US2906800A - Self-ventilating thermocouple well - Google Patents

Self-ventilating thermocouple well Download PDF

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US2906800A
US2906800A US630560A US63056056A US2906800A US 2906800 A US2906800 A US 2906800A US 630560 A US630560 A US 630560A US 63056056 A US63056056 A US 63056056A US 2906800 A US2906800 A US 2906800A
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tube
thermocouple
well
self
ventilating
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US630560A
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Lawrence S Darken
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United States Steel Corp
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United States Steel Corp
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    • GPHYSICS
    • G01MEASURING; TESTING
    • G01KMEASURING TEMPERATURE; MEASURING QUANTITY OF HEAT; THERMALLY-SENSITIVE ELEMENTS NOT OTHERWISE PROVIDED FOR
    • G01K1/00Details of thermometers not specially adapted for particular types of thermometer
    • G01K1/08Protective devices, e.g. casings
    • G01K1/10Protective devices, e.g. casings for preventing chemical attack
    • HELECTRICITY
    • H10SEMICONDUCTOR DEVICES; ELECTRIC SOLID-STATE DEVICES NOT OTHERWISE PROVIDED FOR
    • H10NELECTRIC SOLID-STATE DEVICES NOT OTHERWISE PROVIDED FOR
    • H10N10/00Thermoelectric devices comprising a junction of dissimilar materials, i.e. devices exhibiting Seebeck or Peltier effects

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  • the present invention relates generally to thermocoupies and more particularly to an improved protective tube or well for thermocouples especially suitable for protecting thermocouples from contaminating gases.
  • thermocouples One of the most common causes of failure of noblemetal thermocouples is contamination of the noblemetal wires and the hot thermal junction brought about by the action of reducing gases in the atmosphere where the thermocouple is being used.
  • thermocouples in normal use are ordinarily encased in a protective tube made of refractory material such as porcelain or the like, they are susceptible to the detrimental effects of the action of reducing gases if such gases are present in the surrounding atmosphere. I have found that these gases permeate to some degree the Walls of conventional protective tubes no matter what the composition of the tubes may be.
  • the CO may react with iron oxide which may be present in the atmosphere within the tube in the form of flue dust, or it may react with silicon from the tube itself.
  • iron oxide which may be present in the atmosphere within the tube in the form of flue dust, or it may react with silicon from the tube itself.
  • disassociated FeO is formed, and in the latter volatilized SiO is formed.
  • thermocouple well including an open top outer refractory tube 2 which may be made of porcelain or other suitable material as preferred.
  • An inner tube 4 which may be similar in composition to tube 2, having open ends is concentrically disposed within the tube 2..
  • the diameter of tube2 is greater-thanthe dian'iet'er of tube 4 to the extentthat an annular space 6' is pro vided between the outer wall of tube 4 and inner -wall"" of tube 2.
  • tube-4 The bottom of tube-4 is spaced fromthe-blosed bot-'-" tom of tube 2 and is surrounded'by a solid TingSof porous refractory.
  • the ring 8 maybe rigidly-affixed to tube 4 or any other suitable means as desiredfl'The outer-periphery of ring '8 engages the"iimer"wali of tube 2 and wedgesthe tube 4 in centralized-"position relative to tube 2.
  • thermocouple 10 of conventional desigmhaving a hotjunction-12 at one end and a cold junction (not shown) at its other end is suspended in the tube 4 with an annular space 14 between the exterior of the thermocouple and the interior of the tube 4.
  • Dry porous refractory 16 in powder form, fills the annular space 6 from the refractory ring 8 substantially up to the bottom of the Cool zone.
  • the device of the invention When the device of the invention is in normal use it is vented, in a manner to be more fully described, by the circulation of air passing into the annular space 6 from the open end of tube 2 inwardly through the refractory powder filling 16 and ring 8 and then outwardly through annular space 14 surrounding thermocouple 10, as indicated by the arrows in the figure.
  • the motive force for inducing and maintaining the circulation of air as just described is based on the well known physical phenomenon of thermal transpiration.
  • the refractory filling 16 provides a multiple series of orifices in the Thermal Gradient zone portion of annular space 6 which acts as a thermal pump and forces the air from the cool end of the Thermal Gradient zone toward its warm or hot end.
  • thermocouple Since it is inherent in the metallurgical or other use of a thermocouple that there be a thermal gradient between the hot and cold junctions, this requirement for thermal transpiration is necessarily present. Therefore, all that remains to effect thermal transpiration is to provide a multiple-orifice forming medium in the thermal gradient. The latter is provided by the refractory filling 16. Thus, a means is provided of slow passage of air or other protective atmosphere through the thermocouple well to counteract any reducing gas permeating the well wall. The rate of flow induced by this means is great enough to maintain the atmosphere inside the thermocouple well sufficiently oxidizing as to avoid serious contamination of the thermocouple and at the same time is sufiiciently small that the temperature within the well is substantially unaltered thereby.
  • thermocouple well Too rapid passage of air or other protective atmosphere through the thermocouple well, as could easily result from forced air passage, would seriously alter the temperature inside the well and consequently detrimentally affect the efliciency of the thermocouple. Moreover, usual equipment for forced passage or circulation is apt to be cumbersome, awkward or otherwise impractical in the desired location for the thermocouple.
  • a self ventilating well for a noble-metal thermocouple which comprises an outer tube having a closed bottom and open top, an inner tube having an open top and an open bottom' concentrically disposed within said outer tube with its outer Wall spaced from the inner wall of said outer tube and its bottom spaced from the bottom of said outer tube, said inner tube being adapted to receive said thermocouple therein in concentric spaced relation, and refractory powder in the space between the outer Wall of said inner tube and the inner wall of said outer tube, said refractory having a sintering temperature above the range of temperatures to be measured by said thermocouple and being of approximately .05 to .5 micron particle size.

Description

Sept. 29, 1959 L. s. DARKEN SELF-VENTILATING THERMOCOUPLE WELL Filed Dec. 26. 1956 20m: 0F THERMAL GRADIENT IN VE N 70/? LAWRENCE 6. DAR/(EN,
zaauaa his Attorney.
2,906,800 SELF-VENTILATING THERMOCOUP'ILEWELL Lawrence S.Darkeil', Pa., assignor to United States Steel Corporation, a corporation of New Jersey Application December-.26, 1956, Serial No. 6305560" =1 ClainlTlCl-TQGJY The present invention relates generally to thermocoupies and more particularly to an improved protective tube or well for thermocouples especially suitable for protecting thermocouples from contaminating gases.
One of the most common causes of failure of noblemetal thermocouples is contamination of the noblemetal wires and the hot thermal junction brought about by the action of reducing gases in the atmosphere where the thermocouple is being used.
Although thermocouples in normal use are ordinarily encased in a protective tube made of refractory material such as porcelain or the like, they are susceptible to the detrimental effects of the action of reducing gases if such gases are present in the surrounding atmosphere. I have found that these gases permeate to some degree the Walls of conventional protective tubes no matter what the composition of the tubes may be.
The problem of inaccurate noble-metal thermocouple performance is particularly acute in the iron and steel industry where a substantial amount of reducing gas is produced. For example, blast furnace gas, which contains a high percentage of CO, is used to heat blast furnace stoves. While the heating gas passing through a stove in any given period contains a predominance of CO it is well known that there are isolated areas in the stove where the gas is predominately CO. If one of the stove thermocouples is located in one of these areas its accuracy will be detrimentally affected. The CO permeates the wall of the protective tube or well of the thermocouple and reacts with other elements inside the tube so as to form contaminants which deposit upon the noble-metal wires of the thermocouple. For example, the CO may react with iron oxide which may be present in the atmosphere within the tube in the form of flue dust, or it may react with silicon from the tube itself. In the former case, disassociated FeO is formed, and in the latter volatilized SiO is formed. Under reducing conditions both of these lead to alloying of the noble-metal of the thermocouple as contaminants to an extent suificient to seriously alter the thermoelectric properties thereof.
My objects are to prevent such reducing action within the thermocouple well or tube; to provide means for this purpose in the form of a self-ventilated thermocouple tube or well having airflow-inducing means incorporated therein; and other objects as will be manifest from the following description and drawing.
These and other objects will become more apparent after referring to the following specification and attached drawing, in which a device embodying my invention is illustrated in longitudinal section by way of example.
The illustrative embodiment shown in the drawing is a thermocouple well including an open top outer refractory tube 2 which may be made of porcelain or other suitable material as preferred. An inner tube 4, which may be similar in composition to tube 2, having open ends is concentrically disposed within the tube 2..
ttes Patent i 2,906,800 Patented Sept;
The diameter of tube2 is greater-thanthe dian'iet'er of tube 4 to the extentthat an annular space 6' is pro vided between the outer wall of tube 4 and inner -wall"" of tube 2.
The bottom of tube-4 is spaced fromthe-blosed bot-'-" tom of tube 2 and is surrounded'by a solid TingSof porous refractory. The ring 8 maybe rigidly-affixed to tube 4 or any other suitable means as desiredfl'The outer-periphery of ring '8 engages the"iimer"wali of tube 2 and wedgesthe tube 4 in centralized-"position relative to tube 2.
An insulated noble-metal thermocouple: 10 of conventional desigmhaving a hotjunction-12 at one end and a cold junction (not shown) at its other end is suspended in the tube 4 with an annular space 14 between the exterior of the thermocouple and the interior of the tube 4. The Cool, Thermal Gradient, and Hot zones of the thermocouple well, that exist when the device is in normal use, have been indicated and labeled in the figure of the drawing.
Dry porous refractory 16, in powder form, fills the annular space 6 from the refractory ring 8 substantially up to the bottom of the Cool zone.
When the device of the invention is in normal use it is vented, in a manner to be more fully described, by the circulation of air passing into the annular space 6 from the open end of tube 2 inwardly through the refractory powder filling 16 and ring 8 and then outwardly through annular space 14 surrounding thermocouple 10, as indicated by the arrows in the figure. The motive force for inducing and maintaining the circulation of air as just described is based on the well known physical phenomenon of thermal transpiration. The refractory filling 16 provides a multiple series of orifices in the Thermal Gradient zone portion of annular space 6 which acts as a thermal pump and forces the air from the cool end of the Thermal Gradient zone toward its warm or hot end. Since it is inherent in the metallurgical or other use of a thermocouple that there be a thermal gradient between the hot and cold junctions, this requirement for thermal transpiration is necessarily present. Therefore, all that remains to effect thermal transpiration is to provide a multiple-orifice forming medium in the thermal gradient. The latter is provided by the refractory filling 16. Thus, a means is provided of slow passage of air or other protective atmosphere through the thermocouple well to counteract any reducing gas permeating the well wall. The rate of flow induced by this means is great enough to maintain the atmosphere inside the thermocouple well sufficiently oxidizing as to avoid serious contamination of the thermocouple and at the same time is sufiiciently small that the temperature within the well is substantially unaltered thereby. Too rapid passage of air or other protective atmosphere through the thermocouple well, as could easily result from forced air passage, would seriously alter the temperature inside the well and consequently detrimentally affect the efliciency of the thermocouple. Moreover, usual equipment for forced passage or circulation is apt to be cumbersome, awkward or otherwise impractical in the desired location for the thermocouple.
I have obtained optimum results by using dried magnesium oxide (MgO) powder of approximately .05 micron particle size as the refractory filling 16. Satisfactory results were also obtained by using dried rouge (Fe O or levigated alumina (A1 0 of .05 to .5 micron particle size. The refractories in each case were dried by baking for 1 hour at 1000 to 1200" C. before being packed into the tube. After the refractory has thus been dried and placed in the annular space 6 it may be tamped lightly by hand or rammed under slightly higher materials having sintering temperatures above the range of temperatures to be checked may be used as refractory filler 16; I r 1,
While one embodiment of my invention has been shown and described, it will be apparent that other adaptations and modifications may be made without departing from the scope of the following claim.
I claim: 1 g
A self ventilating well for a noble-metal thermocouple which comprises an outer tube having a closed bottom and open top, an inner tube having an open top and an open bottom' concentrically disposed within said outer tube with its outer Wall spaced from the inner wall of said outer tube and its bottom spaced from the bottom of said outer tube, said inner tube being adapted to receive said thermocouple therein in concentric spaced relation, and refractory powder in the space between the outer Wall of said inner tube and the inner wall of said outer tube, said refractory having a sintering temperature above the range of temperatures to be measured by said thermocouple and being of approximately .05 to .5 micron particle size.
References Cited in the file of.this patent UNITED STATES PATENTS Carter July 31,
US630560A 1956-12-26 1956-12-26 Self-ventilating thermocouple well Expired - Lifetime US2906800A (en)

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Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3935032A (en) * 1973-11-15 1976-01-27 Libbey-Owens-Ford Company Sheathed thermocouple
US4060095A (en) * 1975-08-23 1977-11-29 Koransha Co., Ltd. Thermocouple protecting tube
US5137582A (en) * 1990-11-14 1992-08-11 Kasman David H Thermocouple assembly
WO2016132231A3 (en) * 2015-02-18 2016-11-03 Ardee Technologies Pvt. Ltd. Apparatus and methods for continuous temperature measurement in molten metals

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1640816A (en) * 1925-09-03 1927-08-30 Brown Instr Co Ventilated thermocouple
US1849832A (en) * 1927-04-20 1932-03-15 Gen Electric Thermocouple
US2303704A (en) * 1939-10-10 1942-12-01 Carl L Oseland Temperature responsive device
US2400021A (en) * 1941-09-02 1946-05-07 Benjamin B Schneider Fractionating column
US2757220A (en) * 1955-03-10 1956-07-31 Gen Electric Thermocouple

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1640816A (en) * 1925-09-03 1927-08-30 Brown Instr Co Ventilated thermocouple
US1849832A (en) * 1927-04-20 1932-03-15 Gen Electric Thermocouple
US2303704A (en) * 1939-10-10 1942-12-01 Carl L Oseland Temperature responsive device
US2400021A (en) * 1941-09-02 1946-05-07 Benjamin B Schneider Fractionating column
US2757220A (en) * 1955-03-10 1956-07-31 Gen Electric Thermocouple

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3935032A (en) * 1973-11-15 1976-01-27 Libbey-Owens-Ford Company Sheathed thermocouple
US4060095A (en) * 1975-08-23 1977-11-29 Koransha Co., Ltd. Thermocouple protecting tube
US5137582A (en) * 1990-11-14 1992-08-11 Kasman David H Thermocouple assembly
WO2016132231A3 (en) * 2015-02-18 2016-11-03 Ardee Technologies Pvt. Ltd. Apparatus and methods for continuous temperature measurement in molten metals

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