US2634804A - Apparatus for generating heat - Google Patents
Apparatus for generating heat Download PDFInfo
- Publication number
- US2634804A US2634804A US250764A US25076451A US2634804A US 2634804 A US2634804 A US 2634804A US 250764 A US250764 A US 250764A US 25076451 A US25076451 A US 25076451A US 2634804 A US2634804 A US 2634804A
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- Prior art keywords
- fuel
- air
- valve
- combustion chamber
- chamber
- Prior art date
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- Expired - Lifetime
Links
- 239000000446 fuel Substances 0.000 description 56
- 238000002485 combustion reaction Methods 0.000 description 28
- 238000010438 heat treatment Methods 0.000 description 10
- 239000007788 liquid Substances 0.000 description 9
- 238000004891 communication Methods 0.000 description 8
- 238000013022 venting Methods 0.000 description 7
- 239000004215 Carbon black (E152) Substances 0.000 description 2
- 230000005611 electricity Effects 0.000 description 2
- 229930195733 hydrocarbon Natural products 0.000 description 2
- 150000002430 hydrocarbons Chemical class 0.000 description 2
- 238000010276 construction Methods 0.000 description 1
- 230000001419 dependent effect Effects 0.000 description 1
- 238000010304 firing Methods 0.000 description 1
- 239000012530 fluid Substances 0.000 description 1
- 239000007789 gas Substances 0.000 description 1
- 230000005484 gravity Effects 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000011084 recovery Methods 0.000 description 1
- 230000000452 restraining effect Effects 0.000 description 1
- 230000003068 static effect Effects 0.000 description 1
Images
Classifications
-
- 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
- F24H3/00—Air heaters
- F24H3/006—Air heaters using fluid fuel
Definitions
- This invention relates to a heating apparatus and more particularly to an apparatus for burning liquid or gaseous fuel and producing a maximum yield of heat therefrom.
- the principal object of the invention is the provision of an apparatus for burning a gaseous or liquid fuel in a closed container so as to retain a maximum recovery of heat therefrom.
- a further object of the invention is the provision of an apparatus for burning fuel under controlled conditions and in a stationary atmosphere.
- a still further object of the invention is the provision of an apparatus for burning fuel in a closed container and holding the said burning fuel charge in the said container until the mechanical energy thereof has been translated into heat energy capable of being recovered from the said container.
- the apparatus for burning liquid or gaseous fuel disclosed herein comprises a means of efficiently heating a desired medium through the automatic charging and burning of fuel in a container capable of holding the burning fuel charge and restraining its mechanical energy line or other liquid hydrocarbon.
- the combustion chamber of the device may be utilized for heating air by direct convection or for the purpose of heating a fluid heating medium as desired and the entire device may be formed of relatively simple and inexpensive parts and is of relatively small size in comparison with its heating ability.
- Figure 1 is a plan view with parts broken away and parts in cross section.
- Figure 2 is a horizontal section taken on line 2-2 of Figure 1.
- a circular base l0 has a cylindrical body member forming a combustion chamber H mounted thereon and preferably formed integrally therewith.
- the cylindrical combustion chamber H is preferably provided with heat dissipating fins I2 and is closed at its upper end by a head I3.
- the lower end of the base it forms a closure l4 defining the opposite end wall of the combustion chamber II.
- the head l3 has a venting chamber I5 formed therein as defined by side walls It and an uppermost closure H.
- An exhaust pipe l8 communicates with the venting chamber l5 on one side thereof and an air inlet pipe 153 communicates with the venting chamber on the opposite side thereof.
- a valve 26 normally closes the air inlet pipe H9.
- the head It carries a central vertical body member 2! which positions vertically arranged and horizontally disposed pairs of rollers 22 which serve as movable guides for a valve stem 23, the lower portion of which defines a valve 24. It will be observed that the valve 24 is disposed within a conical restricted upper end portion of the head i3 and is movable vertically against the same so as to close the passageway normally existing between the combustion chamber II and the vent chamber [5 and through the body member 2
- valve stem 23 has a pair of spaced nuts 25 threaded thereon and a bifurcated arm 26 is engaged therebetween, it being observed that the bifurcated arm is integrally formed with the valve 20 and pivoted as at 21 to one of the walls iii of the venting chamber.
- the weight of the valve 24, valve stem 23 and the arm 26 is sufficient to normally maintain the valve 2% in closed position with respect to the air inlet pipe Q9.
- the head i3 is apertured for the reception of spark plugs 28 and they are electrically connected with a suitable power source-in series connection with a switch 29.
- Fuel is introduced into the base Id of the combustion chamber ll through an inlet orifice 3i) which is located at an angle to the point of communication with the base l6 so that fuel introduced thereinto will travel in a circular motion, as shown by the arrows in Figure 2 of the drawings.
- the fuel is supplied from a fuel line 3! which is in communication with a float valve 32, the float portion 33 of which rides the liquid level in a fuel receiving bowl 34.
- a fuel delivering bowl 35 is in communication with the fuel receiving bowl 34 by way of an intercommunicating passageway 36 which incorpo- 3 rates a check valve 31 permitting flow of fuel from the fuel receiving bowl 34 to the fuel delivering bowl 35.
- a fuel delivering pipe 38 extends from a point near the bottom of the fuel delivering bowl 35 to a nozzle 39 positioned in a mixing chamber 40 and defined by a hollow body member M.
- a check valve 42 permits fuel from the pipe 38 to flow into the nozzle 39 but does not permit fuel or pressure to move from the nozzle 39 into the pipe 38.
- Compressed air is delivered to the mixing chamber 40 from the air supply line I9 and through a check valve 43 which permits air to flow into the mixing chamber 40 but does not permit air or pressure to flow backwardly into the air supply line I9.
- the fuel receiving bowl 35 is also in communication with the air supply line I9 as is the switch 29 which is normally biased to open position by a spring 44 and which closes when air pressure in the supply line I9 reaches a predetermined point.
- an air compressor 45 is provided in order that the air pressure in the air supply line I9 can be maintained.
- valve 20 is held in open position by the valve 24 '4 having been moved upwardly into closed position against the head I3.
- Such action bleeds the air line I9 through the venting chamber I5 and the exhaust pipe I8 thus reducing the pressure in the air line I9 to approximately atmospheric pressure and at the same time conveying any fuel charge remaining in the venting chamber I5 outwardly and away therefrom.
- valve 24 When the burning fuel charge has given up its energy in the form of heat through the fins I2 and the pressure in the chamber II has dropped, the valve 24 will again open by gravity action which closes the valve 20 and permits the compressor 45 to re-establish pressure in the air pipe I9 and the device re-cycles.
- the operation of the device is dependent upon the alternate rise and fall of air pressure in the air supply line I9 as the falling of the pressure therein at such time as the valve 20 is open permits the fuel to refill the fuel delivery'bowl 35 by the introduction of a sufficient quantity of fuel therein for the subsequent charging portion of the cycle.
- the pressure switch 29 operates responsive to the fluctuation of the air pressure in the supply line I9, thus alternately energizing and de-energizing the spark plugs 28 at the proper times.
- the firing interval of the apparatus as herein disclosed will run approximately 15 to 20 seconds, a majority of this time comprising the period of heat transfer necessary to dissipate the fuel energy to a point sufiicient to permit the valve 24 to open and the re-cycling of the device to begin.
- the compressor 45 is preferably of the continuous duty type and is driven by a suitable integrally formed electric motor also of the continuous duty type and it will be observed by those skilled in the art that the cost of operating the device is relatively low compared with the quantity of heat produced therefrom.
- relatively small sized apparatus efficiently converts the fuel energy to heat energy which may be used in a desired manner.
- Heating apparatus comprising a combustion chamber, a mixing device for introducing air and fuel into said combustion chamber, valves in said mixing device preventing flow of air and fuel from said combustion chamber, said combustion chamber having an outlet opening therein and a valve arranged partly within said combustion chamber to close said opening responsive to pressure generated by combustion in said chamber and a spark plug in said combustion chamber for igniting a fuel charge therein.
- An automatically re-cycling heating apparatus comprising in combination a combustion chamber, a mixing device for introducing air and fuel mixtures thereinto, valves in said mixing device preventing return flow therethrough, said combustion chamber having an outlet opening therein and a valve arranged to close said opening upon combustion occurring in said chamber, a spark plug in said combustion chamber, a source of electricity for said spark plug, a secondary valve connected to and operated by said first named valve, said secondary valve responsive in opening to closing motion of said first named valve, a source of air pressure and an air line in communication with said source and said secondary valve, a pressure operated switch in communication with said air line and controlling said electricity source a source of liquid fuel in communication with said mxing device, said air line in communcation with said source of fuel and said mixer whereby opening of said secondary valve responsive to closing of said first named valve vents said air line and opens said pressure switch and stops fiow of fuel to said mixing device.
- the heating apparatus disclosed in claim 2 and further characterized by the source of liquid fuel comprising a fuel delivering bowl having a discharge pipe terminating near the bottom thereof and a relatively larger liquid receiving area thereabout defining a relatively large air pressure chamber thereabove.
Description
April 14, 1953 H. ERICKSON 2,634,304
APPARATUS FOR GENERATING HEAT Filed Oct. 10, 1951 if I g E.
INVENTOR.
flan/y 576/4600.
Patented Apr. 14, 1953 UNITED STATES TENT OFFICE 4' Claims. I
This invention relates to a heating apparatus and more particularly to an apparatus for burning liquid or gaseous fuel and producing a maximum yield of heat therefrom.
The principal object of the invention is the provision of an apparatus for burning a gaseous or liquid fuel in a closed container so as to retain a maximum recovery of heat therefrom.
A further object of the invention is the provision of an apparatus for burning fuel under controlled conditions and in a stationary atmosphere.
A still further object of the invention is the provision of an apparatus for burning fuel in a closed container and holding the said burning fuel charge in the said container until the mechanical energy thereof has been translated into heat energy capable of being recovered from the said container.
The apparatus for burning liquid or gaseous fuel disclosed herein comprises a means of efficiently heating a desired medium through the automatic charging and burning of fuel in a container capable of holding the burning fuel charge and restraining its mechanical energy line or other liquid hydrocarbon. The combustion chamber of the device may be utilized for heating air by direct convection or for the purpose of heating a fluid heating medium as desired and the entire device may be formed of relatively simple and inexpensive parts and is of relatively small size in comparison with its heating ability.
With the foregoing and other objects in view which will appear as the description proceeds, the invention resides in the combination and arrangement of parts and in the details of construction hereinafter described and claimed, it being the intention to cover all changes and modifications of the example of the invention herein chosen for purposes of the disclosure, which do not constitute departures from the spirit and scope of the invention.
The invention is illustrated in the accompanying drawing, wherein:
Figure 1 is a plan view with parts broken away and parts in cross section.
Figure 2 is a horizontal section taken on line 2-2 of Figure 1.
By referring to the drawings and Figure 1 in particular it will be seen that a circular base l0 has a cylindrical body member forming a combustion chamber H mounted thereon and preferably formed integrally therewith. The cylindrical combustion chamber H is preferably provided with heat dissipating fins I2 and is closed at its upper end by a head I3. The lower end of the base it forms a closure l4 defining the opposite end wall of the combustion chamber II. The head l3 has a venting chamber I5 formed therein as defined by side walls It and an uppermost closure H. An exhaust pipe l8 communicates with the venting chamber l5 on one side thereof and an air inlet pipe 153 communicates with the venting chamber on the opposite side thereof. A valve 26 normally closes the air inlet pipe H9.
The head It carries a central vertical body member 2! which positions vertically arranged and horizontally disposed pairs of rollers 22 which serve as movable guides for a valve stem 23, the lower portion of which defines a valve 24. It will be observed that the valve 24 is disposed within a conical restricted upper end portion of the head i3 and is movable vertically against the same so as to close the passageway normally existing between the combustion chamber II and the vent chamber [5 and through the body member 2|.
The upper end of the valve stem 23 has a pair of spaced nuts 25 threaded thereon and a bifurcated arm 26 is engaged therebetween, it being observed that the bifurcated arm is integrally formed with the valve 20 and pivoted as at 21 to one of the walls iii of the venting chamber. The weight of the valve 24, valve stem 23 and the arm 26 is sufficient to normally maintain the valve 2% in closed position with respect to the air inlet pipe Q9.
The head i3 is apertured for the reception of spark plugs 28 and they are electrically connected with a suitable power source-in series connection with a switch 29.
Fuel is introduced into the base Id of the combustion chamber ll through an inlet orifice 3i) which is located at an angle to the point of communication with the base l6 so that fuel introduced thereinto will travel in a circular motion, as shown by the arrows in Figure 2 of the drawings. The fuel is supplied from a fuel line 3! which is in communication with a float valve 32, the float portion 33 of which rides the liquid level in a fuel receiving bowl 34. A fuel delivering bowl 35 is in communication with the fuel receiving bowl 34 by way of an intercommunicating passageway 36 which incorpo- 3 rates a check valve 31 permitting flow of fuel from the fuel receiving bowl 34 to the fuel delivering bowl 35. A fuel delivering pipe 38 extends from a point near the bottom of the fuel delivering bowl 35 to a nozzle 39 positioned in a mixing chamber 40 and defined by a hollow body member M. A check valve 42 permits fuel from the pipe 38 to flow into the nozzle 39 but does not permit fuel or pressure to move from the nozzle 39 into the pipe 38.
Compressed air is delivered to the mixing chamber 40 from the air supply line I9 and through a check valve 43 which permits air to flow into the mixing chamber 40 but does not permit air or pressure to flow backwardly into the air supply line I9. The fuel receiving bowl 35 is also in communication with the air supply line I9 as is the switch 29 which is normally biased to open position by a spring 44 and which closes when air pressure in the supply line I9 reaches a predetermined point. In order that the air pressure in the air supply line I9 can be maintained, an air compressor 45 is provided.
In operation, fuel from the fuel receiving bowl 34 flows through the check valve 36 and into the fuel delivering bowl 35 to establish the same level therein as present in the fuel receiving bowl 34. Air from the compressor 45 flows through the line I9 and through the check valve 43, into the mixing chamber 40 and through the orifice 30 into the chamber II. The air flows upwardly through the head I3, the guide member 2I and into the venting chamber I and outwardly through the exhaust pipe I8. At the normal operating pressures of the compressor 45 the valve 24 remains open and the combustion chamber II is thus in communication with the atmosphere through the exhaust pipe I8.
Simultaneously with the delivering of air into the mixing chamber 49, air is delivered to the fuel delivering bowl 35. As the air pressure is established therein, the check valve 31 closes and the air forces the fuel outwardly through the pipe 38 and the nozzle 39 and into the mixing chamber 40 where it is atomized and conveyed along with the air into the combustion chamber by way of the orifice 30. As heretofore mentioned, the introduction of the fuel charge is in a rotating manner, as shown in Figure 2 of the drawings.
As the fuel charge is carried upwardly through the combustion chamber, air pressure in the line I9 overcomes the tension of the spring 44 in the pressure switch 29 and closes the circuit energizing the spark plugs 28 whereupon the fuel charge in the combustion chamber II is ignited. The ignition of the fuel charge results in an initial expanding action of the burning gases of the same which immediately closes the valve 24 and the check valves 42 and 43 which control the fuel and air lines communicating with the mixing chamber 40. The combustion chamber II is thus closed with respect to the atmosphere as well as the air and fuel lines and the fuel charge burns in the closed combustion chamber II. The cylindrical body member defining the combustion chamber II is sufficiently strong to hold the increasing pressures of the burning fuel charge and the mechanical energy thus being restrained is required to give off its energy in the form of heat.
During the time of the burning of the fuel charge in the combustion chamber II, the valve 20 is held in open position by the valve 24 '4 having been moved upwardly into closed position against the head I3. Such action bleeds the air line I9 through the venting chamber I5 and the exhaust pipe I8 thus reducing the pressure in the air line I9 to approximately atmospheric pressure and at the same time conveying any fuel charge remaining in the venting chamber I5 outwardly and away therefrom.
When the burning fuel charge has given up its energy in the form of heat through the fins I2 and the pressure in the chamber II has dropped, the valve 24 will again open by gravity action which closes the valve 20 and permits the compressor 45 to re-establish pressure in the air pipe I9 and the device re-cycles.
It will thus be seen that the operation of the device is dependent upon the alternate rise and fall of air pressure in the air supply line I9 as the falling of the pressure therein at such time as the valve 20 is open permits the fuel to refill the fuel delivery'bowl 35 by the introduction of a sufficient quantity of fuel therein for the subsequent charging portion of the cycle. It will also be seen that the pressure switch 29 operates responsive to the fluctuation of the air pressure in the supply line I9, thus alternately energizing and de-energizing the spark plugs 28 at the proper times.
It has been determined that the firing interval of the apparatus as herein disclosed will run approximately 15 to 20 seconds, a majority of this time comprising the period of heat transfer necessary to dissipate the fuel energy to a point sufiicient to permit the valve 24 to open and the re-cycling of the device to begin.
The compressor 45 is preferably of the continuous duty type and is driven by a suitable integrally formed electric motor also of the continuous duty type and it will be observed by those skilled in the art that the cost of operating the device is relatively low compared with the quantity of heat produced therefrom. In burning such liquid hydrocarbon fuels as gasoline, for example, relatively small sized apparatus efficiently converts the fuel energy to heat energy which may be used in a desired manner.
It will thus be seen that a novel apparatus for burning fuel in a static condition under completely automatic control has been disclosed and which apparatus meets the several objects of the invention.
Having thus described my invention, what I claim is:
1. Heating apparatus comprising a combustion chamber, a mixing device for introducing air and fuel into said combustion chamber, valves in said mixing device preventing flow of air and fuel from said combustion chamber, said combustion chamber having an outlet opening therein and a valve arranged partly within said combustion chamber to close said opening responsive to pressure generated by combustion in said chamber and a spark plug in said combustion chamber for igniting a fuel charge therein.
2. An automatically re-cycling heating apparatus comprising in combination a combustion chamber, a mixing device for introducing air and fuel mixtures thereinto, valves in said mixing device preventing return flow therethrough, said combustion chamber having an outlet opening therein and a valve arranged to close said opening upon combustion occurring in said chamber, a spark plug in said combustion chamber, a source of electricity for said spark plug, a secondary valve connected to and operated by said first named valve, said secondary valve responsive in opening to closing motion of said first named valve, a source of air pressure and an air line in communication with said source and said secondary valve, a pressure operated switch in communication with said air line and controlling said electricity source a source of liquid fuel in communication with said mxing device, said air line in communcation with said source of fuel and said mixer whereby opening of said secondary valve responsive to closing of said first named valve vents said air line and opens said pressure switch and stops fiow of fuel to said mixing device.
3. The heating apparatus disclosed in claim 2 and further characterized by the source of liquid fuel comprising a fuel delivering bowl having a discharge pipe terminating near the bottom thereof and a relatively larger liquid receiving area thereabout defining a relatively large air pressure chamber thereabove.
4. The heating apparatus disclosed in claim 2 and wherein said first named valve is mounted without said combustion chamber and extends within said combustion chamber through said outlet opening thereof and is movable into said outlet opening and wherein said secondary valve is without said combustion chamber.
HENRY L. ERICKSON.
References Cited in the file of this patent UNITED STATES PATENTS
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US250764A US2634804A (en) | 1951-10-10 | 1951-10-10 | Apparatus for generating heat |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US250764A US2634804A (en) | 1951-10-10 | 1951-10-10 | Apparatus for generating heat |
Publications (1)
Publication Number | Publication Date |
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US2634804A true US2634804A (en) | 1953-04-14 |
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ID=22949047
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Application Number | Title | Priority Date | Filing Date |
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US250764A Expired - Lifetime US2634804A (en) | 1951-10-10 | 1951-10-10 | Apparatus for generating heat |
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US (1) | US2634804A (en) |
Cited By (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2959214A (en) * | 1954-11-15 | 1960-11-08 | Swingfire Ltd | Pulse jet apparatus |
US3600116A (en) * | 1969-08-01 | 1971-08-17 | Southwest Res Inst | Air-control system for apparatus displacing material by combustive explosions |
US4281982A (en) * | 1980-02-19 | 1981-08-04 | Institute Of Gas Technology | Method and apparatus of heat-pulsed recuperation of energy |
US4334485A (en) * | 1979-07-30 | 1982-06-15 | Guida Frank C | Method for generating heat energy by intermittent smoke charge combustion |
WO1982002242A1 (en) * | 1980-12-22 | 1982-07-08 | Davis Robert E | Improvements in pulsing combustion |
US4480985A (en) * | 1980-12-22 | 1984-11-06 | Arkansas Patents, Inc. | Pulsing combustion |
US4488865A (en) * | 1980-12-22 | 1984-12-18 | Arkansas Patents, Inc. | Pulsing combustion |
US4556383A (en) * | 1979-09-26 | 1985-12-03 | Stahl Karl Heinz | Resonant burner and starting mechanism therefor |
US4568264A (en) * | 1983-01-14 | 1986-02-04 | Lennox Industries, Inc. | Combustion chamber construction |
US4637792A (en) * | 1980-12-22 | 1987-01-20 | Arkansas Patents, Inc. | Pulsing combustion |
US4651712A (en) * | 1985-10-11 | 1987-03-24 | Arkansas Patents, Inc. | Pulsing combustion |
US4780076A (en) * | 1985-10-11 | 1988-10-25 | Arkansas Patents, Inc. | Power burner |
US5921765A (en) * | 1997-06-30 | 1999-07-13 | Atoliv Asp, Inc. | Periodic, on-demand pressurized gas power source and method of providing same |
Citations (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1051363A (en) * | 1912-01-05 | 1913-01-21 | Emil Anderson | Generator. |
US1052588A (en) * | 1911-04-12 | 1913-02-11 | John Janicki | Hydrocarbon power-generator. |
US1137328A (en) * | 1907-07-18 | 1915-04-27 | Irving C Jennings | Internal-combustion generator. |
US1811654A (en) * | 1925-10-15 | 1931-06-23 | Nat Cold Steam Company | Internally fired heat or power generator |
US2165269A (en) * | 1936-03-11 | 1939-07-11 | Stewart Warner Corp | Automobile heater |
US2175866A (en) * | 1934-04-16 | 1939-10-10 | Philip S Arnold | Fuel burner |
US2235967A (en) * | 1938-04-18 | 1941-03-25 | James J Sunday | Heating system |
US2247977A (en) * | 1938-01-03 | 1941-07-01 | Clarence W Uschold | Oil burning apparatus |
US2414828A (en) * | 1943-07-21 | 1947-01-28 | Stewart Warner Corp | Heating system |
US2553091A (en) * | 1948-09-11 | 1951-05-15 | Harold R Horning | Heater |
-
1951
- 1951-10-10 US US250764A patent/US2634804A/en not_active Expired - Lifetime
Patent Citations (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1137328A (en) * | 1907-07-18 | 1915-04-27 | Irving C Jennings | Internal-combustion generator. |
US1052588A (en) * | 1911-04-12 | 1913-02-11 | John Janicki | Hydrocarbon power-generator. |
US1051363A (en) * | 1912-01-05 | 1913-01-21 | Emil Anderson | Generator. |
US1811654A (en) * | 1925-10-15 | 1931-06-23 | Nat Cold Steam Company | Internally fired heat or power generator |
US2175866A (en) * | 1934-04-16 | 1939-10-10 | Philip S Arnold | Fuel burner |
US2165269A (en) * | 1936-03-11 | 1939-07-11 | Stewart Warner Corp | Automobile heater |
US2247977A (en) * | 1938-01-03 | 1941-07-01 | Clarence W Uschold | Oil burning apparatus |
US2235967A (en) * | 1938-04-18 | 1941-03-25 | James J Sunday | Heating system |
US2414828A (en) * | 1943-07-21 | 1947-01-28 | Stewart Warner Corp | Heating system |
US2553091A (en) * | 1948-09-11 | 1951-05-15 | Harold R Horning | Heater |
Cited By (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2959214A (en) * | 1954-11-15 | 1960-11-08 | Swingfire Ltd | Pulse jet apparatus |
US3600116A (en) * | 1969-08-01 | 1971-08-17 | Southwest Res Inst | Air-control system for apparatus displacing material by combustive explosions |
US4334485A (en) * | 1979-07-30 | 1982-06-15 | Guida Frank C | Method for generating heat energy by intermittent smoke charge combustion |
US4556383A (en) * | 1979-09-26 | 1985-12-03 | Stahl Karl Heinz | Resonant burner and starting mechanism therefor |
US4281982A (en) * | 1980-02-19 | 1981-08-04 | Institute Of Gas Technology | Method and apparatus of heat-pulsed recuperation of energy |
US4480985A (en) * | 1980-12-22 | 1984-11-06 | Arkansas Patents, Inc. | Pulsing combustion |
US4479484A (en) * | 1980-12-22 | 1984-10-30 | Arkansas Patents, Inc. | Pulsing combustion |
US4488865A (en) * | 1980-12-22 | 1984-12-18 | Arkansas Patents, Inc. | Pulsing combustion |
WO1982002242A1 (en) * | 1980-12-22 | 1982-07-08 | Davis Robert E | Improvements in pulsing combustion |
US4637792A (en) * | 1980-12-22 | 1987-01-20 | Arkansas Patents, Inc. | Pulsing combustion |
US4568264A (en) * | 1983-01-14 | 1986-02-04 | Lennox Industries, Inc. | Combustion chamber construction |
US4651712A (en) * | 1985-10-11 | 1987-03-24 | Arkansas Patents, Inc. | Pulsing combustion |
US4780076A (en) * | 1985-10-11 | 1988-10-25 | Arkansas Patents, Inc. | Power burner |
US5921765A (en) * | 1997-06-30 | 1999-07-13 | Atoliv Asp, Inc. | Periodic, on-demand pressurized gas power source and method of providing same |
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