contain no less than 30%, and preferably at least 50% of tantalum.

We have found that, as compared to high temperature air oxidation, corrosion in aqueous conditions such as with the above aqueous acids is much more sensitive to impurities in the metal components of the alloy. Hence, impurities in the alloy should be kept to a minimum for the best results. Most desirably, the carbon content of the alloy should be no more than 0.03%; the oxygen content, no more than about 0.05%; the nitrogen con-tent, no more than 0.008%; the hydrogen content, no more than about 0.001%. 'In addition, no more than about 0.3% of the combined elements aluminum, chromium,

3,128,178 Patented Apr. 7, 1964 controlled atmospheres of argon, helium and the like are employed. Arc furnaces with water-cooled copper hearths and non-consumable electrodes (e.g. 2% thoriatedtungsten tip) were used in the preparations described below. Measured amounts of the metal components were The alloy compositions, all in terms of weight percent, were melted, the button of alloy inverted, and remelted four times before final cooling and solidifying. Alternatively, other furnaces and known melting techniques such as with continuous feed of metal components, inductive heating, or other means could be used with adequate protection against contamination.

In the folloding illustrative examples, most of the all'oys'were clad in 310 stainless steel to avoid oxidation at the high temperatures used in fabrication. Cladding was done by lathe machining the alloy button into circular discs, enclosing them inside a 3 x 3 x A-inch steel sheet having a circular hole in the middle, and welding 2% x 2% x As-inch steel plates on each side. The resulting metal sandwiches of alloys were rolled at 2000 The rolling was done in a Stana-t two-high mill and the metal was reduced 7.5% to 15% per pass to a total of about The alloys were tested for corrosion by exposing them to solutions of 55% sulfuric acid and phosphoric acid sealed in heavy-wall Pyrex ampules. Alloy specimens were prepared by grinding, sanding and finishing of surfaces and edges, and degreasing. Surface areas (generally about 6.5 cm. weights and densities were then determined. The density was measured by weight-in weight-out of water method. The volumes of sulfuric acid and phosphoric acid solutions were 40 and 30 ml., respectively. C-ontaminations due to silica formation in the phosphoric acid tests were avoided by liners of Teflon tubing inside the glass ampules. The corrosion tests were for 72 hours. From the measurements of weight loss, density and surface area, the penetration or corrosion rates in mils per year (i.e., m.p.y.) were determined.

The following table shows the results of tests carried out as described above:

Composition, percent Corrosion rates,

by weight In.p.y.

Number 557 857 Ta Ti v Ni rnsoi at Hard, at

25 5 0 2.5 67. 25 7. 5 0 2.5 61. 25 5 1 Wt. Wt.

galn. gain. 25 7. 5 1 d0 D03 25 5 2 do Do.

1 Weight gain of about .001 gms/cmfl. 2 Weight gain of about .003 gms./cm.

The above tests illustrate the need for nickel in the composition. In alloys Nos. 1 and 2 without nickel, the high penetration or corrosion rates in phosphoric acid show considerable hydrogen embrittlement. On the other hand, alloy compositions 3, 4 and 5 were ductile and were readily hot rolled to give slight weight gains in the corrosion tests. The weight gain shows the formation of an insoluble protective film on the metal surface. The weight gain becomes constant. For example, alloy No. 5, upon exposure to 85% phosphoric acid at 400 F. gained no further weight after continuing the run for 164 hours. Testing alloy No. 5 under the same conditions for a total of 336 hours showed that the constant weight was attained in 48 hours. Similarly, alloy No. 4 when tests in 55% sulfuric acid at 450 F. for a total of 168 hours reached a constant weight in about 48 hours. Unalloyed tantalum or the tantalum alloys Nos. 1 and 2 above show under such conditions a steadily increasing weight loss. The alloys of the present invention are therefore superior since corrosion and hence hydrogen embrittlement are minimized.

For comparison, an alloy without titanium and composed of 74% tantalum, 25 vanadium and 1% nickel recrystallized and cracked on attempted rolling at 2000 F. after cladding. Further, solutionizing of this alloy for 68 hours at 1900 F. did not improve the workability.

Other ductile tantalum-titanium base alloys which illustrate the corrosion resistance (to hot sulfuric and phosphoric acids) alloy compositions of the present in vention are tabulated as follows:

[Cmpositlon, percent by weight] These various ductile, corrosion resistant alloys of the present invention are preferably used as lining materials for vessels and other equipment. They can be applied after rolling or other suitablejabricating manner by conventional methods of welding, brazing, vacuum joining, and the like.

I claim:

1, A ductile metal composition resistant to the action of hot oxidizing and non-oxidizing acids and consisting essentially of, in percent by weight, 1030% of titanium, 3-10% of vanadium, .25 to 3% of nickel, up to 25 columbium, up to 10 tungsten, and the balance essentially tantalum, with the tantalum being present in an amount of at least 2. A ductile metal composition resistant to the action of hot oxidizing and non-oxidizing acids and consisting essentially of, in percent by weight, 20-25% of titanium, 5-7.5% of vanadium, 0.5 to 3% of nickel, up to 25% columbi-um, up to "10% tungsten, and the balance essentially tantalum, with the tantalum being present in an amount of at least References Cited in the file of this patent UNITED STATES PATENTS 1,588,518 Brace June 15, 1926 2,964,399 Lyons Dec. 13, 1960 FOREIGN PATENTS 803,855 Great Britain Apr. 3, 1957 201,297 Austria Dec. 27, 1958

Patent Citations
Cited PatentFiling datePublication dateApplicantTitle
US1588518 *Apr 18, 1919Jun 15, 1926Westinghouse Electric & Mfg CoAlloy of tantalum
US2964399 *Jun 25, 1959Dec 13, 1960Titanium Metals CorpTantalum-titanium corrosion resistant alloy
AT201297B * Title not available
GB803855A * Title not available
Referenced by
Citing PatentFiling datePublication dateApplicantTitle
US3249429 *Dec 27, 1963May 3, 1966Clo E ArmantroutTantalum brazing alloy
US3293741 *Apr 20, 1964Dec 27, 1966Gilliland Ralph GBrazing alloys for refractory metals
US3449118 *Nov 15, 1966Jun 10, 1969Us NavyVanadium-columbium-tantalum alloys
US4496373 *Jun 6, 1984Jan 29, 1985Kernforschungsanlage Julich Gesellschaft Mit Beschrankter HaftungMembrane and its palladium-alloy protective coating contain a smillar metal in equilibrated concentratrion;durability
US7727273Jan 13, 2005Jun 1, 2010Boston Scientific Scimed, Inc.Medical devices and methods of making the same
US7938854May 20, 2010May 10, 2011Boston Scientific Scimed, Inc.Medical devices and methods of making the same
US8349249Feb 19, 2008Jan 8, 2013Heraeus Precious Metals Gmbh & Co. KgMetal alloy for medical devices and implants
US8403980Mar 4, 2010Mar 26, 2013Heraeus Materials Technology Gmbh & Co. KgMetal alloy for medical devices and implants
Classifications
U.S. Classification420/580, 420/427
International ClassificationC22C27/02, C22C27/00
Cooperative ClassificationC22C27/02
European ClassificationC22C27/02