Metallic crucibles and methods of forming the same
10100438 ยท 2018-10-16
Assignee
Inventors
Cpc classification
B22F7/008
PERFORMING OPERATIONS; TRANSPORTING
B22F2203/11
PERFORMING OPERATIONS; TRANSPORTING
B22F2302/45
PERFORMING OPERATIONS; TRANSPORTING
B22F2999/00
PERFORMING OPERATIONS; TRANSPORTING
B22F3/1017
PERFORMING OPERATIONS; TRANSPORTING
B22F3/04
PERFORMING OPERATIONS; TRANSPORTING
C30B15/10
CHEMISTRY; METALLURGY
B22F2998/10
PERFORMING OPERATIONS; TRANSPORTING
B22F7/06
PERFORMING OPERATIONS; TRANSPORTING
B22F7/06
PERFORMING OPERATIONS; TRANSPORTING
B22F3/24
PERFORMING OPERATIONS; TRANSPORTING
B22F3/04
PERFORMING OPERATIONS; TRANSPORTING
C30B11/002
CHEMISTRY; METALLURGY
B22F3/1017
PERFORMING OPERATIONS; TRANSPORTING
B22F3/16
PERFORMING OPERATIONS; TRANSPORTING
B22F5/10
PERFORMING OPERATIONS; TRANSPORTING
Y10T117/1024
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
B22F2998/10
PERFORMING OPERATIONS; TRANSPORTING
B22F3/001
PERFORMING OPERATIONS; TRANSPORTING
B22F2999/00
PERFORMING OPERATIONS; TRANSPORTING
B22F5/00
PERFORMING OPERATIONS; TRANSPORTING
B22F2203/11
PERFORMING OPERATIONS; TRANSPORTING
International classification
C30B35/00
CHEMISTRY; METALLURGY
B22F3/04
PERFORMING OPERATIONS; TRANSPORTING
B22F3/24
PERFORMING OPERATIONS; TRANSPORTING
C30B15/10
CHEMISTRY; METALLURGY
C30B11/00
CHEMISTRY; METALLURGY
B22F5/10
PERFORMING OPERATIONS; TRANSPORTING
B22F5/00
PERFORMING OPERATIONS; TRANSPORTING
B22F7/06
PERFORMING OPERATIONS; TRANSPORTING
B22F3/16
PERFORMING OPERATIONS; TRANSPORTING
B22F7/00
PERFORMING OPERATIONS; TRANSPORTING
Abstract
In various embodiments, a precursor powder is pressed into an intermediate volume and chemically reduced, via sintering, to form a metallic shaped article.
Claims
1. A crucible comprising: an inner surface consisting essentially of (i) an alloy of molybdenum and tungsten or (ii) a mixture of molybdenum and tungsten; extending from the inner surface through only a portion of a thickness of the crucible, an interior zone consisting essentially of (i) an alloy of molybdenum and tungsten or (ii) a mixture of molybdenum and tungsten; and an outer surface, opposite the inner surface, consisting essentially of molybdenum.
2. The crucible of claim 1, wherein a tungsten concentration within the interior zone is graded such that the tungsten concentration decreases toward the outer surface of the crucible.
3. The crucible of claim 2, wherein the tungsten concentration within the interior zone is linearly graded.
4. The crucible of claim 2, wherein the tungsten concentration within the interior zone decreases toward the outer surface of the crucible with an exponential dependence.
5. The crucible of claim 2, wherein the tungsten concentration within the interior zone decreases toward the outer surface of the crucible in accordance with the complementary error function.
6. The crucible of claim 1, wherein a total tungsten content within an entirety of the crucible is between approximately 5% and approximately 20% by weight.
7. A method of fabricating a crucible having a target set of final dimensions, the method comprising: pressing a precursor powder into a volume having intermediate dimensions larger than the final dimensions along at least one direction, the precursor powder comprising a compound comprising (i) molybdenum and (ii) a non-metallic chemical species; thereafter, sintering the pressed precursor powder to (i) chemically reduce the precursor powder, (ii) shrink the volume having intermediate dimensions into the crucible having the final dimensions, and (iii) release a non-metallic by-product; cooling the crucible; after cooling the crucible, disposing tungsten on at least one surface of the crucible; and annealing the crucible, thereby at least one of alloying or mixing the tungsten with the molybdenum to form the crucible comprising (i) an inner surface consisting essentially of (a)an alloy of molybdenum and tungsten or (b) a mixture of molybdenum and tungsten, (ii) an outer surface consisting essentially of molybdenum, and (iii) therebetween, an interior zone extending from the inner surface through only a portion of a thickness of the crucible and consisting essentially of (a) an alloy of molybdenum and tungsten or (b) a mixture of molybdenum and tungsten.
8. The method of claim 7, wherein after cooling and before annealing, the crucible has a density less than approximately 95%.
9. The method of claim 7, wherein annealing the crucible comprises: annealing the crucible at a first temperature to diffuse at least a portion of the tungsten into the crucible; and thereafter, annealing the crucible at a second temperature to alloy at least a portion of the tungsten with the molybdenum of the crucible.
10. The method of claim 9, wherein (i) the first temperature is selected from the range of approximately 800 C. to approximately 1200 C., and (ii) the second temperature is selected from the range of approximately 20000 and approximately 2600 C.
11. The method of claim 9, wherein (i) the first temperature is no greater than 1200 C. and (ii) the second temperature is no less than 2000 C.
12. The method of claim 7, wherein disposing the tungsten on at least one surface of the crucible comprises at least one of applying a slurry or spray deposition.
13. The method of claim 7, wherein the precursor powder comprises molybdenum dimolybdate.
14. The method of claim 13, wherein sintering the pressed powder comprises: sintering at a first temperature to chemically reduce ammonium dimolybdate to molybdenum trioxide; thereafter, sintering at a second temperature to chemically reduce molybdenum trioxide to molybdenum dioxide; thereafter, sintering at a third temperature to chemically reduce molybdenum dioxide to molybdenum; and thereafter, sintering at a fourth temperature to densify molybdenum, thereby forming the crucible.
15. The method of claim 14, wherein (i) the fourth temperature is greater than the third temperature, (ii) the third temperature is greater than the second temperature, (iii) the second temperature is greater than the first temperature, and (iv) the first temperature is selected from the range of approximately 100 C. to approximately 650 C.
16. The method of claim 14, wherein (i) the first temperature is selected from the range of approximately 450 C. to approximately 650 C., (ii) the second temperature is selected from the range of approximately 500 C. to approximately 700 C., (iii) the third temperature is selected from the range of approximately 800 C. to approximately 1000 C., and (iv) the fourth temperature is selected from the range of approximately 1450 C. to approximately 1800 C.
17. The method of claim 7, wherein (i) the pressed precursor powder is sintered in an atmosphere consisting essentially of hydrogen, and (ii) the crucible is annealed in an atmosphere consisting essentially of hydrogen.
18. The method of claim 7, wherein the non-metallic by-product comprises ammonia.
19. The method of claim 7, wherein sintering the pressed precursor powder comprises: heating the pressed precursor powder at a first temperature to (i) chemically reduce the pressed precursor powder to an intermediate product comprising (a) molybdenum and (b) a second non-metallic chemical species, and (ii) release the non-metallic by-product; and thereafter, heating the intermediate product at a second temperature higher than the first temperature to (i) chemically reduce the intermediate product to molybdenum and (ii) release a second non-metallic by-product.
20. The method of claim 19, wherein the second non-metallic by-product and the non-metallic by-product are different.
21. The method of claim 19, wherein (i) the non-metallic by-product comprises ammonia and (ii) the second non-metallic by-product comprises water vapor.
22. The method of claim 7, wherein a tungsten concentration within the interior zone is graded such that the tungsten concentration decreases toward the outer surface of the crucible.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
(1) In the drawings, like reference characters generally refer to the same parts throughout the different views. Also, the drawings are not necessarily to scale, emphasis instead generally being placed upon illustrating the principles of the invention. In the following description, various embodiments of the present invention are described with reference to the following drawings, in which:
(2)
(3)
(4)
(5)
(6)
DETAILED DESCRIPTION
(7) Referring to the cross-section depicted in
(8) After pressing, the pressed precursor powder 100 is sintered to both reduce the precursor powder 100 into substantially pure metal (e.g., Mo) or an alloy or mixture of substantially pure metals (e.g., MoW) and fuse the resulting metal particulates into a solid article. In an exemplary embodiment of the invention, the pressed precursor powder 100 is sintered in a multiple-step process in a reducing atmosphere, e.g., hydrogen gas. For example, in embodiments in which precursor powder 100 includes or consists essentially of ADM, the following multiple-step sintering process may be performed in a furnace and in a hydrogen atmosphere. The pressed powder 100 may first be ramped to approximately 550 C. over, e.g., 30 minutes, and then held at approximately 550 C. for, e.g., 5 hours, during which the ADM is reduced into Mo trioxide. During this step, water vapor and ammonia form as by-products and are removed from the furnace via, e.g., a burning stack in the presence of hydrogen. The temperature may then be raised to approximately 600 C. over, e.g., 30 minutes, and then held at approximately 600 C. for, e.g., 6 hours. During this portion of the cycle, the Mo trioxide is reduced to Mo dioxide, and water vapor formed as a by-product is again exhausted. The temperature may then be ramped to approximately 900 C. over, e.g., 3 hours, and then held at approximately 900 C. for, e.g., 2 hours, during which time the Mo dioxide is reduced to substantially pure Mo and by-product water vapor is exhausted from the furnace. The temperature of the furnace may subsequently be raised to a temperature ranging between approximately 1450 C. and approximately 1800 C. over, e.g., 12-15 hours, at which point the substantially pure Mo is sintered at the selected temperature for, e.g., 10 hours. As shown in the cross-sectional view of
(9) After the sintering at the final elevated temperature, the article 200 may undergo a controlled cool-down cycle. For example, the temperature of the furnace may be ramped back down to approximately 500 C. over, e.g., 30 minutes, and held at approximately 500 C. for, e.g., 5 hours. Thereafter, the atmosphere within the furnace may be changed from hydrogen to one including or consisting essentially of nitrogen for additional dwell time (e.g., approximately 4 hours at approximately 500 C.) and the final cool-down to room temperature. In some embodiments of the present invention, following cool-down the article 200 is itself utilized as a crucible for any of a variety of purposes, e.g., production of sapphire single crystals. As described above, at this stage the article 200 may be fairly porous. For example, the density of article 200 may be between approximately 90% and approximately 95%. Such density may be increased if desired by subjecting article 200 to more aggressive (e.g., higher temperature and/or longer time) sintering during the above-described process and/or in a subsequent sintering process (utilizing, for example, hot isostatic pressing). After such additional treatment, the density of the treated article 200 may be between approximately 97% and approximately 99%.
(10) In other embodiments of the invention, article 200 is merely a pre-crucible or pre-article that is further processed for the improvement of various properties thereof. For example, as depicted in the cross-sectional view of
(11) As shown in the cross-sectional views of
(12) Embodiments of the invention may be utilized to form articles other than crucibles. As shown in
(13) While the articles of
(14) The terms and expressions employed herein are used as terms and expressions of description and not of limitation, and there is no intention, in the use of such terms and expressions, of excluding any equivalents of the features shown and described or portions thereof. In addition, having described certain embodiments of the invention, it will be apparent to those of ordinary skill in the art that other embodiments incorporating the concepts disclosed herein may be used without departing from the spirit and scope of the invention. Accordingly, the described embodiments are to be considered in all respects as only illustrative and not restrictive.