US3615375A

US3615375A - High-temperature oxidation and corrosion-resistant cobalt-base alloys

Info

Publication number: US3615375A
Application number: US1884A
Authority: US
Inventors: Adrian M Beltran; Chester T Sims; Donald E Mcgarrigan
Original assignee: General Electric Co
Current assignee: General Electric Co
Priority date: 1970-01-09
Filing date: 1970-01-09
Publication date: 1971-10-26
Anticipated expiration: 1988-10-26
Also published as: DE2100477B2; CH551490A; GB1309308A; DE2100477A1; FR2075359A5; DE2100477C3

Abstract

Cobalt-base alloys having improved high-temperature strength and ductility characteristics and corrosion resistance consist essentially of, in percent by weight, carbon 0.1 to 0.7, chromium 24 to 35, tungsten 6 to 9, nickel 8.5 to 11.5, boron in an effective amount of about 0.005 up to 0.05, iron up to 2, zirconium 0.1 to 1,7, yttrium 0.03 to 1, with the remainder essentially cobalt except for impurities.

Description

United States Patent Adrian M. Beltran;

Chester T. Sims, Ballston Lake, N.Y.; Donald E. McGarrigan, Blackwood, NJ. 1,884

Jan. 9, 1970 Oct. 26, 1971 General Electric Company Inventors Appl. No. Filed Patented Assignee HIGH-TEMPERATURE OXIDATION AND CORROSION-RESISTANT COBALT-BASE ALLOYS 4 Claims, N0 Drawings U.S. Cl 75/171,

Int. Cl C22c 19/00 Field of Search 75/ 171 [56] References Cited UNITED STATES PATENTS 3,346,378 10/1967 Foster et al. 75/171 Primary Examiner-Richard 0. Dean Attorneys-Harold J. Holt, William C. Crutcher, Bryan C.

Ogden, Frank L. Neuhauser, Oscar B. Waddell and Joseph B. Form an This invention relates to new and useful cobalt which are characterized by strength and increased resistance peratures.

Gas turbines and other equipment which are driven by the forces of combustion gases operate more efficiently as the operating temperature rises. However, at such higher temperatures the strength characteristics of many alloys often decrease rapidly and the alloys become susceptible to corrosion, consisting of both oxidation and hot corrosion, caused by contact with oxidizing and other corrosive constituents of the hot combustion gas streams such as sodium and sulfur. While many alloys aimed at curing such deficiencies have been formulated, there is a constant search for new and better alloys such that only relatively slight improvements often become critical and of unexpected advantage in the higher temperature operating ranges. For example, in gas turbines operating at temperatures of the order of about 1,600 F. with peak temperatures of about 2,000 F an improvement of only 100 F. in the resistance of the materials of construction to the environment represents a notable advance. in a typical gas turbine, an increase in operating temperature from about l,500 F. to l,600 F., represents an increase in power output of about 14 percent and an increase in efficiency of about 1 to 5 percent.

The use of cobalt-base alloys containing relatively large amounts of chromium for high-temperature operation under corrosive conditions is well known. However, it has been the teaching of the prior art that increases in the chromium content of such alloys over about 25 percent by weight actually result in an increase in scaling or surface deterioration. This teaching is set forth, for example, in Journal of the Electrochemical Society, Vol. 103, in a paper by Pfalnikar et al. entitled "High Temperature Scaling of Cobalt-Chromium Alloys." Typical prior art alloys which proceed in the face of this teaching by providing relatively large amounts of chromium, which in critical balance with other alloying constituents provide good high-temperature strength and increased resistance to corrosion, are those set forth in 0.5. Pat. No. 3,383,205, assigned to the same assignee as the present invention.

As pointed out above, there is a constant search toward the improvement of such high-temperature alloys so that they may operate at higher temperatures for longer periods of time under highly corrosive conditions, and it is a primary purpose of the present invention to provide such new and useful improved alloys. Another object is to provide such improved alloys which are useful in other equipment and devices subjected to elevated temperatures and oxidative and corrosive atmospheres, such as furnaces and the like.

Those features of the invention which are believed to be novel are set forth with particularity in the claims appended hereto. The invention will, however, be better understood and further objects thereof appreciated from a consideration of the following description.

Briefly, there are provided by the present invention hightemperature oxidation and corrosion-resistant alloys having a percent by weight content of carbon 0.] to 0.7, chromium 24 to 35, tungsten 6 to 9, nickel 8.5 to 11.5, boron an effective amount of about 0.005 up to 0.05, zirconium 0.1 to 1.7, yttrium 0.03 to 1, iron up to 2 maximum as added with other alloying constituents, with the remainder cobalt except for incidental impurities such as sulfur and phosphorous both less than 0.04 percent, along with silicon, manganese, copper, titanium and the like which should be held to less than about 0.1 percent. It has been found that alloys having the above balanced composition are characterized by substantial increases in corrosion resistance at elevated temperatures, at the same time having improved physical characteristics such as high tensile and rupture strength and ductility.

As pointed out above, the present compositions represent carefully balanced combinations of constituents each of which contributes to the desirable characteristics obtained. Departures from the specified proportions of materials destroy this base alloys improved high-temperature to corrosion at elevated tem- 2 balance and result in materials which have been found to be lacking in one or more desired characteristic. Carbomfor example, is added for strengthening purposes and when lower amounts than those prescribed are used, there is an undesirable loss in strength. In the prescribed range, carbon combines with zirconium and chromium to fonn, respectively, zirconium carbide and Cr c which precipitation-harden the alloy. Zirconium carbide, in particular, remains thermally stable to near the melting point of the alloy; hence, it contributes greatly to strength at very high temperatures. 0n the other hand, carbon in amounts above those prescribed results in embrittlement and loss of strength through excessive precipitation of these two carbides, particularly at grain boundaries. Chromium contributes to the oxidation and corrosion resistance of the material at elevated temperatures and'lesser amounts than those set forth inhibit these characteristics. Larger amounts than those specified result in embrittlement through precipitation of the electron compound sigma, composed in major part of cobalt and chromium, in the alloy 5 matrix and at the grain boundaries. Larger amounts of tungsten than those set forth also enhance formation of sigma phase due to substitution of tungsten in the sigma lattice structure, thus embrittling the alloy. In the prescribed rangejtungsten increases strength by substitutional solid solution hardening of the alloy matrix lattice structure. Lesser amounts of tungsten detract from the strength.

Nickel serves as a matrix stabilizer to maintain the FCC alloy matrix structure, and decreases the tendency toward'formation of embrittling stacking faults. Nickel fails in this role in lesser amounts than those set forth. Higher than prescribed amounts of nickel reduce the high-temperature strength and hot corrosion and oxidation resistance. Boron, which serves as a strengthener, results in embrittlement when used in excess due to the precipitation of metal 'borides at the alloy grain boundaries, and in poor high-temperature strength when used in too small amounts. lron, as pointed out above, is added with other alloying compounds and is not harmful up to the amount allowed, but when present in greater amounts than those prescribed reduces the strength and hot corrosion resistance of the final alloy. Zirconium serves as a strong carbide former, contributing to the high-temperature strength. in amounts either less or greater than that prescribed, high-temperature strength is reduced due to an imbalance of the two major carbide'strengthening precipitates, ZrC and Cr C Yttrium is particularly critical to the hot corrosion resistance including both oxidation and corrosion caused by sodium, sulfur and the like. it is known that yttrium interacts during the oxidation process with the predominant (Ir- 0 oxide scale, enhancing its adherence to the underlying substrate as well as reducing Cr diffusion, therefore reducing oxidation kinetics. These features arise as a result of preferential oxidation of yttrium at key sites, such as grain boundaries near the oxidizing surface, thereby blocking subsequent diffusion. Amounts above those prescribed result in undesirable embrittling due to the precipitation of cobalt/yttrium-rich intermetallic compounds, such as Co Y. The cobalt base, of course, is well known for its contribution to corrosion resistance.

The following examples will illustrate the practice of the invention, it being realized that they are exemplary only and not to be taken as limiting in any way.

As example 1, there was prepared :an alloy consisting of, by weight percent, carbon 0.5, chromium 29, tungsten 7, nickel l0, boron 0.01, iron 1, zirconium 1.5, and yttrium 0.15, the remainder being cobalt except for impurities such as Mn and Si, 01, and S and P, 0.04.

As example 2, there was prepared an alloy consisting essentially of, by weight percent, carbon 0.46, chromium 27.2, tungsten 6.7, nickel l0, boron 0.01 iron 0.71, zirconium 1.29, and yttrium 0.21, with the remainder essentially cobalt except for impurities such as titanium, manganese and silicon, which were present in amounts of less than 0.1 each.

NA-Not taken. 1 HT-l (see Table II), all others as-cast.

TABLE III Mils loss per side Temp, Time, Heat Fuel F. hrs Mas. pen. Surface Example" Natural gas 1, 800 749 3. 0. 3 1 l d 1. 000 500 3. 3 0. 7 (1 2,000 711) 8. 5, 14. 7 5. 8 1,600 600 4.1, 1.4 0 7, 0.4 1. 800 749 4. 2 0. 9 1, 000 590 5. 4 1.0 2, 000 719 8. 7 l. 1 1,600 606 1. t), 2. 2 0. 4. 0.5 1, G00 0, 000 2. 5 1.800 711 2.1 0 7 1,800 6,005 6.3 1,000 737 3. 2 0. 0 d0 .2, 000 044 3.7 1. 6 Residual oil plus NaCL. 1,600 710 1. 5 0. 4 Natural gas l, 600 6,000 4. 8 1.800 750 4.3 Prior art alloy 1,800 6,000 11.0 1, 000 000 5. 8 2,000 700 10. 5 1,600 000 2.0

1 Two separate tests.

From the above table [I] by comparison at the same temperatures, it will be seen that the present alloys are far and away more resistant over long exposure periods to hot corrosion of the oxidative type experienced with natural gas and about equal in resistance to hot corrosion caused by sodium and sulfur and other agents which have an effect similar to that of sodium.

There are provided, then, by the present invention alloys which are suitable as materials of construction which combine superior high-temperature rupture stress with good resistance to hot corrosive influences.

What we claim as new and desire to secure by Letters Patent of the United States is:

1. A cobalt base alloy characterized by good high-temperature strength, ductility, and corrosion resistance consisting essentially of about, by weight, carbon 0.1 to 0.7%, chromium 24 to 35%, tungsten 6 to 9%, nickel 8.5 to l 1.5%, boron an effective amount up to 0.5%, iron, up to 2%, zirconium 0.1 to

1.7%, yttrium 0.03 to 1%, with the remainder essentially cobalt except for impurities.

2. A cobalt base alloy as in claim 1 consisting essentially of about, by weight, carbon 0.5%, chromium 29%, tungsten 7%, nickel 10%, boron 0.10%, iron 1%, zirconium 1.5%, yttrium 0.15%, with the remainder essentially cobalt except for impurities.

3. A cobalt base alloy as in claim .1 consisting essentially of about, by weight, carbon 0.46%, chromium 27.2%, tungsten 6.7%, nickel 10%, boron 0.01%, iron 0.71%, zirconium 1.29%, yttrium 0.21%, with the remainder essentially cobalt except for impurities.

4. A cobalt base alloy as in claim 1 consisting essentially of about, by weight, carbon 0.51%, chromium 28.3%, tungsten 7.23%, nickel 10%, boron 0.10%, iron 0.68%, zirconium 1.23%, yttrium 0.24%, with the remainder essentially cobalt except for impurities.

Claims

2. A cobalt base alloy as in claim 1 consisting essentially of about, by weight, carbon 0.5%, chromium 29%, tungsten 7%, nickel 10%, boron 0.10%, iron 1%, zirconium 1.5%, yttrium 0.15%, with the remainder essentially cobalt except for impurities.
3. A cobalt base alloy as in claim 1 consisting essentially of about, by weight, carbon 0.46%, chromium 27.2%, tungsten 6.7%, nickel 10%, boron 0.01%, iron 0.71%, zirconium 1.29%, yttrium 0.21%, with the remainder essentially cobalt except for impurities.
4. A cobalt base alloy as in claim 1 consisting essentially of about, by weight, carbon 0.51%, chromium 28.3%, tungsten 7.23%, nickel 10%, boron 0.10%, iron 0.68%, zirconium 1.23%, yttrium 0.24%, with the remainder essentially cobalt except for impurities.