|Publication number||US3704182 A|
|Publication date||Nov 28, 1972|
|Filing date||Jun 11, 1969|
|Priority date||Jun 11, 1969|
|Publication number||US 3704182 A, US 3704182A, US-A-3704182, US3704182 A, US3704182A|
|Inventors||Griffiths Leonard B, Shen Yuan-Shou|
|Original Assignee||Mallory & Co Inc P R|
|Export Citation||BiBTeX, EndNote, RefMan|
|Referenced by (6), Classifications (8)|
|External Links: USPTO, USPTO Assignment, Espacenet|
NOV. 28, 1972 GRIFFITHS ETAL 3,704,182
NICKEL-CHROMIUM-BERYLLIUM ALLOY Filed June 11, 1969 4 Sheets-Sheet 1 F145. (5 23 INVENTORS LEONARD Bv GRIFFITHS YUAN-SHOU SHE ATTORNEY Nov. 28, 1972 Filed June 11. 1969 L. B. GRIFFITHS NICKEL-CHROMIUM-BERYLLIUM ALLOY 4 Sheets-Sheet 2 INVENTORS LEONARD B. GRIFFITHS YUAN- SHOU SHEN ATTORNEY WEiGHT GAIN MG/CMZ Nov. 28, 1972 B. GRFFITHS Em 3,704,182-
NICKEL-CHROMIUM-BERYLLIUM ALLOY Filed June 11, 1969 4 Sheets-Sheet 3 lN-IOO 42 Q6 I I CORROSION IN AIR IFJIQ 4 FIG. 5
INVENTORS BY w K M 7 ATTORNEY NOV. 28, 1972 GR|FF|TH$ EI'AL 3,704,182
NICKEL-CHROMIUM-BERYLLIUM ALLOY 4 Sheets-Sheet 4 Filed June 11. 1969 LARSON-MILLER PLOTS OF STRESS- RUPTURE DATA 9 x 2 mwUEw P .T (Log'H-20)x|0 INVENTORS LEONARD B. GRIFFITHS FIG I ATTORNEY United States Patent 3,704,182 NICKEL-CHROMlUM-BERYLLIUM ALLOY Leonard B. Grilfiths and Yuan-Shou Shen, North Reading,
Mass., assignors to P. R. Mallory & Co. Inc., Indianapolis, Ind. Continuation-impart of application Ser. No. 793,814, Jan. 24, 1969. This application June 11, 1969, Ser. No. 832,335
Int. Cl. C22c 19/00 US. Cl. 148-32 8 Claims ABSTRACT OF THE DISCLOSURE This invention relates to a nickel-chromium-beryllium alloy having a microstructure which provides obstacles to plastic flow in the nickel rich matrix phase so that high strength properties are obtained at both room and elevated temperatures. The alloy may also contain other additives including aluminum and/or titanium together with hardeners including molybdenum and/or tungsten, with or without carbon. A method of processing the alloy comprises: melting the alloying ingredients in a crucible while avoiding the presence of oxygen; raising the temperature to 1450 to 1550 C.; casting the alloy in a mold. The alloy may be remelted and cast in an apparatus to eifect abstraction of heat from the casting from one direction only to obtain a directionally orientated microstructure.
This application is a continuation-in-part of application Ser. No. 793,814, filed Jan. 24, 1969 now abandoned.
Alloys containing nickel-chromium and beryllium have been known for some time. For example, such alloys are disclosed in British Pat. 404,012 (for use in surgical sewing needles and dental instruments) and US. Pats. 2,089,587 (for dentures) and 2,150,205 (for engine valves).
However, the advantage of using these alloys in specific proportions resulting in a specific microstructure for both room temperature and high temperature applications requiring high mechanical properties has not previously been recognized.
It is, therefore, an object of the present invention to provide a Ni-Cr-Be alloy having high strength at elevated temperatures.
It is another object of the present invention to provide an alloy which is resistant to oxidation at elevated temperatures.
It is another object of the present invention to provide an alloy having high stress-to-rupture values at elevated temperature.
It is another object of the present invention to provide an alloy having good mechanical properties at room temperature.
It is another object of the present invention to provide an alloy having a microstructure which is resistant to plastic flow at both room and elevated temperatures.
It is another object of the present invention to provide a high temperature alloy which avoids the use of carbides for strengthening.
It is still another object of the present invention to provide a method for processing a high temperature alloy containing nickel-chromium-beryllium in order to obtain a microstructure which has resistance to plastic flow at room and elevated temperatures.
It is another object of the present invention to provide a process for treating an alloy in order to obtain uniaxial as-cast structure.
Other objects will be apparent from the following description and drawings in which:
FIG. 1 is a view of an exemplary microstructure of the alloy of the present invention at 2700 magnifications.
FIG. 2 is a ternary Ni-Cr-Be diagram showing the composition of the eutectic alloy utilized in obtaining the desired microstructure according to the present invention.
FIG. 3 is a plot of weight gain (oxidation) as a function of time, at various temperatures, for the alloy of the present invention and other representative alloys of the prior art.
FIG. 4 is a schematic diagram of apparatus which may be used in casting the alloy of the present invention.
FIG. 5 is a view of the as-cast ingot showing the microscopic directionality of the casting at 20 magnifications.
FIG. 6 is a view of the microstructure of the alloy of the present invention in the directionally cast condition at 1300 magnifications.
FIG. 7 is a Larsen-Miller plot of the stress-rupture data obtained in Example II.
As can be seen from FIG. 1, the microstructure of the nickel-chromium-beryllium alloy of the present invention is composed of a nickel rich solid solution matrix 10 having chromium dissolved therein in solid solution and nickel-beryllide rods (NiBe) 11, in which chromium is also dissolved, interspersed within said matrix.
While the structure is actually the result of a three phase equilibrium transformation, it is useful to consider it as a binary eutectic in which:
( 1) Liquidz Ni +NiBe The reaction occurs at the base of a liquidus valley bounded by the two-phase fields, 1iquid+Ni(Cr) and liquid+Ni(Cr)Be, within the Ni-Cr-Be constitutional system. As can be seen from FIG. 2, the composition at which this reaction takes place is within the temperature range of 1175 to 1275 C. The nickel content of the alloy of the present invention should be about 54 to 72.5 atomic percent. The chromium content should be about 32.5 to 2.5 atomic percent and the beryllium content about 14.5 to 25.5 atomic percent. Furthermore, the composition should be such that upon freezing no two-phase field is intersected, but rather the reaction proceeds at all times in accordance with the three phase reaction given in Equation 1. This occurs at compositions substantially as shown by the solid line in FIG. 2. A variance of about :2 atomic percent of the Ni-Be ratio on either side of the solid line in FIG. 2 may also be used and the desired microstructure will be obtained. Since freezing occurs essentially within the liquidus valley, the temperature dependence of which is only slight, a substantially uniform microstructure is obtained throughout the ingot, in contrast to alloys having a long freezing range.
The presence of the Ni(Cr)Be rods 11 is to be contrasted with the nickel-beryllium binary system wherein the NiBe phase is plate-like. It has been found according to the present invention that the addition of chromium results in the desired rod-shaped beryllide phase.
Generally, in two phase structures of this type, one of the phases predominates at the grain boundaries which results in either brittleness or low strength; however, the
beryllide rods extend completely to the colony boundaries in the alloy of the present invention, as shown in FIG. 6. This phenomenon is very important. The beryllide rods provide obstacles to plastic flow in the nickel rich phase. This feature can be seen in FIGS. 1 and 6; showing slip lines 12 are prevented from propagation by the hard beryllide phase 11. This phenomenon yields a relatively high rate of work hardening. Spacing between rods Within a colony is usually within the range of about 2 to 20 and preferably about 4 to 8 This is computed on the basis of the mean free path distance.
The chromium, in addition to rendering the beryllide phase rod-like, confers some solid solution strengthening both on the nickel and on the beryllide phase. The chromium also provides oxidation resistance. This can be seen from FIG. 3. It is apparent from FIG. 3 that at 1800 F. there is less weight gain (a measure of oxidation) with the alloy of the present invention than with the Inconel 100 (10 Cr, 15 C, Ti, 5.5 A1, 3 Mo, .18 C, bal. Ni) and Rene-Y (Cr 22, Mo 9, Fe 18, W 1 max., Co 2 max., Mn 1.0, Si 1.0 max, .15 C, 0.15 La, bal. Ni) prior art alloys.
Oxygen and nitrogen should each be below 0.5% by weight respectively. Carbon should be below 0.02% by weight unless carbides are to be formed as described hereinafter.
The alloy of the present invention may be prepared by melting together the constituents preferably in elemental form in a refractory crucible made, for example, of MgO, A1 0 or BeO in the absence of oxygen. If desired, the melting may be carried out in an inert atmosphere such as argon or helium. It is also often desirable to utilize a reduced pressure or partial vacuum atmosphere. The melting temperature should be between about 1450 to 1550 C. in order to insure that ample fluidity for subsequent casting is obtained.
The mold to be used in casting the alloy of the present invention may be either of the permanent mold type, for example, made of copper or steel or graphite molds may be utilized. If graphite is utilized, it is preferred to use a beryllium oxide wash in the mold. The casting cooling rate for the casting operation is not critical.
After casting, the ingots are preferably remeltcd and subsequently frozen uniaxially in order to obtain the best properties. For example, one apparatus which may be used for the remelting operation is shown in FIG. 4. The holding screws 20 and 21 hold plates 22 and 23 in place by means of spring fasteners 24. A shielding plate 25 is placed upon the top of holding plate 22 and a chillplate 26 is placed thereon. The chillplate has a water inlet 27 and a water outlet 28 associated therewith which pass through plates 23 and 25 for circulating a cooling fluid therethrough. A starting stub 29 is mounted on the chill plate.
The ingot to be melted 31 is placed in a refractory crucible 30 which may be made of MgO, A1 0 or BeO or refractory oxide materials. In order to effect melting an RF coil 50 is energized to provide sufiicient heat to reach the melting point temperature range given above.
The lowering mechanism comprises a motor 60 mounted on the base 61. The motor is connected to a wire rope or chain 62, which by means of idle wheels 63 and 64, controls the descent of argon adaptor 70 by means of hook 65 is engagement withthe flange 71 of the argon adaptor. The adaptor has an inlet 73 and an outlet 74 for circulation of argon gas. The inlet conduit 73 is in communication with the crucible 73 to provide an argon atmosphere during the melting operation which takes place in the vicinity of coil 50. The argon then passes out of the crucible and through conduit 75 and 74.
The argon adaptor is aflixed to the crucible 30 by conventional fasteners (not shown) so that the adaptor, the crucible and the entire structure excepting coil 50 are lowered upon operation of motor 60, causing the ingot to be melted to move through coil 50. The amount of movement is limited, however, by the space between the coil, and shielding sheet 40.
Initially the motor 60 is utilized to place the meeting point of the starting stub and the ingot to be melted within RF coil 50. RF coil is then energized sufficiently to melt a cross section of the ingot. The ingot is then gradually lowered as freezing occurs from the chill plate 26 upward under the action of the naturally occurring axial temperature gradient from the chill plate upward. For example, the ingot may be lowered at the rate of 1 inch to 2 inches per hour. The casting operation is stopped when the coil reaches a point near shielding sheet 40 or when all of the ingot has been melted. I i
It will be apparent that this arrangement results in a directionally frozen ingot as shown in FIG. 5. However, it will be apparent to those skilled in the art that other casting apparatus which provides for directional freezing can also be utilized. For commercial scale operation, continuous casting equipment in which the ingot is continuously cooled by application of a cooling medium to the already cast portion of the ingot, could be utilized.
The microstructure of the alloy of the present invention in the directionally frozen condition is shown in FIG. 6 and the nickel-matrix 10 again surrounds the Ni(Cr)Be rods 11. The microstructure is also composed of two phase colonies which are greatly elongated in the direction of casting growth; in other words, parallel to the growth axis as shown in FIG. 5. The beryllide phase 21 is uninfluenced by growth conditions, and the axis of the rods varies from colony to colony. Notethe rods in colonies 23 and 24. There is a preferred direction however within each colony. The elongated colonies result in markedly reduced transverse colony boundary area.
In addition to the amounts of Ni, Cr and Be previously stated, a metal selected from the group consisting of aluminum, titanium and mixtures thereof is preferably added in the range of from about each 1 to 5 atomic percent, preferably 2 to 4 atomic percent, each. Preferably aluminum alone, or mixtures of aluminum and titanium are used. The aluminum and/or titanium present reacts with nickel to form the compounds such as Ni Al and Ni Ti. These compounds may be distributed throughout the nickel-rich phase by first providing a solution treatment at a temperature of about 1950 to 2150 F. preferably about 2000 to 2150 F. for a period of 2 to hours, preferably 4 to 50 hours. This heating step is followed by ageing at a temperature of from about 1200 to 1500' F., preferably 1200 to 1400 F. for about 2 to 30 hours, preferably 4 to 16 hours. This results in the Ni Al and/or (Ti, Al)Ni precipitating from solid solution in the form of the 7' phase well known in the art.
It is also preferred to add one or more hardening elements selected from the group consisting of Ma, W, Ta, Nb, Va, Zr, B, Min, Fe, Co and mixtures thereof, in an amount of from about 2 to 10 atomic percent total. Preferably Mo and W are used in the range of about 2 to 2.5 atomic percent Mo and from about 1 to 1.5 atomic percent W. The hardening addition will affect an increase iri1 strength by solid solution hardening of the nickel-rich p ase.
The hardening elements will also form carbides if free carbon is present. While considerable strengthening can be obtained by carbide formation by including carbon in the range 0.06 to 0.12% by weight, according to the preferred embodiment of the invention the carbon content is restricted to not more than .02% by weight so that carbide formation is substantially avoided. During service at elevated temperature the carbides have a tendency to coarsen, causing embrittlement.
As to the properties of the alloy of the present invention, Table I shows that the alloy of the present invention is superior to representative alloys of the prior art from a standpoint of modulus of elasticity and specific modulus (modulus of elasticity divided by density).
TABLE I The resulting castings were 7 inches long by 1% inches in diameter. fig g g igffi f Those specimens which were directionally cast were 5 men 1 remelted and directionally cast in the manner described Anny: 5 above in regard to FIG. 4. Casting rates were 1 to 2 PW6641 86.5 mches per hour. ggg g fi 28 The specimens which were heat treated were solution Udluet 700 30 104 treated at 1120 C. for 4 hours and then air quenched 129 to 760 C. and held for 16 hours.
NR) 10 00, 12 w, 5 A1, 2 Ti, 1 T 05, .1 10 Tensile specimens were then prepared and standard 8 1106. :22 or, zoFeygMo 0, Ni ba1anca tensile tests were carried out at the temperatures given M:11g5C1, 61.%Al,4.5%/Io'a+ 03 '51 (55 1.0 max., in Table III. Room temperature was 68 to 75 1.max., 9.1118X., 1 8811636.
19 Co, 15 or, 5M0 AL Ti, w mu Fe. m The tens1le propert1es are reported in Table III. In N: balance. the table C.C. mdlcates the specimens were conventionally 511? mpmsenumenmn- 15 cast; D.C. indicates the specimens were directionally cast and HT. indicates that the specimens were heat treated prior to testing.
TABLE IIL-MECHANIGAL PROPERTIES OF Nl-Or-Be ALLoYs Specific mechanical T t Mechanical properties, Xl,000 p.s.l.propertles, X1,0J0 in.
G5 Condltemp. Prop. 0. 2 7 E10 0.2 tlon ri limit Y.s. urs pem ii Y nrs Alloy number:
1 0.0. Room 55.5 78.2 132.4 a 290 400 -57.0 -7s.0 -1a25 -204 -401 13.0. Room 68 118.6 10 252 430 -52 -72 -121.0 -205 -448 2 D.0. Room 94.2 113.0 162.8 143 418 501 E11. -95.2 -1140 -154.5 -422 -009 13.0. 1, 400 83. 5 e2. 9 97. 0 e44 352 H.T.
3 5 Room 84.0 111.2 151.4 4 412 551 g1? "1,300 87.0 05.0 123.5 0 352 457 31%: 1,400 82.5 92.0 115.0 7 343 426 D101 1,500 210.5 87.4 104.5 8 3221 387 RT.
4 13.0. Room 103.5 140.0 170.0 4 541 529 EXAMPLE I EXAMPLE II Tensile tests The alloy compositions chosen for testing are given inTable 11.
TABLE II.ALLOY COMPOSITION ATOMIC PERCENT Cr Al Mo W Ni Be Stress-rupture tests TABLE IV.,STB.ESS RUPTURE PROPERTIES OE Ni-Cr-Be ALLOYS Rupture time (hr.)
Norm-The data liste Handbook, 1961 ed. pp. 472-473).
What is claimed is: 1.- An alloy consisting essentially of 54 to 72.5 percent nickel, 32.5 to 2.5 atomic percent chromium, 14.5 to 25.5 atomic percent-beryllium;
a compound forming metal selected from the group consisting of aluminum,-titanium and-mixtureathereof in an amount of about 1 to 5 atomic percent; and a hardening element selected from the "group consisting of molybdenum, tungsten, tantalum,niobium, vanadium, boron, manganese, iron, cobalt'and mixtures thereof in an amount of from about 2 to about atomic percent;
said alloy having a microstructure comprising a nickel matrix and a rod-like phase containingnickeland beryllium dispersed within said matrix.
2. An alloy according to claim 1 in which the composition is such that the solidification proceeds by the three phase reaction LiquidSNi +NiBe.
3. An alloy according to claim 1 in which coloniesof said microstructure are elongated in the direction of solidification. g
. 4. An alloy according to claim 1 in which the spacing between rods is within the range of about 2.to .20 miatomic '1 in Table IV is shown in a Larsen-Miller plot (described in Metal crons, computed on the basis of the mean free path distance. 7
5'.An alloyaccording to claim 2 having a room temperature specific modulus of about 125x10 inch.
6. An alloy according to claim 1 having up to about 0.12% carbon by weight.
"- 'lrArwtlioyacco rding to claim 1 in which said rod-like constituent presents obstacles to plastic flow at room temperature and at elevated temperatures.
8. An alloy according to claim 1 in which the hardening element is selected from the group consisting of W, Mo and mixtures thereof.
References Cited UNITED STATES PATENTS 2,089,587 87193? Touceda -171 2,150,255 3/1939 Touceda 75-171 3,464,817 9/1969 Griffiths 75-171 RICHARD O. DEAN, Primary Examiner Us. 01. X.R.
UNITED STATES PATENT OFFICE CERTIFICATE OF CORRECTION Leonard B. riffiths and Yuan-Shou Shen It iscertified that error appears in the above-identified patent and that said Letters Patent are hereby corrected as shown below:
Col. 3, line 57, after or insert other Col. 3, line 64, delete '"is" and insert therefor in Col. 4, line 54', M0 should be inserted in Place of "Ma" Col. 4, line 55, delete "Min" and substitute therefor Mn Col. 5, line 13, after O3 insert B,-.'
Signed and sealed this lst day of May 1973.
EDWARD M. F ETCHER, JR. 7 ROBERT GOTTSCHALK Attesting Officer Commissioner of Patents FORM PC4050 (10'69) uscoMM-Dc 60376-P69 fi' U.ST GOVERNMENT PRINTING OFFICE I969 0-366-33.
|Citing Patent||Filing date||Publication date||Applicant||Title|
|US3807992 *||Dec 27, 1971||Apr 30, 1974||Toyoda Chuo Kenkyusho Kk||HEAT RESISTANT Ni-Al-Be ALLOYS|
|US4556534 *||Dec 20, 1983||Dec 3, 1985||Dentsply Research & Development Corp.||Nickel based casting alloy|
|US4592890 *||Aug 8, 1983||Jun 3, 1986||Dentsply Research & Development Corp.||Dental prostheses alloy|
|US5980653 *||Jan 23, 1997||Nov 9, 1999||Ngk Metals Corporation||Nickel-copper-beryllium alloy compositions|
|US6093264 *||Aug 2, 1999||Jul 25, 2000||Ngk Metals Corporation||Nickel-copper-beryllium alloy compositions|
|EP0134528A1 *||Jul 25, 1984||Mar 20, 1985||Dentsply International, Inc.||Dental prostheses alloy|
|U.S. Classification||148/427, 148/675, 148/428, 420/442, 148/404|