US3724267A - Heat flux sensing device - Google Patents
Heat flux sensing device Download PDFInfo
- Publication number
- US3724267A US3724267A US00067725A US3724267DA US3724267A US 3724267 A US3724267 A US 3724267A US 00067725 A US00067725 A US 00067725A US 3724267D A US3724267D A US 3724267DA US 3724267 A US3724267 A US 3724267A
- Authority
- US
- United States
- Prior art keywords
- tubes
- conductor
- heat
- fin
- thermocouples
- 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
- 230000004907 flux Effects 0.000 title claims abstract description 18
- 239000004020 conductor Substances 0.000 claims abstract description 30
- 230000005855 radiation Effects 0.000 claims description 5
- 239000012809 cooling fluid Substances 0.000 claims description 2
- 238000001816 cooling Methods 0.000 abstract description 4
- 238000010521 absorption reaction Methods 0.000 abstract description 3
- 230000035882 stress Effects 0.000 description 3
- 239000002826 coolant Substances 0.000 description 2
- 238000009413 insulation Methods 0.000 description 2
- 239000002184 metal Substances 0.000 description 2
- 239000011324 bead Substances 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 238000005259 measurement Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 230000008646 thermal stress Effects 0.000 description 1
Images
Classifications
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01K—MEASURING TEMPERATURE; MEASURING QUANTITY OF HEAT; THERMALLY-SENSITIVE ELEMENTS NOT OTHERWISE PROVIDED FOR
- G01K17/00—Measuring quantity of heat
Definitions
- An elongated conductor extends from between the tubes toward a heat zone on one side of the tubes and is provided with two thermocouples which have junctions at different locations along the length of the conductor, to sense a temperature gradient from which the heat flux through the conductor can be determined.
- the amount of heat absorbed by the tubes is measured at a location by placing thermocouples in a metal heat pad which is welded from face center to face center of two adjacent tubes so that heat from the heat zone or firebox of the boiler will impinge on the pad.
- the thermocouples are placed in the pad a given distance apart so that the temperature difference over that distance can be used to calculate the heat flux.
- the pad conducts heat to what is normally the hottest part of the tube. Consequently, both pad and tubes may overheat.
- the pad is relatively massive and therefore will expand to a greater extent than the adjacent fin which is less massive and at a lower temperature. The result is a tendency toward excessive stresses at the joints between the fin and tubes which are spanned by the metal pad.
- Still another method uses flux meters which are protected by a coolant.
- the practicability of this arrangement is limited by the fact that a separate coolant flow must be maintained for each meter and often an accurate measurement of flow and temperature rise is necessary if the heat flux is to be calculated.
- thermocouples spaced a given distance part along its length.
- the heat will flow longitudinally through the conductor to a tube wall location spaced farther from the heat zone than the hottest portion of the tubes, whereby the thermocouples will indicate a temperature difference from which the heat flux can be determined.
- FIG. 1 is a fragmentary front view in an enlarged scale showing a preferred form of the present invention
- FIG. 2 is a view, partly in section, taken substantially along the line 22 of FIG. 1;
- FIG. 3 is a view showing the connections of the heat conductor to the heat shield and fin.
- adjacent parallel cooling tubes 10 and 11 forming a portion of a furnace wall 12 are joined by a fin 14 which extends longitudinally of the tubes.
- the tube 10 is also joined to a fin 16 which connects to the tube immediately on the left of tube 10 (not shown).
- the tube 11 is connected to the tube immediately to its right (not shown) by a fin 18.
- the furnace wall 12 is made up of many such tubes, each joined to the adjacent tube or tubes by fins. All of the fins join the contiguous tubes so that approximately one-half of the tube is positioned on one side of the fins, and half is on the other side.
- the inner portion of the tube, the portion which communicates directly with the heat zone is as large as the outer portion which defines the outside surface of the furnace wall.
- An elongated heat conductor 20 comprising a pin portion 22 and a base portion 24 which is joined with each of the tubes 10 and 11 in the portions thereof which face each other.
- the base portion 24 has a side 26 which extends into a side portion 28 of the tube 10, and a side 30 which extends into a side portion 32 of the tube 12.
- the pin portion 22 extends from the base portion 24 and toward the inside of the furnace, that is, toward the heat zone.
- the base portion 24 fits snugly in a hole 34 in the fin 14 and as shown in FIG. 2 the base portion 24 extends through the fin 14.
- the hole 34 is recessed along the periphery thereof on the inner side of the fin 14. This allows for a substantial weld bead 35 to be applied and provide a substantial heat conducting path between conductor 20 and fin 14.
- thermocouples 36 and 38 Embedded in the heat conductor 20 are two thermocouples 36 and 38.
- the thermocouples 36 and 38 each extend from outside of the wall through the base portion 24 and terminate in the pin portion 22 at junctions 42 and 44 respectively.
- the junctions 42 and 44 are at different locations along the length of the pin section 22 so that they are different distances from the end of the pin portion 22 which faces the heat zone.
- a radiation shield 46 having a hole 48 of a diameter larger than the pin portion 22 is welded along each of its sides at 50 and 52 to the tubes 10 and 11.
- the end of the pin portion 22 facing the heat zone is positioned coaxially within the hole 48 so that its face is flush with the face of the radiation shield. Because the hole 48 has a larger inside diameter than the pin portion 22, an annular space between the radiant heat shield 46 and pin portion 22 is present. Positioned in this space is a ring of insulation 54.
- the radiant heat shield 46 will also be subject to less stress than would a heat pad because it does not extend over the distance between face centers of adjacent tubes, and also because itconnects to cooler portions of the tubes and 1 1.
- the heat flux in the pin portion 22 can be accurately determined from the temperature gradient in that element.
- the temperature gradient can, of course, be determined from the temperature difference across the junctions 42 and 44, which are a given distance apart along the axis of pin portion 22.
- thermocouples within said conductor said conductor having an end in said heat zone and passing through said orifice to be connected to said fin at a location remote from said end, said thermocouples being disposed between said location and said end,each of said thermocouples having a junction, said two junctions being spaced from one another a given distance along the length of said conductor.
- said conductor comprises a pin portion and a base portion, said base portion being positioned within an aperture in said fin, and said pin portion extending from said base portion toward said heat zone, said junctions being in said pin portion.
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- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Combustion & Propulsion (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Measuring Temperature Or Quantity Of Heat (AREA)
Abstract
Heat absorption rates of cooling tubes are measured accurately without the use of devices which cause high stresses. An elongated conductor extends from between the tubes toward a heat zone on one side of the tubes and is provided with two thermocouples which have junctions at different locations along the length of the conductor, to sense a temperature gradient from which the heat flux through the conductor can be determined.
Description
United States Patent 1 1 Zoschak 51 Apr. 3, 1973 I54] HEAT FLUX SENSlNG DEVICE [75] Inventor: Robert J. Zoschak, Rutherford, NJ.
[73] Assignee: Foster Wheeler Corporation, Livingston, NJ.
[22] Filed: Aug. 28, 1970 [21] Appl. N0.: 67,725
[52] U.S.Cl ..73/190 H, 165/11 [51] Int. Cl. ..G01k 17/00 [58] Field of Search ..73/l5, 190, 340 HF, 341;
[56] References Cited UNITED STATES PATENTS 2/1966 Vrolyk ..73/190 1/1962 Dunlop 4/1968 Connell et al. ..122/6 9/1970 Putmanetal. ..73/l5 8/1965 Macatician ..73/34l Primary Examiner-Jerry W. Myracle Assistant Examinerl -lerbert Goldstein Att0rney.l0hn Maier, III, Marvin A. Naigur and John E, Wilson [57] ABSTRACT Heat absorption rates of cooling tubes are measured accurately without the use of devices which cause high stresses. An elongated conductor extends from between the tubes toward a heat zone on one side of the tubes and is provided with two thermocouples which have junctions at different locations along the length of the conductor, to sense a temperature gradient from which the heat flux through the conductor can be determined.
3 Claims, 3 Drawing Figures HEAT FLUX SENSING DEVICE BACKGROUND OF THE INVENTION There are many situations in industry where it is desirable to measure the amount of heat which is being absorbed by cooling tubes. An example is found in the operation of steam generators having furnace walls made up of parallel tubes which are joined by fins running longitudinally of the tubes. Typically, the fins join the tubes approximately in a plane through the longitudinal axes of the tubes so that the portions of each tube lying on either side of the fins are approximately equal.
In some installations, the amount of heat absorbed by the tubes is measured at a location by placing thermocouples in a metal heat pad which is welded from face center to face center of two adjacent tubes so that heat from the heat zone or firebox of the boiler will impinge on the pad. The thermocouples are placed in the pad a given distance apart so that the temperature difference over that distance can be used to calculate the heat flux.
Such an arrangement has several disadvantages. For one, the pad conducts heat to what is normally the hottest part of the tube. Consequently, both pad and tubes may overheat. In addition, the pad is relatively massive and therefore will expand to a greater extent than the adjacent fin which is less massive and at a lower temperature. The result is a tendency toward excessive stresses at the joints between the fin and tubes which are spanned by the metal pad.
Another way in which heat flux is measured in such a furnace wall is through thermocouples inserted at different depths in chordal holes in the tubes. Such an a.rrangement weakens the tube wall and increases the chances of leakage. It has been found that this arrangement is inherently inaccurate because of difficulty in accurately positioning the thermocouple junctions.
Still another method uses flux meters which are protected by a coolant. The practicability of this arrangement is limited by the fact that a separate coolant flow must be maintained for each meter and often an accurate measurement of flow and temperature rise is necessary if the heat flux is to be calculated.
SUMMARY OF THE INVENTION Itis the object of the present invention to overcome drawbacks found in the prior art, such as those discussed above. Accordingly, extending from between two parallel tubes toward the heat zone is an elongated heat conductor in which are embedded two thermocouples spaced a given distance part along its length. The heat will flow longitudinally through the conductor to a tube wall location spaced farther from the heat zone than the hottest portion of the tubes, whereby the thermocouples will indicate a temperature difference from which the heat flux can be determined.
A BRIEF DESCRIPTION OF THE DRAWING FIG. 1 is a fragmentary front view in an enlarged scale showing a preferred form of the present invention,
FIG. 2 is a view, partly in section, taken substantially along the line 22 of FIG. 1; and
FIG. 3 is a view showing the connections of the heat conductor to the heat shield and fin.
DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENT In FIG. 1, adjacent parallel cooling tubes 10 and 11 forming a portion of a furnace wall 12 are joined by a fin 14 which extends longitudinally of the tubes. The tube 10 is also joined to a fin 16 which connects to the tube immediately on the left of tube 10 (not shown). Similarly, the tube 11 is connected to the tube immediately to its right (not shown) by a fin 18. The furnace wall 12 is made up of many such tubes, each joined to the adjacent tube or tubes by fins. All of the fins join the contiguous tubes so that approximately one-half of the tube is positioned on one side of the fins, and half is on the other side. In other words, the inner portion of the tube, the portion which communicates directly with the heat zone is as large as the outer portion which defines the outside surface of the furnace wall.
An elongated heat conductor 20 comprising a pin portion 22 and a base portion 24 which is joined with each of the tubes 10 and 11 in the portions thereof which face each other. The base portion 24 has a side 26 which extends into a side portion 28 of the tube 10, and a side 30 which extends into a side portion 32 of the tube 12. The pin portion 22 extends from the base portion 24 and toward the inside of the furnace, that is, toward the heat zone.
The base portion 24 fits snugly in a hole 34 in the fin 14 and as shown in FIG. 2 the base portion 24 extends through the fin 14.
As shown in FIG. 3 the hole 34 is recessed along the periphery thereof on the inner side of the fin 14. This allows for a substantial weld bead 35 to be applied and provide a substantial heat conducting path between conductor 20 and fin 14.
Embedded in the heat conductor 20 are two thermocouples 36 and 38. The thermocouples 36 and 38 each extend from outside of the wall through the base portion 24 and terminate in the pin portion 22 at junctions 42 and 44 respectively. The junctions 42 and 44 are at different locations along the length of the pin section 22 so that they are different distances from the end of the pin portion 22 which faces the heat zone.
A radiation shield 46 having a hole 48 of a diameter larger than the pin portion 22 is welded along each of its sides at 50 and 52 to the tubes 10 and 11. The end of the pin portion 22 facing the heat zone is positioned coaxially within the hole 48 so that its face is flush with the face of the radiation shield. Because the hole 48 has a larger inside diameter than the pin portion 22, an annular space between the radiant heat shield 46 and pin portion 22 is present. Positioned in this space is a ring of insulation 54.
In practice, heat impinging upon the area between the tubes 10 and 11 which is not reflected or absorbed by the radiation shield 46 will pass longitudinally down the pin portion 22 of the heat conductor 20 and then through the base portion 24 into the fin 14 and thence into tubes 10 and 11. There will be little thermal stress exerted by the present flux sensing device because there will be little expansion of the conductor 20 in directions perpendicular to the tubes 10 and 11. This is so because unlike a heat pad the conductor 20 has no large dimensions in this direction. In addition, the conductor 20 is cooled because it conducts heat to a comparatively cool portion of tubes 10 and 11, that is, the portions which are adjacent to the fin 14.
The radiant heat shield 46 will also be subject to less stress than would a heat pad because it does not extend over the distance between face centers of adjacent tubes, and also because itconnects to cooler portions of the tubes and 1 1.
Since the pin portion 22 is flush with the heat shield 46 and insulation 54, heat will impinge only on the flat end surface of the pin portion 22. The amount of heat flow per unit area, per unit time, that is, the heat flux, passing axially through the pin portion 22 will therefore be substantially the same as that passing through an equivalent area at or close to the face centers of the tubes. It should be noted that there will be no large difference in temperature between the end surface of the pin portion 22 and the face centers of the tubes to create an appreciable difference in heat flux entering those two elements.
Since the heat flows only axially through the pin portion 22, the heat flux in the pin portion 22 can be accurately determined from the temperature gradient in that element. The temperature gradient can, of course, be determined from the temperature difference across the junctions 42 and 44, which are a given distance apart along the axis of pin portion 22.
Since the heat flux through the present heat flux sensing device is substantially the same as that passing through the areas of the tubes adjacent to their face centers, the heat absorption rate of the tubes is readily and accurately determinable. I
It will be readily apparent to one of ordinary skill in the art that the above describes but one embodiment of the present invention and that it may be modified considerably without exceeding the scope thereof as defined in the following claims.
What is claimed is:
1. In combination, two parallel tubes for flowing a cooling fluid on one side of a heat zone, said tubes being joined by a fin extending longitudinally of and between said tubes, an orifice in said fin, a heat flux sensing device comprising an elongated conductor and two thermocouples within said conductor said conductor having an end in said heat zone and passing through said orifice to be connected to said fin at a location remote from said end, said thermocouples being disposed between said location and said end,each of said thermocouples having a junction, said two junctions being spaced from one another a given distance along the length of said conductor.
2. The structure defined in claim 1 further comprising a radiation shield bridging said two tubes, said shield having a hole, said hole being aligned with said conductor so that heat emanating from said heat zone will impinge against the end of said conductor.
'3. The structure defined in claim 2 wherein said conductor comprises a pin portion and a base portion, said base portion being positioned within an aperture in said fin, and said pin portion extending from said base portion toward said heat zone, said junctions being in said pin portion.
Claims (3)
1. In combination, two parallel tubes for flowing a cooling fluid on one side of a heat zone, said tubes being joined by a fin extending longitudinally of and between said tubes, an orifice in said fin, a heat flux sensing device comprising an elongated conductor and two thermocouples within said conductor said conductor having an end in said heat zone and passing through said orifice to be connected to said fin at a location remote from said end, said thermocouples being disposed between said location and said end, each of said thermocouples having a junction, said two junctions being spaced from one another a given distance along the length of said conductor.
2. The structure defined in claim 1 further comprising a radiation shield bridging said two tubes, said shield having a hole, said hole being aligned with said conductor so that heat emanating from said heat zone will impinge against the end of said conductor.
3. The structure defined in claim 2 wherein said conductor comprises a pin portion and a base portion, said base portion being positioned within an aperture in said fin, and said pin portion extending from said base portion toward said heat zone, said junctions being in said pin portion.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US6772570A | 1970-08-28 | 1970-08-28 |
Publications (1)
Publication Number | Publication Date |
---|---|
US3724267A true US3724267A (en) | 1973-04-03 |
Family
ID=22077980
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US00067725A Expired - Lifetime US3724267A (en) | 1970-08-28 | 1970-08-28 | Heat flux sensing device |
Country Status (2)
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US (1) | US3724267A (en) |
CA (1) | CA933379A (en) |
Cited By (27)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3955617A (en) * | 1974-12-09 | 1976-05-11 | The De Laval Separator Company | Swept surface heat exchanger with dual heat exchange media |
US3979952A (en) * | 1974-07-18 | 1976-09-14 | Ab Svensk Varmematning Cb-System | Device for measuring heat consumption in individual apartments in a centrally heated building |
US4245500A (en) * | 1977-12-30 | 1981-01-20 | Kernforschungszentrum Karlsruhe Gmbh | Sensor for determining heat flux through a solid medium |
US4352290A (en) * | 1980-03-20 | 1982-10-05 | Neils John J | Heat transfer measuring apparatus |
US4480960A (en) * | 1980-09-05 | 1984-11-06 | Chevron Research Company | Ultrasensitive apparatus and method for detecting change in fluid flow conditions in a flowline of a producing oil well, or the like |
US4722610A (en) * | 1986-03-07 | 1988-02-02 | Technology For Energy Corporation | Monitor for deposition on heat transfer surfaces |
US5048973A (en) * | 1990-05-31 | 1991-09-17 | United States Of America, As Represented By The Administrator Of The National Aeronautics And Space Administration | Plug-type heat flux gauge |
US5174654A (en) * | 1992-03-18 | 1992-12-29 | Droege Thomas F | Heat exchanger efficiency monitor |
WO1993001478A2 (en) * | 1991-07-10 | 1993-01-21 | Otf | Calorimetric sensing device for thermal energy consumption |
US5399017A (en) * | 1992-08-19 | 1995-03-21 | Droege; Thomas F. | Method and apparatus for evaluating heat exchanger efficiency |
US6485174B1 (en) * | 2000-10-27 | 2002-11-26 | The Babcock & Wilcox Company | Attachable heat flux measuring device |
US20040101030A1 (en) * | 2002-11-27 | 2004-05-27 | Trapasso David J. | Method and apparatus for inferring a temperature |
US20090020282A1 (en) * | 2005-09-15 | 2009-01-22 | Danfoss A/S | Heat exchanger and method for regulating a heat exchanger |
US20090262777A1 (en) * | 2008-04-18 | 2009-10-22 | General Electric Company | Heat flux measurement device for estimating fouling thickness |
DE102009009592A1 (en) * | 2009-02-19 | 2010-08-26 | Clyde Bergemann Gmbh Maschinen- Und Apparatebau | Measuring device for a heat exchanger |
WO2014187598A1 (en) * | 2013-05-23 | 2014-11-27 | Cockerill Maintenance & Ingenierie S.A. | Heat flow sensor |
DE10393518B4 (en) * | 2002-10-16 | 2014-12-04 | Clyde Bergemann Gmbh | Heat flow measuring device for pressure pipes and method for measuring a heat flow through pressure pipes |
CN104748889A (en) * | 2013-12-26 | 2015-07-01 | 罗斯蒙特公司 | Non-intrusive temperature measurement assembly |
EP3199930A1 (en) * | 2016-01-26 | 2017-08-02 | Miele & Cie. KG | Sensor unit and washing machine |
US20180073996A1 (en) * | 2016-09-12 | 2018-03-15 | Ecolab Usa Inc. | Deposit monitor |
US10670546B2 (en) | 2016-01-25 | 2020-06-02 | Rosemount Inc. | Non-intrusive process fluid temperature calculation system |
US10816285B2 (en) | 2017-02-24 | 2020-10-27 | Ecolab Usa Inc. | Thermoelectric deposit monitor |
US11067520B2 (en) | 2016-06-29 | 2021-07-20 | Rosemount Inc. | Process fluid temperature measurement system with improved process intrusion |
US11226242B2 (en) | 2016-01-25 | 2022-01-18 | Rosemount Inc. | Process transmitter isolation compensation |
US11226255B2 (en) | 2016-09-29 | 2022-01-18 | Rosemount Inc. | Process transmitter isolation unit compensation |
US11320316B2 (en) | 2018-09-28 | 2022-05-03 | Rosemount Inc. | Non-invasive process fluid temperature indication with reduced error |
US11953458B2 (en) | 2019-03-14 | 2024-04-09 | Ecolab Usa Inc. | Systems and methods utilizing sensor surface functionalization |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3018663A (en) * | 1956-09-13 | 1962-01-30 | United States Steel Corp | Furnace lining temperature-thickness measuring apparatus |
US3199352A (en) * | 1962-06-25 | 1965-08-10 | Macatician John | Heat transfer gauge |
US3233458A (en) * | 1961-08-08 | 1966-02-08 | North American Aviation Inc | Heat flux transducer |
US3375628A (en) * | 1965-07-01 | 1968-04-02 | Foster Whceler Corp | Insulated wall construction for heated surfaces |
US3526123A (en) * | 1967-04-11 | 1970-09-01 | Westinghouse Electric Corp | Heat flow sensing device |
-
1970
- 1970-08-28 US US00067725A patent/US3724267A/en not_active Expired - Lifetime
-
1971
- 1971-08-24 CA CA121218A patent/CA933379A/en not_active Expired
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3018663A (en) * | 1956-09-13 | 1962-01-30 | United States Steel Corp | Furnace lining temperature-thickness measuring apparatus |
US3233458A (en) * | 1961-08-08 | 1966-02-08 | North American Aviation Inc | Heat flux transducer |
US3199352A (en) * | 1962-06-25 | 1965-08-10 | Macatician John | Heat transfer gauge |
US3375628A (en) * | 1965-07-01 | 1968-04-02 | Foster Whceler Corp | Insulated wall construction for heated surfaces |
US3526123A (en) * | 1967-04-11 | 1970-09-01 | Westinghouse Electric Corp | Heat flow sensing device |
Cited By (48)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3979952A (en) * | 1974-07-18 | 1976-09-14 | Ab Svensk Varmematning Cb-System | Device for measuring heat consumption in individual apartments in a centrally heated building |
US3955617A (en) * | 1974-12-09 | 1976-05-11 | The De Laval Separator Company | Swept surface heat exchanger with dual heat exchange media |
US4245500A (en) * | 1977-12-30 | 1981-01-20 | Kernforschungszentrum Karlsruhe Gmbh | Sensor for determining heat flux through a solid medium |
US4352290A (en) * | 1980-03-20 | 1982-10-05 | Neils John J | Heat transfer measuring apparatus |
US4480960A (en) * | 1980-09-05 | 1984-11-06 | Chevron Research Company | Ultrasensitive apparatus and method for detecting change in fluid flow conditions in a flowline of a producing oil well, or the like |
US4722610A (en) * | 1986-03-07 | 1988-02-02 | Technology For Energy Corporation | Monitor for deposition on heat transfer surfaces |
US5048973A (en) * | 1990-05-31 | 1991-09-17 | United States Of America, As Represented By The Administrator Of The National Aeronautics And Space Administration | Plug-type heat flux gauge |
WO1993001478A2 (en) * | 1991-07-10 | 1993-01-21 | Otf | Calorimetric sensing device for thermal energy consumption |
WO1993001478A3 (en) * | 1991-07-10 | 1993-03-18 | Otf | Calorimetric sensing device for thermal energy consumption |
US5174654A (en) * | 1992-03-18 | 1992-12-29 | Droege Thomas F | Heat exchanger efficiency monitor |
EP0561056A1 (en) * | 1992-03-18 | 1993-09-22 | Nalco Chemical Company | Heat exchanger efficiency monitor |
US5399017A (en) * | 1992-08-19 | 1995-03-21 | Droege; Thomas F. | Method and apparatus for evaluating heat exchanger efficiency |
US6485174B1 (en) * | 2000-10-27 | 2002-11-26 | The Babcock & Wilcox Company | Attachable heat flux measuring device |
DE10393518B4 (en) * | 2002-10-16 | 2014-12-04 | Clyde Bergemann Gmbh | Heat flow measuring device for pressure pipes and method for measuring a heat flow through pressure pipes |
US6945691B2 (en) * | 2002-11-27 | 2005-09-20 | Delphi Technologies, Inc. | Method and apparatus for inferring a temperature |
US20040101030A1 (en) * | 2002-11-27 | 2004-05-27 | Trapasso David J. | Method and apparatus for inferring a temperature |
US20090020282A1 (en) * | 2005-09-15 | 2009-01-22 | Danfoss A/S | Heat exchanger and method for regulating a heat exchanger |
US10072850B2 (en) * | 2005-09-15 | 2018-09-11 | Danfoss A/S | Heat exchanger and method for regulating a heat exchanger |
US8147130B2 (en) * | 2008-04-18 | 2012-04-03 | General Electric Company | Heat flux measurement device for estimating fouling thickness |
US20090262777A1 (en) * | 2008-04-18 | 2009-10-22 | General Electric Company | Heat flux measurement device for estimating fouling thickness |
US20120067542A1 (en) * | 2009-02-19 | 2012-03-22 | Clyde Bergemann Gmbh Maschinen-Und Apparatebau | Measuring device for a heat exchanger |
US8591102B2 (en) * | 2009-02-19 | 2013-11-26 | Clyde Bergemann GmbH Machinen-und Apparatebau | Measuring device for a heat exchanger |
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US20160084531A1 (en) * | 2013-05-23 | 2016-03-24 | Cockerill Maintenance & Ingenierie S.A. | Heat Flow Sensor |
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US11226242B2 (en) | 2016-01-25 | 2022-01-18 | Rosemount Inc. | Process transmitter isolation compensation |
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US11320316B2 (en) | 2018-09-28 | 2022-05-03 | Rosemount Inc. | Non-invasive process fluid temperature indication with reduced error |
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US12163906B2 (en) | 2019-03-14 | 2024-12-10 | Ecolab Usa Inc. | Deposit monitor |
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