US3444616A - Electric heating element and its fabrication - Google Patents
Electric heating element and its fabrication Download PDFInfo
- Publication number
- US3444616A US3444616A US559024A US55902466A US3444616A US 3444616 A US3444616 A US 3444616A US 559024 A US559024 A US 559024A US 55902466 A US55902466 A US 55902466A US 3444616 A US3444616 A US 3444616A
- Authority
- US
- United States
- Prior art keywords
- metal
- heating
- heating element
- refractory
- oxide
- 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
- 238000005485 electric heating Methods 0.000 title description 10
- 238000004519 manufacturing process Methods 0.000 title description 7
- 238000010438 heat treatment Methods 0.000 description 68
- 229910052751 metal Inorganic materials 0.000 description 56
- 239000002184 metal Substances 0.000 description 56
- 239000012212 insulator Substances 0.000 description 32
- 239000000463 material Substances 0.000 description 31
- 239000000203 mixture Substances 0.000 description 14
- 238000000034 method Methods 0.000 description 13
- 239000002243 precursor Substances 0.000 description 12
- TWNQGVIAIRXVLR-UHFFFAOYSA-N oxo(oxoalumanyloxy)alumane Chemical compound O=[Al]O[Al]=O TWNQGVIAIRXVLR-UHFFFAOYSA-N 0.000 description 11
- 239000000843 powder Substances 0.000 description 11
- 239000011248 coating agent Substances 0.000 description 8
- 238000000576 coating method Methods 0.000 description 8
- UQSXHKLRYXJYBZ-UHFFFAOYSA-N Iron oxide Chemical compound [Fe]=O UQSXHKLRYXJYBZ-UHFFFAOYSA-N 0.000 description 6
- CPLXHLVBOLITMK-UHFFFAOYSA-N Magnesium oxide Chemical compound [Mg]=O CPLXHLVBOLITMK-UHFFFAOYSA-N 0.000 description 6
- 239000011872 intimate mixture Substances 0.000 description 6
- 239000000126 substance Substances 0.000 description 6
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 5
- 229910045601 alloy Inorganic materials 0.000 description 5
- 239000000956 alloy Substances 0.000 description 5
- 238000009826 distribution Methods 0.000 description 5
- 229910000679 solder Inorganic materials 0.000 description 5
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 4
- 239000000395 magnesium oxide Substances 0.000 description 4
- 238000002156 mixing Methods 0.000 description 4
- QGZKDVFQNNGYKY-UHFFFAOYSA-O Ammonium Chemical compound [NH4+] QGZKDVFQNNGYKY-UHFFFAOYSA-O 0.000 description 3
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 description 3
- 229910052782 aluminium Inorganic materials 0.000 description 3
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 3
- 239000010953 base metal Substances 0.000 description 3
- 239000003086 colorant Substances 0.000 description 3
- 239000007789 gas Substances 0.000 description 3
- 239000001257 hydrogen Substances 0.000 description 3
- 229910052739 hydrogen Inorganic materials 0.000 description 3
- 239000011810 insulating material Substances 0.000 description 3
- 238000009413 insulation Methods 0.000 description 3
- 238000002844 melting Methods 0.000 description 3
- 230000008018 melting Effects 0.000 description 3
- 230000003647 oxidation Effects 0.000 description 3
- 238000007254 oxidation reaction Methods 0.000 description 3
- 239000002245 particle Substances 0.000 description 3
- 229910052573 porcelain Inorganic materials 0.000 description 3
- KWIPUXXIFQQMKN-UHFFFAOYSA-N 2-azaniumyl-3-(4-cyanophenyl)propanoate Chemical compound OC(=O)C(N)CC1=CC=C(C#N)C=C1 KWIPUXXIFQQMKN-UHFFFAOYSA-N 0.000 description 2
- GWEVSGVZZGPLCZ-UHFFFAOYSA-N Titan oxide Chemical compound O=[Ti]=O GWEVSGVZZGPLCZ-UHFFFAOYSA-N 0.000 description 2
- WGLPBDUCMAPZCE-UHFFFAOYSA-N Trioxochromium Chemical compound O=[Cr](=O)=O WGLPBDUCMAPZCE-UHFFFAOYSA-N 0.000 description 2
- QCWXUUIWCKQGHC-UHFFFAOYSA-N Zirconium Chemical compound [Zr] QCWXUUIWCKQGHC-UHFFFAOYSA-N 0.000 description 2
- WNROFYMDJYEPJX-UHFFFAOYSA-K aluminium hydroxide Chemical compound [OH-].[OH-].[OH-].[Al+3] WNROFYMDJYEPJX-UHFFFAOYSA-K 0.000 description 2
- 229940090948 ammonium benzoate Drugs 0.000 description 2
- 229910000423 chromium oxide Inorganic materials 0.000 description 2
- 229910052742 iron Inorganic materials 0.000 description 2
- AXZKOIWUVFPNLO-UHFFFAOYSA-N magnesium;oxygen(2-) Chemical compound [O-2].[Mg+2] AXZKOIWUVFPNLO-UHFFFAOYSA-N 0.000 description 2
- 150000002739 metals Chemical class 0.000 description 2
- 229910052759 nickel Inorganic materials 0.000 description 2
- UJVRJBAUJYZFIX-UHFFFAOYSA-N nitric acid;oxozirconium Chemical compound [Zr]=O.O[N+]([O-])=O.O[N+]([O-])=O UJVRJBAUJYZFIX-UHFFFAOYSA-N 0.000 description 2
- BASFCYQUMIYNBI-UHFFFAOYSA-N platinum Chemical compound [Pt] BASFCYQUMIYNBI-UHFFFAOYSA-N 0.000 description 2
- 239000002244 precipitate Substances 0.000 description 2
- 239000000047 product Substances 0.000 description 2
- 230000001681 protective effect Effects 0.000 description 2
- 239000011819 refractory material Substances 0.000 description 2
- 150000003839 salts Chemical class 0.000 description 2
- 239000007787 solid Substances 0.000 description 2
- 238000005979 thermal decomposition reaction Methods 0.000 description 2
- OGIDPMRJRNCKJF-UHFFFAOYSA-N titanium oxide Inorganic materials [Ti]=O OGIDPMRJRNCKJF-UHFFFAOYSA-N 0.000 description 2
- 238000003466 welding Methods 0.000 description 2
- 229910052726 zirconium Inorganic materials 0.000 description 2
- MCSXGCZMEPXKIW-UHFFFAOYSA-N 3-hydroxy-4-[(4-methyl-2-nitrophenyl)diazenyl]-N-(3-nitrophenyl)naphthalene-2-carboxamide Chemical compound Cc1ccc(N=Nc2c(O)c(cc3ccccc23)C(=O)Nc2cccc(c2)[N+]([O-])=O)c(c1)[N+]([O-])=O MCSXGCZMEPXKIW-UHFFFAOYSA-N 0.000 description 1
- VHUUQVKOLVNVRT-UHFFFAOYSA-N Ammonium hydroxide Chemical compound [NH4+].[OH-] VHUUQVKOLVNVRT-UHFFFAOYSA-N 0.000 description 1
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 description 1
- FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical compound [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 description 1
- BPQQTUXANYXVAA-UHFFFAOYSA-N Orthosilicate Chemical compound [O-][Si]([O-])([O-])[O-] BPQQTUXANYXVAA-UHFFFAOYSA-N 0.000 description 1
- 229910000629 Rh alloy Inorganic materials 0.000 description 1
- BQCADISMDOOEFD-UHFFFAOYSA-N Silver Chemical compound [Ag] BQCADISMDOOEFD-UHFFFAOYSA-N 0.000 description 1
- WDEOTCWPXLWTRP-UHFFFAOYSA-N [C+4].[O-2].[Al+3] Chemical compound [C+4].[O-2].[Al+3] WDEOTCWPXLWTRP-UHFFFAOYSA-N 0.000 description 1
- NEIHULKJZQTQKJ-UHFFFAOYSA-N [Cu].[Ag] Chemical compound [Cu].[Ag] NEIHULKJZQTQKJ-UHFFFAOYSA-N 0.000 description 1
- JDVMZTFEYFTCCS-UHFFFAOYSA-N [Ir+3].[O-2].[Zr+4] Chemical compound [Ir+3].[O-2].[Zr+4] JDVMZTFEYFTCCS-UHFFFAOYSA-N 0.000 description 1
- NLHNESWDZWZZBH-UHFFFAOYSA-N [O-2].[Mg+2].[Mo+4].[O-2].[O-2] Chemical compound [O-2].[Mg+2].[Mo+4].[O-2].[O-2] NLHNESWDZWZZBH-UHFFFAOYSA-N 0.000 description 1
- DDHXQDUQHLEATR-UHFFFAOYSA-N [O-2].[O-2].[O-2].[O-2].[Zr+4].[Mo+4] Chemical compound [O-2].[O-2].[O-2].[O-2].[Zr+4].[Mo+4] DDHXQDUQHLEATR-UHFFFAOYSA-N 0.000 description 1
- AZDRQVAHHNSJOQ-UHFFFAOYSA-N alumane Chemical class [AlH3] AZDRQVAHHNSJOQ-UHFFFAOYSA-N 0.000 description 1
- PNEYBMLMFCGWSK-UHFFFAOYSA-N aluminium oxide Inorganic materials [O-2].[O-2].[O-2].[Al+3].[Al+3] PNEYBMLMFCGWSK-UHFFFAOYSA-N 0.000 description 1
- -1 aluminum ammonium hydroxide Chemical compound 0.000 description 1
- LCQXXBOSCBRNNT-UHFFFAOYSA-K ammonium aluminium sulfate Chemical compound [NH4+].[Al+3].[O-]S([O-])(=O)=O.[O-]S([O-])(=O)=O LCQXXBOSCBRNNT-UHFFFAOYSA-K 0.000 description 1
- 239000000908 ammonium hydroxide Substances 0.000 description 1
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 1
- 238000005219 brazing Methods 0.000 description 1
- 229910052804 chromium Inorganic materials 0.000 description 1
- 239000011651 chromium Substances 0.000 description 1
- BIJOYKCOMBZXAE-UHFFFAOYSA-N chromium iron nickel Chemical compound [Cr].[Fe].[Ni] BIJOYKCOMBZXAE-UHFFFAOYSA-N 0.000 description 1
- 230000000052 comparative effect Effects 0.000 description 1
- 150000001875 compounds Chemical class 0.000 description 1
- 239000004020 conductor Substances 0.000 description 1
- 238000010411 cooking Methods 0.000 description 1
- 238000005336 cracking Methods 0.000 description 1
- 238000000354 decomposition reaction Methods 0.000 description 1
- 238000009792 diffusion process 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
- 230000002708 enhancing effect Effects 0.000 description 1
- 230000004907 flux Effects 0.000 description 1
- 239000003517 fume Substances 0.000 description 1
- GKOZUEZYRPOHIO-UHFFFAOYSA-N iridium atom Chemical compound [Ir] GKOZUEZYRPOHIO-UHFFFAOYSA-N 0.000 description 1
- 235000014413 iron hydroxide Nutrition 0.000 description 1
- NCNCGGDMXMBVIA-UHFFFAOYSA-L iron(ii) hydroxide Chemical compound [OH-].[OH-].[Fe+2] NCNCGGDMXMBVIA-UHFFFAOYSA-L 0.000 description 1
- LQBJWKCYZGMFEV-UHFFFAOYSA-N lead tin Chemical compound [Sn].[Pb] LQBJWKCYZGMFEV-UHFFFAOYSA-N 0.000 description 1
- 238000011068 loading method Methods 0.000 description 1
- 229910052749 magnesium Inorganic materials 0.000 description 1
- 239000011777 magnesium Substances 0.000 description 1
- 239000011159 matrix material Substances 0.000 description 1
- 229910001092 metal group alloy Inorganic materials 0.000 description 1
- 229910052863 mullite Inorganic materials 0.000 description 1
- 230000007935 neutral effect Effects 0.000 description 1
- 229910000623 nickel–chromium alloy Inorganic materials 0.000 description 1
- 238000013021 overheating Methods 0.000 description 1
- 230000001590 oxidative effect Effects 0.000 description 1
- 239000001301 oxygen Substances 0.000 description 1
- 229910052760 oxygen Inorganic materials 0.000 description 1
- RVTZCBVAJQQJTK-UHFFFAOYSA-N oxygen(2-);zirconium(4+) Chemical compound [O-2].[O-2].[Zr+4] RVTZCBVAJQQJTK-UHFFFAOYSA-N 0.000 description 1
- 229910052697 platinum Inorganic materials 0.000 description 1
- 238000001556 precipitation Methods 0.000 description 1
- QHGVXILFMXYDRS-UHFFFAOYSA-N pyraclofos Chemical compound C1=C(OP(=O)(OCC)SCCC)C=NN1C1=CC=C(Cl)C=C1 QHGVXILFMXYDRS-UHFFFAOYSA-N 0.000 description 1
- 230000005855 radiation Effects 0.000 description 1
- 239000003870 refractory metal Substances 0.000 description 1
- 239000004065 semiconductor Substances 0.000 description 1
- 229910052709 silver Inorganic materials 0.000 description 1
- 239000004332 silver Substances 0.000 description 1
- 210000004243 sweat Anatomy 0.000 description 1
- 229910001928 zirconium oxide Inorganic materials 0.000 description 1
Images
Classifications
-
- H—ELECTRICITY
- H05—ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
- H05B—ELECTRIC HEATING; ELECTRIC LIGHT SOURCES NOT OTHERWISE PROVIDED FOR; CIRCUIT ARRANGEMENTS FOR ELECTRIC LIGHT SOURCES, IN GENERAL
- H05B3/00—Ohmic-resistance heating
- H05B3/10—Heating elements characterised by the composition or nature of the materials or by the arrangement of the conductor
- H05B3/12—Heating elements characterised by the composition or nature of the materials or by the arrangement of the conductor characterised by the composition or nature of the conductive material
- H05B3/14—Heating elements characterised by the composition or nature of the materials or by the arrangement of the conductor characterised by the composition or nature of the conductive material the material being non-metallic
- H05B3/141—Conductive ceramics, e.g. metal oxides, metal carbides, barium titanate, ferrites, zirconia, vitrous compounds
-
- H—ELECTRICITY
- H05—ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
- H05B—ELECTRIC HEATING; ELECTRIC LIGHT SOURCES NOT OTHERWISE PROVIDED FOR; CIRCUIT ARRANGEMENTS FOR ELECTRIC LIGHT SOURCES, IN GENERAL
- H05B3/00—Ohmic-resistance heating
- H05B3/68—Heating arrangements specially adapted for cooking plates or analogous hot-plates
-
- H—ELECTRICITY
- H05—ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
- H05B—ELECTRIC HEATING; ELECTRIC LIGHT SOURCES NOT OTHERWISE PROVIDED FOR; CIRCUIT ARRANGEMENTS FOR ELECTRIC LIGHT SOURCES, IN GENERAL
- H05B3/00—Ohmic-resistance heating
- H05B3/68—Heating arrangements specially adapted for cooking plates or analogous hot-plates
- H05B3/688—Fabrication of the plates
-
- Y—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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S65/00—Glass manufacturing
- Y10S65/04—Electric heat
-
- Y—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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49002—Electrical device making
- Y10T29/49082—Resistor making
- Y10T29/49101—Applying terminal
Definitions
- FIG. 50 mnmmgmmg wnmmwnmmy
- This invention relates to electric heating elements and more particularly to elements that are fabricated in a solid form.
- the invention described herein relates to the fabrication of electric heating elements and is a division of copending patent application entitled Electric Heating Element and Its Fabrication, Ser. No. 334,999 and now Patent No. 3,309,643.
- heating elements are usually constructed from wire in either of two fashions or from rods made of refractory metals or semiconductor type materials. The latter are very delicate and must be suspended free from contact with oven or heating apparatus in which it is suspended.
- the wire is wound directly onto an insulating material or alternatively embedded within insulating material that fills a metallic tube. In the former element, heating takes place largely by radiation while the latter element heats largely by conduction. In either case, an inherent limitation presents itself in that the units are unable to distribute the heat uniformly with the attendant avoidance of hot spots.
- most heating vessels provide some means for distributing the heat produced by the element in the form of an improved heat conducting quality at the bottom of the vessel or merely providing an increase in mass at the bottom of the metal vessel.
- the present invention overcomes this heat distribution limitation; for effectively, it is an infinite number of heating elements distributed uniformly over a given area. Furthermore, where a large mass is necessarily involved in the heating vessel or in the element itself, because it is embedded in insulating material that in turn fills a metallic tube, a great deal of thermal inertia is experienced. An overall reduction in efficiency results as a consequence of a high terminal inertia. For, as is a normal practice, when a substance has been fully heated it will be removed from the heating element and the power turned off. The quantity of heat that is stored in the system at that moment will be dissipated in the air, that is, wasted.
- the present invention affords an infinite number of heating points, the required temperature of any given point is substantially reduced.
- Conventional heating elements on the other hand have a limited number of heating points thereby attaining much higher spot temperatures for a corresponding overall temperature. This latter feature extends the life of the present invention over that of the conventional unit by eliminating burnouts due to overheating of individual points on the element.
- the usual heating element further confines the heating to a much smaller area when it would be preferable to spread the heat over a much greater area to avoid possible burning of the heated substance.
- the present invention on the contrary spreads the heat over a large area enhancing its use at low heats.
- the present invention can be formed in many desirable shapes of many different colors. As asserted above, the element will operate with lower spot temperatures and is easily cleaned, thereby able to retain the original colors. Such a feature lends a certain esthetic quality to the present invention unknown in the prior art.
- an object of this invention is to provide a simple, more durable electric heating element.
- Another object of this invention is to provide an electric heating element that distributes heat uniformly across its surface.
- Another object of this invention is to provide an electric heating element that has low thermal inertia.
- Another object of this invention is to provide an electric heating element that permits more efiicient heating.
- Another object of this invention is to provide a heating element that has a flat smooth surface that is easily cleaned.
- Another object of this invention is to provide a heating element in color.
- Another object of this invention is to provide a heating element capable of being manufactured in a large variety of shapes including curvilinear forms for ovens.
- FIGURE 1 shows a die where the materials are pressed into shape.
- FIGURE 2 shows a rectangular heating element
- FIGURE 3 shows a round heating element with provision for two separate heats.
- FIGURE 4 is a bottom view of FIGURE 3.
- FIGURE 5A shows the relative heat distribution across the cross section of a conventional heating element.
- FIGURE 5B shows the relative heating distribution across the cross section of the present invention.
- Compartment 12 is filled with a given mixture of one of the following: A1 0 or ZrO or MgO or SiO or other suitable refractory insulators or various combinations thereof and metal.
- refractory insulators are: mullite porcelain A1 0 27 SiO 3 MO+M O); high alumina porcelain to A1 0 4 to 7 SiO, 1 to 4 MO+M O); and steatite porcelain (35 MgO, 60 SiO 5 A1 0 Compartments 11 and 13 are filled with a mixture of the same material bearing a much higher ratio of metal to refractory. To provide elements of consistent resistivities, the material must be proportioned out by weight.
- a given quantity of a finely divided refractory insulator is selected.
- a given quantity of a preselected finely divided (on the order of 325 mesh) metal in the predetermined ratio by volume of metal to refractory insulator is selected.
- one part of Nicrome which is composed of approximately 80% nickel and 20% chromium, can be mixed with four parts aluminum oxide (A1 A portion of that mixture can be remixed in the ratio one part of the mixture to seven parts metal to produce a rich metal mixture for the end zones.
- a metal power and a refractory insulator precursor may be used, or (B) a refractory insulator powder and a metal precursor may be used or (C) both metal and refractory insulators may be used in the form of precursors.
- Finely divided magnesium oxide is mixed with an amount of ammonium chloroplatinate such that upon decomposition of the ammonium chloroplatinate brought about by the careful heating of the mixture, the desired metal to insulator ratio results.
- (C) No. 1 A solution containing desired amounts of an aluminum salt and ferric salts are treated with alkalis or ammonium hydroxide or ammonium benzoate in neutral solution. The resulting precipitate is a very intimate mixture of aluminum hydroxide and iron hydroxide. The mixture is fired at red heat to obtain a mixture of aluminum oxide and iron oxide. This mixture is fired in a stream of hydrogen or other suitable gases at 600 C.- 1000 C. to reduce the iron oxide to iron. The resulting product is a finely divided mixture of iron metal and aluminum oxide.
- the bar is then removed from the cavity of the bottom section 15 of the die and placed in a muffle furnace and heated to a temperature near 1500 C. in an atmosphere such as hydrogen that will prevent oxidizing the metal for approximately 24 hours to cause the metal to diffuse through and around the particles of refractory oxide. The bar is then allowed to cool to room temperature slowly.
- Leads may be attached in a number of different ways. The method used is determined by the type of metal used in the heating element and the final use of the heating element.
- leads may be attached using a lead-tin lbase solder or any other suitable solder, providing the base metal of the heating element lends itself to being wet by such alloys.
- leads may be attached using silver-copper base alloys, or any suitable alloys generally referred to as hard solder or silver solders. Such solders are used with a suitable flux material or a protective gas atmosphere.
- leads may be attached by brazing or welding to the heating element.
- Another method of making a junction is as follows; a part of the metal-rich section of the element is heated until drops of the base metal are caused to sweat out of the insulator-metal matrix. The leads may then be fused directly to the droplet area.
- the element base material is subject to excessive oxidation near its melting point, it must be protected from oxidation during the welding or fusing operation.
- a protective gas or vacuum atmosphere may be used.
- the entire unit is then coated with a glaze of refractory material that insulates the unit electrically and prevents oxid-ation of the base metal if the unit is operated at elevated temperatures.
- the material used in the coating ought to be the same as that used in the fabrication of the heating unit, otherwise stress cracking may develop due to the diiferent coefiicients of expansion of the materials used.
- FIGURE 2 a completed heating element is shown.
- the numbers correspond to the zones indicated in FIG- URE 1.
- Leads 21 are shown attached according to the description above.
- FIGURE 3 a different configuration is shown illustrating that the heating elements can be cast in any desired shape. This configuration is particularly suited for use as a surface burner in a cooking stove.
- FIGURE 4 is a bottom view of the same element. Areas designated 34, '33, 32 are those that are richer in metal than the intermediate areas which are the chief heating areas. Leads 39, 3 8 and 35 are brought down to switch 37.
- various heating levels may be obtained by connecting voltage source 36 across various portions of the element. Assuming the voltage source has perfect regulation (i.e. does not experience a volt-age drop with increased loading), that the resistance from zone 33 to zone 32 is equal to R and that the resistance between zones 33 incl '34 is R which is also equal to [R then:
- the coating of refractory oxide extends over the entire heating element.
- the unit When the unit is placed in stove 40 its top surface will be flush with that of the stove and yet will be insulated electrically from the metal structure of the stove.
- the top of the stove is indented to accommodate the element providing holes at the bottom for the leads of the heating element to pass through.
- the end use of the heating element will determine the metal and the refractory insulation used.
- a low cost refractory insulation such as a silicate or a silicate-oxide system or a pure oxide such as aluminum oxide or magnesium oxide or mixtures of oxide, can be used with a suitable metal.
- a met-a1 alloy such as a nickelchromium alloy or nickel-iron chromium all-y would be the most feasible metal to use in a household stove or oven.
- furnace heating element for use at high temperatures with inert atmospheres or vacuum, a number of different combinations can be used depending largely upon the furnace temperature desired and are listed as follows:
- Zirconium oxide-Iridium may be used up to 2300" C.
- Zirconium oxide-Molybdenum may be used up to 245 0 C.
- Zirconium oxideTungsten may be used up to 2650 C.
- Magnesium oxideTungsten may be used up to 2750 C.
- Aluminum oxide-Carbon may be used up to 1700 C.
- Zirconium oxideGraphite may be used up to 2300 C.
- Furnace heating elements for use at high temperatures in oxygen or air are listed as follows:
- Aluminum oxidePlatinum may be used up to 1700 C.
- Aluminum oxide80% platinum, 20% rhodium alloy may be used up to 1800 C.
- Magnesium oxide-Molybdenum may be used up to 2450 C.
- FIGURE 5 points up the comparative heat distributions of conventional stove heating units and the present invention.
- FIGURE 5A is a cross sectional view of the usual round heating unit when out across its diameter.
- FIGURE 5B is a cross sectional view of the present invention when out across its diameter.
- the heat distribution as represented by the arrows is quite uniform in the present invention while the conventional unit is quite varied.
- the ratio of metal to refractory oxide is determined by the ultimate physical size of the heating unit, and its desired resistivity. Additionally, it will be noted that better conducting metals require a proportionally lower ratio of metal to refractory oxide than a poor conductor of comparable physical size and resistance.
- the size of the element and the material used will also determine the pressure that is to be applied to the material when placed in a die. We have employed pressures ranging from 5000 p.s.i. to 200,000 p.s.-i. in a variety of elements.
- the 7 temperature for diffusion is related to the melting quality of the metal and has ranged between 500 C. and 2000 C.
- an approximate rule of thumb would be to raise the material to a temperature corresponding to two thirds of the metals absolute melting temperature.
- said second quantity having a much higher ratio of metal to refractory insulator
- said second quantity having a much higher ratio of metal to refractory insulator
- said second quantity having a much higher ratio of metal to refractory insulator
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Ceramic Engineering (AREA)
- Resistance Heating (AREA)
Description
May 20,1969
- A. FERRETTIV ET AL ELECTRIC HEATING ELEMENT AND ITS FABRICATION Original Filed Jan. 2, 1,964
FIG. 50 mnmmgmmg wnmmwnmmy;
INVENTORS AUGUST FERRETTI RICHARD W. GERMANN ATTORNEY United States Patent 3,444,616 ELECTRIC HEATING ELEMENT AND ITS FABRICATION August Ferretti, Cambridge, and Richard W. Germann, Boston, Mass., assignors to Massachusetts Institute of Technology, Cambridge, Mass., a corporation of Massachusetts Original application Jan. 2, 1964, Ser. No. 344,999, now Patent No. 3,309,643, dated Mar. 14, 1967. Divided and this application Apr. 22, 1966, Ser. No. 559,024
Int. Cl. H01c 1/14, 17/00 US. Cl. 29-621 4 Claims ABSTRACT OF THE DISCLOSURE The method of producing direct electrical resistance heating elements of any prearranged shape for use at high temperatures consisting of metal dispersed through refractory material.
This invention relates to electric heating elements and more particularly to elements that are fabricated in a solid form.
The invention described herein relates to the fabrication of electric heating elements and is a division of copending patent application entitled Electric Heating Element and Its Fabrication, Ser. No. 334,999 and now Patent No. 3,309,643.
Conventional heating elements are usually constructed from wire in either of two fashions or from rods made of refractory metals or semiconductor type materials. The latter are very delicate and must be suspended free from contact with oven or heating apparatus in which it is suspended. The wire is wound directly onto an insulating material or alternatively embedded within insulating material that fills a metallic tube. In the former element, heating takes place largely by radiation while the latter element heats largely by conduction. In either case, an inherent limitation presents itself in that the units are unable to distribute the heat uniformly with the attendant avoidance of hot spots. To meet this limitation, most heating vessels provide some means for distributing the heat produced by the element in the form of an improved heat conducting quality at the bottom of the vessel or merely providing an increase in mass at the bottom of the metal vessel.
The present invention overcomes this heat distribution limitation; for effectively, it is an infinite number of heating elements distributed uniformly over a given area. Furthermore, where a large mass is necessarily involved in the heating vessel or in the element itself, because it is embedded in insulating material that in turn fills a metallic tube, a great deal of thermal inertia is experienced. An overall reduction in efficiency results as a consequence of a high terminal inertia. For, as is a normal practice, when a substance has been fully heated it will be removed from the heating element and the power turned off. The quantity of heat that is stored in the system at that moment will be dissipated in the air, that is, wasted.
Conventional elements have openings or crevices that permit the entry of unwanted foreign particles. These particles ultimately burn generating fumes and render the heating element difficult to clean. The present invention presenting a perfectly smooth solid surface entirely eliminates this difliculty.
Wherein the present invention affords an infinite number of heating points, the required temperature of any given point is substantially reduced. Conventional heating elements on the other hand have a limited number of heating points thereby attaining much higher spot temperatures for a corresponding overall temperature. This latter feature extends the life of the present invention over that of the conventional unit by eliminating burnouts due to overheating of individual points on the element.
Moreover, when a low, continuous heat is required, the usual heating element further confines the heating to a much smaller area when it would be preferable to spread the heat over a much greater area to avoid possible burning of the heated substance. The present invention on the contrary spreads the heat over a large area enhancing its use at low heats.
The present invention can be formed in many desirable shapes of many different colors. As asserted above, the element will operate with lower spot temperatures and is easily cleaned, thereby able to retain the original colors. Such a feature lends a certain esthetic quality to the present invention unknown in the prior art.
Therefore, an object of this invention is to provide a simple, more durable electric heating element.
Another object of this invention is to provide an electric heating element that distributes heat uniformly across its surface.
Another object of this invention is to provide an electric heating element that has low thermal inertia.
Another object of this invention is to provide an electric heating element that permits more efiicient heating.
Another object of this invention is to provide a heating element that has a flat smooth surface that is easily cleaned.
Another object of this invention is to provide a heating element in color.
Another object of this invention is to provide a heating element capable of being manufactured in a large variety of shapes including curvilinear forms for ovens.
Further objects and advantages of our invention will become more apparent by reference to the following description when taken in conjunction with the accompanying drawings of which:
FIGURE 1 shows a die where the materials are pressed into shape.
FIGURE 2 shows a rectangular heating element.
FIGURE 3 shows a round heating element with provision for two separate heats.
FIGURE 4 is a bottom view of FIGURE 3.
FIGURE 5A shows the relative heat distribution across the cross section of a conventional heating element.
FIGURE 5B shows the relative heating distribution across the cross section of the present invention.
Referring to FIGURE 1, bottom section of a die is shown. The cavity is divided into three compartments by means of paper dividers 13. Compartment 12 is filled with a given mixture of one of the following: A1 0 or ZrO or MgO or SiO or other suitable refractory insulators or various combinations thereof and metal. Common combinations of the refractory insulators are: mullite porcelain A1 0 27 SiO 3 MO+M O); high alumina porcelain to A1 0 4 to 7 SiO, 1 to 4 MO+M O); and steatite porcelain (35 MgO, 60 SiO 5 A1 0 Compartments 11 and 13 are filled with a mixture of the same material bearing a much higher ratio of metal to refractory. To provide elements of consistent resistivities, the material must be proportioned out by weight.
Before the materials are put into a die, they are prepared as follows:
(1) A given quantity of a finely divided refractory insulator is selected.
(2) A given quantity of a preselected finely divided (on the order of 325 mesh) metal in the predetermined ratio by volume of metal to refractory insulator is selected.
(3) The materials are intimately mixed as will be more fully described.
(4) A small quantity of the mixture is then remixed with additional metal powder to increase the ratios of metal to refractory for end zones 11 and 13.
For an inexpensive small heating element for use at 120 volts, one part of Nicrome, which is composed of approximately 80% nickel and 20% chromium, can be mixed with four parts aluminum oxide (A1 A portion of that mixture can be remixed in the ratio one part of the mixture to seven parts metal to produce a rich metal mixture for the end zones.
A simple method of mixing the desired material together is to do so mechanically in a ball mill; however, the substance indicated above would have to be mixed for approximately twenty four hours. A more sophisticated method employing precursor compounds can reduce this mixing period to the order of a few minutes. Several examples of such a method are as follows:
(A) A metal power and a refractory insulator precursor may be used, or (B) a refractory insulator powder and a metal precursor may be used or (C) both metal and refractory insulators may be used in the form of precursors.
(A) No. l. Finely divided iridium powder is mixed with an amount of zirconyl nitrate Zr(NO -n(H O) such that upon the thermal decomposition of the zirconyl nitrate, brought about by the careful heating of the mixture, the desired metal to insulator ratio results.
(A) No. 2. Finely divided nickel-chrome alloy powder is covered with a proper amount of a solution of a soluble salt of aluminum ammonium hydroxide solution or ammonium benzoate solution is added until the precipitation is complete. The gelatinous precipitate of aluminum hydroxide is mixed with the metal powder and then thermally decomposes to form a very intimate mixture of metal alloy and aluminum oxide.
(B) No. l. Finely divided aluminum oxide is mixed with the proper amount of iron oxide and fired in a hydrogen atmosphere at a temperature between 600 C.- 1000 C. The resulting product is an intimate mixture of aluminum oxide and iron.
(B) No. 2. Finely divided magnesium oxide is mixed with an amount of ammonium chloroplatinate such that upon decomposition of the ammonium chloroplatinate brought about by the careful heating of the mixture, the desired metal to insulator ratio results.
(C) No. 1. A solution containing desired amounts of an aluminum salt and ferric salts are treated with alkalis or ammonium hydroxide or ammonium benzoate in neutral solution. The resulting precipitate is a very intimate mixture of aluminum hydroxide and iron hydroxide. The mixture is fired at red heat to obtain a mixture of aluminum oxide and iron oxide. This mixture is fired in a stream of hydrogen or other suitable gases at 600 C.- 1000 C. to reduce the iron oxide to iron. The resulting product is a finely divided mixture of iron metal and aluminum oxide.
(C) No. 2. Proper amounts of ammonium aluminum sulfate (NH Al(S0 are mixed with ammonium chloroplatinate such that upon the thermal decomposition of the mixture by careful heating, the proper desired aluminum oxide to metal ratio results.
The latter methods are used to obtain better mixing of the metal and the refractory insulator in a shorter period of time than can be obtained by mechanical mixing such as ball million.
When the materials have been prepared and placed in their respective compartments of bottom section of the die, dividers 14 are withdrawn. Top section 16 of the die is mated with bottom section 15. The die is then inserted in an hydraulic press and pressure applied. In the case of our example of nickel and aluminum oxide, 160,000
p.s.i. was applied. The bar is then removed from the cavity of the bottom section 15 of the die and placed in a muffle furnace and heated to a temperature near 1500 C. in an atmosphere such as hydrogen that will prevent oxidizing the metal for approximately 24 hours to cause the metal to diffuse through and around the particles of refractory oxide. The bar is then allowed to cool to room temperature slowly.
Leads may be attached in a number of different ways. The method used is determined by the type of metal used in the heating element and the final use of the heating element.
For element use below 300 C., leads may be attached using a lead-tin lbase solder or any other suitable solder, providing the base metal of the heating element lends itself to being wet by such alloys.
For element use below 600 C., leads may be attached using silver-copper base alloys, or any suitable alloys generally referred to as hard solder or silver solders. Such solders are used with a suitable flux material or a protective gas atmosphere.
For element use above 600 C. leads may be attached by brazing or welding to the heating element.
Another method of making a junction is as follows; a part of the metal-rich section of the element is heated until drops of the base metal are caused to sweat out of the insulator-metal matrix. The leads may then be fused directly to the droplet area.
If the element base material is subject to excessive oxidation near its melting point, it must be protected from oxidation during the welding or fusing operation. A protective gas or vacuum atmosphere may be used.
The entire unit is then coated with a glaze of refractory material that insulates the unit electrically and prevents oxid-ation of the base metal if the unit is operated at elevated temperatures. The material used in the coating ought to be the same as that used in the fabrication of the heating unit, otherwise stress cracking may develop due to the diiferent coefiicients of expansion of the materials used.
Many methods of coating the heating element are available; however, a preferred method is that suggested by the Rokide process described in US. Patent No. 2,707,691 wherein pure molten aluminum or zirconium oxide is sprayed on the element. To introduce color into the finished heating element varying amounts of different oxides may be added to the aluminum oxide before it is applied such as chromium oxide and titanium oxide. Chromium oxide produces colors ranging from pink to deep red depending upon the quantity added; while titanium oxide produces various shades of blue. Pure aluminum oxide produces a pure white coating.
In FIGURE 2 a completed heating element is shown. The numbers correspond to the zones indicated in FIG- URE 1. Leads 21 are shown attached according to the description above.
In FIGURE 3 a different configuration is shown illustrating that the heating elements can be cast in any desired shape. This configuration is particularly suited for use as a surface burner in a cooking stove. FIGURE 4 is a bottom view of the same element. Areas designated 34, '33, 32 are those that are richer in metal than the intermediate areas which are the chief heating areas. Leads 39, 3 8 and 35 are brought down to switch 37. Here various heating levels may be obtained by connecting voltage source 36 across various portions of the element. Assuming the voltage source has perfect regulation (i.e. does not experience a volt-age drop with increased loading), that the resistance from zone 33 to zone 32 is equal to R and that the resistance between zones 33 incl '34 is R which is also equal to [R then:
For medium heat 1 or For high heat I R 1 The current being directly representative of the amount of power that can be accommodated by the unit.
The coating of refractory oxide extends over the entire heating element. When the unit is placed in stove 40 its top surface will be flush with that of the stove and yet will be insulated electrically from the metal structure of the stove. The top of the stove is indented to accommodate the element providing holes at the bottom for the leads of the heating element to pass through.
The end use of the heating element will determine the metal and the refractory insulation used.
A low cost refractory insulation, such as a silicate or a silicate-oxide system or a pure oxide such as aluminum oxide or magnesium oxide or mixtures of oxide, can be used with a suitable metal. A met-a1 alloy such as a nickelchromium alloy or nickel-iron chromium all-y would be the most feasible metal to use in a household stove or oven.
.In the use of a furnace heating element, for use at high temperatures with inert atmospheres or vacuum, a number of different combinations can be used depending largely upon the furnace temperature desired and are listed as follows:
(1) Zirconium oxide-Iridium may be used up to 2300" C.
(2) Zirconium oxide-Molybdenum may be used up to 245 0 C.
(3) Zirconium oxideTungsten may be used up to 2650 C.
(4) Magnesium oxideTungsten may be used up to 2750 C.
(5) Aluminum oxide-Carbon may be used up to 1700 C.
(6) Zirconium oxideGraphite may be used up to 2300 C.
Furnace heating elements for use at high temperatures in oxygen or air are listed as follows:
1) Aluminum oxidePlatinum may be used up to 1700 C.
(2) Aluminum oxide80% platinum, 20% rhodium alloy may be used up to 1800 C.
3) Magnesium oxide-Molybdenum may be used up to 2450 C.
FIGURE 5 points up the comparative heat distributions of conventional stove heating units and the present invention. FIGURE 5A is a cross sectional view of the usual round heating unit when out across its diameter. FIGURE 5B is a cross sectional view of the present invention when out across its diameter. The heat distribution as represented by the arrows is quite uniform in the present invention while the conventional unit is quite varied.
The ratio of metal to refractory oxide is determined by the ultimate physical size of the heating unit, and its desired resistivity. Additionally, it will be noted that better conducting metals require a proportionally lower ratio of metal to refractory oxide than a poor conductor of comparable physical size and resistance. The size of the element and the material used will also determine the pressure that is to be applied to the material when placed in a die. We have employed pressures ranging from 5000 p.s.i. to 200,000 p.s.-i. in a variety of elements. The 7 temperature for diffusion is related to the melting quality of the metal and has ranged between 500 C. and 2000 C.
In determining temperature, an approximate rule of thumb would be to raise the material to a temperature corresponding to two thirds of the metals absolute melting temperature.
While we have described the above principles of our invention in connection with specific apparatus, it is to be clearly understood that this description is only made by way of example and not as a limitation on the scope of our invention as set forth in the objects thereof and in the accompanying claims.
What is claimed is:
1. The process of fabricating heating elements comprising the steps of:
combining a preselected quantity of finely divided metal powder with a preselected quantity of finely divided refractory insulator;
combining a second quantity of said finely divided metal powder with a second quantity of finely divided refractory insulator;
said second quantity having a much higher ratio of metal to refractory insulator;
arranging said first and second quantities in a preselected die;
thereby establishing a predesigned configuration of heat ing zones with said first quantity of material and conducting zones with said second quantity of material in the ultimate heating element;
subjecting said material in said die to a predetermined pressure; removing the pressed element; heating said pressed element for sufficient time and at a predetermined temperature to cause said metal to diffuse throughout said refractory insulator;
attaching leads to said metal rich zones formed by said second quantity of material;
coating said heating element with a coat of refractory insulator.
2. The process of fabricating heating elements comprising the steps of:
combining a preselected quantity of a finely divided metal powder with a preselected quantity of a refractory insulator precursor;
combining a second preselected quantity of a finely divided metal powder with a second preselected quantity of a refractory insulator precursor;
heating said substance gently bringing about an intimate mixture of metal powder and refractory insulator; said second quantity having a much higher ratio of metal to refractory insulator;
arranging said first and second quantities in a preselected die;
thereby establishing a predesigned configuration of heating zones with said first quantity of material and conducting zones with said second quantity of material in the ultimate heating element;
subjecting said material in said die to a predetermined pressure;
removing the pressed element;
heating said pressed element for sufiicient time and a at a predetermined temperature to cause said metal to diffuse throughout said refractory insulator;
attaching leads to said metal rich zones formed by said second quantity of material;
coating said heating element with a coat of refractory insulator.
3. The process of fabricating heating elements comprising the steps of:
combining a preselected quantity of a metal precursor and a finely divided refractory insulator;
combining a second preselected quantity of a metal precursor and finely divided refractory insulator;
heating said substances gently bringing about an intimate mixture of metal powder and refractory insulator;
said second quantity having a much higher ratio of metal to refractory insulator;
arranging said first and second quantities in a preselected die;
thereby establishing a predesigned configuration of heating zones with said first quantity of material and conducting zones with said second quantity of material in the ultimate heating element;
subjecting said material in said die to a predetermined pressure;
removing the pressed element;
heating said pressed element for suflicient time and at at a predetermined temperature to cause said metal to diifuse throughout said refractory insulator;
attaching leads to said metal rich zones formed by said second quantity of material;
coating said heating element with a coat of refractory insulator.
4. The process of fabricating heating elements comprising the steps of:
combining a preselected quantity of a metal precursor and a refractory insulator precursor;
combining a second preselected quantity of a metal precursor with a refractory insulator precursor;
heating said substances gently bringing about an intimate mixture of metal powder and refractory insulation;
said second quantity having a much higher ratio of metal to refractory insulator;
arranging said first and second quantities in a preselected die;
thereby establishing a predesigned configuration of heating zones with said first quantity of material and conducting zones with said second quantity of material in the ultimate heating element;
subjecting said material in said die to a predetermined pressure;
removing the pressed element;
heating said pressed element for suflicient time and at a predetermined temperature to cause said metal to diffuse throughout said refractory insulator;
attaching leads to said metal rich zones formed by said second quantity of material;
coating said heating element with a coat of refractory insulator.
References Cited UNITED STATES PATENTS 354,257 12/1886 Slattery 29621 X 1,816,194 7/1931 Power 29-62t1 X 1,978,323 10/1934 Power 29-621 X 2,707,691 5/1955 Wheildon 23983 X 2,883,502 4/ 1959 Rudner.
2,903,666 9/1959 Krellner 29-621 X 3,252,831 5/1966 Ragan. 3,302,272 2/ 1967 Braun 29-621 25 JOHN F. CAMPBELL, Primary Examiner.
J. L. CLINE, Assistant Examiner.
U.S. Cl. X.R.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US559024A US3444616A (en) | 1964-01-02 | 1966-04-22 | Electric heating element and its fabrication |
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US34499964 | 1964-01-02 | ||
| US559024A US3444616A (en) | 1964-01-02 | 1966-04-22 | Electric heating element and its fabrication |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US3444616A true US3444616A (en) | 1969-05-20 |
Family
ID=33456358
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US559024A Expired - Lifetime US3444616A (en) | 1964-01-02 | 1966-04-22 | Electric heating element and its fabrication |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US3444616A (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4417389A (en) * | 1982-02-26 | 1983-11-29 | Kennecott Corporation | Method of terminating carbon ceramic composition resistors for use in high peak power and peak voltage energy dissipation application |
| US6130601A (en) * | 1997-11-24 | 2000-10-10 | Motorola, Inc. | Thick-film resistor having concentric terminals and method therefor |
| US20110252833A1 (en) * | 2008-12-16 | 2011-10-20 | Asahi Glass Company, Limited | Filmed metal member for float glass manufacturing equipment and float glass manufacturing method |
| US11101152B2 (en) * | 2018-03-19 | 2021-08-24 | Tokyo Electron Limited | Phase mixture temperature controlled hot plate |
| EP4621004A1 (en) | 2024-03-18 | 2025-09-24 | Covestro Deutschland AG | Method for recovering fibers from fiber reinforced polyurethane-based composites |
Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US354257A (en) * | 1886-12-14 | slatteey | ||
| US1816194A (en) * | 1927-06-10 | 1931-07-28 | Lynde Bradley | Method of forming resistor units |
| US1978323A (en) * | 1931-07-18 | 1934-10-23 | Allen Bradley Co | Fixed resistor unit and process of forming the same |
| US2707691A (en) * | 1952-08-08 | 1955-05-03 | Norton Co | Coating metals and other materials with oxide and articles made thereby |
| US2883502A (en) * | 1955-01-28 | 1959-04-21 | Us Gasket Company | Electrical resistors and other bodies with negligible temperature coefficient of expansion |
| US2903666A (en) * | 1955-08-23 | 1959-09-08 | Speer Carbon Company | Resistors with integral molded metal terminals |
| US3252831A (en) * | 1964-05-06 | 1966-05-24 | Electra Mfg Company | Electrical resistor and method of producing the same |
| US3302272A (en) * | 1963-12-26 | 1967-02-07 | Air Reduction | Forming a resistor with thin, compressed, contact portions |
-
1966
- 1966-04-22 US US559024A patent/US3444616A/en not_active Expired - Lifetime
Patent Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US354257A (en) * | 1886-12-14 | slatteey | ||
| US1816194A (en) * | 1927-06-10 | 1931-07-28 | Lynde Bradley | Method of forming resistor units |
| US1978323A (en) * | 1931-07-18 | 1934-10-23 | Allen Bradley Co | Fixed resistor unit and process of forming the same |
| US2707691A (en) * | 1952-08-08 | 1955-05-03 | Norton Co | Coating metals and other materials with oxide and articles made thereby |
| US2883502A (en) * | 1955-01-28 | 1959-04-21 | Us Gasket Company | Electrical resistors and other bodies with negligible temperature coefficient of expansion |
| US2903666A (en) * | 1955-08-23 | 1959-09-08 | Speer Carbon Company | Resistors with integral molded metal terminals |
| US3302272A (en) * | 1963-12-26 | 1967-02-07 | Air Reduction | Forming a resistor with thin, compressed, contact portions |
| US3252831A (en) * | 1964-05-06 | 1966-05-24 | Electra Mfg Company | Electrical resistor and method of producing the same |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4417389A (en) * | 1982-02-26 | 1983-11-29 | Kennecott Corporation | Method of terminating carbon ceramic composition resistors for use in high peak power and peak voltage energy dissipation application |
| US6130601A (en) * | 1997-11-24 | 2000-10-10 | Motorola, Inc. | Thick-film resistor having concentric terminals and method therefor |
| US20110252833A1 (en) * | 2008-12-16 | 2011-10-20 | Asahi Glass Company, Limited | Filmed metal member for float glass manufacturing equipment and float glass manufacturing method |
| US11101152B2 (en) * | 2018-03-19 | 2021-08-24 | Tokyo Electron Limited | Phase mixture temperature controlled hot plate |
| EP4621004A1 (en) | 2024-03-18 | 2025-09-24 | Covestro Deutschland AG | Method for recovering fibers from fiber reinforced polyurethane-based composites |
| WO2025195898A1 (en) | 2024-03-18 | 2025-09-25 | Covestro Deutschland Ag | Method for recovering fibres from fibre-reinforced polyurethane-based composites |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US3309643A (en) | Electric heating element | |
| US3444616A (en) | Electric heating element and its fabrication | |
| US3584196A (en) | Automatic electric cooking appliance | |
| US2188667A (en) | Resistor and method of making the same | |
| US2890318A (en) | Aluminum sheathed heating elements in aluminum die castings | |
| EP0501788B1 (en) | Sheathed heater | |
| US2487581A (en) | Electrical resistor and method of making same | |
| US2271995A (en) | Electrical resistance | |
| US2799081A (en) | Electrical contacts | |
| US1155427A (en) | Contact bodies of tungsten. | |
| US3349224A (en) | Heating unit | |
| US1155426A (en) | Method of making contact bodies of tungsten. | |
| JP2503077B2 (en) | Electric heater and heating method using the same | |
| US2140228A (en) | Electrically heated furnace | |
| US485017A (en) | Electric soldering | |
| US2108544A (en) | Cathode heater for electron discharge devices | |
| US1736745A (en) | Electrical heating body and method of manufacturing the same | |
| US2694740A (en) | Pot type furnace for molten metal | |
| US685471A (en) | Thermo-electric couple. | |
| US599352A (en) | Electric resistance-conductor | |
| US2125075A (en) | Electrical heating element | |
| US3479631A (en) | Thermistors | |
| JPS6021448B2 (en) | Electrical insulating material for burying metal heater wires and method for manufacturing the same | |
| US2469800A (en) | Electric heater | |
| JPS6017801B2 (en) | Method for producing silver-nickel composite powder |