US2482580A - Method of making fired vitreous - Google Patents
Method of making fired vitreous Download PDFInfo
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- US2482580A US2482580A US2482580DA US2482580A US 2482580 A US2482580 A US 2482580A US 2482580D A US2482580D A US 2482580DA US 2482580 A US2482580 A US 2482580A
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- alumina
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- 238000004519 manufacturing process Methods 0.000 title description 9
- PNEYBMLMFCGWSK-UHFFFAOYSA-N aluminium oxide Inorganic materials [O-2].[O-2].[O-2].[Al+3].[Al+3] PNEYBMLMFCGWSK-UHFFFAOYSA-N 0.000 description 48
- 239000000203 mixture Substances 0.000 description 36
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N Silicium dioxide Chemical class O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 description 21
- 239000000126 substance Substances 0.000 description 21
- 239000012212 insulator Substances 0.000 description 17
- TWNQGVIAIRXVLR-UHFFFAOYSA-N oxo(oxoalumanyloxy)alumane Chemical compound O=[Al]O[Al]=O TWNQGVIAIRXVLR-UHFFFAOYSA-N 0.000 description 11
- 238000010304 firing Methods 0.000 description 10
- 230000006835 compression Effects 0.000 description 9
- 238000007906 compression Methods 0.000 description 9
- 239000000377 silicon dioxide Substances 0.000 description 9
- 229910052751 metal Inorganic materials 0.000 description 8
- 239000002184 metal Substances 0.000 description 8
- 150000002739 metals Chemical class 0.000 description 8
- 238000000227 grinding Methods 0.000 description 7
- 150000001875 compounds Chemical class 0.000 description 6
- 230000005496 eutectics Effects 0.000 description 6
- 239000010445 mica Substances 0.000 description 6
- 229910052618 mica group Inorganic materials 0.000 description 6
- 238000004017 vitrification Methods 0.000 description 6
- WGLPBDUCMAPZCE-UHFFFAOYSA-N Trioxochromium Chemical compound O=[Cr](=O)=O WGLPBDUCMAPZCE-UHFFFAOYSA-N 0.000 description 5
- 239000004615 ingredient Substances 0.000 description 5
- -1 Aluminum Mercury Antimony Molybdenum Arsenic Nickel Barium Osmium Chemical compound 0.000 description 4
- 229910000423 chromium oxide Inorganic materials 0.000 description 4
- 229910052573 porcelain Inorganic materials 0.000 description 4
- 230000015572 biosynthetic process Effects 0.000 description 3
- 238000001354 calcination Methods 0.000 description 3
- 239000004927 clay Substances 0.000 description 3
- 230000000737 periodic effect Effects 0.000 description 3
- 235000012239 silicon dioxide Nutrition 0.000 description 3
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 3
- DGAQECJNVWCQMB-PUAWFVPOSA-M Ilexoside XXIX Chemical compound C[C@@H]1CC[C@@]2(CC[C@@]3(C(=CC[C@H]4[C@]3(CC[C@@H]5[C@@]4(CC[C@@H](C5(C)C)OS(=O)(=O)[O-])C)C)[C@@H]2[C@]1(C)O)C)C(=O)O[C@H]6[C@@H]([C@H]([C@@H]([C@H](O6)CO)O)O)O.[Na+] DGAQECJNVWCQMB-PUAWFVPOSA-M 0.000 description 2
- FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical compound [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 description 2
- 241000220317 Rosa Species 0.000 description 2
- 238000010521 absorption reaction Methods 0.000 description 2
- 229910052796 boron Inorganic materials 0.000 description 2
- 238000002485 combustion reaction Methods 0.000 description 2
- 238000011109 contamination Methods 0.000 description 2
- 238000002425 crystallisation Methods 0.000 description 2
- 230000008025 crystallization Effects 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 229910052500 inorganic mineral Inorganic materials 0.000 description 2
- 229910052749 magnesium Inorganic materials 0.000 description 2
- 239000011777 magnesium Substances 0.000 description 2
- 229910044991 metal oxide Inorganic materials 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 239000011707 mineral Substances 0.000 description 2
- 229910052700 potassium Inorganic materials 0.000 description 2
- 239000011591 potassium Substances 0.000 description 2
- 239000010453 quartz Substances 0.000 description 2
- 230000035939 shock Effects 0.000 description 2
- 229910052710 silicon Inorganic materials 0.000 description 2
- 239000010703 silicon Substances 0.000 description 2
- 229910052708 sodium Inorganic materials 0.000 description 2
- 239000011734 sodium Substances 0.000 description 2
- ZOXJGFHDIHLPTG-UHFFFAOYSA-N Boron Chemical compound [B] ZOXJGFHDIHLPTG-UHFFFAOYSA-N 0.000 description 1
- OYPRJOBELJOOCE-UHFFFAOYSA-N Calcium Chemical compound [Ca] OYPRJOBELJOOCE-UHFFFAOYSA-N 0.000 description 1
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 description 1
- YCKRFDGAMUMZLT-UHFFFAOYSA-N Fluorine atom Chemical compound [F] YCKRFDGAMUMZLT-UHFFFAOYSA-N 0.000 description 1
- WHXSMMKQMYFTQS-UHFFFAOYSA-N Lithium Chemical compound [Li] WHXSMMKQMYFTQS-UHFFFAOYSA-N 0.000 description 1
- 229910019142 PO4 Inorganic materials 0.000 description 1
- NBIIXXVUZAFLBC-UHFFFAOYSA-N Phosphoric acid Chemical compound OP(O)(O)=O NBIIXXVUZAFLBC-UHFFFAOYSA-N 0.000 description 1
- ZLMJMSJWJFRBEC-UHFFFAOYSA-N Potassium Chemical compound [K] ZLMJMSJWJFRBEC-UHFFFAOYSA-N 0.000 description 1
- 229910052777 Praseodymium Inorganic materials 0.000 description 1
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 description 1
- 239000002253 acid Substances 0.000 description 1
- 150000007513 acids Chemical class 0.000 description 1
- 239000010427 ball clay Substances 0.000 description 1
- VYHWNIHOLQCROR-UHFFFAOYSA-N beryllium platinum Chemical compound [Be].[Pt] VYHWNIHOLQCROR-UHFFFAOYSA-N 0.000 description 1
- 229910052797 bismuth Inorganic materials 0.000 description 1
- 229910052793 cadmium Inorganic materials 0.000 description 1
- 229910052792 caesium Inorganic materials 0.000 description 1
- TVFDJXOCXUVLDH-UHFFFAOYSA-N caesium atom Chemical compound [Cs] TVFDJXOCXUVLDH-UHFFFAOYSA-N 0.000 description 1
- 229910052791 calcium Inorganic materials 0.000 description 1
- 239000011575 calcium Substances 0.000 description 1
- WUKWITHWXAAZEY-UHFFFAOYSA-L calcium difluoride Chemical compound [F-].[F-].[Ca+2] WUKWITHWXAAZEY-UHFFFAOYSA-L 0.000 description 1
- 229910001634 calcium fluoride Inorganic materials 0.000 description 1
- 229910052804 chromium Inorganic materials 0.000 description 1
- 239000011651 chromium Substances 0.000 description 1
- 229910052681 coesite Inorganic materials 0.000 description 1
- 239000000567 combustion gas Substances 0.000 description 1
- 238000013329 compounding Methods 0.000 description 1
- 238000009833 condensation Methods 0.000 description 1
- 230000005494 condensation Effects 0.000 description 1
- 239000004020 conductor Substances 0.000 description 1
- 239000000470 constituent Substances 0.000 description 1
- 230000007797 corrosion Effects 0.000 description 1
- 238000005260 corrosion Methods 0.000 description 1
- 229910052906 cristobalite Inorganic materials 0.000 description 1
- 230000002939 deleterious effect Effects 0.000 description 1
- 230000000881 depressing effect Effects 0.000 description 1
- 230000002542 deteriorative effect Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- KZHJGOXRZJKJNY-UHFFFAOYSA-N dioxosilane;oxo(oxoalumanyloxy)alumane Chemical compound O=[Si]=O.O=[Si]=O.O=[Al]O[Al]=O.O=[Al]O[Al]=O.O=[Al]O[Al]=O KZHJGOXRZJKJNY-UHFFFAOYSA-N 0.000 description 1
- 239000010433 feldspar Substances 0.000 description 1
- 239000011737 fluorine Substances 0.000 description 1
- 229910052731 fluorine Inorganic materials 0.000 description 1
- 150000002222 fluorine compounds Chemical class 0.000 description 1
- 230000004927 fusion Effects 0.000 description 1
- FWUTXJDHHFEYOG-UHFFFAOYSA-N gallium thorium Chemical compound [Ga].[Th] FWUTXJDHHFEYOG-UHFFFAOYSA-N 0.000 description 1
- 239000007789 gas Substances 0.000 description 1
- 229910052732 germanium Inorganic materials 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- XLYOFNOQVPJJNP-ZSJDYOACSA-N heavy water Substances [2H]O[2H] XLYOFNOQVPJJNP-ZSJDYOACSA-N 0.000 description 1
- 239000012535 impurity Substances 0.000 description 1
- 229910052738 indium Inorganic materials 0.000 description 1
- 229910052741 iridium Inorganic materials 0.000 description 1
- 150000002611 lead compounds Chemical class 0.000 description 1
- 229910000464 lead oxide Inorganic materials 0.000 description 1
- 229910052744 lithium Inorganic materials 0.000 description 1
- 238000003754 machining Methods 0.000 description 1
- GVALZJMUIHGIMD-UHFFFAOYSA-H magnesium phosphate Chemical compound [Mg+2].[Mg+2].[Mg+2].[O-]P([O-])([O-])=O.[O-]P([O-])([O-])=O GVALZJMUIHGIMD-UHFFFAOYSA-H 0.000 description 1
- 239000004137 magnesium phosphate Substances 0.000 description 1
- 229960002261 magnesium phosphate Drugs 0.000 description 1
- 229910000157 magnesium phosphate Inorganic materials 0.000 description 1
- 235000010994 magnesium phosphates Nutrition 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 230000008018 melting Effects 0.000 description 1
- 238000002844 melting Methods 0.000 description 1
- 229910052863 mullite Inorganic materials 0.000 description 1
- ISUBZZYLOBVUCH-UHFFFAOYSA-N octane tetraethylplumbane Chemical compound CCCCCCCC.CC[Pb](CC)(CC)CC ISUBZZYLOBVUCH-UHFFFAOYSA-N 0.000 description 1
- YEXPOXQUZXUXJW-UHFFFAOYSA-N oxolead Chemical compound [Pb]=O YEXPOXQUZXUXJW-UHFFFAOYSA-N 0.000 description 1
- 230000005502 phase rule Effects 0.000 description 1
- 235000011007 phosphoric acid Nutrition 0.000 description 1
- 239000004033 plastic Substances 0.000 description 1
- 239000000843 powder Substances 0.000 description 1
- 239000011369 resultant mixture Substances 0.000 description 1
- 229910052701 rubidium Inorganic materials 0.000 description 1
- ABTOQLMXBSRXSM-UHFFFAOYSA-N silicon tetrafluoride Chemical compound F[Si](F)(F)F ABTOQLMXBSRXSM-UHFFFAOYSA-N 0.000 description 1
- 229910052851 sillimanite Inorganic materials 0.000 description 1
- 238000005245 sintering Methods 0.000 description 1
- 229910052682 stishovite Inorganic materials 0.000 description 1
- 239000000454 talc Substances 0.000 description 1
- 229910052623 talc Inorganic materials 0.000 description 1
- 229910052714 tellurium Inorganic materials 0.000 description 1
- PORWMNRCUJJQNO-UHFFFAOYSA-N tellurium atom Chemical compound [Te] PORWMNRCUJJQNO-UHFFFAOYSA-N 0.000 description 1
- 229910052716 thallium Inorganic materials 0.000 description 1
- BKVIYDNLLOSFOA-UHFFFAOYSA-N thallium Chemical compound [Tl] BKVIYDNLLOSFOA-UHFFFAOYSA-N 0.000 description 1
- 229910001258 titanium gold Inorganic materials 0.000 description 1
- 229910052905 tridymite Inorganic materials 0.000 description 1
- 229910052721 tungsten Inorganic materials 0.000 description 1
- 239000010937 tungsten Substances 0.000 description 1
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
- C04B35/66—Monolithic refractories or refractory mortars, including those whether or not containing clay
-
- 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
- C04B35/01—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on oxide ceramics
- C04B35/10—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on oxide ceramics based on aluminium oxide
- C04B35/101—Refractories from grain sized mixtures
- C04B35/105—Refractories from grain sized mixtures containing chromium oxide or chrome ore
Definitions
- the discovery and invention relateIin general to compositions of matter for vitreous, products and the like, and for vitrifiable bodies and the like, and methods of making the same.
- the discovery and invention particularly relate to substancesrequiring high temperatures for vitrification, and more particularly to compositions of matter including aluminum oxide, and this application is a division of my application, Serial No. 456,414, filed August 27, 1942 now Patent No. 2,413,441, Dec. 31, 1946.
- Spark plug insulators adapted for use in a high compression internal combustion engine such as an aircraft engine or motor become increasingly difficult to roduce, the. higher the compression of the engine, and the tendency is always to increase the compression of an aircraft engine whenever possible.
- Mica has been used for the insulators of aircraft engine spark plugs, .but most mica having the required special mineral and physical proper.- ties must be imported into the United States, the forming and machining of mica insulators is relatively costly, and the quality of .mica insulators is not'always satisfactory.
- Mica being a natural mineral and containing a varying amount of chemically combined water of crystallization in its composition, tends to decompose when heated giving up its water of crystallization and deteriorating in, crystalline form to that of an anhydrous powder, and thus deteriorates rapidly from its initial characteristics when used as a spark plug insulator in a high compression engine.
- mica With the development for" higher compression motors, mica becomes increasingly unsatisface tory as an insulator for the spark plugs for the motors, and othersubstances have been used including ordinary porcelain and mulliteporcelain.
- Ordinary porcelain such as a, composition of feldspar, pure clay, and flint fired to a temperature of 2300 to 2500 F., constitutes a superior. form of burned clay product, but for spark plug insulator use has relatively poor resistance to the thermal shock imposed upon the spark plug insulators of a high compression motor.
- nary porcelain also has insufficient thermal conductivity for use as tisfactory aircraft engine spark plug insulatorgzand furthermore is subject to attack by the lead compounds present in the combustion gases of high octane tetra ethyl lead s'eli e 7
- Mullite porcelains composed chiefly of clay and silica minerals, suchas sillimanite, fired together at a temperature of approximately 2700 E, develop into strong crystalline structures having improved mechanical strength andimproved hot dielectric strength as compared to ordinary porcelains, but still lacking sufficient thermal conductivity and chemical stability necessary for use as spark plug insulators in high compression aircraft motors.
- the effect on the alumina will be about in the samedegree.
- Thealumina in the resultant mixture or body is over Whelmingly the predominant material, and the resultant body has substantially the properties of that of pure alumina.
- the chromirunoxide produces in the fired article a strong pink or rose color at room temperature. Without the chromium oxide the fired articles are White in'color.
- the strong pink or rose color produced in the fired article by the chromium oxide changes when hot, as when the article is in use as an insulator in aircraft engine spark 1 plug, to black which imparts to the insulator the property of greater heat absorption by the absorption of radiant heat from the gases of combustion in the engine cylinder, the radiant heat being otherwise reflected by White or coated bodies.
- the chromium oxide is added and small quantities of other substances selected from a wide variety of metallic oxides and compounds.
- the total amount of the added substances should preferably not exceed 8% of the total composition, the remaining 92% being alumina. It is preferable that the total number of added substances be more than three.
- the alumina in the body composition or mixture should be in excess of 92% and preferably in excess of 95%. It has been found impractical from a firing standpoint to vitrify mixtures much in excess of 95% alumina. However the properties of the product are much improved as the alumina is increased, and laboratory products have been made at temperatures of 3400" F. in which compositions as high as 98% of alumina were vitrified, yielding an excellent product, but impractical to produce in commercial practice at present because of the exceedingly high temperature required.
- the alumina is preferably in excess of 99% A1203 and as stated free from alkalis in excess of .05% and also free from silica in excess of .05%.
- the silica content of the body is minimized by aa'saaeo avoiding silica contamination inthe processing,
- patalssiumr V. i i patalssiumr V. i i.
- fluorides such as magnesium in the form of talc may be used to a limited extent without harmful results from subsequent silica contamination, because the fluorine set free by thereaction resulting from the firing of the bodycomposition combines with the silica to formgaseous silicon tetrafluoride which escapes and.- constitutes avolitilization of the silicon.
- the principal ingredient of the body composition is calcined aluminum oxide, which before use in the compounding of the body is highly refined and freed of soluble impurities by lixiviation after being ground to a sub-microscopic grain size.
- quartz stones are generally used as grinding media, and in the grinding the abrasiveness of the calcined alumina on the quartz grinding stones causes about 1 to 2% of silica to be ground into the alumina so that the alumina after grinding has a composition of 98 to 98 A1203 and 1 to 2% SiO2.
- a rubber lined mill is used, and the grinding balls are formed of fired alumina, thereby avoiding the pick-up of silica in the ground alumina.
- Eutectics are formed between alumina and a combination of various other substances. However the formation of these eutectics requires initially a very high temperature, at which point the firing range of the mixture is very short due to the sudden depression of the melting point at the temperature of the formation of the eutectics.
- Body composition II p Per cent Alumina, aluminum oxide 92.25 Talc, magnesium silicate 1.2.5 Fluorspar, calcium fluoride e 2.00 Clay, aluminum silicate 3.50 Chromium oxide 1.00
- Body composition III Per cent Alumina, aluminum oxide 91.68 Talc, magnesium silicate 1.25 Whiting, calcium carbonate 2.57 Clay, aluminum silicate 3.50 Chromium oxide 1.00
- compositions of matter and the method steps of making the same deequivalents.
- the method of making a fired vitreous product from a body including upwards of 92 per cent by weight of calcined alumina which includes lixiviating the calcined alumina making a mixture of the alumina and more than three other metallic compounds, forming the mixture, and firing the formed mixture to vitrification, and thus producing a fired product consisting of aluminum oxide of upwards of 92 per cent and oxides of the added metals.
- a fired vitreous prodnot from a body including upwards of 92 per cent by weight of calcined alumina which includes lixiviating the calcined alumina, making a mixture of the alumina and more than three other metallic compounds, forming the mixture, and firing the formed mixture to vitrification, and thus producing a fired product consisting of aluminum oxide of upwards of 92 per cent and ozides of the added metals,the alumina before calcining and lixiviation comprising in excess of 99 per cent aluminum oxide and free from alkalis in excess of 0.05 per cent.
- the method of making a fired vitreous product from a body including upwards of 92 per cent by weight of calcined alumina which includes lixiviating the calcined alumina, making a mixture of the alumina and more than three other metallic compounds, forming the mixture, and firing the formed mixture to vitrification, and 'thus producing a fired product consisting of aluminum oxide of upwards of 92 per cent and oxides of the added metals, the alumina before calcining and l ixiviation comprising in excess of 99 per cent aluminum oxide and free from alkalis in excess of 0.05 per cent and free from silica in excess of 0.05 per cent 4.
- the method of making a fired vitreous prodnot from a body including upwards of 92 per cent by weight of alumina which includes lixiviating the alumina, making a mixture of the alumina and more than three other metallic compounds,
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- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Ceramic Engineering (AREA)
- Manufacturing & Machinery (AREA)
- Materials Engineering (AREA)
- Structural Engineering (AREA)
- Organic Chemistry (AREA)
- Compositions Of Oxide Ceramics (AREA)
Description
Patented Sept. 20, 1949 METHOD OF MAKING FIRED VITREOUS PRODUCT Harold R. Feichter, Canton, Ohio, 'assignor to United States Quarry Tile Company, Canton, Ohio, a corporation of Delaware No Drawing.
1942, plication 4 Claims.
The discovery and invention relateIin general to compositions of matter for vitreous, products and the like, and for vitrifiable bodies and the like, and methods of making the same.
The discovery and invention particularly relate to substancesrequiring high temperatures for vitrification, and more particularly to compositions of matter including aluminum oxide, and this application is a division of my application, Serial No. 456,414, filed August 27, 1942 now Patent No. 2,413,441, Dec. 31, 1946.
Products made by vitrifying or firing at high temperaturesbody compositions having as their principal constituent aluminum oxide are used as spark plug insulators, particularly for aircraft engines, wear resistant and similar parts having extreme hardness, and for other purposes.
Spark plug insulators adapted for use in a high compression internal combustion engine such as an aircraft engine or motor become increasingly difficult to roduce, the. higher the compression of the engine, and the tendency is always to increase the compression of an aircraft engine whenever possible.
Mica has been used for the insulators of aircraft engine spark plugs, .but most mica having the required special mineral and physical proper.- ties must be imported into the United States, the forming and machining of mica insulators is relatively costly, and the quality of .mica insulators is not'always satisfactory.
Mica being a natural mineral and containing a varying amount of chemically combined water of crystallization in its composition, tends to decompose when heated giving up its water of crystallization and deteriorating in, crystalline form to that of an anhydrous powder, and thus deteriorates rapidly from its initial characteristics when used as a spark plug insulator in a high compression engine.
With the development for" higher compression motors, mica becomes increasingly unsatisface tory as an insulator for the spark plugs for the motors, and othersubstances have been used including ordinary porcelain and mulliteporcelain.
Ordinary porcelain, such as a, composition of feldspar, pure clay, and flint fired to a temperature of 2300 to 2500 F., constitutes a superior. form of burned clay product, but for spark plug insulator use has relatively poor resistance to the thermal shock imposed upon the spark plug insulators of a high compression motor.
Furthermore ordinary porcelain has a low dielectric strength, particularly when hot, and is in fact an electrical conductor when hot. Ordi- Original application August 27, Serial No. 456,414. Divided and this ap- July 27, 1945, Serial No. 607,487
nary porcelain also has insufficient thermal conductivity for use as tisfactory aircraft engine spark plug insulatorgzand furthermore is subject to attack by the lead compounds present in the combustion gases of high octane tetra ethyl lead s'eli e 7 Mullite porcelains, composed chiefly of clay and silica minerals, suchas sillimanite, fired together at a temperature of approximately 2700 E, develop into strong crystalline structures having improved mechanical strength andimproved hot dielectric strength as compared to ordinary porcelains, but still lacking sufficient thermal conductivity and chemical stability necessary for use as spark plug insulators in high compression aircraft motors.
It has been determined to be desirable for use as spark plug insulators in high compression aircraft motors to provide a fired composition of matter having the greatest attainable combination of the followingproperties:
1. vitreousness to a high degree and extremely low porosity;
2. Hot dielectric strength in excess of meg-- ohms at 1000 F.;
3. Resistance to thermal shock so as not to be subject to fracture when quenched in water at room temperature from a temperature of 400 F.;
4. Mechanical strength greater than 100,000
' lbs. per sq. in. in compression;
5. Thermal expansion of 7.00 x 10 6. High thermal conductivity;
'7. Hardness and resistance to wear such that the hardness is 9 or over on Mohs scale;
8. Inert with common acids at normal temperatures, that is not subject to appreciable loss in hot or cold HCl, H2804, HNOc, or H3PO4;
9. Resistant to corrosion in molten lead oxide;
10. Absorptive of radiant energy.
Pure aluminum oxide has been found to attain a combination of the above properties satisfactory for use in the vitrified state as insulators for aircraft engine spark plugs. I
The commercial production of vitrified articles from pure aluminum oxide, or alumina, has not been found practicable because of the extremely high temperatures required to bring about the condensation of a pure alumina body to the point of complete vitreousness free from porosity, and because the lack of plasticity of pure alumina renders its formation as a body into any particular shape such as that of an insulator very difficult.
By the present discovery and invention, it has been found that the presence of a very small amount of substantially any other inorganic substance in a body otherwise including substantially all alumina will produce a pronounced depression in the temperature necessary for the vitrification of the body composition, and will improve the forming adaptability,
It has further been. discovered that a combination of a relatively great variety of other substances to a total of a Very small amount in a body, the remainder of which is substantially all alumina, has a more pronounced effect in depressing the vitrification temperature than when only one or two other substances with alumina are used for the body.
It has further been discovered that by using a combination of four or more other substances with alumina in the body, that the total amount of the added substances can be kept very low in proportion to the alumina and that in this Way the properties of the body and the fired product are predominantly those of alumina, and stability is attained in the production of the fired products without the sacrifice of any substantial amount of the desired properties of the major ingredient alumina.
Plotting the efiects of the various added substances on a phase rule diagram reveals a levelling off of the efiects through the combination of the various added ingredients, so that instead of sharp changes afiecting the combination, the
changes are more gradual and the firing range of the combination is greatly extended and sta b-ilized.
Furthermore, the addition of a relatively great variety of substances to the predominant alumina provides a factor of safety against the variations that normally exist in the commercial forms of the substances, so that a more stable and dependable body is obtained through the use in the body composition of a wide variety of substances added to the alumina.
Also it has been discovered that regardless of the specified substance added to the alumina, if added in minute amount, the effect on the alumina will be about in the samedegree. Thealumina in the resultant mixture or body is over Whelmingly the predominant material, and the resultant body has substantially the properties of that of pure alumina.
In attaining a combination of the highest degree of the above enumerated properties for a fired composition of matter for use as aircraft engine spark plug insulators, it has been found preferable to use body combinations of aluminum oxide with the addition of chromium oxide in a minor quantity plus the addition of small quantities of other inorganic substances preferably the oxides of the other metals.
In particular the chromirunoxide produces in the fired article a strong pink or rose color at room temperature. Without the chromium oxide the fired articles are White in'color. The strong pink or rose color produced in the fired article by the chromium oxide changes when hot, as when the article is in use as an insulator in aircraft engine spark 1 plug, to black which imparts to the insulator the property of greater heat absorption by the absorption of radiant heat from the gases of combustion in the engine cylinder, the radiant heat being otherwise reflected by White or coated bodies.
To the predominant alumina, the chromium oxide is added and small quantities of other substances selected from a wide variety of metallic oxides and compounds.
The total amount of the added substances should preferably not exceed 8% of the total composition, the remaining 92% being alumina. It is preferable that the total number of added substances be more than three.
All the added substances are selected from the following metals in their oxide or other compound forms:
Aluminum Mercury Antimony Molybdenum Arsenic Nickel Barium Osmium Beryllium Platinum Bismuth Potassium Boron Praseodymium Cadmium Rubidium Caesium Scandium Calcium Selenium Cerium Silicon Chromium Silver Cobalt Sodium Col'umbium Strontium Copper Tantalum Dysprosium Thallium Gallium Thorium Germanium Tin Gold Titanium Indium Tungsten Iridium Tellurium Iron Uranium Lanthanum Vanadium Lead Yttrium Lithium Zinc Magnesium Zirconium Manganese The above metals are included in groups l2345678 of the periodic table of elements of matter.
While it has been found that the presence of the alkalis of group 1 of the periodic table of elements, particularly sodium and potassium, are deleterious to the fired composition in causing a reduction in hot dielectric strength, it is a practical impossibility to avoid traces to measurable amountsof these substances in the body.
Furthermore, it has been found that a proportion of these alkalis not in excess of .05% does not sufficiently deteriorate the body dielectrically to cause. any seriously harmful results, and that their presence in combination with other substances, particularly the alkaline earths of group 2 of the periodic table of elements and boron, develops low fusion combinations and intensifies the fiuxing action of the mass. Therefore allowance for the presence of these alkaline substances is made in the particular body compositions of the present discovery and invention.
The alumina in the body composition or mixture should be in excess of 92% and preferably in excess of 95%. It has been found impractical from a firing standpoint to vitrify mixtures much in excess of 95% alumina. However the properties of the product are much improved as the alumina is increased, and laboratory products have been made at temperatures of 3400" F. in which compositions as high as 98% of alumina were vitrified, yielding an excellent product, but impractical to produce in commercial practice at present because of the exceedingly high temperature required.
The alumina is preferably in excess of 99% A1203 and as stated free from alkalis in excess of .05% and also free from silica in excess of .05%.
The silica content of the body is minimized by aa'saaeo avoiding silica contamination inthe processing,
free from the alkalis, lithium, sodium, and
patalssiumr V. i i. However, by the introduction of fluorides into the body compositiomsilicates of the metals, such as magnesium in the form of talc may be used to a limited extent without harmful results from subsequent silica contamination, because the fluorine set free by thereaction resulting from the firing of the bodycomposition combines with the silica to formgaseous silicon tetrafluoride which escapes and.- constitutes avolitilization of the silicon.
Describing one particular composition of matter or body composition I of the discovery and invention and the method of making the same, the principal ingredient of the body composition is calcined aluminum oxide, which before use in the compounding of the body is highly refined and freed of soluble impurities by lixiviation after being ground to a sub-microscopic grain size.
To 92 parts by weight of this purified and finely ground alumina A1203 is added and thoroughly mixed 1 parts of calcium fluoride CaFz and 1 parts magnesium phosphate Mg3(PO4) 2.4H2O.
4 parts of plastic ball clay A12O3.2SiO2.2H2O and 1 part of chromic oxide CrzOs.
In the grinding of the alumina to sub-microscopic grain size quartz stones are generally used as grinding media, and in the grinding the abrasiveness of the calcined alumina on the quartz grinding stones causes about 1 to 2% of silica to be ground into the alumina so that the alumina after grinding has a composition of 98 to 98 A1203 and 1 to 2% SiO2.
In the preferred manner of grinding the alumina for the bodies of the present invention, a rubber lined mill is used, and the grinding balls are formed of fired alumina, thereby avoiding the pick-up of silica in the ground alumina.
It has further been discovered that the initial calcination of the fluxing ingredients alone or in combination with part or all of the alumina is desirable before the final body is formed and the final firing effected.
Eutectics are formed between alumina and a combination of various other substances. However the formation of these eutectics requires initially a very high temperature, at which point the firing range of the mixture is very short due to the sudden depression of the melting point at the temperature of the formation of the eutectics.
When however the mixture is fused or calcined and then ground and re-formed, as the final body composition, upon the second heating, the sintering point is reached at a much lower tem perature because of the previously formed eutectics.
A combination of many ingredients yields a superior result than when only few are used, since the eutectics formed between alumina and a wide variety of substances in combination provides a wide range of temperature over which the various eutectics are active, whereas with a lesser number, the range is correspondingly shorter.
The: above described body composition 1 after thesecond firing to a temperature of over 3000" F.,. produces afired-product' consisting of alumimum in excess of 92%, and the oxides of the added metals, silicon, calcium, chromium, and magnesium, the fired product having desired propertieszas; set forthherein' for. use as an aircraft spark. plug; insulator, and. other purposes.
Examples of other body compositions, made according: to the present discovery and invention, and processed as set forth herein to produce the improvedzflred product including alumina and other metallicoxides, are as follows:
Body composition II p Per cent Alumina, aluminum oxide 92.25 Talc, magnesium silicate 1.2.5 Fluorspar, calcium fluoride e 2.00 Clay, aluminum silicate 3.50 Chromium oxide 1.00
Body composition III Per cent Alumina, aluminum oxide 91.68 Talc, magnesium silicate 1.25 Whiting, calcium carbonate 2.57 Clay, aluminum silicate 3.50 Chromium oxide 1.00
100.00 Body composition IV Per cent Alumina, aluminum oxide 92.04 Talc, magnesium silicate 1.25 Barium carbonate 0.89 Whiting, calcium carbonate 0.44 Clay, aluminum silicate 3.50 Chromium oxide 1.00 Beryllium silicate 0.88
The embodiments of the compositions of matter and the method steps of making the same deequivalents.
I claim:
1. The method of making a fired vitreous product from a body including upwards of 92 per cent by weight of calcined alumina, which includes lixiviating the calcined alumina making a mixture of the alumina and more than three other metallic compounds, forming the mixture, and firing the formed mixture to vitrification, and thus producing a fired product consisting of aluminum oxide of upwards of 92 per cent and oxides of the added metals.
2. The method of making a fired vitreous prodnot from a body including upwards of 92 per cent by weight of calcined alumina, which includes lixiviating the calcined alumina, making a mixture of the alumina and more than three other metallic compounds, forming the mixture, and firing the formed mixture to vitrification, and thus producing a fired product consisting of aluminum oxide of upwards of 92 per cent and ozides of the added metals,the alumina before calcining and lixiviation comprising in excess of 99 per cent aluminum oxide and free from alkalis in excess of 0.05 per cent.
3. The method of making a fired vitreous product from a body including upwards of 92 per cent by weight of calcined alumina, which includes lixiviating the calcined alumina, making a mixture of the alumina and more than three other metallic compounds, forming the mixture, and firing the formed mixture to vitrification, and 'thus producing a fired product consisting of aluminum oxide of upwards of 92 per cent and oxides of the added metals, the alumina before calcining and l ixiviation comprising in excess of 99 per cent aluminum oxide and free from alkalis in excess of 0.05 per cent and free from silica in excess of 0.05 per cent 4. The method of making a fired vitreous prodnot from a body including upwards of 92 per cent by weight of alumina, which includes lixiviating the alumina, making a mixture of the alumina and more than three other metallic compounds,
REFERENCES CITED The following references are of record in the file of this patent:
UNITED STATES PATENTS Number Name Date Re. 22,648 Heany June 5, 1945 2,033,300 Reichmann Mar. 10, 1936 2,278,442 Heany Apr, 7, 1942 2,308,115 Schwartzwalder et a1. Jan 12, 1943 2,310,953 Heany Q Feb. 16, 1943 2,336,182 McDougal et a1. Dec. 7, 1943 2,391,454
Heany Dec. 25, 1945
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US2482580A true US2482580A (en) | 1949-09-20 |
Family
ID=3436625
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US2482580D Expired - Lifetime US2482580A (en) | Method of making fired vitreous |
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| Country | Link |
|---|---|
| US (1) | US2482580A (en) |
Cited By (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2618567A (en) * | 1950-10-19 | 1952-11-18 | Norton Co | Molded alumina |
| US2631940A (en) * | 1951-10-25 | 1953-03-17 | Harry C Dunegan | Ceramic composition |
| US2631353A (en) * | 1953-03-17 | Stabilized alumina peebles | ||
| US2665219A (en) * | 1954-01-05 | Ceramic material | ||
| US2680278A (en) * | 1948-10-11 | 1954-06-08 | Phillips Petroleum Co | Alumina pebble |
| US2748007A (en) * | 1951-09-12 | 1956-05-29 | Libbey Owens Ford Glass Co | Glass refractory composition |
| US2760875A (en) * | 1951-10-31 | 1956-08-28 | Gen Motors Corp | Ceramic composition and process for making same |
| US3022685A (en) * | 1958-04-23 | 1962-02-27 | American Drill Bushing Co | Ceramic drill bushing |
| US20070290591A1 (en) * | 2006-06-19 | 2007-12-20 | Lykowski James D | Electrode for an Ignition Device |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2033300A (en) * | 1932-11-19 | 1936-03-10 | Siemens Ag | Method of making compact bodies consisting of pure magnesium oxide or beryllium oxide |
| US2278442A (en) * | 1937-04-07 | 1942-04-07 | Heany Ind Ceramic Corp | Process of making ceramics, abrasives, and the like from alumina, and products thereof |
| US2308115A (en) * | 1943-01-12 | Ceramic body and method of making | ||
| US2310953A (en) * | 1943-02-16 | Ceramic from bauxite and process of | ||
| US2336182A (en) * | 1940-05-31 | 1943-12-07 | Gen Motors Corp | Ceramic article and method of making same |
| US2391454A (en) * | 1945-12-25 | Process of making aluminous |
-
0
- US US2482580D patent/US2482580A/en not_active Expired - Lifetime
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2308115A (en) * | 1943-01-12 | Ceramic body and method of making | ||
| US2310953A (en) * | 1943-02-16 | Ceramic from bauxite and process of | ||
| US2391454A (en) * | 1945-12-25 | Process of making aluminous | ||
| US2033300A (en) * | 1932-11-19 | 1936-03-10 | Siemens Ag | Method of making compact bodies consisting of pure magnesium oxide or beryllium oxide |
| US2278442A (en) * | 1937-04-07 | 1942-04-07 | Heany Ind Ceramic Corp | Process of making ceramics, abrasives, and the like from alumina, and products thereof |
| US2336182A (en) * | 1940-05-31 | 1943-12-07 | Gen Motors Corp | Ceramic article and method of making same |
Cited By (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2631353A (en) * | 1953-03-17 | Stabilized alumina peebles | ||
| US2665219A (en) * | 1954-01-05 | Ceramic material | ||
| US2680278A (en) * | 1948-10-11 | 1954-06-08 | Phillips Petroleum Co | Alumina pebble |
| US2618567A (en) * | 1950-10-19 | 1952-11-18 | Norton Co | Molded alumina |
| US2748007A (en) * | 1951-09-12 | 1956-05-29 | Libbey Owens Ford Glass Co | Glass refractory composition |
| US2631940A (en) * | 1951-10-25 | 1953-03-17 | Harry C Dunegan | Ceramic composition |
| US2760875A (en) * | 1951-10-31 | 1956-08-28 | Gen Motors Corp | Ceramic composition and process for making same |
| US3022685A (en) * | 1958-04-23 | 1962-02-27 | American Drill Bushing Co | Ceramic drill bushing |
| US20070290591A1 (en) * | 2006-06-19 | 2007-12-20 | Lykowski James D | Electrode for an Ignition Device |
| US7823556B2 (en) * | 2006-06-19 | 2010-11-02 | Federal-Mogul World Wide, Inc. | Electrode for an ignition device |
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