EP3301362B1 - Procédé de régulation d'écoulements turbulents - Google Patents

Procédé de régulation d'écoulements turbulents Download PDF

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Publication number
EP3301362B1
EP3301362B1 EP16191924.6A EP16191924A EP3301362B1 EP 3301362 B1 EP3301362 B1 EP 3301362B1 EP 16191924 A EP16191924 A EP 16191924A EP 3301362 B1 EP3301362 B1 EP 3301362B1
Authority
EP
European Patent Office
Prior art keywords
flow
actuator
signal
duct
air
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.)
Active
Application number
EP16191924.6A
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German (de)
English (en)
Other versions
EP3301362A1 (fr
Inventor
Rainer Lochschmied
Mike Schmanau
Bernd Schmiederer
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Siemens AG
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Siemens AG
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Priority to ES16191924T priority Critical patent/ES2792874T3/es
Application filed by Siemens AG filed Critical Siemens AG
Priority to PL16191924T priority patent/PL3301362T3/pl
Priority to HUE16191924A priority patent/HUE049484T2/hu
Priority to EP16191924.6A priority patent/EP3301362B1/fr
Priority to RU2017133736A priority patent/RU2674104C1/ru
Priority to CN201710917791.8A priority patent/CN107883399B/zh
Priority to US15/722,129 priority patent/US11175039B2/en
Publication of EP3301362A1 publication Critical patent/EP3301362A1/fr
Application granted granted Critical
Publication of EP3301362B1 publication Critical patent/EP3301362B1/fr
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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23NREGULATING OR CONTROLLING COMBUSTION
    • F23N1/00Regulating fuel supply
    • F23N1/02Regulating fuel supply conjointly with air supply
    • F23N1/025Regulating fuel supply conjointly with air supply using electrical or electromechanical means
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23NREGULATING OR CONTROLLING COMBUSTION
    • F23N1/00Regulating fuel supply
    • F23N1/02Regulating fuel supply conjointly with air supply
    • F23N1/022Regulating fuel supply conjointly with air supply using electronic means
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23NREGULATING OR CONTROLLING COMBUSTION
    • F23N1/00Regulating fuel supply
    • F23N1/02Regulating fuel supply conjointly with air supply
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23DBURNERS
    • F23D14/00Burners for combustion of a gas, e.g. of a gas stored under pressure as a liquid
    • F23D14/46Details, e.g. noise reduction means
    • F23D14/60Devices for simultaneous control of gas and combustion air
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23NREGULATING OR CONTROLLING COMBUSTION
    • F23N1/00Regulating fuel supply
    • F23N1/02Regulating fuel supply conjointly with air supply
    • F23N1/027Regulating fuel supply conjointly with air supply using mechanical means
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23NREGULATING OR CONTROLLING COMBUSTION
    • F23N5/00Systems for controlling combustion
    • F23N5/18Systems for controlling combustion using detectors sensitive to rate of flow of air or fuel
    • F23N2005/181Systems for controlling combustion using detectors sensitive to rate of flow of air or fuel using detectors sensitive to rate of flow of air
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23NREGULATING OR CONTROLLING COMBUSTION
    • F23N2223/00Signal processing; Details thereof
    • F23N2223/12Integration
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23NREGULATING OR CONTROLLING COMBUSTION
    • F23N2223/00Signal processing; Details thereof
    • F23N2223/14Differentiation
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23NREGULATING OR CONTROLLING COMBUSTION
    • F23N2225/00Measuring
    • F23N2225/04Measuring pressure
    • F23N2225/06Measuring pressure for determining flow
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23NREGULATING OR CONTROLLING COMBUSTION
    • F23N2233/00Ventilators
    • F23N2233/06Ventilators at the air intake
    • F23N2233/08Ventilators at the air intake with variable speed
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23NREGULATING OR CONTROLLING COMBUSTION
    • F23N2235/00Valves, nozzles or pumps
    • F23N2235/02Air or combustion gas valves or dampers
    • F23N2235/06Air or combustion gas valves or dampers at the air intake
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23NREGULATING OR CONTROLLING COMBUSTION
    • F23N2235/00Valves, nozzles or pumps
    • F23N2235/02Air or combustion gas valves or dampers
    • F23N2235/10Air or combustion gas valves or dampers power assisted, e.g. using electric motors
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23NREGULATING OR CONTROLLING COMBUSTION
    • F23N5/00Systems for controlling combustion
    • F23N5/18Systems for controlling combustion using detectors sensitive to rate of flow of air or fuel

Definitions

  • Fluctuations in the air ratio ⁇ occur due to changes in air temperature and / or air pressure. Combustion devices are therefore set with an excess of air. This measure serves to avoid unsanitary combustion. A disadvantage of the adjustment of combustion devices to an excess of air is a reduced efficiency of the system.
  • Speed sensors and air pressure switches can also be used to measure the air throughput.
  • a disadvantage of speed sensors is that they are not sensitive to fluctuations in air temperature and air pressure.
  • a disadvantage of air pressure switches is that air pressure monitoring is only possible at a certain pressure. After all, by using several switches, air pressure can be monitored at several pressures. However, readjustment in the entire operating range of the combustion device has hitherto hardly been possible. A solution for adjustment at one point has also previously required two units.
  • EP1236957B1 was issued on November 2, 2006 and deals with the adaptation of a burner-operated heater to an air-exhaust system.
  • EP1236957B1 discloses a pressure sensor / air mass sensor 28 which is arranged in the air supply 14 or exhaust gas discharge of a heating device.
  • a controller 30 regulates a blower 26 based on the signal from the sensor 28.
  • An operating characteristic curve 40 is stored in order to adjust the instantaneous air volume flow to a required air volume flow.
  • a temperature sensor 35 is provided to improve the control behavior in the event of large temperature differences and with regard to emergency running properties.
  • EP2556303B1 is issued on February 24, 2016 and deals with a pneumatic system with mass balancing.
  • EP2556303B1 discloses a Venturi nozzle 5, which generates negative pressure, with a mass flow sensor 6 in an additional channel 7.
  • a controller 9 regulates the speed of a blower 1 as a function of the signal from the sensor 6.
  • German patent DE102004055715B4 was issued on March 22, 2007 and deals with the setting of the air ratio of a combustion device. According to DE102004055715B4 an air mass flow m L is adjusted to an increased value so that hygienic combustion occurs.
  • Other methods for controlling a burner device are from the EP1243857 , the DE102010010952 and the US2009 / 111065 known.
  • the aim of the present disclosure is to improve the regulation of flows in combustion devices, in particular in the presence of turbulence.
  • the present disclosure teaches an improved method for controlling a burner device according to claim 1.
  • the quantity setting of one or more actuators for setting the air flow is determined from a given air flow via a respectively stored functional relationship.
  • One of the actuators for setting the air flow is regulated with the aid of the flow sensor in the side channel in such a way that the predetermined value of the air flow is reached.
  • the quantity setting of the fuel and the air flow are assigned to one another. This can be done either by a fixed assignment and / or by an assignment as a result of a ⁇ regulation.
  • the burner output is determined via the air flow, which is determined via the mass flow sensor in the side channel. With the aid of the mass flow sensor, influences such as air temperature and / or barometric pressure on the air are compensated. If the air ratio ⁇ is kept constant by means of a control system, the burner output remains (almost) the same regardless of the type of fuel.
  • FIG. 1 shows a system comprising a burner 1, a heat consumer 2, a blower 3 with adjustable speed and a motor-adjustable flap 4.
  • the motor-adjustable flap 4 is arranged after the air inlet 27.
  • the heat consumer 2 heat exchanger
  • the flow (particle flow and / or mass flow) 5 of the fluid air can be according to FIG. 1 can be set both by the motor-adjustable flap 4 and by the speed setting 22 of the fan.
  • the air flow rate 5 can also be adjusted solely by the speed of the fan 3.
  • Pulse width modulation can be used, for example, to adjust the speed of the fan 3.
  • the motor of the fan is connected to an inverter. The speed of the fan is therefore adjusted via the frequency of the converter.
  • the flow rate 6 (for example particle flow and / or mass flow) of the fluid fuel through the fuel supply channel 38 is set by a fuel flap 9.
  • the fuel flap 9 is a (motor-adjustable) valve.
  • combustible gases such as natural gas and / or propane gas and / or hydrogen are suitable as fuel.
  • a liquid fuel such as heating oil can also be used as fuel.
  • the flap 9 is motorized adjustable oil pressure regulator in the return of the oil nozzle replaced.
  • the safety shutdown function and / or closing function is implemented by the redundant safety valves 7-8.
  • the safety valves 7-8 and / or the fuel flap 9 are implemented as an integrated unit (s).
  • the burner 1 is an internal combustion engine.
  • an internal combustion engine of a plant with cogeneration is possible.
  • Fuel is added to the air stream 5 in and / or upstream of the burner 1.
  • the mixture is burned in the combustion chamber of the heat consumer 2.
  • the heat is transported in the heat consumer 2.
  • heated water is discharged to heating elements via a pump and / or an item is heated (directly) in industrial furnaces.
  • the exhaust gas flow 10 is discharged (into the environment) via an exhaust gas path 30, for example a chimney.
  • the regulating and / or control and / or monitoring device 16 sets the blower 3 via the signal 22 and the air flap 4 via the signal 23 to the in the regulating and / or control and / or monitoring device 16 (in the form of a Characteristic).
  • the regulating and / or control and / or monitoring device 16 preferably comprises a (non-volatile) memory. Those are in the memory Values stored.
  • the position of the fuel flap 9 is specified via the signal 26.
  • the safety shut-off valves 7, 8 are opened via the signals 24, 25.
  • the safety shut-off valves 7, 8 are kept open during operation.
  • a safety-related position report can be implemented, for example, using redundant position transmitters. If a safety-related feedback about the speed is required, this can take place via the (bidirectional) signal line 22 using (safety-related) speed sensors. For this purpose, redundant speed sensors can be used, for example, and / or the measured speed can be compared with the target speed.
  • the control and feedback signals can be transmitted via different signal lines and / or via a bidirectional bus, for example a CAN bus.
  • a side channel 28 is provided in front of the burner.
  • a small amount of outflowing air 15 flows out through the side channel 28.
  • the air 15 flows out into the room from which the fan 3 draws the air.
  • the outflowing air 15 flows into the combustion chamber of the heat consumer 2.
  • the air flows back into the air duct 11.
  • a flow resistance element an orifice
  • the side channel 28 forms a flow divider together with the burner 1 and the exhaust gas path 30 of the heat consumer 2.
  • the side channel 28 can be both an outflow channel and an inflow channel with respect to the air channel 11, depending on the pressure conditions.
  • a flow resistance element (in the form of an orifice) 14 is attached in the side channel 28. With the flow resistance element 14, the amount of outflowing air 15 of the flow divider is defined.
  • the person skilled in the art recognizes that the function of the orifice 14 as a defined flow resistance can also be realized by a tube of a defined length (and diameter).
  • the person skilled in the art further recognizes that the function of the orifice 14 can also be realized using a laminar flow element and / or by means of another defined flow resistance.
  • the passage area of the flow resistance element 14 is adjustable by a motor.
  • the passage area of the flow resistance element 14 can be adjusted in order to avoid and / or eliminate blockages caused by floating particles.
  • the flow resistance element 14 can be opened and / or closed.
  • the passage area of the flow resistance element is preferably adjusted several times in order to avoid and / or eliminate blockages.
  • the flow rate 15 in the side channel 28 depends on the passage area of the flow resistance element 14. Therefore, the value of the flow 5 is via characteristic values stored in the (non-volatile) memory for the measured values of the flow 15 for each passage area used Flow resistance elements 14 deposited. The value of flow 5 can thus be determined from the measured values of flow 15.
  • the flow (particle flow and / or mass flow) through the side channel 28 is a measure of the air flow 5 through the burner. Influences due to changes in density of the air are compensated for by changes in the absolute pressure and / or the air temperature by the mass flow sensor 13.
  • the flow 15 is normally very much smaller than the air flow 5.
  • the air flow 5 is therefore (practically) not influenced by the side channel 28.
  • the (particle and / or mass) flow 15 through the side channel 28 is at least a factor 100, preferably at least a factor 1000, more preferably at least a factor 10000, less than the (particle and / or Mass) stream 5 through the air duct 11.
  • FIG 2 the detail in the area of the side channel 28 is shown enlarged.
  • a mass flow sensor 13 With the aid of a mass flow sensor 13, the value of the air flow 15 in the side channel 28 is recorded.
  • the signal from the sensor is transmitted to the regulating and / or control and / or monitoring device 16 via the signal line 21.
  • the signal In the regulating and / or control and / or monitoring device 16, the signal is mapped to a value of the air flow 15 through the side duct 28 and / or the air flow 5 through the air duct 11.
  • a signal processing device is present at the location of the mass flow sensor 13.
  • the signal processing device has a suitable interface in order to transmit a signal (to a value of the air flow) processed to the regulating and / or control and / or monitoring device 16.
  • Sensors such as the mass flow sensor 13 allow the measurement at high flow velocities especially in connection with Incinerators in operation. Typical values of such flow velocities are between 0.1 m / s and 5 m / s, 10 m / s, 15 m / s, 20 m / s, or even 100 m / s.
  • Mass flow sensors which are suitable for the present disclosure are, for example, OMRON® D6F-W or type SENSOR TECHNICS® WBA sensors.
  • the usable range of these sensors typically begins at speeds between 0.01 m / s and 0.1 m / s and ends at a speed such as 5 m / s, 10 m / s, 15 m / s, 20 m / s, or even 100 m / s.
  • lower limits like 0.1 m / s can be combined with upper limits like 5 m / s, 10 m / s, 15 m / s, 20 m / s, or even 100 m / s.
  • the signal processing device can contain a filter.
  • the filter averages over fluctuations in the signal caused by turbulence.
  • a suitable filter such as a moving average filter, a filter with a finite impulse response, a filter with an infinite impulse response, a Chebyshev filter, etc.
  • the filter is designed as a (programmable) electronic circuit.
  • the combination of damming probe 12, flow resistance element 14 and filter is advantageous.
  • the filter allows frequency portions of the fluctuations in the signal of the mass flow sensor 13 to be compensated for, which can hardly be compensated for via the damming probe 12 and / or the flow resistance element 14.
  • the damming probe 12 preferably integrates pressure fluctuations of the mass flow 5 in the feed channel 11 of greater than 10 Hz, more preferably greater than 50 Hz.
  • the flow resistance element 14 preferably dampens pressure fluctuations of the mass flow 5 in the feed channel 11 by a factor of 5, more preferably more than a factor of 10 or even more than a factor of 40.
  • the filter integrates fluctuations in the range greater than 1 Hz, preferably greater than 10 Hz.
  • individual or all signal lines 21 - 26 are designed as (eight-wire) computer network cables with (or without) energy transmission integrated in the cable.
  • the units connected to the signal lines 21-26 advantageously communicate not only via the signal lines 21-26, but are also supplied with energy for their operation via suitable signal lines 21-26. Power up to 25.5 watts can ideally be transmitted through signal lines 21-26.
  • individual or all of the units connected to the signal lines 21 - 26 have internal energy stores such as accumulators and / or (super) capacitors. This ensures in particular the energy supply to the connected units in the event that the powers of those units exceed the powers which can be transmitted via the signal lines 21-26.
  • the signals can also be transmitted via a two-wire, bidirectional bus, eg a CAN bus.
  • the illustrated form of measuring a flow in a side channel 28 is particularly advantageous for combustion devices.
  • the air flow 5 in the air duct 11 between the fan 3 and the burner 1 is (in many cases) turbulent.
  • the flow fluctuations due to turbulence are of the same order of magnitude as the average value of the air flow 5. This makes a direct measurement of the value of the air flow 5 (considerably) more difficult.
  • the flow fluctuations occurring in the side duct 28 are significantly smaller than the flow fluctuations in the air duct 11 generated by the fan 3 FIG 2 Arrangement shown a significantly improved signal-to-noise ratio of the signal of the mass flow sensor 13.
  • the side channel 28 is constructed so that (practically) no relevant macroscopic flow profile of the air flow 15 is obtained.
  • the air flow 15 preferably sweeps laminarly over the mass flow sensor 13.
  • the person skilled in the art uses, among other things, the Reynolds number Re D for dividing the mass flow 15 of a fluid in the side channel 28 with diameter D into laminar or turbulent. According to one Embodiments apply flows with Reynolds numbers Re D ⁇ 4000, particularly preferably with Re D ⁇ 2300, further preferably with Re D ⁇ 1000 as laminar.
  • the passage area of the flow resistance element 14 is preferably dimensioned to allow a defined, preferably laminar, flow profile (of a mass flow 15) to arise in the side channel 28.
  • a defined flow profile in the side channel 28 is characterized by a defined speed distribution of a mass flow 15 as a function of the radius of the side channel 28. The mass flow 15 is therefore not chaotic.
  • a defined flow profile is unique for each flow quantity 15 in the side channel 28. With a defined flow profile, the flow value measured locally on the mass flow is representative of the flow rate in the side channel 28. It is therefore representative of the flow rate 5 in the feed channel 11.
  • a defined flow profile (of a mass flow 15) in the side channel 28 is preferably not turbulent.
  • a defined flow profile (of a mass flow 15) in the side channel 28 can have a (parabolic) speed distribution depending on the radius of the side channel 28.
  • the damming probe 12 is in fluid communication with the air duct 11 via the openings 31.
  • the total area of the openings 31 (the cross-section through which the openings 31 can flow) is significantly larger than the passage area of the flow resistance element 14.
  • the passage area of the flow resistance element 14 is therefore (practically) decisive for the value of the air flow 15 through the side channel 28.
  • the total cross-section through which the openings 31 can flow through is at least a factor of 2, preferably at least a factor of 10, particularly preferably at least a factor of 20, larger than the passage area of the flow resistance element 14.
  • the person skilled in the art chooses a small area for the total area of the openings 31 in relation to the cross section of the damming probe 12. Fluctuations in the turbulent main flow 5 therefore have no (practical) effect. A calm back pressure builds up in the tube of the damming probe.
  • the total cross-section through which the openings 31 can flow is smaller by at least a factor of 2, preferably at least a factor of 5, particularly preferably at least a factor of 10, than the cross-section of the congestion probe 12.
  • the individual openings of the inlet 31 preferably have diameters of less than 5 mm, more preferably less than 3 mm, particularly preferably less than 1.5 mm.
  • FIG 3 shows as opposite FIG. 1 modified embodiment a system with a motor-adjustable air flap 4.
  • the air flap 4 is arranged downstream of the blower 3.
  • the air flap 4 is also arranged downstream of the side channel 28.
  • the system out FIG 3 allows the position of the air flap 4 and / or the fan speed to be determined for each power point. This results (reversibly clearly) from each flow value 5 and the (reported) position of the air flap 4 and / or the (reported) speed of the fan 3, a flow value 15 in the side channel 28.
  • FIG 4 shows as opposite FIG. 1 and FIG 3 modified embodiment a system with mixing device 17 in front of the blower 3.
  • fuel is not mixed with air at burner 1. Instead, fuel is added to the air flow 5 by means of a mixing device 17 upstream of the blower 3. Accordingly, the fuel-air mixture is found in the blower 3 (and in the duct 11). The The fuel-air mixture is then burned in the burner 1 in the combustion chamber of the heat consumer 2.
  • the air 15 flows in on the suction side via the mass flow sensor 13.
  • the blower 3 generates a vacuum at this location.
  • the side channel 28 is an inflow channel.
  • the side channel 28 is advantageously arranged in front of the mixing device 17. A possible negative pressure generated by the mixing device 17 thus has no effect on the flow 15 (particle flow and / or mass flow) through the side channel 28.
  • the fluid flow 5 can only be adjusted via the blower 3 with the aid of the signal line 22.
  • a (motorized adjustable flap) can also be installed.
  • a flap is arranged on the pressure side or suction side of the blower 3.
  • the flap can be installed instead of the flow resistance element 18. It is then practically designed as a motor-adjustable flow resistance element (with feedback).
  • the mass flow sensor 13 is easy to attach to practically any system on the suction side. Also in FIG 3 and FIG 4 compensate disclosed systems Changes in density of the air such as FIG. 1 spelled out. The particle and / or mass flow 5 of the fluid through the burner 1 is determined in each case.
  • the flow 15 in the side channel 28 is measured with a mass flow sensor 13.
  • the mass flow sensor 13 is arranged in the inflow / outflow channel 28.
  • the mass flow sensor 13 advantageously works on the anemometer principle.
  • An (electrically) operated heater heats the fluid.
  • the heating resistor can also be used as a temperature measuring resistor.
  • the reference temperature of the fluid is measured in a measuring element arranged in front of the heating resistor.
  • the reference temperature measuring element can also be designed as a resistor, for example in the form of a PT-1000 element.
  • the heating resistor and the reference temperature resistor are arranged on one chip.
  • the person skilled in the art recognizes that the heating must be sufficiently thermally decoupled from the reference temperature measuring element.
  • the anemometer can be operated in two possible ways.
  • the heating resistor is heated with a constant, known heating power, heating voltage and / or heating current.
  • the temperature difference between the heater and the reference temperature measuring element is a measure of the flow (particle flow and / or mass flow) in the side channel 28. It is thus also a measure of the flow 5 (particle flow and / or mass flow) of the main flow (through channel 11).
  • the heater is heated in a closed temperature control loop. This results in a constant temperature of the heater.
  • the temperature of the heater (apart from fluctuations due to the control) is equal to the temperature of the setpoint of the control loop.
  • the setpoint of the temperature of the heater is determined by a constant temperature difference to the measured temperature of the Reference temperature measuring element is added.
  • the constant temperature difference corresponds to the excess temperature of the heater compared to the reference temperature measuring element.
  • the power introduced into the heater is a measure of the flow (particle flow and / or mass flow) in the side channel 28. It is thus also a measure of the flow 5 (particle flow and / or mass flow) of the main flow.
  • FIG 5 teaches how a pressure divider with bypass channel 29 can be constructed in such cases.
  • a second flow resistance element 19 is then located behind the first flow resistance element 14 with a larger passage area.
  • the pressure is therefore divided between the two flow resistance elements 14 and 19.
  • the passage areas of the flow resistance elements 14 and 19 determine the division of the pressure.
  • a further flow resistance element 20 is arranged in front of the mass flow sensor 13 in the bypass channel 29.
  • the person skilled in the art chooses the passage area of the flow resistance element 20 to be sufficiently large.
  • the person skilled in the art also selects a passage area of the flow resistance element 20 which is adapted to the mass flow sensor 13.
  • the sub-flow divider constructed in this way can then be used (reversibly unambiguously) to determine the flow rate 5 (particle flow and / or mass flow) through channel 11.
  • the mass flow sensor 13 can be implemented redundantly (twice) with a comparison of results.
  • the double version initially affects the Mass flow sensor 13 itself and the signal processing device.
  • the result comparison can then be carried out in secure hardware and / or software at the location of the sensors and / or in the regulating and / or control and / or monitoring device 16.
  • the side channel 28 is implemented redundantly (twice).
  • Each redundantly present side channel 28 preferably includes a flow resistance element 14. This allows errors due to clogged flow resistance elements 14 to be detected.
  • the branch for the second side channel is preferably between the flow resistance element 14 and the damming probe 12.
  • the damming probe 12 can be assumed to be fail-safe due to the (comparatively) large openings 31.
  • the (double) redundant structure of the signal processing device also allows errors in the signal processing device to be recognized.
  • the measured values of the redundant mass flow sensors 13, preferably with additional averaging in each case are compared with one another by subtraction.
  • the difference ⁇ then lies within a threshold value band - ⁇ 1 ⁇ ⁇ ⁇ ⁇ 2nd with the limits ⁇ 1 and ⁇ 2 .
  • the difference ⁇ for each setpoint value of the flow rate 5 can be compared and evaluated.
  • the flow rate 5 (particle flow and / or mass flow) through channel 11 can be regulated by means of the sensor signal 21 via the blower 3.
  • all air actuators 4, with the exception of the speed of the fan 3 are each set to a permanently entered setpoint position.
  • the target positions are for the required flow rate 5 (particle flow and / or mass flow) through channel 11 in the regulating and / or control and / or monitoring device 16.
  • the speed of the fan 3 is adjusted until the sensor measured value 21 reaches the value for the required flow rate stored in the memory.
  • FIG 6 shows the control loop.
  • the setpoint 32 associated with the required flow rate 5 (particle flow and / or mass flow) through channel 11 for the flow rate 15 in the side channel 28 is stored in the memory of the regulating and / or control and / or monitoring device 16.
  • a comparison between the setpoint 32 and the signal 21 of the mass flow sensor 13 results in a setpoint-actual deviation 33 via a (device for) difference formation 35.
  • the control signal 22 is given for the blower 3.
  • the blower 3 In response to the actuating signal 22, the blower 3 generates the throughflow 5 (particle flow and / or mass flow) through channel 11.
  • the signal 21 is, with the aid of the aforementioned measuring arrangement 34, comprising the side channel 28, at least one flow resistance element 14, the mass flow sensor 13 and optionally the Jam probe 12 generated.
  • the signal 21 is a (reversibly unique) measure of the flow rate 5 (particle flow and / or mass flow) through channel 11.
  • the control circuit disclosed here compensates for changes in air density. Such changes occur, for example, as a result of temperature fluctuations and / or changes in absolute pressure.
  • controller 29 can also be implemented as a fuzzy logic controller and / or as a neural network.
  • control signal 22 for the blower 3 can be a pulse-width-modulated signal, for example.
  • control signal 22 for the fan 3 is an alternating current generated by a (matrix) converter. The frequency of the AC corresponds to (is proportional to) the speed of the fan 3.
  • the target positions of the actuators 4 must be determined fail-safe. This is done, for example, using two position sensors (angle sensors, stroke sensors, light barriers, etc.).
  • the optional (electronic) filter 36 smoothes the measurement signal.
  • the filter 36 can be designed adaptively according to one embodiment.
  • the measurement signal is averaged over a long, maximum integration time (for example two seconds to five seconds) as a comparison value using a moving average filter. If a measured value deviates from the mean value of the measured values or alternatively from the target value 32 outside a predetermined range, a target value jump is assumed. The measured value is now used directly as the actual value.
  • the control loop therefore reacts immediately with the sampling rate of the control loop.
  • the integration time is increased step by step with (each) scan of the control loop.
  • the value integrated in this way is used as the actual value. This continues until the maximum integration time is reached.
  • the control loop is now considered stationary.
  • the value averaged in this way is now used as the actual value.
  • the disclosed method enables an exact stationary measurement signal with maximum dynamics.
  • the assignment of the positions 23 of the at least one air actuator 4 and the setpoint 32 for the mass flow sensor 13 is a function of the flow rate 5 (particle flow and / or mass flow) through channel 11.
  • the Function stored in a table. Intermediate values between the points defined by the table are interpolated linearly. As an alternative, intermediate values between the points defined by the table are interpolated by a polynomial over several neighboring values and / or over (cubic) splines. The person skilled in the art recognizes that other forms of interpolation can also be implemented.
  • the regulating and / or control and / or monitoring device 16 has a reading device for identification on the basis of radio-frequency waves (RFID reading device).
  • RFID reading device The regulating and / or control and / or monitoring device 16 is designed to use the reading device to read operating parameters such as formulas (of polynomials defined in sections) and / or like the aforementioned tables from a so-called (RFID) transponder.
  • the operating parameters are then stored in the (non-volatile) memory of the regulating and / or control and / or monitoring device 16. If necessary, they can be read out and / or used by a microprocessor.
  • the table below shows the setpoint for the mass flow sensor 13 in the side channel 28 and the values for the motorized flap 4.
  • the table below also shows the values for a further (motor-adjustable) flap or valve which acts on the flow 5 (particle flow and / or mass flow) through channel 11.
  • further actuators can be added in the form of columns. According to a special embodiment, none of the flaps are present. This eliminates the corresponding columns.
  • a specific value of flow rate 5 particle flow and / or mass flow
  • the two values between which the desired value of flow rate 5 lies are searched in the table. The position between the two values is then determined. If the desired value of the flow rate 5 is an amount s% between the values k and k + 1 (1 ⁇ k ⁇ n), then the angle of the (motor-adjustable) flap or valve 4 at a distance of s% between the angles k and approached k + 1. The same applies to the angle (the position) of the (motor-adjustable) further flap or the further valve.
  • the flow rate 5 can be specified as an absolute number and / or relative to a value, preferably to the flow rate 5 at the greatest power value. The flow value is then stored, for example, as a percentage of the flow 5 of the greatest power value.
  • the positions of the at least one air actuator 4 are stored as a polynomial as a function of the flow rate 5 (particle flow and / or mass flow) through channel 11 instead of the aforementioned table.
  • the positions of the at least one air actuator 4 are stored as functions defined in sections as a function of the flow rate 5 (particle flow and / or mass flow) through channel 11.
  • the positions of the at least one air actuator 4 are stored as a (valve) opening curve (s).
  • the design can be made fail-safe.
  • the at least one actuator 4 from the aforementioned table can monitor its position.
  • the flow 15 (particle flow and / or mass flow) through the side channel 28 is detected in a safety-related manner.
  • the position of the actuator 9 with which the fuel throughput 6 is set can also be included in the table shown above. This position can be both the position of a flap and / or the position or opening of a fuel valve and / or a measured flow value from the fuel throughput 6.
  • the air throughput 5 thus becomes synonymous with the performance value, since the fuel throughput 6 and the air throughput 5 are firmly connected to one another.
  • the fuel throughput 6 or the position of the fuel actuator 9 can be defined for setting the power.
  • the assigned air throughput 5 can be determined in the table on the basis of the characteristic curve and / or on the basis of the linear interpolation between the table values.
  • the positions of the air actuators 4 and the setpoint value of the mass flow 32 in air can be as above described are interpolated in a table and / or determined using another mathematical assignment.
  • the values for the flow rate 5 are given absolutely in the regulating and / or control and / or monitoring device 16. According to another embodiment, the values for the flow rate 5 are specified in the regulating and / or control and / or monitoring device 16 relative to a specific value of the flow rate. The values for the flow are preferably specified in the regulating and / or control and / or monitoring device 16 relative to the maximum throughput 5 (in air) at maximum output.
  • the fuel throughput 6 is not directly assigned to the air throughput 5.
  • the position of the fuel flap or the fuel valve 9 is assigned to the fuel throughput 6 in a second functional assignment. As with air, this can be done using a table as shown below.
  • Fuel flow 6 (Motor-adjustable) fuel flap or fuel valve 9 Value 1 Angle 1 Value 2 Angle 2 ... ... Value n Angle n
  • the fuel throughput 6 stored in the table is an absolute or relative value for an air ratio ⁇ 0 .
  • the fuel throughput 6 stored in the table is also a absolute or relative value for the fuel present in the fuel supply during a setting process.
  • the air ratio ⁇ 0 is usually specified during the setting process.
  • the functional assignment takes place during the setting process mentioned.
  • the fuel throughput 6 of the delivered fuel is assigned to the air throughput 5 defined in the linearized scale at a defined air ratio ⁇ 0 .
  • the position of the fuel actuator 9 is thus mapped onto a linear scale of the fuel throughput 6.
  • L min is the minimum air requirement of the fuel, ie the ratio of air throughput 5, which is necessary under conditions of stoichiometry, to fuel throughput 6.
  • L min is a quantity that depends on the composition of the fuel or the type of fuel.
  • the fuel composition has the minimum air requirement L min0 .
  • V ⁇ L 0 ⁇ 0 ⁇ L min 0 ⁇ V ⁇ G 0 between the air flow rate during the setting process V ⁇ L 0 , the air ratio during the setting process ⁇ 0 , the minimum air requirement during the setting process L min 0 and the fuel flow rate during the setting process V ⁇ G 0 .
  • V ⁇ RL V ⁇ RG .
  • the relative air throughput is therefore equal to the relative fuel throughput as was also determined during the setting process based on the maximum values.
  • the fuel throughput 6 must also be reduced by the factor F or the air throughput 5 must be increased by the factor F.
  • Both values, air throughput 5 and fuel throughput 6, are each on an almost linear scale. It is therefore sufficient to know the factor F for one performance point in order to calculate the fuel throughput 6 for each performance point from the values stored in the setting if the air throughput 5 is used as the performance variable. If the fuel throughput 6 is used as the output variable 5, the correct air throughput 5 can be calculated for each output point.
  • the corresponding positions can then be set for a predetermined power value.
  • the delivery rate of the blower 3 can be adjusted accordingly.
  • the current value for fuel throughput 6 is thus assigned to the current value of air throughput 5 via a fixed factor.
  • a base factor is determined during the setting as shown above. For a direct representation of air throughput 5 or fuel throughput 6, it is ⁇ 0 ⁇ L min 0 . For a representation of air throughput 5 or fuel throughput 6 relative to the respective maximum values from the setting process, it is preferably set to one.
  • the air throughput 5 or the fuel throughput 6 are adjusted by the factor 1 / F compared to the stored setting values.
  • the factor F is determined by changing the composition of the fuel using A control, this value also applies to all Credit points.
  • the linear scales for air throughput 5 and fuel throughput 6 the output can be changed much faster than the ⁇ control would allow.
  • ⁇ control and power adjustment are decoupled from each other. This is very advantageous because, due to the system runtimes and the time constants of the system, the A control loop regulates environmental changes much more slowly than the performance should be changed in comparison. Typical environmental changes are air temperature, air pressure, fuel temperature and / or fuel type. Such changes usually occur so slowly that the ⁇ control loop is sufficiently fast for this.
  • a ⁇ control can be implemented with the help of an O 2 sensor in the exhaust gas.
  • the person skilled in the art can easily calculate the air ratio ⁇ from the derived measured value of an O 2 sensor in the exhaust gas.
  • the fuel throughput 6 is readjusted via the ⁇ control loop when the composition of the fuel changes, so that the burner output remains almost constant.
  • the reason for this is that the energy content for most commonly used fuels correlates (approximately) linearly with the minimum air requirement L min .
  • the control loop after FIG 6 also compensates for errors in the fan and / or regulates them. Faults in the blower 3 are, for example an increased slip of the fan wheel and / or errors in the (electronic) control. Furthermore, gross errors of the blower 3, which can no longer be corrected, can be detected. For this purpose, it is detected whether the control rotational speed 22 of the blower 3 lies outside a band predetermined for each flow 5 through the duct 11. For this purpose, upper and lower limit values of the speed and / or the control signals 22 of the fan 3 are advantageously stored in the aforementioned table for given flow rates 5 (particle flow and / or mass flow) through the channel 11.
  • the values are particularly preferably stored in a (non-volatile) memory of the regulating and / or control and / or monitoring device 16.
  • upper and lower limit values for the speed and / or the control signals 22 of the blower 3 are stored on the basis of functions (defined in sections) such as, for example, straight lines and / or polynomials.
  • the flow rate 5 through channel 11 can also be regulated by another actuator.
  • the flow rate 5 through channel 11 can also be regulated by another actuator.
  • FIG 6 replace the regulation of the blower 3 by regulating the (motor-adjustable) flap 4.
  • all actuators including the blower 3, with the exception of the regulated position of the (motor-adjustable) flap or of the valve 4 are set to a permanently entered setpoint position.
  • the respective target position for a given flow rate 5 (particle flow and / or mass flow) through channel 11 is stored in the (non-volatile) memory of the regulating and / or control and / or monitoring device 16.
  • the positions of the actuators and the setpoint 32 of the flow 15 through the side channel 28 are also stored here as a function of the flow 5 through channel 11, as already mentioned above.
  • the interpolation is carried out as described above.
  • the regulation of the (motor-adjustable) flap or valve 4 means that the position of that Actuator is replaced by the speed of the fan 3.
  • a correspondingly adjusted table is shown below: Flow 5 (particle flow and / or mass flow) through channel 11 Fan 3 (Motor-adjustable) additional flap or valve Setpoint 32 for flow 15 (particle flow and / or mass flow) through side channel 28 Value 1 Speed 1 Angle 1 Flow value 1 Value 2 Speed 2 Angle 2 Flow value 2 ... ... ... ... ... Value n Speed n Angle n Flow value n
  • the target positions of the actuators must be determined fail-safe. This is done, for example, using two position sensors (angle sensors, stroke sensors, speed sensors, Hall sensors, etc.).
  • the controller 37 uses the controller 37, the (motor-adjustable) flap 4 or the valve is adjusted until the signal 21 of the mass flow sensor 13 in the side channel 28 reaches the value for the required flow rate stored in the memory.
  • the speed of the fan 3 cannot be changed.
  • the flow rate 5 through channel 11 is set exclusively via the (motor-adjustable) further flap or the further valve.
  • the flap position 9 can also be directly included in the table.
  • a second assignment for the fuel quantity 6 can also be formed here. The assignment of the linearized scale from fuel throughput 6 to the linearized scale from air throughput 5 is determined by a factor as described above.
  • Parts of a control device or a method according to the present disclosure can be implemented as hardware, as a software module, which is executed by a computing unit, or using a cloud computer, or using a combination of the aforementioned options.
  • the software may include firmware, a hardware driver that runs within an operating system, or an application program.
  • the present disclosure therefore also relates to a computer program product which contains the features of this disclosure or carries out the necessary steps.
  • the functions described can be stored as one or more commands on a computer-readable medium.
  • Computer-readable media include working memory (RAM), magnetic working memory (MRAM), only readable memory (ROM), flash memory, electronically programmable ROM (EPROM), electronically programmable and erasable ROM (EEPROM), registers of a computing unit A hard drive, a removable storage device, optical storage, or any suitable medium that can be accessed by a computer or other IT devices and applications.
  • RAM working memory
  • MRAM magnetic working memory
  • ROM only readable memory
  • EPROM electronically programmable ROM
  • EEPROM electronically programmable and erasable ROM
  • registers of a computing unit A hard drive, a removable storage device, optical storage, or any suitable medium that can be accessed by a computer or other IT devices and applications.
  • the present disclosure teaches a method according to the invention.
  • the side channel 28 and the feed channel 11 of the burner device are in fluid communication.
  • the at least one second actuator 3, 4 is preferably designed to receive a control signal 37.
  • the flow 15 through the side channel 28 is preferably a mass flow (of a gaseous fluid).
  • the flow 5 through the feed channel 11 is preferably a mass flow (of a gaseous fluid).
  • the at least one first actuator 4, 3 and the at least one second actuator 3, 4 preferably act in series (in a row) on the feed channel 11.
  • the at least one first actuator 4, 3 and the at least one second actuator 3, 4 are arranged in a row (in the feed channel 11).
  • the present disclosure further teaches the aforementioned method as a preferred embodiment, wherein the processing of the requested flow 5 through the supply channel 11 to a desired value 32 of the flow 15 through the side channel 28 reversibly and unambiguously assigns (the requested flow 5 through the supply channel 11) includes the target value 32 of the flow 15 through the side channel 28).
  • the present disclosure further teaches one of the aforementioned methods, wherein a control signal is generated (by the controller 37) for the at least one second actuator 3, 4 using a proportional-integral controller 37.
  • the proportional-integral controller 37 is a self-adaptive controller.
  • the present disclosure further teaches one of the aforementioned methods, wherein the generation of a control signal (by the controller 37) for the at least one second actuator 3, 4 takes place using a proportional-integral-derivative controller 37.
  • the proportional-integral-derivative controller 37 is a self-adaptive controller.
  • the present disclosure further teaches one of the aforementioned methods, the at least one a second actuator of the burner device comprises a blower 3 with adjustable speed, wherein the blower 3 with adjustable speed comprises a drive, and wherein the blower 3 is preferably arranged in the feed channel 11 of the burner device.
  • the present disclosure further teaches one of the aforementioned methods, the generated control signal 22, 23 to the at least one second actuator 3, 4 being a pulse-width-modulated signal.
  • the present disclosure also teaches one of the aforementioned methods, the generated control signal 22, 23 to the at least one second actuator 3, 4 being a converter signal with a frequency that corresponds to the speed of the fan 3.
  • the present disclosure further teaches one of the aforementioned methods, the at least one first actuator of the burner device comprising a motor-adjustable flap 4 with a drive, and preferably the motor-adjustable flap 4 is arranged in the feed channel 11 of the burner device.
  • the present disclosure further teaches one of the aforementioned methods, wherein when the control signal 22, 23 is generated by the controller 37, a difference between the setpoint value 32 and the actual value 21 is formed for the at least one second actuator 3, 4.
  • the present disclosure further teaches one of the aforementioned methods, the processing of the second signal 21 generated by the mass flow sensor 13 comprising filtering the second signal 21 generated by the mass flow sensor 13.
  • the present disclosure further teaches one of the aforementioned methods, wherein the processing of the second signal 21 generated by the mass flow sensor 13 comprises filtering with a 3dB threshold of the second signal 21 generated by the mass flow sensor 13, the 3dB threshold of the filtering being set up in this way is that fluctuations in the signal 21 of a frequency greater than 1 Hz, preferably greater than 10 Hz, are integrated.
  • the present disclosure further teaches one of the aforementioned methods, wherein the requested flow 5 through the supply channel 11 is assigned to a (a value of) the position of the at least one first actuator 4, 3 on the basis of a predetermined table, in which values the requested flow 5 through the supply channel 11 values of the positions of the at least one first actuator 4, 3 are assigned.
  • the present disclosure further teaches one of the aforementioned methods, wherein the requested flow rate 5 through the supply channel 11 is assigned to a (a value of) the position of the at least one first actuator 4, 3 on the basis of a predetermined table with subsequent interpolation, whereby Values of the requested flow 5 through the supply channel 11 are assigned values of the positions of the at least one first actuator 4, 3, preferably also values of the positions of each actuator different from the at least one second actuator 3, 4 in the predetermined table.
  • the present disclosure further teaches one of the aforementioned methods, wherein the assignment of the requested flow 5 through the supply channel 11 to a (a value of) the position of the at least one first actuator 4, 3 on the basis of a predetermined (sectionally defined) function (polynomial ) in which values the requested flow 5 through the supply channel 11 values of the positions of the at least one first actuator 4, 3, preferably also values of the positions of each of the at least one second actuator 3, 4 different actuator, are assigned.
  • a predetermined (sectionally defined) function polynomial
  • the present disclosure further teaches one of the aforementioned methods, wherein when generating the control signal 22, 23 (by the controller 37) for the at least one second actuator 3, 4, the amount of a difference between the target value 32 and the actual value 21 is formed and the amount of the difference between the target value 32 and the actual value 21 is compared with a predetermined threshold value, and wherein the threshold value is preferably a function of the target value 32.
  • the present disclosure further teaches the aforementioned methods, the (predetermined) lower threshold value and / or (predetermined) upper threshold value being a function of the requested flow rate 5 through the supply channel 11.
  • the present disclosure further teaches the aforementioned methods, the controller 37 comprising a (non-volatile) memory and the (predetermined) lower threshold value and / or (predetermined) upper threshold value being stored in the memory of the controller 37.
  • the controller 37 is preferably designed to read the (predefined) lower threshold value and / or the (predefined) upper threshold value from the (non-volatile) memory.
  • the present disclosure further teaches the aforementioned methods, the controller 37 comprising a (non-volatile) memory and the table and / or the polynomial function being stored in the memory of the controller 37.
  • the controller 37 is preferably designed to read the table and / or the polynomial function from the (non-volatile) memory.
  • the present disclosure further teaches the aforementioned method, wherein the allocation of the flow of fuel 6 through the fuel supply channel 38 to values of the fuel actuator 9 using a universal table (ideally with subsequent interpolation) and / or using a universal (at least sectionally defined) one polynomial function takes place, the method additionally comprises the step: Assignment of the position (s) of each actuator 4, 3, 9, which is different from the at least one second actuator 3, 4 of the burner device, to a flow 5 of a fluid through the supply channel 11 on the basis of the universal table or a universal polynomial function defined at least in sections.
  • the present disclosure further teaches the aforementioned methods, the controller 37 comprising a (non-volatile) memory and the universal table and / or the universal polynomial function being stored in the memory of the controller 37.
  • the controller 37 is preferably designed to read the universal table and / or the universal polynomial function from the (non-volatile) memory.
  • the present disclosure further teaches one of the aforementioned methods, the method additionally comprising the step: Mapping a flow 6 of fuel through the fuel supply channel 38 to a flow 5 of a fluid through the supply channel 11 based on a constant factor between the flow 6 of a fuel through the fuel supply channel 38 and the flow 5 of a fluid through the supply channel 11.
  • the ⁇ control of the burner device is preferably integrated in the controller 37.
  • the signal generated by the probe in the exhaust duct 30 is preferably a function of an air ratio of a fluid stream in the exhaust duct and / or a function of an oxygen content of a fluid stream in the exhaust duct.
  • the probe in the exhaust duct 30 is preferably a ⁇ probe and / or an O 2 probe (oxygen probe).
  • the present disclosure further teaches one of the aforementioned methods, the method additionally comprising the step: Determining a performance of the burner device on the basis of the target value 32 of the controller 37 and / or on the basis of the value of the requested flow 5 through the supply channel 11.
  • the present disclosure further teaches, as a preferred embodiment, a non-volatile computer readable storage medium that stores an instruction set for execution by at least one processor that, when executed by a processor, also performs one of the aforementioned methods.

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Regulation And Control Of Combustion (AREA)
  • Flow Control (AREA)

Claims (10)

  1. Procédé de régulation d'un dispositif de brûleur au moyen d'un capteur de débit massique (13) dans un conduit latéral (28) d'un conduit d'alimentation (11) du dispositif de brûleur, d'un régulateur (37), d'au moins un premier actionneur (4, 3) agissant sur le conduit d'alimentation (11) et d'au moins un second actionneur (3, 4) agissant sur le conduit d'alimentation (11), dans lequel le au moins un premier actionneur (4, 3) et le au moins un second actionneur (3, 4) sont conçus pour recevoir des signaux, le procédé comprenant les étapes consistant à :
    solliciter un débit (5) d'un fluide à travers le conduit d'alimentation (11),
    associer le débit sollicité (5) à travers le conduit d'alimentation (11) à une position du au moins un premier actionneur (4, 3),
    générer un premier signal (23, 22) pour le au moins un premier actionneur (4, 3), dans lequel le premier signal généré (23, 22) est une fonction de la position du au moins un premier actionneur (4, 3) associée au débit sollicité (5) à travers le conduit d'alimentation (11),
    délivrer le premier signal généré (23, 22) à au moins un premier actionneur (4, 3),
    générer un second signal (21) par le capteur de débit massique (13), dans lequel le second signal (21) est une fonction d'un débit (15) à travers le conduit latéral (28),
    transformer le second signal (21) généré par le capteur de débit massique (13) en une valeur réelle du débit (15) à travers le conduit latéral (28),
    transformer le débit sollicité (5) à travers le conduit d'alimentation (11) en une valeur de consigne (32) du débit (15) à travers le conduit latéral (28),
    générer un signal de régulation (22, 23) par le régulateur (37) pour le au moins un second actionneur (3, 4) en fonction de la valeur réelle du débit à travers le conduit latéral (28) et en fonction de la valeur de consigne (32) du débit (15) à travers le conduit latéral (28),
    délivrer le signal de régulation (22, 23) généré à au moins un second actionneur (3, 4),
    dans lequel :
    un premier élément de résistance à l'écoulement (14) et un second élément de résistance à l'écoulement (19) sont disposés dans le conduit latéral (28), le premier élément de résistance à l'écoulement possédant une surface de passage supérieure à celle du second élément de résistance à l'écoulement,
    le conduit latéral (28) comprend un conduit de contournement (29) comportant un troisième élément de résistance à l'écoulement (20),
    le capteur de débit massique (13) est disposé dans le conduit de contournement (29) du conduit latéral (28), l'élément de résistance à l'écoulement (20) étant disposé avant le capteur de débit massique (13), et
    le au moins un premier actionneur (4, 3) et le au moins un second actionneur (3, 4) sont disposés en série.
  2. Le procédé selon la revendication 1, dans lequel la transformation du débit sollicité (5) à travers le conduit d'alimentation (11) en une valeur de consigne (5) du débit (15) à travers le conduit latéral (28) comprend une association unique réversible du débit sollicité (5) à travers le conduit d'alimentation (11) à la valeur de consigne (32) du débit (15) à travers le conduit latéral (28) .
  3. Le procédé selon l'une des revendications 1 ou 2, dans lequel la génération d'un signal de régulation pour le au moins un second actionneur (3, 4) s'effectue au moyen d'un régulateur (37) à action proportionnelle et intégrale ou au moyen d'un régulateur (37) à action proportionnelle, intégrale et dérivée.
  4. Le procédé selon l'une des revendications 1 à 3, dans lequel le au moins un second actionneur du dispositif de brûleur comprend un ventilateur (3) à vitesse de rotation réglable, le ventilateur à vitesse de rotation réglable (3) comprenant un entraînement, et le ventilateur (3) étant disposé dans le conduit d'alimentation (11) du dispositif de brûleur.
  5. Le procédé selon l'une des revendications 1 à 4, dans lequel le signal de régulation (22, 23) généré pour le au moins un second actionneur (3, 4) est un signal modulé en largeur d'impulsion ou est un signal de convertisseur ayant une fréquence qui correspond à une vitesse de rotation d'un au moins un second actionneur (3, 4) configuré sous forme d'un ventilateur (3).
  6. Le procédé selon l'une des revendications 1 à 5, dans lequel le au moins un premier actionneur du dispositif de brûleur est un clapet (4) réglable de façon motorisée doté d'un dispositif d'entraînement et le clapet réglable de façon motorisée (4) est disposé dans le conduit d'alimentation (11) du dispositif de brûleur.
  7. Le procédé selon l'une des revendications 1 à 6, dans lequel la transformation du second signal (21) généré par le capteur de débit massique (13) comprend une filtration du second signal (21) généré par le capteur de débit massique (13).
  8. Le procédé selon l'une des revendications 1 à 7, dans lequel l'association du débit sollicité (5) à travers le conduit d'alimentation (11) à une position du au moins un premier actionneur (4, 3) est effectuée au moyen d'une table prédéterminée, dans laquelle des valeurs du débit sollicité (5) à travers le conduit d'alimentation (11) sont associées à des valeurs de positions du au moins un premier actionneur (4,3) .
  9. Le procédé selon l'une des revendications 1 à 8, le procédé comprenant en outre l'étape consistant à :
    déterminer une puissance du dispositif de brûleur sur la base de la valeur de consigne (32) du régulateur (37) et/ou sur la base de la valeur du débit sollicité (5) à travers le conduit d'alimentation (11).
  10. Support de mémoire lisible par ordinateur non volatile, qui stocke un jeu d'instructions à exécuter par au moins un processeur, qui lorsqu'elles sont exécutées par un processeur, mettent en œuvre un procédé comprenant les étapes selon l'une des revendications 1 à 9.
EP16191924.6A 2016-09-30 2016-09-30 Procédé de régulation d'écoulements turbulents Active EP3301362B1 (fr)

Priority Applications (7)

Application Number Priority Date Filing Date Title
PL16191924T PL3301362T3 (pl) 2016-09-30 2016-09-30 Sposób regulacji przepływów turbulentnych
HUE16191924A HUE049484T2 (hu) 2016-09-30 2016-09-30 Eljárás turbulens áramlás szabályozására
EP16191924.6A EP3301362B1 (fr) 2016-09-30 2016-09-30 Procédé de régulation d'écoulements turbulents
ES16191924T ES2792874T3 (es) 2016-09-30 2016-09-30 Regulación de flujos turbulentos
RU2017133736A RU2674104C1 (ru) 2016-09-30 2017-09-28 Регулирование турбулентных потоков
CN201710917791.8A CN107883399B (zh) 2016-09-30 2017-09-30 调节紊流流动
US15/722,129 US11175039B2 (en) 2016-09-30 2017-10-02 Regulating turbulent flows

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
EP16191924.6A EP3301362B1 (fr) 2016-09-30 2016-09-30 Procédé de régulation d'écoulements turbulents

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EP3301362A1 EP3301362A1 (fr) 2018-04-04
EP3301362B1 true EP3301362B1 (fr) 2020-03-25

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US (1) US11175039B2 (fr)
EP (1) EP3301362B1 (fr)
CN (1) CN107883399B (fr)
ES (1) ES2792874T3 (fr)
HU (1) HUE049484T2 (fr)
PL (1) PL3301362T3 (fr)
RU (1) RU2674104C1 (fr)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP4050258A1 (fr) 2021-02-26 2022-08-31 Siemens Aktiengesellschaft Détermination des performances d'une unité de brûleur à gaz à l'aide d'un paramètre de combustible
EP4194749A1 (fr) 2021-12-13 2023-06-14 Siemens Aktiengesellschaft Commande et/ou régulation d'un dispositif de combustion
EP4306912A1 (fr) 2022-07-12 2024-01-17 Siemens Aktiengesellschaft Dispositif de combustion pourvu de capteur de débit massique
DE102022122811A1 (de) 2022-09-08 2024-03-14 Vaillant Gmbh Verfahren zum Betreiben eines Heizgerätes, Computerprogramm, Regel- und Steuer-gerät, Brennstoffdurchflussregler und Heizgerät
EP4397908A1 (fr) 2023-01-06 2024-07-10 Siemens Aktiengesellschaft Régulation de quantité de carburant et/ou régulation de quantité d'air

Families Citing this family (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10696906B2 (en) 2017-09-29 2020-06-30 Marathon Petroleum Company Lp Tower bottoms coke catching device
US10677469B2 (en) * 2017-10-19 2020-06-09 Haier Us Appliance Solutions, Inc. Fuel supply system for a gas burner assembly
DE102018104242A1 (de) * 2018-02-26 2019-08-29 Eberspächer Climate Control Systems GmbH & Co. KG Verfahren zum Betreiben eines brennstoffbetriebenen Fahrzeugheizgeräts
US12000720B2 (en) 2018-09-10 2024-06-04 Marathon Petroleum Company Lp Product inventory monitoring
US11428407B2 (en) * 2018-09-26 2022-08-30 Cowles Operating Company Combustion air proving apparatus with burner cut-off capability and method of performing the same
US12031676B2 (en) 2019-03-25 2024-07-09 Marathon Petroleum Company Lp Insulation securement system and associated methods
US11975316B2 (en) 2019-05-09 2024-05-07 Marathon Petroleum Company Lp Methods and reforming systems for re-dispersing platinum on reforming catalyst
CA3212048A1 (fr) * 2019-05-30 2020-11-30 Marathon Petroleum Company Lp Procedes et systemes pour minimiser les emissions de so2 et de co dans les rechauffeurs de tirage naturel
US11384301B2 (en) 2020-02-19 2022-07-12 Marathon Petroleum Company Lp Low sulfur fuel oil blends for stability enhancement and associated methods
US11692704B2 (en) 2020-05-11 2023-07-04 Rheem Manufacturing Company Systems and methods for dynamic boiler control
RU2753797C1 (ru) * 2020-07-10 2021-08-23 Общество С Ограниченной Ответственностью "Научно-Производственное Объединение "Экоспас" Установка мобильная термической утилизации и способ её использования
US11951661B2 (en) * 2020-12-02 2024-04-09 International Automotive Components Group Na, Inc. Process and article produced by injection molding
US11905468B2 (en) 2021-02-25 2024-02-20 Marathon Petroleum Company Lp Assemblies and methods for enhancing control of fluid catalytic cracking (FCC) processes using spectroscopic analyzers
US11702600B2 (en) 2021-02-25 2023-07-18 Marathon Petroleum Company Lp Assemblies and methods for enhancing fluid catalytic cracking (FCC) processes during the FCC process using spectroscopic analyzers
US20220268694A1 (en) 2021-02-25 2022-08-25 Marathon Petroleum Company Lp Methods and assemblies for determining and using standardized spectral responses for calibration of spectroscopic analyzers
US11898109B2 (en) 2021-02-25 2024-02-13 Marathon Petroleum Company Lp Assemblies and methods for enhancing control of hydrotreating and fluid catalytic cracking (FCC) processes using spectroscopic analyzers
EP4108988A1 (fr) * 2021-06-24 2022-12-28 BDR Thermea Group B.V. Procédé et dispositif pour commander le fonctionnement d'une chaudière
US11692141B2 (en) 2021-10-10 2023-07-04 Marathon Petroleum Company Lp Methods and systems for enhancing processing of hydrocarbons in a fluid catalytic cracking unit using a renewable additive
US11802257B2 (en) 2022-01-31 2023-10-31 Marathon Petroleum Company Lp Systems and methods for reducing rendered fats pour point

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20090111065A1 (en) * 2007-10-31 2009-04-30 Gene Tompkins Method and apparatus for controlling combustion in a burner

Family Cites Families (34)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2093025A5 (fr) * 1970-05-26 1972-01-28 Bailey Controle
GB1571906A (en) * 1977-11-22 1980-07-23 British Gas Corp Air fuel gas ratio controls for burners
US4930454A (en) * 1981-08-14 1990-06-05 Dresser Industries, Inc. Steam generating system
DE8335294U1 (de) * 1983-12-09 1984-03-22 Basf Ag, 6700 Ludwigshafen Andruckfeder für Bandkassetten und Bandkassetten damit
DE3703934A1 (de) * 1986-02-11 1987-08-13 Vaillant Joh Gmbh & Co Einrichtung zur steuerung der brennstoff- und/oder luftzufuhr zum brenner einer waermequelle
US4717071A (en) * 1986-06-16 1988-01-05 Ametek, Inc. Combustion trim control apparatus
US5037291A (en) * 1990-07-25 1991-08-06 Carrier Corporation Method and apparatus for optimizing fuel-to-air ratio in the combustible gas supply of a radiant burner
RU2067259C1 (ru) 1992-04-01 1996-09-27 Попыванов Геннадий Серафимович Устройство определения избытка воздуха в камере сгорания
DE4337703C1 (de) 1993-11-05 1995-03-23 Dungs Karl Gmbh & Co Mehrfachstellgerät mit eingangsseitigem Regler
FR2723630B1 (fr) 1994-08-11 1996-09-20 Seet Procede et dispositif de reglage automatique d'un bruleur a gaz pour chaudiere
DE19501749C2 (de) * 1995-01-21 2003-03-13 Stiebel Eltron Gmbh & Co Kg Verfahren und Vorrichtung zum Steuern eines Gas-Gebläsebrenners
JP3031856B2 (ja) * 1996-02-02 2000-04-10 株式会社サムソン ボイラのインバータによる風量調整方法
US5929581A (en) * 1997-10-22 1999-07-27 Hewlett-Packard Company Proportional integral fan controller for computer
US5997280A (en) * 1997-11-07 1999-12-07 Maxon Corporation Intelligent burner control system
RU2141604C1 (ru) * 1998-08-04 1999-11-20 Зислин Григорий Семенович Система автоматического управления тепловым режимом агрегата
US6019593A (en) * 1998-10-28 2000-02-01 Glasstech, Inc. Integrated gas burner assembly
US20010051321A1 (en) * 2000-02-15 2001-12-13 La Fontaine Robert D. Optimizing fuel combustion in a gas fired appliance
RU2169311C1 (ru) 2000-04-12 2001-06-20 Чувашский государственный университет им. И.Н. Ульянова Способ управления процессом горения в камере
DE10109808C2 (de) 2001-03-01 2003-12-04 Bosch Gmbh Robert Verfahren und Vorrichtung zur Anpassung eines brennerbetriebenen Heizgerätes an ein Luft-Abgas-System
DE10114405B4 (de) * 2001-03-23 2011-03-24 Ebm-Papst Landshut Gmbh Gebläse für Verbrennungsluft
CN1228568C (zh) 2001-03-23 2005-11-23 多孔燃烧器技术销售有限责任公司 用于设定空气比率的方法和装置
DE102004055715C5 (de) 2004-06-23 2014-02-06 Ebm-Papst Landshut Gmbh Verfahren zur Einstellung von Betriebsparametern an einer Feuerungseinrichtung und Feuerungseinrichtung
DE102006001299A1 (de) 2006-01-11 2007-07-12 Eckhart Weber Holzpellet-Blockheizkraftwerk mit Stirlingmotor in Brennwerttechnik
RU2349838C2 (ru) * 2007-01-25 2009-03-20 Артур Ирекович Ямаев Способ автоматического регулирования подачи воздуха в топку отопительного котла
US20100112500A1 (en) * 2008-11-03 2010-05-06 Maiello Dennis R Apparatus and method for a modulating burner controller
DE102010010952A1 (de) * 2010-03-10 2011-09-15 Ebm-Papst Landshut Gmbh Pneumatischer Verbund mit Massenausgleich
DE102013104837A1 (de) 2012-05-11 2013-11-14 Fisher-Rosemount Systems, Inc. Verfahren und Vorrichtung zum Steuern von Verbrennungsprozesssystemen
TWM448642U (zh) 2012-06-22 2013-03-11 Sheng Zhun Entpr Co Ltd 燃燒裝置廢氣回流再使用控制系統
US9234661B2 (en) * 2012-09-15 2016-01-12 Honeywell International Inc. Burner control system
US10422531B2 (en) 2012-09-15 2019-09-24 Honeywell International Inc. System and approach for controlling a combustion chamber
US10317076B2 (en) 2014-09-12 2019-06-11 Honeywell International Inc. System and approach for controlling a combustion chamber
ITVI20120229A1 (it) 2012-09-21 2014-03-22 Pietro Fiorentini Spa Sistema di misurazione della portata di un gas e impiego di detto sistema di misurazione in un metodo per determinare l'errore di un misuratore di flusso durante il normale funzionamento senza scollegarlo dalle tubazioni
US20140261111A1 (en) 2013-03-14 2014-09-18 Resource Rex, LLC Combustion Efficiency Control System with a Stoichiometric Controller for a Laminar Burner System
JP2015083779A (ja) 2013-10-25 2015-04-30 三菱日立パワーシステムズ株式会社 ガスタービン燃焼器及びガスタービン燃焼器の制御方法

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20090111065A1 (en) * 2007-10-31 2009-04-30 Gene Tompkins Method and apparatus for controlling combustion in a burner

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP4050258A1 (fr) 2021-02-26 2022-08-31 Siemens Aktiengesellschaft Détermination des performances d'une unité de brûleur à gaz à l'aide d'un paramètre de combustible
EP4194749A1 (fr) 2021-12-13 2023-06-14 Siemens Aktiengesellschaft Commande et/ou régulation d'un dispositif de combustion
EP4306912A1 (fr) 2022-07-12 2024-01-17 Siemens Aktiengesellschaft Dispositif de combustion pourvu de capteur de débit massique
DE102022122811A1 (de) 2022-09-08 2024-03-14 Vaillant Gmbh Verfahren zum Betreiben eines Heizgerätes, Computerprogramm, Regel- und Steuer-gerät, Brennstoffdurchflussregler und Heizgerät
EP4397908A1 (fr) 2023-01-06 2024-07-10 Siemens Aktiengesellschaft Régulation de quantité de carburant et/ou régulation de quantité d'air

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EP3301362A1 (fr) 2018-04-04
CN107883399A (zh) 2018-04-06
ES2792874T3 (es) 2020-11-12
US20180094809A1 (en) 2018-04-05
HUE049484T2 (hu) 2020-09-28
CN107883399B (zh) 2020-01-10
PL3301362T3 (pl) 2020-08-24
US11175039B2 (en) 2021-11-16

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