DUAL VENTURI SINGLE CHAMBER GAS BURNER
20200408402 ยท 2020-12-31
Inventors
Cpc classification
F23N1/005
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F23N2241/08
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F24C3/082
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F23N2237/10
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F23D2900/14063
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F23D14/06
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F24C3/126
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F23D2900/14062
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F24C3/085
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
F23D14/06
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F23D14/64
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F23N1/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Abstract
A cooking appliance is provided, including a gas burner assembly for a cooktop floor of a cooking appliance. The gas burner assembly includes a burner body having a single combustion chamber and a plurality of flame ports in fluid communication with the single combustion chamber, a first mixing tube in fluid communication with the single combustion chamber and configured to supply a first air-gas mixture to the single combustion chamber, and a second mixing tube in fluid communication with the single combustion chamber and configured to supply a second air-gas mixture to the single combustion chamber.
Claims
1. A gas burner assembly for a cooktop floor of a cooking appliance, the gas burner assembly comprising: a burner body having a single combustion chamber and a plurality of flame ports in fluid communication with the single combustion chamber; a first mixing tube in fluid communication with the single combustion chamber and configured to convey a first air-gas mixture to the single combustion chamber; and a second mixing tube in fluid communication with the single combustion chamber and configured to convey a second air-gas mixture to the single combustion chamber.
2. The gas burner assembly of claim 1, wherein a size of the first mixing tube is different than a size of the second mixing tube.
3. The gas burner assembly of claim 1, wherein the first mixing tube is a first venturi and the second mixing tube is a second venturi.
4. The gas burner assembly of claim 3, wherein a size of a first constriction of the first venturi is different than a size of a second constriction of the second venturi.
5. The gas burner assembly of claim 1, wherein the first mixing tube is configured for a first turndown ratio and the second mixing tube is configured for a second turndown ratio.
6. The gas burner assembly of claim 5, wherein the first turndown ratio of the first mixing tube is different than the second turndown ratio of the second mixing tube.
7. The gas burner assembly of claim 1, further comprising: a first orifice injecting a first gas supply into the first mixing tube for mixing with atmospheric air to provide the first air-gas mixture that is supplied to the single combustion chamber; and a second orifice injecting a second gas supply into the second mixing tube for mixing with atmospheric air to provide the second air-gas mixture that is supplied to the single combustion chamber.
8. The gas burner assembly of claim 7, wherein a size of the first orifice is different than a size of the second orifice.
9. The gas burner assembly of claim 7, wherein a size of one of the first orifice and the second orifice determines a minimum simmer flow rate of the gas burner.
10. The gas burner assembly of claim 1, further comprising: at least one control valve controlling a flow of a first gas supply to the first mixing tube and a flow of a second gas supply to the second mixing tube.
11. The gas burner assembly of claim 10, wherein the at least one control valve is configured to provide a maximum flow rate to the single combustion chamber by simultaneously providing a maximum flow rate of the first gas supply to the first mixing tube and a maximum flow rate of the second gas supply to the second mixing tube.
12. The gas burner assembly of claim 10, wherein the at least one control valve is configured to provide a minimum simmer flow rate to the single combustion chamber by terminating a flow rate of the first gas supply to the first mixing tube while providing a minimum flow rate of the second gas supply to the second mixing tube.
13. The gas burner assembly of claim 10, wherein the at least one control valve is a two-stage control valve comprising: an inlet configured to receive a main gas supply from a gas line; a first outlet configured to supply the flow of the first gas supply to the first mixing tube; and a second outlet configured to supply the flow of the second gas supply to the second mixing tube.
14. The gas burner assembly of claim 1, further comprising: a first control valve configured to separately control a flow of a first gas supply to the first mixing tube; and a second control valve configured to separately control a flow of a second gas supply to the second mixing tube.
15. The gas burner assembly of claim 14, further comprising: a control unit configured to separately control the first control valve and the second control valve.
16. The gas burner assembly of claim 15, wherein the control unit is configured to control the first control valve and the second control valve to provide a maximum flow rate to the single combustion chamber by simultaneously providing a maximum flow rate of the first gas supply from the first control valve to the first mixing tube and a maximum flow rate of the second gas supply from the second control valve to the second mixing tube.
17. The gas burner assembly of claim 15, wherein the control unit is configured to provide a simmer setting by controlling the first control valve to terminate a flow rate of the first gas supply from the first control valve to the first mixing tube and controlling the second control valve to provide a minimum flow rate of the second gas supply capable of being provided by the second control valve to the second mixing tube.
18. A cooking appliance comprising: a cooktop floor; and the gas burner assembly of claim 1, wherein the burner body is disposed on the cooktop floor.
19. The cooking appliance of claim 18, wherein an entry opening of each of the first mixing tube and the second mixing tube is disposed below the cooktop floor and each of the first mixing tube and the second mixing tube are configured to draw atmospheric air therein from a space below the cooktop floor.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
[0012] These and other aspects and features of embodiments of the present invention will be better understood after a reading of the following detailed description, together with the attached drawings, wherein:
[0013]
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[0022]
DETAILED DESCRIPTION OF THE EXEMPLARY EMBODIMENTS OF THE INVENTION
[0023] The present invention now is described more fully hereinafter with reference to the accompanying drawings, in which embodiments of the invention are shown. This invention may, however, be embodied in many different forms and should not be construed as limited to the embodiments set forth herein; rather, these embodiments are provided so that this disclosure will be thorough and complete, and will fully convey the scope of the invention to those skilled in the art.
[0024] With reference to
[0025]
[0026] As shown in
[0027] With reference again to the examples in
[0028] As shown in the examples in
[0029] A primary gas supply line or connection 302 can be configured to supply a first gas flow F1 (i.e., first gas volumetric flow) to the first orifice or jet 214 to be injected into the first venturi 210 (e.g., for high fire operation of the combustion chamber 203) and the secondary gas supply line or connection 306 can be configured to supply a second gas flow F2 (i.e., second gas volumetric flow) to the second orifice or jet 224 to be injected into the second venturi 220 (e.g., for low fire operation, or for both high fire and low fire operation of the combustion chamber 203). The primary gas supply line/connection 302 and secondary gas supply line/connection 306 can include one or more gas supply lines, tubes, pipes, etc. configured to convey gas to each of the gas orifices or jets 214, 224 from one or more other components, such as one or more control valves (e.g., 304, 308, 310, etc.) coupled to the main gas supply 300, a gas manifold coupled to the main gas supply 300, etc. In other examples, the primary and secondary gas lines/connections 302, 306 can be provided by a direct connection or coupling between the gas orifices or jets 214, 224 and one or more other components, such as a direction connection or coupling with a respective control valve (e.g., an outlet of a respective control valve 304, 308, 310, etc.).
[0030] The gas supply (i.e., gas volumetric flow F1, F2) from the main gas supply 300 to each of the gas orifices or jets 214, 224 can be separately controllable, for example, by a dual or two stage control valve 310, as shown for example in
[0031] In other examples, as shown in the example in
[0032] In some examples, a size of the first mixing tube 210 (e.g., first venturi) can be different from a size of the second mixing tube 220 (e.g., second venturi). For example, the size of the tapered or constricted passageways 212, 222 of the venturis 210, 220 can be different in order to optimize operation of the respective mixing tube 210, 220 within a range that is most efficient within a particular turndown ratio of the burner (e.g., maximum to minimum heat output of the burner) while minimizing or avoiding problems with backpressure caused by other internal or external components of the appliance. The first venturi 210 can be used for a primary gas supply to the combustion chamber 203 for high fire operation and the second venturi 220 can be used for a secondary gas supply to the combustion chamber 203 for low fire operation, or for both high fire and low fire operation of the combustion chamber. Each venturi 210, 220 can be configured and/or optimized for a smaller turndown ratio of the burner, such as a 5 to 1 turndown ration, thereby resulting in a lower turndown in pressure for each venturi 210, 220.
[0033] In other examples, a size of the first gas jet or orifice 214 can be different from a size of the second gas jet or orifice 224, for example, to optimize operation of the respective mixing tube 210, 220 within a range that is most efficient within a particular turndown range while minimizing or avoiding problems with backpressure caused by other internal or external components of the appliance. The first gas jet or orifice 214 can be used for a primary gas supply to the combustion chamber 203 for high fire operation and the second gas jet or orifice 224 can be used for a secondary gas supply to the combustion chamber 203 for low fire operation or for both high fire and low fire operation of the combustion chamber 203.
[0034] With reference again to the examples in
[0035] An example operation of a gas burner assembly according to one of the exemplary embodiments of the invention shown, for example, in
[0036] A gas surface cooking unit 100 (as shown for example in
[0037] With reference to the example embodiments shown in
[0038] The flow of the primary and secondary gas F1, F2 through the first and second venturis 210, 220, respectively, draws air (in these examples, primary air drawn from below the cooktop floor 102) into the first and second venturis 210, 220, respectively, and mixes the air with the primary and secondary gas F1, F2 such that a first air-gas mixture and a secondary air-gas mixture are injected into to the same, single combustion chamber 203. The primary and secondary air-gas mixtures will flow through the single combustion chamber 203 and exit the ports 204 of the burner body 202, where the exiting air-gas mixture can be ignited by one or more igniters (not shown) to provide a flame ring (e.g., a single, annular flame ring around the burner body 202).
[0039] As the user rotates the control knob 106 from the HIGH position towards a LOW position, the primary side of the two-stage gas valve 310 can be configured to gradually or intermittently meter down the gas flow rate of the primary gas F1 being supplied from the first outlet of the two-stage gas valve 310 to the first gas jet or orifice 214 and into the first venturi 210, while the gas flow rate of the secondary gas F2 from the second outlet of the two-stage gas valve 310 remains constant through this range such that the gas flow rate of the secondary gas F2 being supplied from the second outlet of the two-stage gas valve 310 to the second gas jet or orifice 224 and into the second venturi 220 remains at a constant full pressure.
[0040] When the control knob 106 of the two-stage gas valve 310 reaches the LOW position, the primary side of the two-stage gas valve 310 terminates the flow of the primary gas F1 flowing from the first outlet to the first gas jet or orifice 214 into the first venturi 210, while the gas flow rate of the secondary gas F2 of the two-stage gas valve 310 remains constant such that the gas pressure of the secondary gas F2 flowing from the second outlet and being injected from the second gas jet or orifice 224 into the second venturi 220 remains at the constant full pressure.
[0041] As a user continues to rotate the control knob 106 from the LOW position towards a SIMMER position, the secondary side of the two-stage gas valve 310 can be configured to gradually or intermittently meter down the gas flow rate of the secondary gas F2 being supplied to the second gas jet or orifice 224 and injected into the second venturi 220 until the gas flow rate of the secondary gas F2 reaches a minimum gas flow rate capable of being provided by the secondary side of the two-stage gas valve 310. In this example, the final simmer rate can be selected or determined, for example, by the minimum gas flow rate capable of being provided by the secondary side of the two-stage gas valve 310, by the size of the second orifice 224, and/or by a size of the venturi 222.
[0042] According to these examples, at a HIGH fire position, the total gas flow delivered to the single combustion chamber 203 is the sum of the primary and secondary gases F1, F2 delivered by both the primary and secondary orifices 214, 224 to the venturis 210, 220. At the LOW fire position, the total gas flow delivered to the single combustion chamber 203 includes only the secondary gas F2 delivered by the secondary orifice 214 to the second venturi 220, since the primary side of the gas valve 310 is turned off. At the SIMMER fire position, the total gas flow delivered to the single combustion chamber 203 includes only the minimum gas flow rate of the secondary gas F2 capable of being provided by the secondary side of the two-stage gas valve 310, in the examples shown in
[0043] The example embodiments shown in
[0044] As the user rotates the control knob 106 from the HIGH position towards a LOW position, the control unit 400 can be configured to gradually or intermittently meter down the gas flow rate of the primary gas F1 being supplied from the control valve 304 to the first gas jet or orifice 214 and into the first venturi 210, while the gas flow rate of the secondary gas F2 from the control valve 308 remains constant through this range such that the gas flow rate of the secondary gas F2 being supplied from the control valve 308 to the second gas jet or orifice 224 and into the second venturi 220 remains at a constant full pressure.
[0045] When the control knob 106 of the two-stage gas valve 310 reaches the LOW position, the control unit 400 terminates the flow of the primary gas F1 flowing from the control valve 304 to the first gas jet or orifice 214 into the first venturi 210, while the gas flow rate of the secondary gas F2 from the control valve 308 remains constant such that the gas pressure of the secondary gas F2 flowing from the control valve 308 and being injected from the second gas jet or orifice 224 into the second venturi 220 remains at the constant full pressure.
[0046] As a user continues to rotate the control knob 106 from the LOW position towards a SIMMER position, the control unit 400 can be configured to gradually or intermittently meter down the gas flow rate of the secondary gas F2 being supplied from the control valve 308 to the second gas jet or orifice 224 and injected into the second venturi 220 until the gas flow rate of the secondary gas F2 reaches a minimum gas flow rate capable of being provided by the control valve 308. In this example, the final simmer rate can be selected or determined, for example, by the minimum gas flow rate capable of being provided by the control valve 308, by the size of the second orifice 224, and/or by a size of the venturi 222.
[0047] According to the examples in
[0048] Other arrangements and operation of a gas burner assembly are possible within the spirit and scope of the invention. For example, the dual venturi, single chamber gas burner can be configured as a fully sealed cup burner or top breather burner, which relies on all air (e.g., primary and secondary air) for combustion being supplied/drawn from above the cooktop surface, or a bottom breather burner, which is designed to have the primary air supplied from below the cooktop surface and the secondary air for combustion being drawn from above the cooktop surface. A gas burner assembly also can be configured as a multi-stage burner or a stacked burner having a plurality of stacked burners with at least one of the burners being a dual venturi, single chamber gas burner having improved stability at LOW fire and SIMMER fire positions and reducing the simmer rate of the gas top burner to provide desirable low, or ultra-low, simmer functions.
[0049] The present invention has been described herein in terms of several preferred embodiments. However, modifications and additions to these embodiments will become apparent to those of ordinary skill in the art upon a reading of the foregoing description. It is intended that all such modifications and additions comprise a part of the present invention to the extent that they fall within the scope of the several claims appended hereto.