EP1588099B1 - Gas cooker - Google Patents
Gas cooker Download PDFInfo
- Publication number
- EP1588099B1 EP1588099B1 EP04701602A EP04701602A EP1588099B1 EP 1588099 B1 EP1588099 B1 EP 1588099B1 EP 04701602 A EP04701602 A EP 04701602A EP 04701602 A EP04701602 A EP 04701602A EP 1588099 B1 EP1588099 B1 EP 1588099B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- gas
- control
- secondary line
- point according
- cooking point
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
Links
- 238000010411 cooking Methods 0.000 claims description 14
- 230000000903 blocking effect Effects 0.000 claims 2
- 230000037431 insertion Effects 0.000 claims 1
- 238000003780 insertion Methods 0.000 claims 1
- 210000000056 organ Anatomy 0.000 abstract description 6
- 238000010438 heat treatment Methods 0.000 description 7
- 238000004519 manufacturing process Methods 0.000 description 6
- 238000010586 diagram Methods 0.000 description 2
- 230000001105 regulatory effect Effects 0.000 description 2
- 240000001439 Opuntia Species 0.000 description 1
- 235000004727 Opuntia ficus indica Nutrition 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F24—HEATING; RANGES; VENTILATING
- F24C—DOMESTIC STOVES OR RANGESĀ ; DETAILS OF DOMESTIC STOVES OR RANGES, OF GENERAL APPLICATION
- F24C3/00—Stoves or ranges for gaseous fuels
- F24C3/12—Arrangement or mounting of control or safety devices
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23N—REGULATING OR CONTROLLING COMBUSTION
- F23N1/00—Regulating fuel supply
- F23N1/005—Regulating fuel supply using electrical or electromechanical means
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F24—HEATING; RANGES; VENTILATING
- F24C—DOMESTIC STOVES OR RANGESĀ ; DETAILS OF DOMESTIC STOVES OR RANGES, OF GENERAL APPLICATION
- F24C3/00—Stoves or ranges for gaseous fuels
- F24C3/12—Arrangement or mounting of control or safety devices
- F24C3/126—Arrangement or mounting of control or safety devices on ranges
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23N—REGULATING OR CONTROLLING COMBUSTION
- F23N2235/00—Valves, nozzles or pumps
- F23N2235/12—Fuel valves
- F23N2235/18—Groups of two or more valves
Definitions
- the present invention relates to a gas hob.
- the gas hob has at least one gas burner and a control arrangement for setting a heating power of the gas burner. Furthermore, the control arrangement has at least one control element arranged in a gas main line to the gas burner, which adjusts a gas flow guided to a burner nozzle, and at least one auxiliary line running parallel to the control element with associated shut-off device for opening and closing the secondary line.
- a generic gas hob which has a valve control arrangement in a gas supply to a gas burner.
- the gas supply line branches into a number of parallel-connected partial gas lines, which are connected to the burner nozzle.
- a switching valve for switching on and off of the partial gas flow flowing through it and a throttle element for throttling the partial gas flow flowing through it are arranged.
- the object of the present invention is to provide a gas hob with at least one gas burner whose control arrangement enables reliable burner operation.
- the object is achieved by a gas cooking point with the features of claim 1.
- the at least one secondary line connected in parallel with a control element has a flow resistance limiting the gas flow rate in the secondary line. This is smaller than the flow resistance formed by the burner nozzle. A pressure drop in the gas flow through the secondary line is therefore greatly reduced. The greatly reduced pressure drop when the bypass is open leads to an improved primary air intake in the area of the Burner nozzle. The flame formation at the gas burner is therefore much more reliable at high gas flow rates.
- the flow resistance in the secondary line can be determined in different ways.
- the gas flow rate limiting flow resistance is determined by the smallest passage cross-section in the secondary line.
- the smallest passage cross section in the secondary line is thus dimensioned larger than the passage cross section of the burner nozzle.
- the secondary line is open only for setting the maximum gas flow rate.
- the secondary line is therefore not used for setting partial gas flow rates.
- the flow resistance in the bypass may be reduced to a negligible extent with respect to the flow resistance in the gas main. Irrespective of whether the control element arranged in the gas main line is open or closed, the maximum gas throughput always occurs when the secondary line is open.
- the control arrangement may preferably have a number of control lines connected in parallel to one another with corresponding control or regulating members. These branch off from the gas main line and can each guide a partial gas flow rate to the burner nozzle. Compared to conventional gas cocks, no hysteresis effects arise with such a control arrangement.
- the parallel control lines allow a much more accurate adjustment of the partial gas flow rate.
- the maximum gas flow rate is established when all control lines of the control arrangement are open. In this case, however, the pressure loss in the control arrangement is substantially greater than when using a conventional, fully open gas cock. As a result of the secondary line according to the invention, the pressure loss at maximum gas throughput can be effectively reduced, in particular in the case of this control arrangement.
- a switching valve with associated control throttle can be provided in the control lines.
- the control throttle serves the limitation the gas flow rate to a partial gas flow rate.
- the switching valve has only a closed and an open position.
- the number of fittings in the secondary line such as the number of shut-off, control or regulating organs, limited to only one unthrottled obturator.
- control lines are combined in a housing, for example a valve block.
- the secondary line can be integrated in the housing of the control arrangement. A factory mounting of the controls or throttle elements is simplified when the throttle elements are removably inserted into mounting holes of the control lines of the housing of the control arrangement.
- a conventional valve block is first prepared with a number of control lines.
- control lines - with the exception of at least one control line - throttle elements are used.
- the unthrottled control line forms the secondary line according to the invention.
- the mounting opening of the unthrottled control line to be closed by a non-throttling closure element.
- it can be mounted in the unthrottled control lines of the valve block, a throttle element whose passage cross-section is larger than the passage cross-section of the burner nozzle. From a manufacturing point of view, it is particularly advantageous if the assembly opening in the unthrottled control line is completely dispensed with in the production of the valve block.
- FIG. 1 is a highly schematic diagram of a belonging to a gas burner gas burner 1 shown. This is connected via a main line 3 with a gas pipeline network. In the main line 3, a control arrangement 5 is arranged. By means of the control arrangement 5, a gas flow rate to the gas burner 1 is set in accordance with a desired heat output of the gas burner 1. Not shown are the usual for the gas hob security elements, such as a thermocouple and an associated solenoid valve for safety shutdown of the gas burner when extinguishing a flame.
- the gas hob security elements such as a thermocouple and an associated solenoid valve for safety shutdown of the gas burner when extinguishing a flame.
- the control arrangement 5 has three control lines 7, 9, 11 connected in parallel and a secondary line 13 connected in parallel thereto. Both the control lines 7, 9, 11 and the secondary line 13 branch off from the main line 3 and then reunite to a burner feed line 15. This opens into a burner nozzle 14.
- This opens into a burner nozzle 14.
- In each of these lines 7, 9, 11, 13 is one electrically actuated magnetic switching valve 17 is arranged.
- the magnetic switching valves 17 are switchable from a closed position into an open position and can be activated via signal lines 19 by means of an electronic control device 21. Via the control device 21, a user can set heating power levels of the gas burner 1. As later from the FIG. 2 is described, is set in accordance with the selected Schuticiansscribe a partial gas flow rate Q 1 to Q 7 to the maximum gas flow rate Q 8 .
- the control device 21 can control the magnetic switching valves 17 independently of each other.
- the arranged in the control lines 7, 9, 11 solenoid valves 17 are throttle elements 23, 25, 27 connected downstream.
- the Indian FIG. 6 indicated diameter d 1 of each throttle element 23, 25, 27 determines its passage cross-section.
- the diameters d 1 in the control lines 7, 9, 11 are designed to be substantially smaller than a passage cross-section of the burner nozzle 14. Thus, in the present case, the diameter of the burner nozzle 14 in about 0.5 mm.
- the throttle diameter d 1 of the throttle elements 23, 25, 27 is between 0.1 and 0.3 mm.
- the secondary line 13 In contrast to the control lines 7, 9, 11, the secondary line 13 is unthrottled. As a result, the flow resistance in the unthrottled secondary line 13 is reduced as much as possible. Opposite the control lines 7, 9, 11, the pressure loss through the opened secondary line 13 is negligible. When the secondary line 13 is open, the maximum gas throughput Q 8 is therefore passed through the secondary line 13 without any significant pressure loss. To reduce the flow resistance of the passage cross section in the secondary line 13 is dimensioned substantially larger than the passage cross section of the burner nozzle 14th
- the passage cross sections of the throttle elements 23, 25, 27 are designed factory. In the present case, about 65% of the maximum gas flow rate is conducted to the burner nozzle 14 when the control lines 7, 9, 11 are open. In this case, the first throttle element 23 allows about 20%, the second throttle element 25 about 24% and the third throttle element 27 about 30% of the maximum gas flow rate.
- the heating power levels are adjustable by means of the electronic control device 21.
- the partial gas flow rates Q 1 to Q 7 go from in the FIG. 2 shown flow characteristic of the control assembly 5. If the user selects the eighth heating power stage, then the electronic control device 21 opens the solenoid valve 17 in the secondary line 13. As a result, the maximum gas flow rate Q 8 to the burner nozzle 14 is set.
- both the control lines 7, 9, 11 and the secondary line 13 are integrated in a housing 33 shaped as a compact valve block.
- the valve block 33 made of plastic has on one side a semi-circular in side view inlet port 35. This sits positively on an outer circumference of the pipe designed as a main line 3.
- the main line 3 is gas-tight pressed to the inlet port 35.
- an outlet port 37 is formed on the valve block 33.
- the burner supply line 15 is inserted gas-tight.
- four solenoid valve heads 39 of the solenoid valves 17 are mounted in the valve block 33.
- valve block 33 is shown in a side sectional view.
- the region of the inlet connection 35, 37 is shown in a first sectional plane X.
- a second sectional plane Y Parallel to this, in a second sectional plane Y, the central area of the valve block 33 between the inlet and outlet ports 35, 37 is shown.
- a third sectional plane Z of the region of the outlet port 37 is shown. From the FIG. 4 shows that in the valve block 33 to each other opposite horizontal blind holes 41, 43 extend. These each open into the inlet port 35 and into the outlet port 37 of the valve block 33 and are aligned parallel to each other.
- the control lines 7, 9, 11 connect the inlet bag bore 41 with the outlet bag bore 43.
- each of the control lines 7, 9, 11 has a valve channel 45.
- the valve channel 45 extends perpendicular to the horizontal blind holes 41, 43.
- a channel end of the valve channel 45 opens into a circular recess 51, which in Valve block 33 is incorporated.
- the circular recess 51 forms a valve seat for a valve plate 53 of the solenoid valve head 39, as shown in the FIG. 4 indicated by dashed lines.
- a first passage channel 55 with a small diameter which leads to the inlet bag bore 41.
- the valve channel 45 is connected to the outlet bag bore 43 via a second passage 57.
- Each of the control lines 7, 9, 11 extending between the blind bores 41, 43 is consequently formed by the first passage 55, the valve passage 45 and the second passage 57.
- valve plate 53 of the solenoid valve heads 39 is located on the recessed valve seat 51.
- the valve channel 45 of the corresponding control line is closed, whereby the control line is closed as such.
- the valve plate 53 is out of engagement with the valve seat 51. In this case, the corresponding control line is open.
- the recessed valve seat 51 opens each of the valve channels 45 in a mounting hole 59.
- the throttle elements 23, 25, 27 can be mounted, as shown in the FIG. 6 is indicated.
- the throttle element 25 is designed as an insert nozzle. This can be screwed into the mounting opening 59 of the valve channel 45.
- the configuration of the secondary line 13 in the valve block 33 is explained below.
- the secondary line 13 is formed according to the control lines through the first passageway 55, the valve channel 45 and the second passageway 57.
- the secondary line 13 is unthrottled. That is, that no insert nozzle 25 is arranged in the secondary line 13.
- the largest possible passage cross section in the secondary line 13 is achieved.
- the diameter d 2 of the passage channel 55 is about 1.5 to 2 mm.
- the diameter d 2 of the first passageway 55 is considerably larger than the diameter of the burner nozzle 14.
- a closure element 61 is inserted. This closes the mounting opening 59, without throttling the secondary line 13.
- the closure member 61 may be omitted when the factory production of the valve block 33 is completely dispensed with the mounting hole in the secondary line 13. In this case, the secondary line 13 is closed in the region of the mounting holes 59 in the valve block 33, without the secondary line 13 is throttled.
- control arrangement 5 it is also possible, by cyclically switching on and off of the solenoid valves 17 of the control lines 7, 9, 11 to achieve small continuous heating powers on the gas burner 1. It is advantageous that in the control arrangement 5, a re-ignition at each preset heating power can be done very reliable.
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- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Feeding And Controlling Fuel (AREA)
- Continuous Casting (AREA)
- Separation By Low-Temperature Treatments (AREA)
- Magnetic Heads (AREA)
Abstract
Description
Die vorliegende Erfindung betrifft eine Gaskochstelle. Die Gaskochstelle weist zumindest einen Gasbrenner und eine Steueranordnung zur Einstellung einer Heizleistung des Gasbrenners auf. Ferner weist die Steueranordnung zumindest ein in einer Gashauptleitung zum Gasbrenner angeordnetes Steuerorgan, das einen zu einer Brennerdüse geführten Gasdurchsatz einstellt, und zumindest eine zum Steuerorgan parallel verlaufende Nebenleitung mit zugeordnetem Absperrorgan zum Ćffnen und SchlieĆen der Nebenleitung auf.The present invention relates to a gas hob. The gas hob has at least one gas burner and a control arrangement for setting a heating power of the gas burner. Furthermore, the control arrangement has at least one control element arranged in a gas main line to the gas burner, which adjusts a gas flow guided to a burner nozzle, and at least one auxiliary line running parallel to the control element with associated shut-off device for opening and closing the secondary line.
Aus
Die Aufgabe der vorliegenden Erfindung besteht darin, eine Gaskochstelle mit zumindest einem Gasbrenner bereitzustellen, dessen Steueranordnung einen zuverlƤssigen Brennerbetrieb ermƶglicht.The object of the present invention is to provide a gas hob with at least one gas burner whose control arrangement enables reliable burner operation.
Die Aufgabe ist durch eine Gaskochstelle mit den Merkmalen des Patentanspruches 1 gelƶst. Gemäà dem kennzeichnenden Teil des Patentanspruches 1 weist die zumindest eine parallel zu einem Steuerorgan geschaltete Nebenleitung einen den Gasdurchsatz in der Nebenleitung begrenzenden Strƶmungswiderstand auf. Dieser ist kleiner als der durch die Brennerdüse gebildete Strƶmungswiderstand ausgebildet. Ein Druckverlust im Gasstrom durch die Nebenleitung ist daher stark verringert. Der bei geƶffneter Nebenleitung stark verringerte Druckverlust führt zu einer verbesserten PrimƤrluftansaugung im Bereich der Brennerdüse. Die Flammenbildung am Gasbrenner ist daher bei groĆen Gasdurchflussmengen wesentlich zuverlƤssiger.The object is achieved by a gas cooking point with the features of
Der Strƶmungswiderstand in der Nebenleitung kann auf unterschiedliche Weisen festgelegt werden. In einer fertigungstechnisch einfachen Realisierung der Erfindung wird der maĆgeblich, den Gasdurchsatz begrenzende Strƶmungswiderstand durch den kleinsten Durchlassquerschnitt in der Nebenleitung bestimmt. Der kleinste Durchlassquerschnitt in der Nebenleitung ist somit grƶĆer als der Durchlassquerschnitt der Brennerdüse dimensioniert.The flow resistance in the secondary line can be determined in different ways. In a manufacturing technology simple realization of the invention, the decisive, the gas flow rate limiting flow resistance is determined by the smallest passage cross-section in the secondary line. The smallest passage cross section in the secondary line is thus dimensioned larger than the passage cross section of the burner nozzle.
Von Vorteil ist es, wenn in einem Kochstellenbetrieb die Nebenleitung lediglich zur Einstellung des maximalen Gasdurchsatzes geöffnet ist. Die Nebenleitung wird also nicht zur Einstellung von Teilgasdurchsätzen eingesetzt. In diesem Fall kann der Strömungswiderstand in der Nebenleitung gegenüber dem Strömungswiderstand in der Gashauptleitung auf ein vernachlässigbares Ausmaà verringert werden. Unabhängig davon, ob das in der Gashauptleitung angeordnete Steuerorgan geöffnet oder geschlossen ist, stellt sich daher bei geöffneter Nebenleitung stets der maximale Gasdurchsatz ein.It is advantageous if in a hotplate operation, the secondary line is open only for setting the maximum gas flow rate. The secondary line is therefore not used for setting partial gas flow rates. In this case, the flow resistance in the bypass may be reduced to a negligible extent with respect to the flow resistance in the gas main. Irrespective of whether the control element arranged in the gas main line is open or closed, the maximum gas throughput always occurs when the secondary line is open.
Bevorzugt kann die Steueranordnung eine Anzahl zueinander parallel geschalteter Steuerleitungen mit entsprechenden Steuer- oder Regelorganen aufweisen. Diese zweigen von der Gashauptleitung ab und kƶnnen jeweils einen Teilgasdurchsatz zur Brennerdüse leiten. Im Vergleich zu herkƶmmlichen GashƤhnen ergeben sich bei einer solchen Steueranordnung keinerlei Hysterese-Effekte. Die parallel geschalteten Steuerleitungen ermƶglichen eine wesentlich genauere Einstellung des Teilgasdurchsatzes. Der maximale Gasdurchsatz stellt sich ein, wenn alle Steuerleitungen der Steueranordnung geƶffnet sind. In diesem Fall ist jedoch der Druckverlust in der Steueranordnung wesentlich grƶĆer als bei Verwendung eines herkƶmmlichen, vollstƤndig geƶffneten Gashahns. Durch die erfindungsgemƤĆe Nebenleitung kann insbesondere bei dieser Steueranordnung der Druckverlust bei maximalem Gasdurchsatz wirkungsvoll verringert werden.The control arrangement may preferably have a number of control lines connected in parallel to one another with corresponding control or regulating members. These branch off from the gas main line and can each guide a partial gas flow rate to the burner nozzle. Compared to conventional gas cocks, no hysteresis effects arise with such a control arrangement. The parallel control lines allow a much more accurate adjustment of the partial gas flow rate. The maximum gas flow rate is established when all control lines of the control arrangement are open. In this case, however, the pressure loss in the control arrangement is substantially greater than when using a conventional, fully open gas cock. As a result of the secondary line according to the invention, the pressure loss at maximum gas throughput can be effectively reduced, in particular in the case of this control arrangement.
Als Absperr- oder Regelorgane kƶnnen in den Steuerleitungen jeweils ein Schaltventil mit zugeordneter Steuerdrossel vorgesehen sein. Die Steuerdrossel dient der Begrenzung des Gasdurchsatzes auf einen Teilgasdurchsatz. Im Gegensatz zu einem Proportionalventil mit kontinuierlicher Verstellung weist das Schaltventil lediglich eine SchlieĆ- und eine Offenstellung auf.As a shut-off or control organs in each case a switching valve with associated control throttle can be provided in the control lines. The control throttle serves the limitation the gas flow rate to a partial gas flow rate. In contrast to a proportional valve with continuous adjustment, the switching valve has only a closed and an open position.
Zur Verringerung des Strƶmungswiderstandes in der Nebenleitung ist die Zahl von Einbauten in der Nebenleitung, etwa die Zahl der Absperr-, Steuer- oder Regelorgane, auf lediglich ein ungedrosseltes Absperrorgan beschrƤnkt.To reduce the flow resistance in the secondary line, the number of fittings in the secondary line, such as the number of shut-off, control or regulating organs, limited to only one unthrottled obturator.
Aus Platzgründen ist es vorteilhaft, wenn die Steuerleitungen in einem Gehäuse, beispielsweise einem Ventilblock zusammengefasst sind. Vorteilhaft kann die Nebenleitung in dem Gehäuse der Steueranordnung integriert sein. Eine werksseitige Montage der Steuerelemente oder Drosselelemente ist vereinfacht, wenn die Drosselelemente herausnehmbar in Montageöffnungen der Steuerleitungen des Gehäuse der Steueranordnung eingesetzt sind.For reasons of space, it is advantageous if the control lines are combined in a housing, for example a valve block. Advantageously, the secondary line can be integrated in the housing of the control arrangement. A factory mounting of the controls or throttle elements is simplified when the throttle elements are removably inserted into mounting holes of the control lines of the housing of the control arrangement.
In einem fertigungstechnisch besonders einfachen Herstellungsverfahren der Steueranordnung wird zunƤchst ein herkƶmmlicher Ventilblock mit einer Anzahl von Steuerleitungen hergestellt. In den Steuerleitungen sind - mit Ausnahme von zumindest einer Steuerleitung - Drosselelemente eingesetzt. Die ungedrosselte Steuerleitung bildet die erfindungsgemƤĆe Nebenleitung.In a production technology particularly simple manufacturing process of the control arrangement, a conventional valve block is first prepared with a number of control lines. In the control lines - with the exception of at least one control line - throttle elements are used. The unthrottled control line forms the secondary line according to the invention.
Anstelle eines Drosselelements die Montageƶffnung der ungedrosselten Steuerleitung durch ein nicht drosselndes Verschlusselement verschlossen sein. Alternativ kann in der ungedrosselten Steuerleitungen des Ventilblocks ein Drosselelement montiert sein, dessen Durchlassquerschnitt grƶĆer als der Durchlassquerschnitt der Brennerdüse ist. Fertigungstechnisch besonders vorteilhaft ist es, wenn bei der Herstellung des Ventilblockes auf die Montageƶffnung in der ungedrosselten Steuerleitung gƤnzlich verzichtet wird.Instead of a throttle element, the mounting opening of the unthrottled control line to be closed by a non-throttling closure element. Alternatively it can be mounted in the unthrottled control lines of the valve block, a throttle element whose passage cross-section is larger than the passage cross-section of the burner nozzle. From a manufacturing point of view, it is particularly advantageous if the assembly opening in the unthrottled control line is completely dispensed with in the production of the valve block.
Nachfolgend ist ein Ausführungsbeispiel der Erfindung anhand der beigefügten Figuren beschrieben. Es zeigen:
- Fig. 1
- ein schematisiertes Blockschaltbild mit einem Gasbrenner einer Gaskochstelle und einer Steueranordnung;
- Fig. 2
- eine Durchflusscharakteristik der in der
Fig. 1 gezeigten Steueranordnung; - Fig. 3
- einen Ventilblock der Steueranordnung in einer Seitenansicht;
- Fig. 4
- der Ventilblock der Steueranordnung in einer Seitenschnittdarstellung;
- Fig. 5
- eine Schnittdarstellung entlang der Linie A-A aus der
; undFigur 4 - Fig. 6
- eine Schnittdarstellung entlang der Linie B-B aus der
.Figur 4
- Fig. 1
- a schematic block diagram with a gas burner of a gas hob and a control arrangement;
- Fig. 2
- a flow rate characteristic in the
Fig. 1 shown control arrangement; - Fig. 3
- a valve block of the control arrangement in a side view;
- Fig. 4
- the valve block of the control arrangement in a side sectional view;
- Fig. 5
- a sectional view taken along the line AA from the
FIG. 4 ; and - Fig. 6
- a sectional view taken along the line BB from the
FIG. 4 ,
In der
Die Steueranordnung 5 weist drei parallel geschaltete Steuerleitungen 7, 9, 11 sowie eine parallel dazu geschaltete Nebenleitung 13 auf. Sowohl die Steuerleitungen 7, 9, 11 als auch die Nebenleitung 13 zweigen von der Hauptleitung 3 ab und vereinen sich anschlieĆend wieder zu einer Brennerzuleitung 15. Diese mündet in eine Brennerdüse 14. In jeder dieser Leitungen 7, 9, 11, 13 ist jeweils ein elektrisch betƤtigbares Magnetschaltventil 17 angeordnet. Die Magnetschaltventile 17 sind von einer SchlieĆstellung in eine Offenstellung schaltbar und über Signalleitungen 19 mittels einer elektronischen Steuereinrichtung 21 ansteuerbar. Ćber die Steuereinrichtung 21 kann ein Benutzer Heizleistungsstufen des Gasbrenners 1 einstellen. Wie spƤter anhand der
Die Steuereinrichtung 21 kann die Magnetschaltventile 17 unabhƤngig voneinander ansteuern. Den in den Steuerleitungen 7, 9, 11 angeordneten Magnetventilen 17 sind Drosselelemente 23, 25, 27 nachgeschaltet. Der in der
Im Unterschied zu den Steuerleitungen 7, 9, 11 ist die Nebenleitung 13 ungedrosselt. Dadurch ist der Strƶmungswiderstand in der ungedrosselten Nebenleitung 13 grƶĆtmƶglich verringert. Gegenüber den Steuerleitungen 7, 9, 11 ist der Druckverlust durch die geƶffnete Nebenleitung 13 vernachlƤssigbar. Bei geƶffneter Nebenleitung 13 wird der maximale Gasdurchsatz Q8 daher ohne grƶĆeren Druckverlust durch die Nebenleitung 13 geleitet. Zur Reduzierung des Strƶmungswiderstandes ist der Durchlassquerschnitt in der Nebenleitung 13 wesentlich grƶĆer dimensioniert als der Durchlassquerschnitt der Brennerdüse 14.In contrast to the
Die Durchlassquerschnitte der Drosselelemente 23, 25, 27 werden werksseitig ausgelegt. Vorliegend werden bei geƶffneten Steuerleitungen 7, 9, 11 ca. 65 % des maximalen Gasdurchsatzes zur Brennerdüse 14 geleitet. Hierbei lƤsst das erste Drosselelement 23 ca. 20%, das zweite Drosselelement 25 ca. 24% und das dritte Drosselelement 27 ca. 30% des maximalen Gasdurchsatzes durch. Mittels der drei Steuerleitungen 7, 9, 11 ergeben sich durch Kombinationen der Offen- und SchlieĆstellungen der Magnetventile 17 in den drei Steuerleitungen acht (d.h. 23) Heizleistungsstufen mit den unterschiedlichen TeilgasdurchsƤtzen 0 und Q1 bis Q7. Die Heizleistungsstufen sind mittels der elektronischen Steuereinrichtung 21 einstellbar. Die TeilgasdurchsƤtze Q1 bis Q7 gehen aus der in der
Gemäà der Durchflusscharakteristik in der
In den folgenden
In der
Im einzelnen weist jede der Steuerleitungen 7, 9, 11 einen Ventilkanal 45 auf. Der Ventilkanal 45 verläuft senkrecht zu den horizontalen Sackbohrungen 41, 43. Ein Kanalende des Ventilkanals 45 mündet in eine kreisförmige Aussparung 51, die im Ventilblock 33 eingearbeitet ist. Die kreisförmige Aussparung 51 bildet einen Ventilsitz für einen Ventilteller 53 des Magnetventilkopfes 39, wie es in der
In der SchlieĆstellung der Magnetventile 17 liegt der Ventilteller 53 der Magnetventilkƶpfe 39 auf dem ausgesparten Ventilsitz 51. Damit ist der Ventilkanal 45 der entsprechenden Steuerleitung geschlossen, wodurch die Steuerleitung als solche geschlossen ist. In der Offenstellung des Magnetventils 17 ist der Ventilteller 53 auĆer Anlage mit dem Ventilsitz 51. In diesem Fall ist die entsprechende Steuerleitung geƶffnet.In the closed position of the
Gegenüber dem ausgesparten Ventilsitz 51 mündet jeder der Ventilkanäle 45 in eine Montageöffnung 59. In die Montageöffnung 59 sind die Drosselelemente 23, 25, 27 montierbar, wie es in der
Anhand der
Mit der vorliegenden Steueranordnung 5 ist es auch möglich, durch zyklisches Ein- und Ausschalten der Magnetventile 17 der Steuerleitungen 7, 9, 11 kleine kontinuierliche Heizleistungen am Gasbrenner 1 zu erreichen. Vorteilhaft ist es, dass bei der Steueranordnung 5 eine Wiederzündung bei jeder voreingestellten Heizleistung sehr zuverlässig erfolgen kann.With the
Claims (13)
- Gas cooking point with at least one gas burner (1) and a control arrangement (5) for setting a heat output of the gas burner (1), which control arrangement comprises at least one control element (23, 25, 27), which is arranged in a gas main line (3, 15) to the gas burner (1) and which sets a gas throughput (Q1 to Q8) to be conducted to a burner nozzle (14), and at least one secondary line (13), which extends parallel to the control element, for the burner nozzle (14) with an associated blocking element (17) for opening and closing the secondary line (13), characterised in that the flow resistance, which limits the gas throughput, in the secondary line (13) is formed to be lower than the flow resistance formed by the burner nozzle (14).
- Gas cooking point according to claim 1, characterised in that the flow resistance limiting the gas throughput is formed by the smallest passage cross-section in the secondary line (13).
- Gas cooking point according to claim 1 or 2, characterised in that the smallest passage cross-section in the secondary line (13) is formed to be larger than the passage cross-section of the burner nozzle (14).
- Gas cooking point according to any one of the preceding claims, characterised in that the secondary line (15) is opened at least at the time of the setting of a maximum gas throughput (Q8).
- Gas cooking point according to claim 4, characterised in that the secondary line (13) is closed at the time of setting of a part gas throughput (Q1 to Q7) and is opened only when the maximum gas throughput (Q8) is set.
- Gas cooking point according to any one of the preceding claims, characterised in that the blocking element (17) for opening and closing the secondary line (13) is constructed as an unthrottled switching valve.
- Gas cooking point according to any one of the preceding claims, characterised in that the control arrangement (5) comprises a number of control elements (23, 25, 27), which are connected in parallel and which are provided in control lines (7, 9, 11) branching off from the main line (3, 15).
- Gas cooking point according to claim 7, characterised in that the control lines (7, 9, 11) and the secondary line (13) are formed in a common housing (33).
- Gas cooking point according to one of claims 7 and 8, characterised in that the control and secondary lines (7, 9, 11, 13) each have a mounting opening (59) for insertion of the control elements (23, 25, 27).
- Gas cooking point according to claim 9, characterised in that the mounting opening (59) of the secondary line (13) is closed by, for example, a closure element (61).
- Gas cooking point according to any one of the preceding claims, characterised in that the control arrangement (5) is so designed that the part gas throughputs (Q1 to Q7) up to approximately 60% of the maximum gas throughput (Q8) increase at a substantially constant first gradient.
- Gas cooking point according to claim 11, characterised in that the part gas throughputs (Q1 to Q7) from approximately 60% of the maximum gas throughput (Q8) to the maximum gas throughput (Q8) increase at a second gradient greater than the first gradient.
- Gas cooking point according to any one of the preceding claims, characterised in that when the maximum gas throughput (Q8) is set the main line, particularly the control lines (7, 9, 11) branching off the main line (3, 15), is or are open.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| EP04701602A EP1588099B1 (en) | 2003-01-13 | 2004-01-13 | Gas cooker |
Applications Claiming Priority (4)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| EP03360005 | 2003-01-13 | ||
| EP03360005 | 2003-01-13 | ||
| PCT/EP2004/000171 WO2004063629A1 (en) | 2003-01-13 | 2004-01-13 | Gas cooking equipment and method for producing gas cooking equipment |
| EP04701602A EP1588099B1 (en) | 2003-01-13 | 2004-01-13 | Gas cooker |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| EP1588099A1 EP1588099A1 (en) | 2005-10-26 |
| EP1588099B1 true EP1588099B1 (en) | 2011-03-16 |
Family
ID=32695663
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| EP04701602A Expired - Lifetime EP1588099B1 (en) | 2003-01-13 | 2004-01-13 | Gas cooker |
Country Status (6)
| Country | Link |
|---|---|
| US (1) | US7513247B2 (en) |
| EP (1) | EP1588099B1 (en) |
| AT (1) | ATE502257T1 (en) |
| DE (1) | DE502004012305D1 (en) |
| ES (1) | ES2363223T3 (en) |
| WO (1) | WO2004063629A1 (en) |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20070006865A1 (en) | 2003-02-21 | 2007-01-11 | Wiker John H | Self-cleaning oven |
| DE10322217B4 (en) * | 2003-05-16 | 2005-03-10 | Miele & Cie | Adjustment device for a gas cooking appliance and gas cooking appliance |
| US9585400B2 (en) | 2004-03-23 | 2017-03-07 | The Middleby Corporation | Conveyor oven apparatus and method |
| US8087407B2 (en) | 2004-03-23 | 2012-01-03 | Middleby Corporation | Conveyor oven apparatus and method |
| US8001957B2 (en) | 2005-08-16 | 2011-08-23 | Bsh Bosch Und Siemens Hausgeraete Gmbh | Device for increasing power for a limited time |
| KR100805630B1 (en) * | 2006-12-01 | 2008-02-20 | 주ģķģ¬ ź²½ėėė¹ģ | Combustion apparatus for a gas boiler |
| US8146584B2 (en) * | 2006-12-01 | 2012-04-03 | Carrier Corporation | Pressure switch assembly for a furnace |
| US20080127963A1 (en) * | 2006-12-01 | 2008-06-05 | Carrier Corporation | Four-stage high efficiency furnace |
| ES2310491B1 (en) * | 2007-06-21 | 2009-10-27 | Bsh Electrodomesticos EspaƱa, S.A. | COMMAND PROVISION FOR A GAS KITCHEN. |
| WO2009062281A1 (en) * | 2007-11-16 | 2009-05-22 | Wolfedale Engineering Limited | Temperature control apparatus for a barbeque grill |
| US8863734B2 (en) * | 2008-12-01 | 2014-10-21 | General Electric Company | Gas grill |
| EA022147B1 (en) * | 2009-07-24 | 2015-11-30 | ŠŃŃ ŠŠ¾Ń УнГ Š”ŠøŠ¼ŠµŠ½Ń Š„Š°ŃŃŠ³ŠµŃŠµŃŠµ ŠŠ¼Š±Ń | Switch of a gas valve unit |
| AU2010275355B2 (en) | 2009-07-24 | 2014-10-23 | Bsh Hausgerate Gmbh | Actuating mechanism of a gas valve unit |
| CN102549340B (en) * | 2009-07-24 | 2015-04-01 | Bshåäøå脿éØåå®¶ēØēµåØęéå ¬åø | Structure of a gas valve unit |
| US8839714B2 (en) | 2009-08-28 | 2014-09-23 | The Middleby Corporation | Apparatus and method for controlling a conveyor oven |
| PL2572143T3 (en) * | 2010-05-20 | 2014-12-31 | Bsh Hausgeraete Gmbh | Gas valve unit having two gas outlets |
| DE102010039009A1 (en) | 2010-08-06 | 2012-02-09 | BSH Bosch und Siemens HausgerƤte GmbH | Gas valve unit |
| DE102010039010A1 (en) | 2010-08-06 | 2012-02-09 | BSH Bosch und Siemens HausgerƤte GmbH | Gas valve unit |
| DE202010018527U1 (en) * | 2010-08-13 | 2017-05-29 | Ebm-Papst Landshut Gmbh | Mixing device for mixing combustion air and gas and firing device |
| US8881769B2 (en) * | 2010-09-20 | 2014-11-11 | Bsh Bosch Und Siemens Hausgeraete Gmbh | Structure of a gas-valve unit |
| TR201907500T4 (en) | 2010-10-15 | 2019-06-21 | Bsh Hausgeraete Gmbh | GAS VALVE UNIT |
| US8783243B2 (en) | 2010-10-25 | 2014-07-22 | General Electric Company | Lockout system for surface burners of a cooking appliance |
| WO2012080051A2 (en) * | 2010-12-14 | 2012-06-21 | BSH Bosch und Siemens HausgerƤte GmbH | Gas valve unit for a dual circuit burner |
| PL2756229T3 (en) | 2011-09-16 | 2017-10-31 | Bsh Hausgeraete Gmbh | Gas valve unit |
| ES2430939R1 (en) * | 2012-05-22 | 2014-03-03 | BSH ElectrodomƩsticos EspaƱa S.A. | Gas heated cooking appliance |
| DE102012017207A1 (en) * | 2012-08-31 | 2014-03-06 | Robert Bosch Gmbh | Method for controlling a hydraulic valve arrangement and hydraulic valve arrangement |
| ES2799415T3 (en) * | 2013-03-13 | 2020-12-17 | Bsh Hausgeraete Gmbh | Gas valve unit |
| US9841191B2 (en) | 2015-04-22 | 2017-12-12 | Whirlpool Corporation | Appliance with electronically-controlled gas flow to burners |
| TR201906193T4 (en) | 2016-03-17 | 2019-05-21 | Bsh Hausgeraete Gmbh | Gas fitting and cooking device. |
| WO2017218695A1 (en) | 2016-06-14 | 2017-12-21 | The Middleby Corporation | Convection conveyor oven manifold and damper system |
| TR201611375A2 (en) * | 2016-08-12 | 2018-02-21 | Bsh Ev Aletleri San Ve Tic As | A Control Knob Equipped With a Gear Box For Controlling Power Level Of a Burner in a Gas Cooker |
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|---|---|---|---|---|
| US4134719A (en) * | 1976-09-27 | 1979-01-16 | Velie Wallace W | Multi-flame fuel burner for liquid and gaseous fuels |
| AT400075B (en) * | 1991-08-06 | 1995-09-25 | Vaillant Gmbh | METHOD FOR ADJUSTING A GAS HEATER PROVIDED WITH A BURNER BY PRESETING A GAS FLOW RATE AND DEVICE FOR SETTING THIS GAS FLOW RATE |
| DE19627539A1 (en) * | 1996-07-09 | 1998-01-15 | Gaggenau Werke | Method and device for controlling the flame size of gas-operated cooking or baking devices |
| DE19815636C2 (en) * | 1998-04-07 | 2000-07-06 | Truma Geraetetechnik Gmbh & Co | Heater with turbo level |
| DE19905198A1 (en) * | 1999-02-09 | 2000-08-10 | Agt Gas Technology Gmbh | Cooking range for gas stoves |
| US6322354B1 (en) * | 2000-07-17 | 2001-11-27 | Wolf Appliance Company, Llc | Stacked dual gas burner |
| US6609904B2 (en) * | 2001-01-03 | 2003-08-26 | Wen-Chou Chen | Gas furnace control arrangement |
-
2004
- 2004-01-13 DE DE502004012305T patent/DE502004012305D1/en not_active Expired - Lifetime
- 2004-01-13 ES ES04701602T patent/ES2363223T3/en not_active Expired - Lifetime
- 2004-01-13 WO PCT/EP2004/000171 patent/WO2004063629A1/en not_active Ceased
- 2004-01-13 AT AT04701602T patent/ATE502257T1/en active
- 2004-01-13 EP EP04701602A patent/EP1588099B1/en not_active Expired - Lifetime
- 2004-01-13 US US10/540,241 patent/US7513247B2/en not_active Expired - Fee Related
Also Published As
| Publication number | Publication date |
|---|---|
| US7513247B2 (en) | 2009-04-07 |
| ES2363223T3 (en) | 2011-07-27 |
| WO2004063629A1 (en) | 2004-07-29 |
| DE502004012305D1 (en) | 2011-04-28 |
| EP1588099A1 (en) | 2005-10-26 |
| US20060016444A1 (en) | 2006-01-26 |
| ATE502257T1 (en) | 2011-04-15 |
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