US1588473A - Method of making carborundum structures - Google Patents
Method of making carborundum structures Download PDFInfo
- Publication number
- US1588473A US1588473A US61633A US6163325A US1588473A US 1588473 A US1588473 A US 1588473A US 61633 A US61633 A US 61633A US 6163325 A US6163325 A US 6163325A US 1588473 A US1588473 A US 1588473A
- Authority
- US
- United States
- Prior art keywords
- pieces
- carborundum
- furnace
- uniting
- structures
- 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
- 229910010271 silicon carbide Inorganic materials 0.000 title description 28
- 238000004519 manufacturing process Methods 0.000 title description 4
- 238000010438 heat treatment Methods 0.000 description 14
- 238000000034 method Methods 0.000 description 13
- 239000000203 mixture Substances 0.000 description 10
- HBMJWWWQQXIZIP-UHFFFAOYSA-N silicon carbide Chemical compound [Si+]#[C-] HBMJWWWQQXIZIP-UHFFFAOYSA-N 0.000 description 9
- 230000001590 oxidative effect Effects 0.000 description 5
- 239000013078 crystal Substances 0.000 description 4
- 239000000463 material Substances 0.000 description 4
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 3
- 229910052799 carbon Inorganic materials 0.000 description 3
- 239000003575 carbonaceous material Substances 0.000 description 3
- RTZKZFJDLAIYFH-UHFFFAOYSA-N Diethyl ether Chemical compound CCOCC RTZKZFJDLAIYFH-UHFFFAOYSA-N 0.000 description 2
- 239000000571 coke Substances 0.000 description 2
- 239000004576 sand Substances 0.000 description 2
- 238000002485 combustion reaction Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 239000003292 glue Substances 0.000 description 1
- 238000000465 moulding Methods 0.000 description 1
- 239000002245 particle Substances 0.000 description 1
Images
Classifications
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B35/00—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
- C04B35/515—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on non-oxide ceramics
- C04B35/56—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on non-oxide ceramics based on carbides or oxycarbides
- C04B35/565—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on non-oxide ceramics based on carbides or oxycarbides based on silicon carbide
- C04B35/573—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on non-oxide ceramics based on carbides or oxycarbides based on silicon carbide obtained by reaction sintering or recrystallisation
Definitions
- This invention relates to a method of making carborundum structures.
- my invention may be embodied in a variety of forms, in its preferred embodiment it is applied to the manufacture of monolithic carborundum linings for the in-- terior of furnaces such as the lining of the combustion or heating chamber of a rever beratory furnace.
- Such linings serve to conduct heat to the mufile and at the same time preventescape of any gas fromthe heat ng chamber to the -muflie chamber.
- lining of this character which is free'from joints or cracks is, of course, desirable. -When, however, attempts have been made to make such a lining without joints or cracks by mak-,
- FIG. 1 is a diagrammatic sectional view of a portion of the interior of a recrystallizing furnace, showing a.
- Fig. 2 is a diagrammatic transverse section taken on the line 22 of Fig. 1 and Figs. 3 and 4 are views similar respectively to Figs. 1 and 2, but showing four carborundum plates in position to be joined to form a mufiie open atthe ends.
- the recrystallizing furnace contains a heating element d surrounded by carborundum mixture which 'is composed of coke, sand and sawdust in the proper proportions and the articles to be recrystallized are placed in the proximity of the heating element d so that when the furnace has been run the crystalline form of carborundum will surround the article to be recrystallized as shown by the dottedline e. If now, as m the case of Figs. 1 and 2, the plates at and b m The object ture as in the ordinary way of running a carsilicon carbide which comprises heating.
- These plates such as a and b may be either placed in the furnace in the green form, that is to say finely crushed carborundum crystals bonded together with some temporary bond such as glue, in which case only the plate 6 and the part of plate a inside the crystalline zone whose boundary is 6 would be recrystallized. The plate outside the boundary e would be still in an unrecrystallized condition, that is to say the crystals in the plate at this point would still retain the.
- the plates a andb might also be first recrystallized separately or the plate (1 might be recrystallized and the plate I) might be a green plate. This would depend entirely upon the size, shape and convenience of handling the plates a and b.
- silicon carbide which consists in placing said pieces in substantial contact with one another with carbonaceous material between their contacting surfaces, and raising the temperature of said surfaces to approximately 1800 C. or over by a flow of heat in a direction substantially at right angles to said surfaces.
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- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Ceramic Engineering (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Manufacturing & Machinery (AREA)
- Materials Engineering (AREA)
- Structural Engineering (AREA)
- Organic Chemistry (AREA)
- Ceramic Products (AREA)
- Crystals, And After-Treatments Of Crystals (AREA)
Description
' t0 hjoined June 15 1926. 1,588,473
J. KELLEHER METHOD MAKING CARBORUNDUM STRUCTURES Filed Oofi. 10, 1925 @31 1 Gwen @013 Patented June 15, 1926.
' UNITED STATES" JAMES KELLEHER, OF CHIPPAWA, ONTARIO, CANADA, A SSIGNOR TO HARPER ELE C- TRIO FURNACE CORPORATION, A CORPORATION OF NEW YORK.
METHOD OF MAKING CARBORUNDUM- STRUCTURES.
'Applicatton filed October 10,1925. Serial No. 61,683.
This invention relates to a method of making carborundum structures.
lVhile my invention may be embodied in a variety of forms, in its preferred embodiment it is applied to the manufacture of monolithic carborundum linings for the in-- terior of furnaces such as the lining of the combustion or heating chamber of a rever beratory furnace. Such linings serve to conduct heat to the mufile and at the same time preventescape of any gas fromthe heat ng chamber to the -muflie chamber. lining of this character which is free'from joints or cracks is, of course, desirable. -When, however, attempts have been made to make such a lining without joints or cracks by mak-,
nace, preferably in such a manner that the.
surface of contact is at right angles to the flow of heat in the furnace, and if a small amount of loose silicon carbide mix be placed between the two pieces, then upon heating the material to the recrystallizing temperature these two pieces will be found to be joined together, apparently by a growth of crystal from one piece to the other. In this manner large and complicated sections may be built up. 1
While a carborundum mix such as coke, sawdust and sand may be used between the surfaces which it is desired to join, this is not absolutelyessential as fine carborundum grains Wlll act in a similar manner, and in;
fact if two pieces of carborundum ware re crystallized, or-to be recrystallized, be placed in the furnace in close proximity without any bonding material whatever, a union may be effected. I. however, preferably use some bonding material. To effect the union I find that it is preferable to have'a certain amount of carbon present and the atmosphere in which the pieces are heated should be non-oxidizing. The temperature to which they are heated should be a proximately 18009 C. or over. W'hile have mentioned a recrystallizing furnace as the furnace in which the heating is efiected, it is obvious that furnaces of other kinds may be em loyed.
In eating green ware for the purpose of recrystallizing the same, it is customary to embed the ware in carborundum mix. lVhen' large structures of more or less complicated form are made by joining portions of the structure in the manner above described, it is preferable to recrystallize the various parts of the structure before joining the parts to ether, because this avoids the necessity o embedding the entire structure in mix. When the'recrystallized parts" are joined, I may then embed merely the joint in the mix.
In the accompanying drawing, which il-' lustrates one way in which my invention may be carried out, Fig. 1 is a diagrammatic sectional view of a portion of the interior of a recrystallizing furnace, showing a.
heater and two plates ofcarborundum in position to be joined to one another.
Fig. 2 is a diagrammatic transverse section taken on the line 22 of Fig. 1 and Figs. 3 and 4 are views similar respectively to Figs. 1 and 2, but showing four carborundum plates in position to be joined to form a mufiie open atthe ends.
The recrystallizing furnace contains a heating element d surrounded by carborundum mixture which 'is composed of coke, sand and sawdust in the proper proportions and the articles to be recrystallized are placed in the proximity of the heating element d so that when the furnace has been run the crystalline form of carborundum will surround the article to be recrystallized as shown by the dottedline e. If now, as m the case of Figs. 1 and 2, the plates at and b m The object ture as in the ordinary way of running a carsilicon carbide which comprises heating.
borundum furace and the furnace run for its correct length of time and energy input and when the plates 6 and a are removed it will be found that they have joined together due to crystalline growth between the two plates at the joint 0.
These plates such as a and b may be either placed in the furnace in the green form, that is to say finely crushed carborundum crystals bonded together with some temporary bond such as glue, in which case only the plate 6 and the part of plate a inside the crystalline zone whose boundary is 6 would be recrystallized. The plate outside the boundary e would be still in an unrecrystallized condition, that is to say the crystals in the plate at this point would still retain the.
original size of the crystal particles as used in molding the green plate and would not be bonded together. i
The plates a andb might also be first recrystallized separately or the plate (1 might be recrystallized and the plate I) might be a green plate. This would depend entirely upon the size, shape and convenience of handling the plates a and b.
In the form shown in Figs. 3 and 4 the procedure would be similar to the one already described in connection with Flgs. 1
' and 2. The plates at and 6?) would be first joined and then the hollow trough would be turned upside down and the plate a would.
them in. contact with one another to a temperature of approximately 1800 C. or over, in a non-oxidizing atmosphere.
2.-The method of uniting two pieces of recrystallized silicon carbide which comprises heating them in contact with one another to a temperature of approximately 1800 C. or over in a non-oxidizing atmos- .phere in the presence of carbon.
I 3. The method of uniting and recrystallizing two pieces of molded unrecrystallized silicon carbide which comprises heating them in contact with one another to a temperature of approximately 1800 C. or over,]
1n a non-oxidizing atmosphere.
4. The method of uniting and recrystallizing two pieces of molded unrecrystallized silicon carbide which comprises heating them in contact with one another to a temperature of approximately 1800 C. or over in a non-oxidizing atmosphere in the pres: ence of carbon.
5. The method of uniting two pieces of silicon carbide which consists of placing said pieces in substantial contact with one another with finely divide-d carborundum between their contacting faces, and heating the pieces while so positioned to approximately 1800 G.;or over.
6. The method of uniting two pieces of silicon carbide which consists of placing said pieces in substantial contact with one another with carborundum mix between their contacting faces, and heating the pieces while so positioned to approximately 1800 C. or-over.'
7. The method of uniting two pieces of silicon carbide which consists of placing said pieces in substantial contact with one another with carbonaceous material between their contacting faces, and heating the pieces whileso positioned to approximately 1800 C. or over.
silicon carbide which consists in placing said pieces in substantial contact with one another with carbonaceous material between their contacting surfaces, and raising the temperature of said surfaces to approximately 1800 C. or over by a flow of heat in a direction substantially at right angles to said surfaces.
9. The method of uniting two pieces of silicon carbide which consists in placing said pieces in substantial contact with one another with carborundum' material "between their contacting surfaces, and raising the temperature of said surfaces to a proximately,'1800 C. or over by a flow of eat in a direction substantially'at right angles to said surfaces.
10. The method of uniting and recrystallizing two pieces of molded unrecrystallized sil con carbide which consists in placing said pieces in substantial contact with one another with carbonaceous material between their. contacting surfaces and raising thev until the same is converted into crystalline carborundum. v V p 12. The method of uniting and recrystallizin two pieces of unrecrystallized carborun um which consists in mounting said I pieces in a furnace in contact with one another, embedding the pieces in carborundum .8. The method of uniting two pieces of 9 7 mix and heating the furnace until the mix is converted into crystalline carborunduin.
13. The method of forming a structure by uniting several pieces of carborundum which consists in placing a plurality of said pieces in contact in a furnace and embedding the portions of said pieces adjacent their contacting surfaces in carborundum mix, heatborundum in contact vwith the structure so formed and uniting said other piece thereto by embedding and heating as above set forth.
JAMES KELLEHER.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US61633A US1588473A (en) | 1925-10-10 | 1925-10-10 | Method of making carborundum structures |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US61633A US1588473A (en) | 1925-10-10 | 1925-10-10 | Method of making carborundum structures |
Publications (1)
Publication Number | Publication Date |
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US1588473A true US1588473A (en) | 1926-06-15 |
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US61633A Expired - Lifetime US1588473A (en) | 1925-10-10 | 1925-10-10 | Method of making carborundum structures |
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Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2568157A (en) * | 1951-09-18 | Process of making refractory bodies | ||
US2637890A (en) * | 1950-09-11 | 1953-05-12 | Stark Ceramics Inc | Method of making metallic and clay articles |
US3171871A (en) * | 1960-07-19 | 1965-03-02 | Norton Co | Method of making electrical heater bars |
FR2315353A1 (en) * | 1975-06-25 | 1977-01-21 | Norton Co | GAS-TIGHT SILICON CARBIDE PART |
US6440242B1 (en) * | 1998-12-22 | 2002-08-27 | Japan Cell, Co., Ltd. | Method of joining synthetic corundum, method of manufacturing synthetic corundum cell, and synthetic corundum cell |
US6858274B2 (en) | 1998-12-22 | 2005-02-22 | Rion Co., Ltd. | Synthetic corundum cell |
-
1925
- 1925-10-10 US US61633A patent/US1588473A/en not_active Expired - Lifetime
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2568157A (en) * | 1951-09-18 | Process of making refractory bodies | ||
US2637890A (en) * | 1950-09-11 | 1953-05-12 | Stark Ceramics Inc | Method of making metallic and clay articles |
US3171871A (en) * | 1960-07-19 | 1965-03-02 | Norton Co | Method of making electrical heater bars |
FR2315353A1 (en) * | 1975-06-25 | 1977-01-21 | Norton Co | GAS-TIGHT SILICON CARBIDE PART |
US6440242B1 (en) * | 1998-12-22 | 2002-08-27 | Japan Cell, Co., Ltd. | Method of joining synthetic corundum, method of manufacturing synthetic corundum cell, and synthetic corundum cell |
US6858274B2 (en) | 1998-12-22 | 2005-02-22 | Rion Co., Ltd. | Synthetic corundum cell |
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