US3097686A - Furnace system - Google Patents
Furnace system Download PDFInfo
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- US3097686A US3097686A US28588A US2858860A US3097686A US 3097686 A US3097686 A US 3097686A US 28588 A US28588 A US 28588A US 2858860 A US2858860 A US 2858860A US 3097686 A US3097686 A US 3097686A
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F24—HEATING; RANGES; VENTILATING
- F24H—FLUID HEATERS, e.g. WATER OR AIR HEATERS, HAVING HEAT-GENERATING MEANS, e.g. HEAT PUMPS, IN GENERAL
- F24H1/00—Water heaters, e.g. boilers, continuous-flow heaters or water-storage heaters
- F24H1/22—Water heaters other than continuous-flow or water-storage heaters, e.g. water heaters for central heating
- F24H1/24—Water heaters other than continuous-flow or water-storage heaters, e.g. water heaters for central heating with water mantle surrounding the combustion chamber or chambers
- F24H1/26—Water heaters other than continuous-flow or water-storage heaters, e.g. water heaters for central heating with water mantle surrounding the combustion chamber or chambers the water mantle forming an integral body
- F24H1/28—Water heaters other than continuous-flow or water-storage heaters, e.g. water heaters for central heating with water mantle surrounding the combustion chamber or chambers the water mantle forming an integral body including one or more furnace or fire tubes
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F22—STEAM GENERATION
- F22B—METHODS OF STEAM GENERATION; STEAM BOILERS
- F22B33/00—Steam-generation plants, e.g. comprising steam boilers of different types in mutual association
- F22B33/02—Combinations of boilers having a single combustion apparatus in common
- F22B33/08—Combinations of boilers having a single combustion apparatus in common of boilers of water tube type with boilers of fire-tube type
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23C—METHODS OR APPARATUS FOR COMBUSTION USING FLUID FUEL OR SOLID FUEL SUSPENDED IN A CARRIER GAS OR AIR
- F23C9/00—Combustion apparatus characterised by arrangements for returning combustion products or flue gases to the combustion chamber
Definitions
- the present invention provides a heating system having substantially increased efiiciency which incorporates a selective feed back of flue gases from the exhaust system of -a combustion chamber to the input wherein the fed back exhaust gases are mixed with fuel and air entering the combustion chamber.
- the selectivity is exercised through a vortex tube which separates the exhaust gases into relatively warm and cold components.
- the cold Component is permitted to exhaust to the atmosphere and only the warm component is fed back to the input of the heating system.
- Another object of the present invention to provide a heating system having sele'ctive feed back of portions of the flue gas exhaust to the system input.
- Another object of the present invention is to provide a heating system with flue gas feed back and incorporating means for separating the exhaust gas into distinct components and feeding back only the hotter Component to the system input.
- FIGURE 1 is schematic diagram showing in simplified form the basic heating 'system of the invention and,
- FIGURE 2 is a schematic diagram of a modified embodiment of the heating system of the present invention.
- the heating system of the present invention generally indicated at comprises a gas inlet conduit 12 which -supplies either ambient or super charged air to the input of an air blower 14.
- Fuel is supplied from any suitable source to the system through a supply pipe 16 connected to a restricted portion 18 in the output line 20 of the blower which restricted portion defines a venturi connection so that the pressurized air flowing from outlet 20 through the restriction 18 draws fuel from pipe 16.
- the pressurized air-fuel mixture passes through -a check valve 22 in the direction of the arrow to :a combustion chamber .surrounding the cooler gas.
- Patented July 16, 1963 ice 24 forming the major heating chamber of the furnacc system.
- Vortex tube 28 is the type sometimes referred to as a Ranque- Hilsch tube first described by G. Ranque in U.S. Patent 1,952,28l.
- the vortex tube is of the uniflow type with the relatively hot and cold gas outlets positioned at the same end of the tube.
- the vortex tube 28 comprises a generator chamber 30 and a vortex generator 32 having a tangential inlet 34 through which the high pressure gases gain access to the central tubular channel 36 of the vortex tube.
- the gases are cause-d to spiral through the tube so the cooler portions of the gas collect in a central stream and the warmer portions collect in an outer iannular stream
- the central cooler stream is extracted through a central restriction 38 and passes to ⁇ atmosphere through outlet conduit 40. Hotter portions of the flue gas pass outwardly through the outer re'striction 42 to a hot gas feed back line 44.
- Feed back line 44 Supplies the hotter portion of the exhaust or flue gases to the inlet conduit 12 where these hotter portions are mixed with the incoming air supplied to a blower 14 and tend to preheat this air.
- the air-fuel mixture feed to the combustion chamber is controlled so that it contains approxim-ately 200% excess air. This excess air serves to sustain complete combustion and further lowers the temperature in the combustion chamber to an acceptable Value.
- the combustion chamber and Vortex tube are surrounded by an insulating jacket 46 containing a heat exchange fluid such ⁇ ras water as indicated at 48 which takes heat produced in the combustion chamber from the outer surface of the vortex tube 36 and from the hot gas feed back line '44.
- Cold water may be supplied to the Water jacket through inlet 50 from a suitable supply and the hot water is drawn oli through 'outlet conduit 52.
- FIGURE 2 shows a schematic diagram of a modified embodment of the heating system of the present invention with like elements bearing like reference numerals.
- the blower is eliminated and in its place the combustion chamber -is fed by means of a novel injecter and check valve arrangement.
- water to be heated is circulated through the jacket 46 from inlet conduit 50 by suitable means such as the circulating pump 54 and is drawn off through Conduit 52.
- the hotter portion of the exhaust or flue gases is drawn off from the periphery of the Hilsch tube and fed back through line 44.
- a portion of the combustion products is fed through pipe 58 from the combustion chamber 24 into a converging-diverging nozzle 60 where the combustion products attain supersonic velocities.
- the stream of high velocity combustion products impinges on ambient air supplied by way of line 62 and check valve 64 imparting velocity to the air molecules.
- the air and combustion products enter a diffuser 66 where they are compressed to a pressure higher than the pressure existing in the combustion chamber. This high pressure air and combustion mixture then picks up the fuel at the throat of venturi 68 and enters the combustion chamber through line 70 to sustain the steady flow combustion process. In so doing the mixture passes through check valves 72 and 74.
- the fuel is fed from a suitable source to line 75 and through a venturi 76 where it picks up a small amount of ambient air from line 78.
- the fuel and small quantity of ambient air enter the system at venturi 68 between the two check valves 72 and 74.
- the air-fuel mixture supplied by way of venturi 68 into the combustion chamber is adequate during the starting of the furnace.
- the gases flowing through the injecter comprising nozzle 60 'and diffuser 66 acts to pull more air from line 62.
- the increased pull of :air from line 62 in turn acts to pull rnore fuel by way of Venturi 68 as it passes through the venturi between the check valves and the system automatically builds up to an Operating level.
- the check valve 64 in the air line serves only to prevent reverse flow in the event of a malfunction in the injecter.
- the present invention provides a novel heating system of substantially increased etficiency which theoretically may possess a thermal eiiiciency greater than 100% by actually cooling down the exhaust gases below ambient temperature.
- An important feature of the present invention is the selective feed back of a hot component of exhaust gas to the combustion chamber inlet with the separation of the exhaust gas into a hot component being accompanied by a separation of the remaining portion of the exhaust gas into a colder component.
- a furnace system comprising a combustion chamber, means for supplying fuel to said chamber, means forming an output path for combustion products from said chamber, means in said path for dividing the combustion products into relatively hot and cold components and means for feeding at least a portion of said hot component back to said combustion chamber.
- combustion chamber includes means forming a fuel input, and means for mixing said feed back portion with fuel at the input to said combustion chamber.
- a system according to claim 3 including means for mixing said feed back portion with said combustion gas to preheat said gas prior to its entrance into said chamber.
- a system according to claim 4 wherein said vortex tube is of the uniflow type having hot and cold gas outlets at the same end of the tube.
- a system according to claim 5 including means for maintaining a circulating heat transfer medium in heat xchange relation with the outer surface of said vortex tube and said hot component feed back means.
- a furnace system comprising a combustion chamber, a blower for supplying air to said chamber, a fuel inlet to said chamber, means forming an output path for combustion products from said chamber, a vortex tube in said path for dividing the combustion products into relatively hot and cold components and a feed back line connecting the periphery of said vortex tube with the input of said blower whereby the hot component of said combustion products is fed back to preheat the air passing through said blower into said combustion chamber.
- a furnace system including means for maintaining a heat exchange fluid medium in contact with the outer surface of said vortex tube and the outer surface of said feed -back line.
- a furnace system comprising a combustion chamber, means forming an air-fuel mixture ⁇ inlet to said chamber, means forming an output path for combustion products from said chamber, a vortex tube in said path -for dividing the combustion products into relatively hot and cold components, means for feedin'g a portion of the combustion products from said chamber through a return line to said mixture inlet, and means for feeding back said hot component from the periphery of said vortex tube to said return line.
- said return line includes a nozzle capable of passing uids at supersonic velocities and said hot component enters said return line at the output 'of said nozzle.
- a system according to claim 13 including means for maintaining a heat exchange fluid medium in constaet with the outer surface of said vortex tube and said hot component feed 'back means.
Description
R` D. MORROW FURNACE SYSTEM Filed May 12, 1960 July 16, 1963 Robert D. Mor-raw BY g I f d c ATTORNEYS United States Patent 3,097,686 FURNACE SYSTEM Robert D. Morrow, Baltimore, Md., assignor to Product Development Associates, Ltd., Baltimo'e, Md. Filed May 12, 1960, Ser. No. 28,588 14 Claims. (Cl. 158-1) This invention relates to a furnace system for heating water or 'another suitable fluid medium and more particularly to a heating system wherein the hotter portions of the flue gases are fed back into the input of a combustion chamber.
Various systems are known wherein portions of the exhaust products or flue gases are fed back to the -input of a comb ustion chamber to improve the overall efiiciency of a heating system. However, these systems suffer from the serious disadvantage in tha-t there is little -or no selectivity exercised with respect to which portions -of the flue gas are recrculated through the system. In most instances the feed back gases are selected on :a quantity basis with a certain percentage passing through 'a ratio valve or other type of valving system so that a certain portion of the entire exhaust gas composition -is recirculated to the combustion chamber.
The present invention provides a heating system having substantially increased efiiciency which incorporates a selective feed back of flue gases from the exhaust system of -a combustion chamber to the input wherein the fed back exhaust gases are mixed with fuel and air entering the combustion chamber. The selectivity is exercised through a vortex tube which separates the exhaust gases into relatively warm and cold components. The cold Component is permitted to exhaust to the atmosphere and only the warm component is fed back to the input of the heating system. In this way it is possible to reduce the temperature of the exiting gases from the system and consequently substantially increase the thermal eficiency of the furnace. It is theoretically possible by actually cooling the exhaust gases below atmospheric temperature to obtain a thermal efficiency for the' heating system of the present invention of over 100% It is therefore, a primary object of the present invention to provide a -novel heating system having increased efficiency.
Another object of the present invention to provide a heating system having sele'ctive feed back of portions of the flue gas exhaust to the system input.
Another object of the present invention is to provide a heating system with flue gas feed back and incorporating means for separating the exhaust gas into distinct components and feeding back only the hotter Component to the system input.
These and other objeets and advantages of the invention will be more apparent upon reference to the following specification, claims 'and appended drawings wherein:
FIGURE 1 is schematic diagram showing in simplified form the basic heating 'system of the invention and,
FIGURE 2 is a schematic diagram of a modified embodiment of the heating system of the present invention.
Referring to the drawings and particularly to FIGURE l, the heating system of the present invention generally indicated at comprises a gas inlet conduit 12 which -supplies either ambient or super charged air to the input of an air blower 14. Fuel is supplied from any suitable source to the system through a supply pipe 16 connected to a restricted portion 18 in the output line 20 of the blower which restricted portion defines a venturi connection so that the pressurized air flowing from outlet 20 through the restriction 18 draws fuel from pipe 16. The pressurized air-fuel mixture passes through -a check valve 22 in the direction of the arrow to :a combustion chamber .surrounding the cooler gas.
Patented July 16, 1963 ice 24 forming the major heating chamber of the furnacc system.
Combusti-on products from chamber 24 pass outwardly in the direction of the arrow through a second check valve 26 to a conventional uniflow vortex tube 28. Vortex tube 28 is the type sometimes referred to as a Ranque- Hilsch tube first described by G. Ranque in U.S. Patent 1,952,28l. In the system illustrated the vortex tube is of the uniflow type with the relatively hot and cold gas outlets positioned at the same end of the tube.
It is well known that in operation a vortex tube divides a compressed gas into two moving streams each with a different temperature. The outer stream is substantially hotter than the inner one. The exact mode of operation is not fully understood and several theories have been advanced for explaining the operation of these tubes. One of the most widely accepted theories presumes that the gas is broken up into separate helical gyrating layers with the inner layer compressing the outer layer through centrifugal force and giving up some ot its energy to the outer layer. The energy given up is represented by an increase in temperature of the outer layer and a decrease in temperature of the inner layer each of which may be separately 'removed from the same end of a uniflow tube by means 'of suitably positioned and throttled concentric apertures. It 'has been found that a maximum temperature differential between the exiting relatively hot and cool gas streams is obtained by a division of 30% of cold gas and 70% hot gas. Temperature differentials of as much as F. are not unusual.
As shown the vortex tube 28 comprises a generator chamber 30 and a vortex generator 32 having a tangential inlet 34 through which the high pressure gases gain access to the central tubular channel 36 of the vortex tube. The gases are cause-d to spiral through the tube so the cooler portions of the gas collect in a central stream and the warmer portions collect in an outer iannular stream The central cooler stream is extracted through a central restriction 38 and passes to `atmosphere through outlet conduit 40. Hotter portions of the flue gas pass outwardly through the outer re'striction 42 to a hot gas feed back line 44.
Feed back line 44 Supplies the hotter portion of the exhaust or flue gases to the inlet conduit 12 where these hotter portions are mixed with the incoming air supplied to a blower 14 and tend to preheat this air. In operation, the air-fuel mixture feed to the combustion chamber is controlled so that it contains approxim-ately 200% excess air. This excess air serves to sustain complete combustion and further lowers the temperature in the combustion chamber to an acceptable Value.
The combustion chamber and Vortex tube are surrounded by an insulating jacket 46 containing a heat exchange fluid such `ras water as indicated at 48 which takes heat produced in the combustion chamber from the outer surface of the vortex tube 36 and from the hot gas feed back line '44. Cold water may be supplied to the Water jacket through inlet 50 from a suitable supply and the hot water is drawn oli through 'outlet conduit 52.
In operation, as the air fuel mixture burns in the com bustion chamber the pressure in the chamber -rises` forcing the flue gases into the vortex generator of the vortex tube. Water is circulated over the chamber and tube extracting heat to be used for any suitable hot Water heating system application such as tap water or for use in a hot water type radiant heating system. The products of combustion are removed from the center :or colder section of the vortex tube through outlet conduit 40. The excess air tends to be retained in the outer air stream of the vortex tube and is returned to the high pressure side lOf the combustion chamber.
FIGURE 2 shows a schematic diagram of a modified embodment of the heating system of the present invention with like elements bearing like reference numerals. In the system of FIGURE 2-the blower is eliminated and in its place the combustion chamber -is fed by means of a novel injecter and check valve arrangement. As in the embodiment of FIGURE 1, water to be heated is circulated through the jacket 46 from inlet conduit 50 by suitable means such as the circulating pump 54 and is drawn off through Conduit 52.
The hotter portion of the exhaust or flue gases is drawn off from the periphery of the Hilsch tube and fed back through line 44. A portion of the combustion products is fed through pipe 58 from the combustion chamber 24 into a converging-diverging nozzle 60 where the combustion products attain supersonic velocities. The stream of high velocity combustion products impinges on ambient air supplied by way of line 62 and check valve 64 imparting velocity to the air molecules. The air and combustion products enter a diffuser 66 where they are compressed to a pressure higher than the pressure existing in the combustion chamber. This high pressure air and combustion mixture then picks up the fuel at the throat of venturi 68 and enters the combustion chamber through line 70 to sustain the steady flow combustion process. In so doing the mixture passes through check valves 72 and 74.
The fuel is fed from a suitable source to line 75 and through a venturi 76 where it picks up a small amount of ambient air from line 78. The fuel and small quantity of ambient air enter the system at venturi 68 between the two check valves 72 and 74. The air-fuel mixture supplied by way of venturi 68 into the combustion chamber is adequate during the starting of the furnace. However, once the furnace is started the gases flowing through the injecter comprising nozzle 60 'and diffuser 66 acts to pull more air from line 62. The increased pull of :air from line 62 in turn acts to pull rnore fuel by way of Venturi 68 as it passes through the venturi between the check valves and the system automatically builds up to an Operating level. The check valve 64 in the air line serves only to prevent reverse flow in the event of a malfunction in the injecter.
It is apparent from the above that the present invention provides a novel heating system of substantially increased etficiency which theoretically may possess a thermal eiiiciency greater than 100% by actually cooling down the exhaust gases below ambient temperature. An important feature of the present invention is the selective feed back of a hot component of exhaust gas to the combustion chamber inlet with the separation of the exhaust gas into a hot component being accompanied by a separation of the remaining portion of the exhaust gas into a colder component.
The invention may be embodied in other specific forms without departing from the spirit or essential characteristics thereof. The present ernbodiments are therefore to be considered in all respects as illustrative and not restrictive, the scope of the invention being ndicated by the apperded claims rather than by the foregoing description, and all changes which come within the meaning and range of equivalency of the claims are therefore intended to be embraced therein.
What is claimed and desired to be Secured by United States Letters Patent is:
1. A furnace system comprising a combustion chamber, means for supplying fuel to said chamber, means forming an output path for combustion products from said chamber, means in said path for dividing the combustion products into relatively hot and cold components and means for feeding at least a portion of said hot component back to said combustion chamber.
2. A system according to claim 1 wherein said combustion chamber includes means forming a fuel input, and means for mixing said feed back portion with fuel at the input to said combustion chamber.
3. A furnace system comprising a combustion chamber including means forming a fuel input, means for supplying a combustion gas to said chamber, means forming an output path for combustion products from said chamber, a vortex tube in said path for dividing the combustion products into relatively hot and cold components and means for feeding =at least a portion of said hot component back to the input of said combustion chamber.
4. A system according to claim 3 including means for mixing said feed back portion with said combustion gas to preheat said gas prior to its entrance into said chamber.
5. A system according to claim 4 wherein said vortex tube is of the uniflow type having hot and cold gas outlets at the same end of the tube.
6. A system according to claim 5 including means for maintaining a circulating heat transfer medium in heat xchange relation with the outer surface of said vortex tube and said hot component feed back means.
7. A system according to claim 6 wherein said heat exchange medium `is water.
8. A furnace system comprising a combustion chamber, a blower for supplying air to said chamber, a fuel inlet to said chamber, means forming an output path for combustion products from said chamber, a vortex tube in said path for dividing the combustion products into relatively hot and cold components and a feed back line connecting the periphery of said vortex tube with the input of said blower whereby the hot component of said combustion products is fed back to preheat the air passing through said blower into said combustion chamber.
9. A system according to claim 8 wherein fuel is supplied to said combustion chamber through a venturi inserted between said blower and said chamber.
10. A furnace system according to claim 9 including means for maintaining a heat exchange fluid medium in contact with the outer surface of said vortex tube and the outer surface of said feed -back line.
11. A furnace system comprising a combustion chamber, means forming an air-fuel mixture `inlet to said chamber, means forming an output path for combustion products from said chamber, a vortex tube in said path -for dividing the combustion products into relatively hot and cold components, means for feedin'g a portion of the combustion products from said chamber through a return line to said mixture inlet, and means for feeding back said hot component from the periphery of said vortex tube to said return line.
12. A system according to claim ll wherein said return line includes a nozzle capable of passing uids at supersonic velocities and said hot component enters said return line at the output 'of said nozzle.
13. A system according to claim 12 wherein said nozzle feeds a difuser wherein said hot components are compressed above the pressure in said combustion chamber.
14. A system according to claim 13 including means for maintaining a heat exchange fluid medium in constaet with the outer surface of said vortex tube and said hot component feed 'back means.
References Cited in the file of this patent UNITED STATES PATENTS %4,031 Leahy July 12, 1910 1,719,684 Besta July 2, 1929 l,753,432 Isom Apr. 8, 1930 1,837,7l3 Jacobus Dec. 22, 1931 1,952,28l Ranque Mar. 27, 1934 FOREIGN PATENTS 1,1l9,245 France Apr. 3, 1956
Claims (1)
1. A FURNACE SYSTEM COMPRISING A CUMBUSTION CHAMBER, MEANS FOR SUPPLYING FUEL TO SAID CHAMBER, MEANS FORMING AN OUTPUT PATH FOR COMBUSTION PRODUCTS FROM SAID CHAMBER, MEANS IN SAID PATH FOR DRIVING THE COMBUSTION PRODUCTS INTO RELATIVELY HOT AND COLD COMPONENTS AND MEANS FOR FEEDING AT LEAST A PORTION OF SAID HOT COMPONENT BACK TO SAID COMBUSTION CHAMBER.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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US28588A US3097686A (en) | 1960-05-12 | 1960-05-12 | Furnace system |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
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US28588A US3097686A (en) | 1960-05-12 | 1960-05-12 | Furnace system |
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US3097686A true US3097686A (en) | 1963-07-16 |
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US28588A Expired - Lifetime US3097686A (en) | 1960-05-12 | 1960-05-12 | Furnace system |
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Cited By (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3397028A (en) * | 1966-08-11 | 1968-08-13 | Bbc Brown Boveri & Cie | High-temperature fuel element apparatus |
US3456438A (en) * | 1966-10-04 | 1969-07-22 | Philips Corp | Thermodynamic engine |
US3516807A (en) * | 1966-04-06 | 1970-06-23 | Texas Instruments Inc | Apparatus for producing hydrogen gas by the partial oxidation of a carbonaceous fuel containing hydrogen |
US4089629A (en) * | 1975-02-12 | 1978-05-16 | Pietro Fascione | Process and apparatus for controlled recycling of combustion gases |
US4995807A (en) * | 1989-03-20 | 1991-02-26 | Bryan Steam Corporation | Flue gas recirculation system |
US5269679A (en) * | 1992-10-16 | 1993-12-14 | Gas Research Institute | Staged air, recirculating flue gas low NOx burner |
US5350293A (en) * | 1993-07-20 | 1994-09-27 | Institute Of Gas Technology | Method for two-stage combustion utilizing forced internal recirculation |
US5413477A (en) * | 1992-10-16 | 1995-05-09 | Gas Research Institute | Staged air, low NOX burner with internal recuperative flue gas recirculation |
US5584182A (en) * | 1994-04-02 | 1996-12-17 | Abb Management Ag | Combustion chamber with premixing burner and jet propellent exhaust gas recirculation |
US5623829A (en) * | 1996-01-17 | 1997-04-29 | Btu International | Vortex tube cooling system for solder reflow convection furnaces |
US5666944A (en) * | 1993-06-17 | 1997-09-16 | Pvi Industries, Inc. | Water heating apparatus with passive flue gas recirculation |
US20040033460A1 (en) * | 2002-08-14 | 2004-02-19 | Roger Lanary | Burner and method of burning gas in a furnace |
US20090057434A1 (en) * | 2007-08-29 | 2009-03-05 | Rafael MUSTAFAEV | Fluid heater |
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US1719684A (en) * | 1929-07-02 | of dttisbttbg | ||
US1753432A (en) * | 1927-05-25 | 1930-04-08 | Sinclair Refining Co | Art of cracking hydrocarbons |
US1837713A (en) * | 1926-03-09 | 1931-12-22 | Fuller Lehigh Co | Furnace and method of operating the same |
US1952281A (en) * | 1931-12-12 | 1934-03-27 | Giration Des Fluides Sarl | Method and apparatus for obtaining from alpha fluid under pressure two currents of fluids at different temperatures |
FR1119245A (en) * | 1955-01-07 | 1956-06-18 | Heurtey & Cie | Method for controlling the temperature of a heated enclosure and devices applying this method |
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US1719684A (en) * | 1929-07-02 | of dttisbttbg | ||
US964031A (en) * | 1904-05-31 | 1910-07-12 | Louis K Leahy | Liquid-hydrocarbon-burning apparatus. |
US1837713A (en) * | 1926-03-09 | 1931-12-22 | Fuller Lehigh Co | Furnace and method of operating the same |
US1753432A (en) * | 1927-05-25 | 1930-04-08 | Sinclair Refining Co | Art of cracking hydrocarbons |
US1952281A (en) * | 1931-12-12 | 1934-03-27 | Giration Des Fluides Sarl | Method and apparatus for obtaining from alpha fluid under pressure two currents of fluids at different temperatures |
FR1119245A (en) * | 1955-01-07 | 1956-06-18 | Heurtey & Cie | Method for controlling the temperature of a heated enclosure and devices applying this method |
Cited By (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3516807A (en) * | 1966-04-06 | 1970-06-23 | Texas Instruments Inc | Apparatus for producing hydrogen gas by the partial oxidation of a carbonaceous fuel containing hydrogen |
US3397028A (en) * | 1966-08-11 | 1968-08-13 | Bbc Brown Boveri & Cie | High-temperature fuel element apparatus |
US3456438A (en) * | 1966-10-04 | 1969-07-22 | Philips Corp | Thermodynamic engine |
US4089629A (en) * | 1975-02-12 | 1978-05-16 | Pietro Fascione | Process and apparatus for controlled recycling of combustion gases |
US4995807A (en) * | 1989-03-20 | 1991-02-26 | Bryan Steam Corporation | Flue gas recirculation system |
US5269679A (en) * | 1992-10-16 | 1993-12-14 | Gas Research Institute | Staged air, recirculating flue gas low NOx burner |
US5413477A (en) * | 1992-10-16 | 1995-05-09 | Gas Research Institute | Staged air, low NOX burner with internal recuperative flue gas recirculation |
US5666944A (en) * | 1993-06-17 | 1997-09-16 | Pvi Industries, Inc. | Water heating apparatus with passive flue gas recirculation |
US5350293A (en) * | 1993-07-20 | 1994-09-27 | Institute Of Gas Technology | Method for two-stage combustion utilizing forced internal recirculation |
US5584182A (en) * | 1994-04-02 | 1996-12-17 | Abb Management Ag | Combustion chamber with premixing burner and jet propellent exhaust gas recirculation |
US5623829A (en) * | 1996-01-17 | 1997-04-29 | Btu International | Vortex tube cooling system for solder reflow convection furnaces |
WO1997026489A1 (en) * | 1996-01-17 | 1997-07-24 | Btu International, Inc. | Vortex tube cooling system for furnaces |
US20040033460A1 (en) * | 2002-08-14 | 2004-02-19 | Roger Lanary | Burner and method of burning gas in a furnace |
US7429173B2 (en) * | 2002-08-14 | 2008-09-30 | Hamworthy Combustion Engineering Limited | Burner and method of burning gas in a furnace |
US20090057434A1 (en) * | 2007-08-29 | 2009-03-05 | Rafael MUSTAFAEV | Fluid heater |
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