PULSE COMBUSTER AND PROCESS

Abstract: A pulse combustor (10) having a combined mixing and ignition chamber (13) in communication with a fuel inlet tube (11) and an air inlet tube (12). A main combustion chamber (15) which first splits into a plurality of downstream combustion chamber branches (16), each of which further split into a plurality of exhaust tubes (20). The combustion chamber branches of the main combustion chamber have a slot (23) between them with at least one reinforcing strut (25) secured between the combustion chamber branches within the slot. Each exhaust tube has an exhaust manifold end in communication with an exhaust manifold (21). The process includes the steps of introducing air through the air inlet flapper valve into a mixing zone. Fuel is introduced through the fuel inlet flapper valve into the mixing zone. A combustible fuel/air mixture is formed within the mixing and ignition chamber and is ignited there to complete combustion within the combustion chamber. Combustion product gases are exhausted through the combustion chamber branches and further exhausted through the exhaust tubes.

Description: Field of the Invention A pulse combustor having a combined mixing and ignition chamber in communication with a combustion chamber having combustion chamber branches. A plurality of exhaust tubes extend from the combustion chamber to an exhaust manifold. A process for pulse combustion in a horizontal pulse combustor having a fuel inlet valve, an air inlet valve, a combustion chamber, and a plurality of downstream combustion chamber branches each having a plurality of downstream exhaust tubes. Description of the Prior Art Pulsing combustion devices and processes are generally known to the art. Putnam et al., U.S. Patent 4,314,444, discloses a two-stage apparatus for burning a fuel and a combustion-sustaining gas. A portion of fuel is burned in a first stage having pulse combustors. The remaining fuel is burned in a second combustion stage with gas that is aspirated using backflow through an aerodynamic valve inlet. The '444 patent discloses a valveless pulse combustor in which the flow of gas in one direction is stronger than the flow of the gas in an opposite direction. The '444 patent teaches a plurality of pulse combustors wherein each pulse combustor has only one combustion chamber and only one outlet conduit. The second combustion stage has one combustion chamber with a multiplicity of exhaust tubes. The '444 patent teaches a vertical arrangement for the heating apparatus. Kitchen, U.S. Patent 4,241,723, discloses a pulse combustion heater having a combustion chamber and at least one exhaust pipe forming a resonant system with a chamber. The combustion chamber is in the form of a one-piece bronze casting having an internal cavity which is generally of flattened spherical shape. Whitacre, U.S. Patent 3,554,182, teaches a liquid heater, especially adapted for liquid submerged uses, for example for heating a swimming pool. The combustion generated is of the pulse type and the combustion chamber in which the fuel-air mixture is ignited has a body of material of high radiating potential, such as ceramic, which is heated in the combustion chamber and which radiates heat to the enclosing heat-conducting walls of the chamber in contact with the liquid to be heated. Severyanin, Russian Patent 826,137, discloses a pulsating combustion unit having an ignition chamber connected to an exhaust chamber through two resonance pipes. One of the resonance pipes has a length which exceeds the length of the other resonance pipe by 3 times to increase combustion efficiency. Combustion products reach the exhaust chamber in an anti-phase thus reducing sound radiation. Davis, U.S. Patent 4,637,792, describes a pulsing combustion device having a combustion chamber and a floating valve member mounted in reciprocal relation in the wall of the combustion chamber where reciprocation of the floating valve closes and opens communication through ports between the supply of a combustible mixture and the combustion chamber. The '792 patent teaches a single elongated combustion chamber burner shell which defines a combustion chamber. Davis, U.S. Patent 4,651,712, teaches a pulsing combustion device having a combustion chamber with an inlet for a combustible mixture and an unvalved outlet open to the atmosphere for combustion gases. The '712 patent describes an elongated combustion chamber shell or burner shell which defines a combustion chamber. The combustible mixture is ignited and burned in a single combustion chamber. Adams, U.S. Patent 4,465,024, and Adams, U.S. Patent 4,545,329, teach a water heater having a water tank with a water inlet, a water outlet, and an opening in the side wall of the tank. The combustion chamber assembly has a submergible portion which is adapted to fit within the opening in the tank side wall. The submergible combustion chamber portion comprises a single cylindrical elongated member having an open end and an opposite closed end. A plurality of curved fire tubes are joined to and extend from the closed end of the combustion chamber to a single flue. The Adams patents disclose power combustion systems where fuel and air are force fed to the point where combustion occurs. Cook, U.S. Patent 4,257,355, teaches a cold water inlet tube located in a horizontal position adjacent the bottom of a commercial water heater. The water heater has a tank formed of a cylindrical shell which is enclosed by a lower head and an upper head. A plurality of vertical flues are disposed inside the tank and extend from the end of the combustion chamber to a single flue. The system operates with a natural draft venting system and not a pulse combustion system. Asakawa, U.S. Patent 3,665,153, teaches an apparatus and method for heating water to generate steam or provide hot water. A burner is positioned in a combustion chamber having heat exchanger pipes passing from one end of the combustion chamber to a chimney. The combustion system operates with a natural draft venting system, not an acoustically tuned pulse combustion system. Lovekin, U.S. Patent 1,170,834, teaches a thermostatic valve mechanism which supplies gas to a burner of a heater. Fig. 1 of the '834 patent shows a single corrugated combustion chamber with a flue exiting from one end. Document Patent Abstracts of Japan, vol.10, No 96, (M-469)(2153) 12th April 1986, JP-A-60232 404 teaches a pulse combustor wherein the heat transfer to the surrounding medium is increased by increasing the number of exhaust tubes from the combustion chamber. SUMMARY OF THE INVENTION The object of the invention is to provide a pulse combustor which has an improved heat transfer to the surrounding medium. This object is attained through the characterizing features of claim 1. BRIEF DESCRIPTION OF THE DRAWINGS Fig. 1 shows a top view of a pulse combustor having a main combustion chamber with two combustion chamber branches and a plurality of exhaust tubes according to one embodiment of this invention, Fig. 1 does not show the exhaust manifold of the pulse combustor; Fig. 2 shows a cross-sectional view along line 2-2 of a submerged pulse combustor as shown in Fig. 1; Fig. 3 shows a cross-sectional view along line 3-3 of a pulse combustor as shown in Fig. 1; Fig. 4 shows an end view of a pulse combustor having a main combustion chamber with four combustion chamber branches and two slots according to one embodiment of this invention; Fig. 5 shows a perspective view of a pulse combustor having a main combustion chamber with four combustion chamber branches and two slots according to one embodiment of this invention; and Fig. 6 shows a perspective view of a pulse combustor with the main combustion chamber and four combustion chamber branches having corrugated sides according to one embodiment of this invention. DESCRIPTION OF THE PREFERRED EMBODIMENTS Pulse combustion is an acoustically controlled oscillating combustion where sinusoidal pressure waves are generated in a combustion chamber. After initial ignition, combustion will continue without further ignition from an ignition source such as a spark plug or the like. The frequency of oscillation within the combustion chamber is mainly a function of the combustion chamber volume, the total cross-sectional area of the exhaust tubes, the length of the exhaust tubes and the speed of sound. One major advantage of this invention is the greatly enhanced heat transfer as compared with the heat transfer achieved in a conventional combustor. In a combustor according to this invention, a major portion of heat is transferred through the walls of the combustion chamber, thus a configuration having increased surface area without a proportional increase in the volume of the combustion chamber provides greater heat transfer. In a preferred embodiment of this invention, a process for pulse combustion occurs within pulse combustor 10 as shown in Figs. 1, 2 and 3. The process preferably occurs within a pulse combustor 10 having fuel inlet valve means, air inlet valve means, combustion chamber 15, and a plurality of downstream combustion chamber branches 16. Each combustion chamber branch 16 is in communication with a plurality of downstream exhaust tubes 20. The pulse combustion process begins with introducing air through the air inlet valve means into mixing and ignition chamber 13. In an 8th embodiment the air inlet valve means comprises at least one air inlet flapper valve 17 positioned upstream from and in communication with mixing and ignition chamber 13, as shown in Fig. 1. Fuel is introduced through the fuel inlet valve means into mixing and ignition chamber 13, as shown in Fig. 1. In a 9th embodiment of this invention, the fuel inlet valve means comprises at least one fuel inlet flapper valve 18 positioned upstream from and in communication with mixing and ignition chamber 13. Preferably, the fuel is a gaseous fuel suitable for combustion within the combustion zone. It is apparent that the air inlet valve means and/or the fuel inlet valve means may comprise other known valves suitable for pulse combustion. In particular, a suitable flapper check valve for either the air or fuel is described in allowed U.S. Patent Application having Serial No. 229,129, filed August 5, 1988, which is incorporated into this patent application by reference. The fuel and air introduced into the mixing chamber combine to form a combustible fuel/air mixture within the mixing zone. The fuel/air mixture is then ignited to produce combustion within combustion chamber 15. Combustion product gases are then exhausted through combustion chamber branches 16 and then further exhausted through exhaust tubes 20. The mixing zone includes the volume of mixing and ignition chamber 13 which is located upstream from combustion chamber 15. It is apparent that combustion may occur in mixing and ignition chamber 13 and continue in combustion chamber 15. The combustion product gases are preferably exhausted through downwardly sloping exhaust tubes 20. Such downward slope of each exhaust tube 20, as shown in Figs. 2 and 3, prevents build-up of condensate within each exhaust tube 20. The process further includes the step of exhausting the combustion product gases into exhaust manifold 21 which is positioned downstream from exhaust tubes 20. The pulse combustor 10 includes exhaust tubes 20 and exhaust manifold 22 are submerged within a fluid, preferably water, as shown in Fig. 2 by liquid level 29. Heat transfer from pulse combustor 10 to the surrounding fluid can be increased by pulse combustor 10 having at least a portion of the exterior surface of combustion chamber 15 and/or combustion chamber branches 16 with corrugations 30, as shown in Fig. 6. The heat transfer can also be increased by having at least one fin secured to the exterior surface of combustion chamber 15 and/or combustion chamber branch 16. To accommodate proper fluid flow conditions throughout pulse combustor 10, one third embodiment of this invention includes each exhaust tube 20 having a cross-sectional area less than the cross-sectional area of each combustion chamber branch 16. In the 11th embodiment, the summation of the cross-sectional areas of each exhaust tube 20 within each combustion chamber branch is less than the of cross-sectional area of each combustion chamber branch 16. In the 12th embodiment, the summation of cross-sectional areas of each combustion chamber branch 16 is less than the cross-sectional area of combustion chamber 15. In the apparatus of this invention as shown in Figs. 1, 2 and 3, pulse combustor 10 has fuel inlet tube 11 and air inlet tube 12 sealably secured to mixing and ignition chamber wall 33 and in communication with mixing and ignition chamber 13 as defined by mixing and ignition chamber wall 33. It is apparent that fuel inlet tube 11 and air inlet tube 12 can be sealably secured to mixing and ignition chamber wall 33 by a welded connection, a screwed connection, by having fuel inlet tube 11 and air inlet tube 12 as channels within a block in lieu of tubes, or the like. Fuel inlet tube 11 injects fuel and air inlet tube 12 injects combustion air into mixing and ignition chamber 13 forming a combustible fuel/air mixture within mixing and ignition chamber 13. An ignition source is located within mixing and ignition chamber 13 for igniting the fuel/air mixture within mixing and ignition chamber 13. It is apparent that ignitor 18 can be a spark plug, glow plug or other ignition source known to the art. Once combustion occurs from an initial ignition source, pulse combustor 10 will operate and combustion will continue without further ignition from the initial ignition source, such as the spark plug, glow plug or the like. Main combustion chamber 15 as defined by main combustion chamber wall 35 is in communication with mixing and ignition chamber 13. The main combustion chamber 15 has transition plate 14 sealably secured to one end of main combustion chamber wall 35. Transition plate 14 has a through hole in communication with mixing and ignition chamber 13. It is apparent that mixing and ignition chamber wall 33 can secure to either transition plate 14 or combustion chamber wall 35 by a welded connection, a screwed connection, by having mixing and ignition chamber wall 33 and main combustion chamber wall 35 one molded piece, or the like. As shown in Fig. 1, main combustion chamber 15 splits into a plurality of downstream combustion chamber branches 16 as defined by combustion chamber branch walls 36. A plurality of exhaust tubes 20 are attached to main combustion chamber wall 35 and/or combustion chamber branch wall 36 along a longitudinal axis of main combustion chamber 15. Figs. 1 and 3 show main combustion chamber 15 having two combustion chamber branches 16 and several exhaust tubes 20. Figs. 4, 5, 6 and 7 show main combustion chamber 15 having four combustion chamber branches 16. It is apparent that main combustion chamber 15 can split into two or more downstream combustion chamber branches 16. Such branching arrangement provides increased heat transfer by providing more surface area and increased contact of the combustion gases with the inside surfaces of the heat exchanger. Combustion chamber branches 16 have "U" shaped slot 23 located between combustion chamber branches 16 of main combustion chamber 15. At least one reinforcing strut 25 spans slot 23 and is secured between combustion chamber branch walls 36. Reinforcing strut 25 provides rigid support for combustion chamber branch walls 36. The combustion chamber branches 16 of main combustion chamber 15 have end plates 24 sealably secured to combustion chamber branch walls 36. It is apparent that combustion chamber branches 16 can be sealed by having combustion chamber walls 36 welded together, by having one molded piece, by being connected to another chamber or tube, or the like. Depending upon the specific design of pulse combustor 10, combustion can be completed either in main combustion chamber 15 or combustion can continue in main combustion chamber 15 and carry into combustion chamber branches 16 for completion of combustion. Whether complete combustion occurs in main combustion chamber 15 or carries into combustion chamber branches 16 depends upon the total volume and configuration of main combustion chamber 15 and combustion chamber branches 16. The location of complete combustion also depends upon the flame speed, reaction time, and the number, spacing and size of exhaust tubes 20. Preferably complete combustion occurs within main combustion chamber 15 and does not carry into combustion chamber branches 16. As shown in Figs. 1, 2 and 3, each exhaust tube 20 has a chamber end sealably secured to and in communication with main combustion chamber wall 35 and/or combustion chamber branch wall 36. Each exhaust tube 20 also has an exhaust manifold end sealably secured to and in communication with exhaust manifold 21 as shown in Fig. 2. A plurality of exhaust tubes 20 are sealably secured to main combustion chamber wall 35 and combustion chamber branch walls 36 along a longitudinal axis of main combustion chamber 15 and along the longitudinal axis of combustion chamber branches 16. Such longitudinal arrangement provides increased heat transfer by providing more surface area for heat exchange. It is apparent that exhaust tubes 20 can be sealably secured to main combustion chamber wall 35 and/or combustion chamber branch walls 36 and exhaust manifold 21 by using welded connections, screwed connections, channel means or the like. The exhaust tubes 20 have a downwardly sloped and staggered configuration as shown in Figs. 2 and 3. It is apparent that exhaust tubes 20 can have other tortuous shaped configurations. However, staggered exhaust tubes 20 provide a convenient configuration for attaching a plurality of exhaust tubes 20 to main combustion chamber wall 35 and/or combustion chamber branch walls 36. Downwardly sloped exhaust tubes 20 prevent water or condensation from the flue gas from collecting in exhaust tubes 20. With the downwardly sloped configuration, any condensate can drain into exhaust manifold 21 from which such condensation can be easily removed. Condensation will collect either during initial start-up of a relatively cold pulse combustor 10 or when pulse combustor 10 acts as a condensing unit and achieves very high thermal efficiencies. Each combustion chamber branch 16 has a cross-sectional area less than the cross-sectional area of main combustion chamber 15. Each exhaust tube 20 has a cross-sectional area less than the cross-sectional area of the combustion chamber branch 16 to which the exhaust tube 20 is in communication. Exhaust tubes 20 can be secured to main combustion chamber wall 35 and/or combustion chamber branch walls 36 at a location where combustion is nearly complete, preferably exhaust tubes 20 are secured to combustion chamber branch walls 36 so that the combustion gases flow through combustion chamber branches 16 providing heat transfer to combustion chamber branch walls 36 rather than flowing primarily through the path of least resistance which would be those exhaust tubes 20 secured to main combustion chamber wall 35. In one embodiment of this invention, main combustion chamber wall 35 and combustion chamber branch wall 36 are corrugated and thus provide greater surface area for increased heat transfer. Figs. 6 and 7 show main combustion chamber wall 35 and combustion chamber branch walls 36 having corrugations. It is apparent that main combustion chamber wall 35 and/or combustion chamber branch wall 36 can have fins or other heat transfer means secured to the walls for increased heat transfer. Figs. 4, 5 and 6 show main combustion chamber 15 having four combustion chamber branches 16. As shown in Fig. 4, a plurality of exhaust tubes 20 have a downwardly sloped and curved configuration extending between main combustion chamber 15 and exhaust manifold 21. It is apparent that pulse combustor 10, including exhaust tubes 20, can fit within shell 28, or the like, as shown in Figs. 2 and 3. Fig. 2 shows pulse combustor 10 operating as a steam boiler where pulse combustor 10, exhaust tubes 20 and exhaust manifold 22 are submerged within shell 28. Liquid level 29 indicates the water level or other liquid level within shell 28. Several design considerations exist for a pulse combustor according to this invention. Main combustion chamber 15 must have the proper size for a prescribed fuel/air mixture input range. An oversized main combustion chamber 15 may lack proper aspiration capabilities. An undersized main combustion chamber 15 may generate excessive noise levels which are difficult and costly to attenuate. Main combustion chamber 15 must have enough surface area to provide proper heat transfer and main combustion chamber wall 35 and/or combustion chamber branch walls 36 must have enough surface area for easy and proper attachment of exhaust tubes 20. As the cross-sectional area of combustion chamber branches 16 decreases, velocity of the hot combustion products increases thus improving heat transfer. Reinforcement struts 25 provide rigid support for combustion chamber branch walls 36 and also reduce the vibration of the sheet metal surfaces of combustion chamber branch walls 36. For a combustor having a given total volume of the combustion chamber and any associated combustion chamber branches, pulse combustor 10 according to this invention will have greater overall heat transfer and thus greater heat transfer per unit of surface area than a conventional single combustion chamber pulse combustor having the same total volume.

Claims: A pulse combustor of the type having a mixing chamber, ignition chamber (13), fuel inlet means (11) and air inlet means (12), said air inlet means and said fuel inlet means introducing air and fuel respectively to form a combustible fuel/air mixture, and ignition means (18) for igniting said combustible fuel/air mixture, characterized by said combustion chamber (15) having a plurality of downstream combustion chamber branches, being separated from each other by a slot each combustion chamber branch (16) having a plurality of exhaust tubes (20) having one end in communication with said combustion chamber branch. A pulse combustor according to claim 1 characterized by the cross-sectional area of each said combustion chamber branch (16) being less than the cross-sectional area of said combustion chamber (15). A pulse combustor according to claim 1 characterized by the cross-sectional area of each said exhaust tube (20) being less that the cross-sectional area of each said combustion chamber branch (16) with which said exhaust tube (20) is in communication. A pulse combustor according to claim 1, characterized by said combustion chamber branches (16) of said combustion chamber (15) further comprising at least one reinforcing strut (25) secured between said at least one combustion chamber branch wall (36) of each said combustion chamber branch. A pulse combustor according to claim 3, characterized by said combustion chamber branches (16) of said combustion chamber (15) further comprising at least one reinforcing strut (25) secured between said at least one combustion chamber branch wall (36) of adjacent said combustion chamber branches (16). A pulse combustor according to claim 1, characterized by said at least one combustion chamber branch wall (36) having corrugated sides. A pulse combustor according to claim 1 characterized by a plurality of fins secured to said at least one combustion chamber wall (35) and said at least one combustion chamber branch wall (36). A pulse combustor according to claim 1 characterized by the air inlet valve means through which the air passes further comprising at least one air inlet flapper valve (17) positioned upstream from and in communication with the mixing and ignition chamber (13). A pulse combustor according to claim 1 characterized by the fuel inlet valve means through which the fuel passes further comprising at least one fuel inlet flapper valve (18) positioned upstream from and in communication with the mixing and ignition chamber (13). A pulse combustor according to claim 1 characterized by the step of increasing heat transfer to fluid surrounding an exterior surface of the pulse combustor by having at least one fin secured to the exterior surface (35) of the pulse combustor. A pulse combustor according to claim 1 characterized by a tube summation of tube cross-sectional areas of each exhaust tube (20) within a corresponding combustion chamber branch (16) being less than a cross-sectional area of the corresponding combustion chamber branch. A pulse combustor according to claim 1 characterized by a branch summation of each branch cross-sectional area of each combustion chamber branch (16) being less than a chamber cross-sectional area of the combustion chamber (15). A process for pulse combustion in a horizontal pulse combustor in accordance with claim 1 having fuel inlet valve means (18), air inlet valve means (17) a mixing and ignition chamber (13) and a combustion chamber (15) with the steps of: introducing air through the air inlet valve means (17) and into a mixing and ignition chamber (13) ; introducing fuel through the fuel inlet valve means (18) and into the mixing and ignition chamber (13); forming a combustible fuel/air mixture within the mixing and ignition chamber; igniting the fuel/air mixture to begin combusting within the mixing and ignition chamber; characterized by the steps of: exhausting combustion product gases downstream through a plurality of combustion chamber branches (16) and further through a plurality of downstream exhaust tubes (20) of each of the combustion chamber branches(16). A process according to claim 13 characterized by the combustion of the fuel/air mixture continuing into the combustion chamber (15).

Inventors: KARDOS, PETER
Applicants: GAS RESEARCH INSTITUTE
Application year: 1989
Main classification: F23C11
IPC codes: F24H1, F23C15, F23C6