US3117001A - Crain refinement of beryllium with tungsten carbide and titanium diboride - Google Patents
Crain refinement of beryllium with tungsten carbide and titanium diboride Download PDFInfo
- Publication number
- US3117001A US3117001A US859617A US85961759A US3117001A US 3117001 A US3117001 A US 3117001A US 859617 A US859617 A US 859617A US 85961759 A US85961759 A US 85961759A US 3117001 A US3117001 A US 3117001A
- Authority
- US
- United States
- Prior art keywords
- beryllium
- tungsten carbide
- titanium diboride
- refinement
- crain
- 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
Links
Images
Classifications
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C32/00—Non-ferrous alloys containing at least 5% by weight but less than 50% by weight of oxides, carbides, borides, nitrides, silicides or other metal compounds, e.g. oxynitrides, sulfides, whether added as such or formed in situ
- C22C32/0047—Non-ferrous alloys containing at least 5% by weight but less than 50% by weight of oxides, carbides, borides, nitrides, silicides or other metal compounds, e.g. oxynitrides, sulfides, whether added as such or formed in situ with carbides, nitrides, borides or silicides as the main non-metallic constituents
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C25/00—Alloys based on beryllium
Definitions
- the present invention relates to the grain refinement of as-cast beryllium and more particularly relates to an inoculation process whereby beryllium of fine grain structure is readily and conveniently produced. Even more specifical y, my invention relates to the inoculation of molten beryllium with tungsten carbide or titanium diboride, or mixtures thereof to result in a fine grain structure in the as-cast metal.
- as-cast beryllium is characterized by a coarse rain structure, and that because of this, a melt thereof so prepared is characterized by poor physical and metallurgical properties.
- the brittleness of the metal may be substantially directly correlated with the relative coarseness of the grains comprising the as-cast ingot. Not only does the brittleness result, but furthermore, there also are present serious strength defects.
- as-cast beryllium which is characterized by exceptionally fine grain structure and improved physical properties resulting therefrom may be produced by the inoculation of beryllium prior to the casting thereof with small amounts of tungsten carbide or titanium di'ooride or mixtures thereof.
- Such inoculating agents act as seeds for crystal growth phenomena as the molten beryllium cools from a liquid to a solid.
- Such seeds are selected as to be capable of being wetted by the molten beryllium.
- the inoculants as hereinafter set out are added to the molten beryllium prior to the solidification thereof in the refined grain structure.
- a primary object of my invention is to provide a process for the grain refinement of as-cast beryllium.
- a more specific object of my invention is to improve the grain structure of as-cast beryllium by inoculating molten beryllium metal with small amounts of tungsten carbide, titanium diboride, or mixtures thereof.
- a further object of my invention is to provide a novel composition of matter, namely fine grain beryllium metal inoculated with small amounts of material selected from the group consisting of tungsten carbide, titanium diboride and mixtures thereof.
- FIGURE 1 is a photograph of an unalloyed beryllium button showing a single beryllium grain in cross section. Such photograph was taken with polarized light after the button was etched in hydrofluoric acid solution in 95% ethanol. The magnification is 5.5 X;
- FIGURE 2 is a photograph of an unalloyed beryllium fragment illustrating the typical coarse grains found therein. The photograph was taken by polarized light, but in this particular instance the button was unetched. Magnification is 5.5 X;
- FEGURE 3 is a photograph of a beryllium button inoculated at the bottom surface thereof with titanium diboride. Polarized light, unetched, 5.5
- FIGURE 4 is a photograph of a beryllium button, inoculated at tr e bottom surface thereof with tungsten carbide. Polarized light, unetched, 5.5 X;
- FIGURE 5 is a photograph of the same material as set out in FIGURE 4 except that the magnification is 25X.
- the as-cast beryllium made in accordance with the teachings of the prior art has a coarse grain structure and is known to skilled metallurgists, such coarseness of grains is indicative of poor physical and metallurgical properties of the melt.
- FIGURES 3, 4, and 5 which disclose the inoculated beryl liurn, it is seen that there results a considerable improvement and refinement of the beryllium grains at the inoculated surface.
- the inoculants may be added to the beryllium in the molten state in amounts from 0.1% to 3% by weight to provide the grain refinement improvements hereinabove indicated. I have most successfully employed such inoculants in particulate form of about -300 mesh. Ultrafine powders should not be employed since the materials should not completely dissolve in the molten beryllium if they are to act as seeds thereof.
- the seed powders may be added to the molten beryllium in a number of ways. For example, in making the melts demonstrated in FIGURES 3-5, commercial grade beryllium pieces were first consolidated into a button by resistance melting. The button was then positioned atop the inoculant powder and the composite remelted again by resistance melting. This gave the results as illustrated.
- Another means of inoculating comprises pouring the molten beryllium into a mold which is lined with inoculant powder.
- Other equivalent means are deemed within the scope of my invention.
- a composition consisting essentially of from 0.1% to 3% by weight of a material selected from the group consisting of tungsten carbide, titanium diboride and mixtures thereof, balance beryllium.
- a composition consisting essentially of from 0.1% to 3% by weight of tungsten carbide, balance beryllium.
- a composition consisting essentially of from 0.1% to 3% by weight of titanium diboride, balance beryllium.
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Manufacture And Refinement Of Metals (AREA)
Description
Jan. 7, 1964 F. A. CROSSLEY 3,117,001
GRAIN REFINEMENT OF BERYLLIUM WITH TUNGSTEN CARBIDE AND TITANIUM DIBORIDE 2 Sheets-Sheet 1 Filed Dec. 15, 1959 [27 2 511 [LE P flax 2k /7. crqss/ey M 1 g z q a M 9 Jan. 7, 1964 F. A. CROSSLEY 3,117,001
GRAIN REFINEMENT OF BERYLLIUM WITH TUNGSTEN CARBIDE AND TITANIUM DIBORIDE Filed Dec. 15, 1959 2 Sheets-Sheet 2 [Yr En [27F Patented Jan. 19%4 The present invention relates to the grain refinement of as-cast beryllium and more particularly relates to an inoculation process whereby beryllium of fine grain structure is readily and conveniently produced. Even more specifical y, my invention relates to the inoculation of molten beryllium with tungsten carbide or titanium diboride, or mixtures thereof to result in a fine grain structure in the as-cast metal.
it is known by those skilled in the art to which the present invention most closely pertains that as-cast beryllium is characterized by a coarse rain structure, and that because of this, a melt thereof so prepared is characterized by poor physical and metallurgical properties. In fact, for example, the brittleness of the metal may be substantially directly correlated with the relative coarseness of the grains comprising the as-cast ingot. Not only does the brittleness result, but furthermore, there also are present serious strength defects. It is to the reduction of beryllium grain size and the refinement of the grains thereof, along with the physical and metallurgical improvements of the as-cast material that my invention is primarily directed, and as is set out in greater detail below, by practicing the invention as herein taught and claimed, marked improvements in beryllium structure and properties are readily achieved. Such improvements and the utility of my invention are illustrated in the photographs accompanying the pres nt specification.
I have discovered that as-cast beryllium which is characterized by exceptionally fine grain structure and improved physical properties resulting therefrom may be produced by the inoculation of beryllium prior to the casting thereof with small amounts of tungsten carbide or titanium di'ooride or mixtures thereof. Such inoculating agents act as seeds for crystal growth phenomena as the molten beryllium cools from a liquid to a solid. Such seeds are selected as to be capable of being wetted by the molten beryllium. The inoculants as hereinafter set out are added to the molten beryllium prior to the solidification thereof in the refined grain structure.
Accordingly, a primary object of my invention is to provide a process for the grain refinement of as-cast beryllium.
A more specific object of my invention is to improve the grain structure of as-cast beryllium by inoculating molten beryllium metal with small amounts of tungsten carbide, titanium diboride, or mixtures thereof.
A further object of my invention is to provide a novel composition of matter, namely fine grain beryllium metal inoculated with small amounts of material selected from the group consisting of tungsten carbide, titanium diboride and mixtures thereof.
Other objects, features and advantages of my invention will become apparent to those skilled in this particular art from the following detailed disclosure thereof and the attached photographs which illustrate the beneficial results of my invention and wherein:
FIGURE 1 is a photograph of an unalloyed beryllium button showing a single beryllium grain in cross section. Such photograph was taken with polarized light after the button was etched in hydrofluoric acid solution in 95% ethanol. The magnification is 5.5 X;
FIGURE 2 is a photograph of an unalloyed beryllium fragment illustrating the typical coarse grains found therein. The photograph was taken by polarized light, but in this particular instance the button was unetched. Magnification is 5.5 X;
FEGURE 3 is a photograph of a beryllium button inoculated at the bottom surface thereof with titanium diboride. Polarized light, unetched, 5.5
FIGURE 4 is a photograph of a beryllium button, inoculated at tr e bottom surface thereof with tungsten carbide. Polarized light, unetched, 5.5 X;
FIGURE 5 is a photograph of the same material as set out in FIGURE 4 except that the magnification is 25X.
Referring first to FIGURES 1 and 2, it is seen that the as-cast beryllium made in accordance with the teachings of the prior art has a coarse grain structure and is known to skilled metallurgists, such coarseness of grains is indicative of poor physical and metallurgical properties of the melt.
In contradistinction to the coarseness of the grain structure of the unalloyed as-cast beryllium, referring next to FIGURES 3, 4, and 5 which disclose the inoculated beryl liurn, it is seen that there results a considerable improvement and refinement of the beryllium grains at the inoculated surface.
The inoculants may be added to the beryllium in the molten state in amounts from 0.1% to 3% by weight to provide the grain refinement improvements hereinabove indicated. I have most successfully employed such inoculants in particulate form of about -300 mesh. Ultrafine powders should not be employed since the materials should not completely dissolve in the molten beryllium if they are to act as seeds thereof.
The seed powders may be added to the molten beryllium in a number of ways. For example, in making the melts demonstrated in FIGURES 3-5, commercial grade beryllium pieces were first consolidated into a button by resistance melting. The button was then positioned atop the inoculant powder and the composite remelted again by resistance melting. This gave the results as illustrated.
Another means of inoculating comprises pouring the molten beryllium into a mold which is lined with inoculant powder. Other equivalent means are deemed within the scope of my invention.
It will be understood that modifications and variations may be effected wtihout departing from the spirit or scope of the novel concepts of my invention.
I claim as my invention:
1. A composition consisting essentially of from 0.1% to 3% by weight of a material selected from the group consisting of tungsten carbide, titanium diboride and mixtures thereof, balance beryllium.
2. A composition consisting essentially of from 0.1% to 3% by weight of tungsten carbide, balance beryllium.
3. A composition consisting essentially of from 0.1% to 3% by weight of titanium diboride, balance beryllium.
References Cited in the file of this patent UNITED STATES PATENTS 2,791,025 Krefeld et al. May 7, 1957 2,793,949 Imich May 28, 1957 2,911,297 Florenz Nov. 3, 1959 2,942,335 Wellborn June 28, 1960 OTHER REFERENCES Aluminum Alloy Castings, Carrington, ublished by
Claims (1)
1. A COMPOSITION CONSISTING ESSENTIALLY OF FROM 0.1% TO 3% BY WEIGHT OF A MATERIAL SELECTED FROM THE GROUP CONSISTING OF TUNGSTEN CARBIDE, TITANIUM DIBORIDE AND MIXTURES THEREOF, BALANCE BERYLLIUM.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US859617A US3117001A (en) | 1959-12-15 | 1959-12-15 | Crain refinement of beryllium with tungsten carbide and titanium diboride |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US859617A US3117001A (en) | 1959-12-15 | 1959-12-15 | Crain refinement of beryllium with tungsten carbide and titanium diboride |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US3117001A true US3117001A (en) | 1964-01-07 |
Family
ID=25331344
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US859617A Expired - Lifetime US3117001A (en) | 1959-12-15 | 1959-12-15 | Crain refinement of beryllium with tungsten carbide and titanium diboride |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US3117001A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4306907A (en) * | 1979-03-29 | 1981-12-22 | Charles Stark Draper Laboratory, Inc. | Age hardened beryllium alloy and cermets |
| US4471028A (en) * | 1981-05-14 | 1984-09-11 | Pioneer Electronic Corporation | Honeycomb core diaphragm |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2791025A (en) * | 1951-09-14 | 1957-05-07 | Deutsche Edelstahlwerke Ag | Sintered hard metals |
| US2793949A (en) * | 1950-12-18 | 1957-05-28 | Imich Georges | Method of preparing composite products containing metallic and non-metallic materials |
| US2911297A (en) * | 1956-05-05 | 1959-11-03 | Hugo Wachenfeld | Processes for the introduction of alloying constituents into metal melts |
| US2942335A (en) * | 1955-02-03 | 1960-06-28 | Firth Sterling Inc | Carbide metal |
-
1959
- 1959-12-15 US US859617A patent/US3117001A/en not_active Expired - Lifetime
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2793949A (en) * | 1950-12-18 | 1957-05-28 | Imich Georges | Method of preparing composite products containing metallic and non-metallic materials |
| US2791025A (en) * | 1951-09-14 | 1957-05-07 | Deutsche Edelstahlwerke Ag | Sintered hard metals |
| US2942335A (en) * | 1955-02-03 | 1960-06-28 | Firth Sterling Inc | Carbide metal |
| US2911297A (en) * | 1956-05-05 | 1959-11-03 | Hugo Wachenfeld | Processes for the introduction of alloying constituents into metal melts |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4306907A (en) * | 1979-03-29 | 1981-12-22 | Charles Stark Draper Laboratory, Inc. | Age hardened beryllium alloy and cermets |
| US4471028A (en) * | 1981-05-14 | 1984-09-11 | Pioneer Electronic Corporation | Honeycomb core diaphragm |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US4140555A (en) | Nickel-base casting superalloys | |
| CN103421991B (en) | A kind of Composite metamorphic cast aluminum alloy and its preparation method and application | |
| CN110157935B (en) | Al-V-B refiner for casting aluminum-silicon alloy, its preparation method and application | |
| EP2401411B1 (en) | Process for producing improved grain refining aluminium-titanium-boron master alloys for aluminum foundry alloys | |
| CN106609331B (en) | High-ductility diecast magnesium alloy and its manufacturing process | |
| CN101781720A (en) | Preparation method of Mg2Si reinforced magnesium alloy | |
| CN109402455B (en) | Magnetic particle reinforced aluminum matrix composite material and preparation method thereof | |
| US10494699B2 (en) | Method of refining aluminum alloy | |
| CN107815575A (en) | A kind of magnesium aluminum alloy casting ingot | |
| CN107858574A (en) | A kind of weak texture wrought magnesium alloy of multielement complex intensifying and preparation method thereof | |
| CA1045827A (en) | Grain refining of aluminum | |
| Telli et al. | Effect of antimony additions on hardness and tensile properties of directionally solidified Al–Si eutectic alloy | |
| Kuz'min et al. | Production of primary silumins ingots modified with strontium | |
| US3117001A (en) | Crain refinement of beryllium with tungsten carbide and titanium diboride | |
| CN114231777B (en) | Bromine-containing refining agent for rapid sedimentation rare earth magnesium alloy, preparation method and application | |
| CN111304509A (en) | A kind of refined magnesium alloy by adding VN particles and preparation method thereof | |
| CN100389221C (en) | High fluidity lost foam casting magnesium alloy and its melting method | |
| EP2295608B1 (en) | Aluminium-based grain refiner | |
| CN106011567A (en) | Magnesium alloy casting and preparation method thereof | |
| US2841490A (en) | Method for making improved gray cast iron | |
| US4420460A (en) | Grain refinement of titanium alloys | |
| US2620270A (en) | Method of improving magnesium and the binary magnesium-base alloy of magnesium and manganese | |
| US2628899A (en) | Aluminum-magnesium casting alloys | |
| US2399104A (en) | Process for producing castings of aluminum-beryllium alloys | |
| US3969160A (en) | High-strength ductile uranium alloy |