US2631095A - Alloy adapted for prosthetic articles - Google Patents

Alloy adapted for prosthetic articles Download PDF

Info

Publication number
US2631095A
US2631095A US145598A US14559850A US2631095A US 2631095 A US2631095 A US 2631095A US 145598 A US145598 A US 145598A US 14559850 A US14559850 A US 14559850A US 2631095 A US2631095 A US 2631095A
Authority
US
United States
Prior art keywords
alloy
beryllium
melting point
nickel
content
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
US145598A
Inventor
Emil S Griffiths
William D Cashman
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Consolidated Car Heating Co Inc
Original Assignee
Consolidated Car Heating Co Inc
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Consolidated Car Heating Co Inc filed Critical Consolidated Car Heating Co Inc
Priority to US145598A priority Critical patent/US2631095A/en
Application granted granted Critical
Publication of US2631095A publication Critical patent/US2631095A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C19/00Alloys based on nickel or cobalt
    • C22C19/03Alloys based on nickel or cobalt based on nickel
    • C22C19/05Alloys based on nickel or cobalt based on nickel with chromium
    • C22C19/051Alloys based on nickel or cobalt based on nickel with chromium and Mo or W
    • C22C19/055Alloys based on nickel or cobalt based on nickel with chromium and Mo or W with the maximum Cr content being at least 20% but less than 30%
    • AHUMAN NECESSITIES
    • A61MEDICAL OR VETERINARY SCIENCE; HYGIENE
    • A61KPREPARATIONS FOR MEDICAL, DENTAL OR TOILETRY PURPOSES
    • A61K6/00Preparations for dentistry
    • A61K6/80Preparations for artificial teeth, for filling teeth or for capping teeth
    • A61K6/84Preparations for artificial teeth, for filling teeth or for capping teeth comprising metals or alloys

Definitions

  • alloys containing chromium, nickel, cobalt, beryllium and molybdenum are especially adapted for the casting of prosthetic articles uch as dentures and the like, and while such alloys are highly resistant to corrosion they do exhibit a definite loss of lustre when highly polished specimens thereof "are exposed to very dilute lactic acid solutions.
  • a denture formed of such an alloy and which, initially, is highly polished loses its high lustre when exposed to lactic acid in concentrations of the order encountered in the human mouth.
  • the surface corrosion which eiiects this loss of lustre doe not in any way weaken or otherwise affect the function of the denture but it is highly objectionable from an aesthetic viewpoint.
  • the principal object, therefore, of our invention is to provide an alloy of the character denot be less than 65,000 to 70,000 p. s. i. although scribed-which will retain its surface lustre when a highly polished section thereof is exposed to lactic acid in concentrations of the order encountered in the human mouth; which will have a yield point sufficiently high to permit dentures, for example, having attenuated portions, such as clasps thereon, to be cast therefrom; and which will have a melting point sufiiciently low to permit it to be cast in investments of the plaster bound silica type.
  • the object of our invention is to provide a balanced alloy of the character described in which the reduction in the yield strength and the increase in the melting point, which occur when the beryl lium content is reduced to a point where it does not affect the retention of lustre, are offset by the addition of other elements.
  • -A further object of our invention is to provide an alloy which can be processed to produce a casting characterized by a relatively fine grain size.
  • the temperature of the molds at the time the molten metal is introduced therein be a low aspossible.
  • the permissible mold temperature is governed by the amount of thermal expansion which can be obtained by heating the mold to that temperature and, by the ability of the alloy being cast to flow freely and register the fine details present in the mold.
  • Plaster bound silica investment provides adequate thermal expansion to compensate for metal shrinkage at much lower temperature than the highly refractory investment material used with alloys having high melting points.
  • a further object of our invention is to provide an alloy having a melting range which is low enough to permit its being cast in a plaster bound silica type investment and fluid enough to permit its flowing in relatively thin sections when the mold 3 temperature is in the range of about 900 to 1300 F.
  • Alloy 60 will not lose its lustre in dilute lactic acid but it has a hardness value of only C 19 (corresponding to a yield strength of about 60,000 p. s. i.) and therefore would not have suflicient strength for all applications. Furthermore, the melting point is too high to permit its use in a plaster bound invest ment. However, by adding copper, as in alloy 138, the hardness value is increased to C 24 and the yield strength is raised to 78,000 D. s. i. The addition of copper does not substantially afiect the melting which is about 2475 F. If 4% of manganese is added, as in alloy 139 the melting point is reduced to about 2325 F. which is low enough to permit the casting of the alloy in a plaster bound investment. It will also be noted that the manganese addition does not aifect the hardness.
  • Alloys 19, 20, and 24 further illustrate the effectiveness of copper as a hardener and manganese as a means of reducing the melting point.
  • alloy 20 which has no copper therein, has a hardness of C 28 and a melting point of 2300 F.
  • the hard- 4 ness is increased to C 38 and the melting point is raised to about 2375 F.
  • Alloy 24 which contains both manganese and copper retains the high hardness of alloy 19 and has substantially the same melting point (2300 F.) as alloy 20.
  • alloy 24 with alloy 25 indicates how the hardness and melting point may be controlled by manipulating the ratio of nickel to cobalt while keeping the combined content of these two elements constant.
  • alloy 24 with a nickel-cobalt ratio of 1 to 1.5 has a hardness of C 40 and a melting point of about 2300 F.
  • the nickel-cobalt ratio to 1.5 to 1 is decreased to C 35 and the melting point to 2250" F.
  • the beryllium content while small, has a very pronounced effect on the physical properties, the melting point, and the casting characteristics of the alloy. If the beryllium content exceeds 1.2% the concentration of the beryllium intermetallic phase becomes so great that it is visible on the surface of polished specimens of the alloy when they are subjected to the action of a dilute lactic acid solution. By maintaining the beryllium content below this level, loss of lustre is avoided.
  • Manganese in excess of about 8% causes a reaction with the investment, even when the maximum beryllium content is employed, and, for this reason, should be avoided. Furthermore, since the manganese is used partially to oiiset the rise in the melting point associated with a lowering of the beryllium content, the manganese, as a rule, should be present in the lower portion of its range when the beryllium is present in the upper portion of its range, and vice versa.
  • the copper is added as a hardening agent to offset the drop in yield strength associated with the reduction in beryllium. Therefore, the copper should ordinarily be present in the lower portion in its range when the beryllium is present in the upper portion of its range.
  • Nickel and cobalt are more or less interchangeable in order to vary the yield strength and ductility of the resulting alloy. Thus, a high cobalt content tends to raise the yield strength and usually the melting point, while high nickel, on the other hand, tends to give a softer, lower meltin point alloy.
  • the preferred ratio of nickel to cobalt has been found to be from 1 to 2, to 1 to 1 /2.

Landscapes

  • Health & Medical Sciences (AREA)
  • Oral & Maxillofacial Surgery (AREA)
  • Chemical & Material Sciences (AREA)
  • Veterinary Medicine (AREA)
  • Engineering & Computer Science (AREA)
  • Animal Behavior & Ethology (AREA)
  • General Health & Medical Sciences (AREA)
  • Public Health (AREA)
  • Epidemiology (AREA)
  • Plastic & Reconstructive Surgery (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Materials For Medical Uses (AREA)
  • Dental Preparations (AREA)

Description

Patented Mar. 10, 1953 ALLOY ADAPTED FOR PROSTHETIC ARTICLES:
Emil S. Griffiths and William D. Cashman,
Albany, N. Y., assignors to Consolidated Car- Heating Company, Inc., Albany, N. Y., a corporation of New York No Drawing. Application February 21, 1950, Serial N 0. 145,598
2 Claims. (ems-in) Our invention relates to alloys and particularly to alloys suitable for making prosthetic articles.
It has heretofore been suggested that alloys containing chromium, nickel, cobalt, beryllium and molybdenum are especially adapted for the casting of prosthetic articles uch as dentures and the like, and while such alloys are highly resistant to corrosion they do exhibit a definite loss of lustre when highly polished specimens thereof "are exposed to very dilute lactic acid solutions. Thus, a denture formed of such an alloy and which, initially, is highly polished, loses its high lustre when exposed to lactic acid in concentrations of the order encountered in the human mouth. The surface corrosion which eiiects this loss of lustre doe not in any way weaken or otherwise affect the function of the denture but it is highly objectionable from an aesthetic viewpoint.
We have investigated the reason for this loss of lustre and find that it is due to the fact that the beryllium forms an inter-metallic phase in the alloy which darkens when exposed to lactic acid. These darkened areas throughout the matrix cause the loss of reflection or lustre. While this inter-metallic phase persists to a certain degree as long as there is any beryllium present in the alloy, and beryllium is an essential element which endows the alloy with the fluidity at casting temperatures necessary to cause the metal to now into the smaller mold cavities we have found that by reducing theberyllium to a comparatively low percentage the.
detrimental effect thereof on the retention of a high surface lustre is so reduced that it is no longer objectionable.
However, when the beryllium content is lowered to the extent necessary to avoid loss of lustre other diiiiculties are encountered such as the yield point for full dentures, or those without clasps, may be somewhat lower than this.
Furthermore, it is desirable to produce an alloy which may be cast in a plaster bound silica type investment, and to accomplish this the melting point of the alloy cannot exceed about 2450 to 2500 F.
The principal object, therefore, of our invention is to provide an alloy of the character denot be less than 65,000 to 70,000 p. s. i. although scribed-which will retain its surface lustre when a highly polished section thereof is exposed to lactic acid in concentrations of the order encountered in the human mouth; which will have a yield point sufficiently high to permit dentures, for example, having attenuated portions, such as clasps thereon, to be cast therefrom; and which will have a melting point sufiiciently low to permit it to be cast in investments of the plaster bound silica type. More specifically the object of our invention is to provide a balanced alloy of the character described in which the reduction in the yield strength and the increase in the melting point, which occur when the beryl lium content is reduced to a point where it does not affect the retention of lustre, are offset by the addition of other elements.
-A further object of our invention is to provide an alloy which can be processed to produce a casting characterized by a relatively fine grain size.
' It i well known that, at room temperature, the common metals and alloys are harder and stronger in the fine grain condition than in the coarse grain condition. In small cross-sections, such as those present in a prosthetic article where coarse grains may limit the total number of grains in the cross-section to 10 or less, the production of the desired physical properties is much more difficult than is the case with a fine grain material. One factor having a pronounced effect on grain size, is the rate at which the casting is cooled during the solidification thereof.
In order to obtain a rapid cooling rate during the solidification of the metal in the mold, it is desirable that the temperature of the molds at the time the molten metal is introduced therein, be a low aspossible. Those familiar with the art of casting prosthetic articles will realize that the permissible mold temperature is governed by the amount of thermal expansion which can be obtained by heating the mold to that temperature and, by the ability of the alloy being cast to flow freely and register the fine details present in the mold. Plaster bound silica investment provides adequate thermal expansion to compensate for metal shrinkage at much lower temperature than the highly refractory investment material used with alloys having high melting points. Therefore, more specifically, a further object of our invention is to provide an alloy having a melting range which is low enough to permit its being cast in a plaster bound silica type investment and fluid enough to permit its flowing in relatively thin sections when the mold 3 temperature is in the range of about 900 to 1300 F.
The essential ingredients of our alloy and their percentages, by weight, of the total composition are:
Percent Chromium 15 to 27 Beryllium 0.2 to 1.2 Manganese 2 to 8 Molybdenum 3 to 12 Copper 2 to 10 the balance being nickel and cobalt, each between about 5% and about 50% with the combined nickel-cobalt content being from 42% to about 77%.
The preferred ranges of the essential ingredients of our alloy are:
Percent Chromium 20 to 25 Molybdenum 5 to Beryllium 0.5 to 1.0 Manganese 3 to 6 Copper 3 to 6 the balance being nickel and cobalt; the nickel being present in quantities from about 18% to about 40% and the cobalt being present in quantities from about to about 50%; the combined nickel-cobalt content being from about 52% to about 68%.
A consideration of the alloys set forth in the following table will be helpful in understanding our invention.
Percentage by Weight H8111 Alloy No. ness,
Ni Co Cr Mo Be Mn Cu RC 26 30 12 1 6 38 26 25 12 1 6- 28 20 30 25 12 1 6 6 40 3D 20 25 12 1 6 6 30. 5 20 25 12 0. 5 6 6 25 33. 5 20 25 12 0. 7 6 3 25 20 45. 2 28 6 0. 8 19 2O 45. 2 25 6 0. S 3 24 20 41. 2 25 B 0. 8 4 3 24 20 41. 2 22 8 O. 8 4 4 27 19. 8 41. 2 22 8 1. (l 4 4 32 It has been found that both the yield strength and hardness of the base alloy decrease and the melting point rises when the beryllium content is lowered. Alloy 60, for example, will not lose its lustre in dilute lactic acid but it has a hardness value of only C 19 (corresponding to a yield strength of about 60,000 p. s. i.) and therefore would not have suflicient strength for all applications. Furthermore, the melting point is too high to permit its use in a plaster bound invest ment. However, by adding copper, as in alloy 138, the hardness value is increased to C 24 and the yield strength is raised to 78,000 D. s. i. The addition of copper does not substantially afiect the melting which is about 2475 F. If 4% of manganese is added, as in alloy 139 the melting point is reduced to about 2325 F. which is low enough to permit the casting of the alloy in a plaster bound investment. It will also be noted that the manganese addition does not aifect the hardness.
Alloys 19, 20, and 24 further illustrate the effectiveness of copper as a hardener and manganese as a means of reducing the melting point. Thus, alloy 20, which has no copper therein, has a hardness of C 28 and a melting point of 2300 F. By substituting 6% of copper for the 6% of manganese, as in alloy 19, the hard- 4 ness is increased to C 38 and the melting point is raised to about 2375 F. Alloy 24 which contains both manganese and copper retains the high hardness of alloy 19 and has substantially the same melting point (2300 F.) as alloy 20.
A comparison of alloy 24 with alloy 25 indicates how the hardness and melting point may be controlled by manipulating the ratio of nickel to cobalt while keeping the combined content of these two elements constant. Thus alloy 24 with a nickel-cobalt ratio of 1 to 1.5 has a hardness of C 40 and a melting point of about 2300 F. By changing the nickel-cobalt ratio to 1.5 to 1, as in alloy 25, the hardness is decreased to C 35 and the melting point to 2250" F.
In general, it has been found that if the chromium content falls appreciably below 15% there is a marked reduction in the corrosion resistance of the alloy. On the other hand, if it exceeds 30%, an additional chromium rich phase begins to appear in the microstructure and the alloy becomes quite brittle.
Alloys having a molybdenum content as high as 18% have been melted and investigated, but these high molybdenum alloys have a rather high specific gravity which is undesirable in a prosthetic article, and, in remelting, the molybdenum seems to oxidize excessively, even though the beryllium content of the alloy does afford some protection. Therefore, while the upper limit of the molybdenum range is not critical, it has been found that more desirable alloys are obtained when the maximum molybdenum content is limited to 12%. The molybdenum contributes to both the corrosion resistance and the fluidity of the alloy and, while the lower limit of the molybdenum range is not critical it has been found to be approximately 3%.
The beryllium content while small, has a very pronounced effect on the physical properties, the melting point, and the casting characteristics of the alloy. If the beryllium content exceeds 1.2% the concentration of the beryllium intermetallic phase becomes so great that it is visible on the surface of polished specimens of the alloy when they are subjected to the action of a dilute lactic acid solution. By maintaining the beryllium content below this level, loss of lustre is avoided.
The manganese addition required to ofiset the rise in the melting point caused by lowering the beryllium content tends to make the alloy react with the silica of the investment. Unles a certain minimum beryllium content is maintained, the surface condition of the casting becomes so poor that it cannot be used. This minimum is approximately 0.2%.
Manganese in excess of about 8% causes a reaction with the investment, even when the maximum beryllium content is employed, and, for this reason, should be avoided. Furthermore, since the manganese is used partially to oiiset the rise in the melting point associated with a lowering of the beryllium content, the manganese, as a rule, should be present in the lower portion of its range when the beryllium is present in the upper portion of its range, and vice versa.
The copper is added as a hardening agent to offset the drop in yield strength associated with the reduction in beryllium. Therefore, the copper should ordinarily be present in the lower portion in its range when the beryllium is present in the upper portion of its range. Nickel and cobalt are more or less interchangeable in order to vary the yield strength and ductility of the resulting alloy. Thus, a high cobalt content tends to raise the yield strength and usually the melting point, while high nickel, on the other hand, tends to give a softer, lower meltin point alloy. For general applications the preferred ratio of nickel to cobalt has been found to be from 1 to 2, to 1 to 1 /2.
What we claim is:
1. An alloy adapted for use in the manufacture of prosthetic articles and characterized by its retention of a bright surface lustre when highly polished and subjected to the action of dilute lactic acid in concentrations of the order encountered in the human mouth; said all-y comprising a plurality of elements of which the following, in the proportions, by weight, set forth below are the only necessary elements to attain said characteristics:
Percent Chromium 20 to 25 Molybdenum 5 to Beryllium 0.5 to 1.0 Manganese 3 to 6 Copper 3 to 6 and the balance being nickel from 18% to 40% and cobalt from 20% to 50% with a combined nickel and cobalt content from about 52% to about 68%.
2. An alloy adapted for use in the manufacture of prosthetic articles and characterized by its retention of a bright surface lustre when highly polished and subjected to the action of dilute lactic acid in concentrations of the order encountered in the human mouth; said alloy comprising a plurality of elements of which the following, in the proportions, by weight, set forth below are the only necessary elements to attain said characteristics:
Percent Chromium 15 to 27 Molybdenum 3 to 12 Beryllium 0.2 to 1.2 Manganese 2 to 8 Copper 2 to 10 the balance being nickel and cobalt, each between about 5% and about with a combined nickel and cobalt content of at least 42%.
EMIL S. GRIFFITHS. WILLIAM D. CASHlWAN.
REFERENCES CITED The following references are of record in the file of this patent:
UNITED STATES PATENTS

Claims (1)

1. AN ALLOY ADAPTED FOR USE IN THE MANUFACTURE OF PROSTHETIC ARTICLES AND CHARACTERIZED BY ITS RETENTION OF A BRIGHT SURFACE LUSTRE WHEN HIGHLY POLISHED AND SUBJECTED TO THE ACTION OF DILUTE LACTIC ACID IN CONCENTRATIONS OF THE ORDER ENCOUNTERED IN THE HUMAN MOTH; SAID ALLOY COMPRISING A PLURALITY OF ELEMENTS OF WHICH THE FOLLOWING, IN THE PROPORTIONS, BY WEIGHT, SET FORTH BELOW ARE THE ONLY NECESSARY ELEMENTS TO ATTAIN SAID CHARACTERISTICS:
US145598A 1950-02-21 1950-02-21 Alloy adapted for prosthetic articles Expired - Lifetime US2631095A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US145598A US2631095A (en) 1950-02-21 1950-02-21 Alloy adapted for prosthetic articles

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US145598A US2631095A (en) 1950-02-21 1950-02-21 Alloy adapted for prosthetic articles

Publications (1)

Publication Number Publication Date
US2631095A true US2631095A (en) 1953-03-10

Family

ID=22513795

Family Applications (1)

Application Number Title Priority Date Filing Date
US145598A Expired - Lifetime US2631095A (en) 1950-02-21 1950-02-21 Alloy adapted for prosthetic articles

Country Status (1)

Country Link
US (1) US2631095A (en)

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3177074A (en) * 1962-04-23 1965-04-06 Duriron Co Cobalt base alloys
US3727299A (en) * 1971-05-26 1973-04-17 Krupp Gmbh Method for making a dental appliance
US3837838A (en) * 1972-12-18 1974-09-24 M Mohammed High strength, ductile cobalt-base dental alloy
JPS50104122A (en) * 1974-01-24 1975-08-16
JPS533919A (en) * 1976-07-01 1978-01-14 Sankin Ind Co Dental alloy
US4461618A (en) * 1982-01-25 1984-07-24 Johnson & Johnson Dental Products Company Process for producing a dental restoration
EP0149134A2 (en) * 1983-12-20 1985-07-24 Dentsply International, Inc. Nickel based casting alloy
US4592890A (en) * 1983-08-08 1986-06-03 Dentsply Research & Development Corp. Dental prostheses alloy

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1115239A (en) * 1914-02-27 1914-10-27 Samuel W Parr Alloy.
US1572996A (en) * 1920-12-09 1926-02-16 Commentry Fourchambault & Deca Alloy
US1587994A (en) * 1924-11-15 1926-06-08 Alloys Foundry Company Composition of matter for alloy of metals
US1945679A (en) * 1929-04-09 1934-02-06 Metal & Thermit Corp Corrosion resistant alloy
US2048166A (en) * 1931-10-01 1936-07-21 Int Nickel Co Copper-nickel-titanium alloys
US2072911A (en) * 1935-05-17 1937-03-09 Cons Car Heating Co Inc Alloy
US2309136A (en) * 1940-05-04 1943-01-26 Edmund A Steinbock Process for preparing an alloy for cast dentures

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1115239A (en) * 1914-02-27 1914-10-27 Samuel W Parr Alloy.
US1572996A (en) * 1920-12-09 1926-02-16 Commentry Fourchambault & Deca Alloy
US1587994A (en) * 1924-11-15 1926-06-08 Alloys Foundry Company Composition of matter for alloy of metals
US1945679A (en) * 1929-04-09 1934-02-06 Metal & Thermit Corp Corrosion resistant alloy
US2048166A (en) * 1931-10-01 1936-07-21 Int Nickel Co Copper-nickel-titanium alloys
US2072911A (en) * 1935-05-17 1937-03-09 Cons Car Heating Co Inc Alloy
US2309136A (en) * 1940-05-04 1943-01-26 Edmund A Steinbock Process for preparing an alloy for cast dentures

Cited By (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3177074A (en) * 1962-04-23 1965-04-06 Duriron Co Cobalt base alloys
US3727299A (en) * 1971-05-26 1973-04-17 Krupp Gmbh Method for making a dental appliance
US3837838A (en) * 1972-12-18 1974-09-24 M Mohammed High strength, ductile cobalt-base dental alloy
JPS50104122A (en) * 1974-01-24 1975-08-16
JPS5244534B2 (en) * 1974-01-24 1977-11-09
JPS533919A (en) * 1976-07-01 1978-01-14 Sankin Ind Co Dental alloy
JPS5530581B2 (en) * 1976-07-01 1980-08-12
US4461618A (en) * 1982-01-25 1984-07-24 Johnson & Johnson Dental Products Company Process for producing a dental restoration
US4592890A (en) * 1983-08-08 1986-06-03 Dentsply Research & Development Corp. Dental prostheses alloy
EP0149134A2 (en) * 1983-12-20 1985-07-24 Dentsply International, Inc. Nickel based casting alloy
EP0149134A3 (en) * 1983-12-20 1985-08-28 Dentsply International, Inc. Nickel based casting alloy
US4556534A (en) * 1983-12-20 1985-12-03 Dentsply Research & Development Corp. Nickel based casting alloy

Similar Documents

Publication Publication Date Title
EP1266974B1 (en) Gold alloys and master alloys for obtaining them
US2631095A (en) Alloy adapted for prosthetic articles
US2309136A (en) Process for preparing an alloy for cast dentures
US3464817A (en) Alloy composition and method of forming the same
US2156757A (en) Dental casting alloy
US3116145A (en) Tungsten-hafnium alloy casting
US2072911A (en) Alloy
US2795501A (en) Copper base alloys
US2280170A (en) Aluminum alloy
US2089587A (en) Denture
US2947624A (en) High temperature alloy
US2162252A (en) Dental casting alloy
US2720459A (en) Highly wear-resistant zinc base alloy
US2460817A (en) Alloy suitable for use at high temperatures
US1932843A (en) Aluminum alloys
US1946130A (en) Ferrous alloy
US2761778A (en) Alloy
US2072910A (en) Alloy
US2081392A (en) Denture
US2220084A (en) Alloy
US2752242A (en) Copper-nickel-titanium alloy and process for making same
JPS6341975B2 (en)
US2280173A (en) Aluminum alloy
US1932846A (en) Aluminum alloys
US2733991A (en) Alimilnum-magnesiijm casting alloys