EP0682210B1 - Combustion control apparatus - Google Patents

Combustion control apparatus Download PDF

Info

Publication number
EP0682210B1
EP0682210B1 EP95103639A EP95103639A EP0682210B1 EP 0682210 B1 EP0682210 B1 EP 0682210B1 EP 95103639 A EP95103639 A EP 95103639A EP 95103639 A EP95103639 A EP 95103639A EP 0682210 B1 EP0682210 B1 EP 0682210B1
Authority
EP
European Patent Office
Prior art keywords
flow
amount
duct
combustion
flame vibration
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
Application number
EP95103639A
Other languages
German (de)
French (fr)
Other versions
EP0682210A1 (en
Inventor
Kazuo C/O Yamatake-Honeywell Co. Ltd. Seki
Yasuji C/O Yamatake-Honeywell Co. Ltd. Morita
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Azbil Corp
Original Assignee
Azbil Corp
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
Application filed by Azbil Corp filed Critical Azbil Corp
Publication of EP0682210A1 publication Critical patent/EP0682210A1/en
Application granted granted Critical
Publication of EP0682210B1 publication Critical patent/EP0682210B1/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • 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
    • F23N5/184Systems for controlling combustion using detectors sensitive to rate of flow of air or fuel using electronic means
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23NREGULATING OR CONTROLLING COMBUSTION
    • F23N5/00Systems for controlling combustion
    • F23N5/16Systems for controlling combustion using noise-sensitive detectors
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23NREGULATING OR CONTROLLING COMBUSTION
    • F23N2225/00Measuring
    • F23N2225/04Measuring pressure
    • 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
    • F23N2235/12Fuel valves
    • F23N2235/16Fuel valves variable flow or proportional valves

Definitions

  • the present invention relates to a combustion control apparatus for preventing flame vibration which occurs in a burning appliance, for example, a gas combustion type hot water supply system.
  • gas combustion type hot water systems which mixes combustion air supplied from a fan motor, provided on an end of a duct and gas (city gas, propane gas), and burns them in order to obtain hot water through a heat exchanger mounted beside the burner, for example.
  • flame vibration which means expansion and contraction of flame from the burner, occurs in a hot water supply system which locally heats combustion air flowing within a duct. If flame vibration occurs, uncomfortable noise is generated. Depending on situations, a burner or a heat exchanger may be damaged. There is such a method in order to prevent flame vibration available as determines whether or not flame vibration occurs by detecting vibration of fire current flowing between the surface of a burner and a heat exchanger and controlling the condition of combustion depending on the vibration of the fire current.
  • an object of the present invention is to solve the aforementioned problem and provide a combustion control apparatus capable of effectively preventing flame vibration by controlling the condition of combustion depending on the amplitude of flame vibration.
  • the combustion control apparatus of the present invention is provided with a detecting means for detecting the amount of flow of combustion air flowing through a duct, the detecting means being mounted near the node of pressure distribution within the duct, and is further provided with a control means for determining the amplitude of flame vibration according to the change of air flowing therethrough, controlling the amount of flowing air when flame vibration is small and controlling the amount of flowing fuel as well as the amount of flowing air when flame vibration increases.
  • the combustion control apparatus is capable of detecting the amount of the air flow stably and further detecting even slight changes of the amount of the flow to achieve highly accurate detection of the changes of the amount of flowing air. Further, the control means determines the amplitude of flame vibration according to the changes of the air flow, controls the amount of the combustion air when flame vibration is small and further controls the amount of flowing fuel when flame vibration increases in order to effectively prevent flame vibration.
  • Fig. 1 is a partial sectional view of the structure of an embodiment of the present invention.
  • Fig. 2 is a front view of a flow meter applied to the embodiment shown in Fig. 1.
  • Fig. 3 is a perspective view of a flow sensor in the flow meter shown in Fig. 2.
  • Fig. 4(a) is a partial sectional view of a hot water supply system for explaining the mounting positions of a gas burner and a flow sensor.
  • Fig. 4(b) is a characteristic view for showing the pressure distribution of combustion air in a duct.
  • Fig. 4(c) is a characteristic view for showing the flow speed distribution of combustion air in the duct.
  • Fig. 1 is a partial sectional view for showing the structure of an embodiment of the present invention.
  • reference numeral 1 denotes a duct having a fan motor 2 which is provided on an end of the duct 1.
  • the fan motor 2 comprises a fan which rotates at a predetermined rotation speed. External air is sucked by the fan and fed into the duct 1.
  • the air outlet of the fan motor 2 is provided with a dumper 3 for adjusting the amount of combustion air flowing into the duct 1.
  • the dumper 3 is rotated around a shaft 5 by a driving unit 4.
  • the degree of the opening of the damper 3 is adjusted so that the air fuel ratio (air: fuel) of a gas burner is approximately 1.2. The reason why the air fuel ratio is fixed to 1.2 is that combustion under this ratio is most excellent.
  • a gas burner 6 is provided in the downstream of the duct 1.
  • the gas burner 6 is supplied with a predetermined amount of gas (city gas, propane gas) from outside the duct.
  • propane gas is used as fuel gas
  • the gas is supplied from a gas cylinder 7.
  • a heat exchanger 8 is provided downward of the gas burner 6.
  • the heat exchanger 8 comprises cooling pipes of copper and fins connecting them. Water supplied from an end of the cooling pipe passes through the cooling pipe and then is discharged from the other end. The other end of the duct 1 discharges combustion gas passing through the duct 1, as an exhaust port.
  • a flow sensor 9a is mounted in the center of the fan motor 2 and a flow sensor 9b is mounted adjacent to the gas burner 6, upward of the gas burner 6.
  • the flow sensors 9a, 9b detect the amount of combustion air flowing through the duct 1 and supply a flow signal FS corresponding to the amount of passing air to a control circuit 10.
  • thermal type flow sensors are used as the flow sensors 9a, 9b.
  • only one flow sensor 9 is depicted to facilitate understanding of the following description.
  • Fig. 2 is a front view showing the structure of the thermal type flow sensor.
  • the thermal type flow sensor comprises two cylinders 21, 22 mounted in parallel to each other so that they are perpendicular to the direction of air flowing through the duct 1, a portion in which the ends of the cylinders protruding outside the duct 1 are connected to a through hole 25 of the sensor body 24 by means of tubes 26, 27 and a flow sensor portion 28 provided within the through hole 25.
  • Fig. 3 shows the structure of the flow sensor portion 28.
  • Fig. 3 is a perspective view showing the flow sensor portion 28 of the thermal type flow sensor.
  • the flow sensor portion 28 has a diaphragm 32 less than 20 ⁇ m in thickness on a semiconductor chip 31 which is 1.7 mm square and further a micro flow sensor placed on the diaphragm, the micro flow sensor containing an exothermic resisting pattern and a heat sensitive resisting pattern.
  • the exothermic resisting pattern becomes to be exothermic.
  • the resistance of the heat sensitive resisting pattern is set to a certain constant value. Combustion air flowing through the duct 1 enters one cylinder 21 through a hole 21a, passes through the tube 26, the through hole 25, and the tube 27, and finally goes out from a hole 22a of the other cylinder 22. At this time, heat on the semiconductor chip changes depending on the amount of air flowing over the micro flow sensor. Consequently, the resistance of the heat sensitive pattern changes. The change of the resistance is detected by the control circuit 10.
  • the flow sensor portion 28 is constructed with a very small structure, the flow sensor has a very high sensitivity and an excellent responsibility (several meters sec), so that it is always capable of measuring the amount of flow accurately. It is permissible to provide the internal surfaces of the cylinders 21, 22 of the micro flow sensor with minute unevenness in order to collect dust contained in combustion air. Or it is permissible to provide the internal surfaces of the cylinders 21, 22 of the micro flow sensor with a trap, a partition plate coated with adhesive or porous agent or a dust catching plate.
  • the control circuit 10 measures the change of the resistance of the heat sensitive resisting pattern.
  • the change of the resistance of the heat sensitive resisting pattern corresponds to the change of the flow amount of combustion air.
  • the control circuit 10 determines that flame vibration occurs and transmits control signals S1, S2.
  • the control signal S1 is supplied to the driving unit 4 and the control signal S2 is supplied to a gas flow adjusting valve 11.
  • the driving unit 4 drives the damper 3 according to the control signal S1 and adjusts the degree of the opening in order to control the flow amount of combustion air flowing through the duct 1. Or it is permissible to control the flow amount of combustion air flowing through the duct 1 by changing the rotation speed of the fan motor 2.
  • the adjusting valve 11 controls the flow amount of gas supplied to the gas burner 6 according to the control signal S2.
  • Figs. 4(a), 4(b), 4(c) are figures for explaining the method for determining the mounting positions of the gas burner and the flow sensor.
  • Fig. 4(a) is a partial sectional view of the same hot water supply system as shown in Fig. 1.
  • Fig. 4(b) is a characteristic diagram for showing the pressure distribution of combustion air in the duct
  • Fig. 4(c) is a characteristic diagram for showing the flow speed distribution of combustion air within the duct.
  • the flow sensors 9a, 9b are mounted in the vicinity of a position in which the amplitude of pressure is minimized or the amplitude of flow speed is maximized. Because the change of pressure is small at this position, it is possible to detect the amount of air flow stably and further it is possible to detect a minute change of air flow. Further, because flame vibration is maximum, it is possible to achieve a high precision detection. Whether or not flame vibration occurs is determined by the change of air flow detected by the flow sensors 9a, 9b, that is, a deflection of the amplitude of pressure or amplitude of flow speed.
  • the control circuit 10 drives the driving unit 4 by the control signal S1 depending on the change of flow in order to adjust the degree of the opening of the damper 3 or the rotation speed of the fan. As a result, the air fuel ratio of the gas burner 6 is changed, so that the combustion condition changes, thereby suppressing flame vibration. If flame vibration increases to produce noise, the change of the flow amount thereof detected by the flow sensors 9a, 9b increases.
  • the control circuit 10 outputs the control signal S2 corresponding to the change of the flow amount as well as the control signal S1.
  • the adjusting valve 11 is driven so as to adjust the amount of the flow of gas.
  • the amount of the flow amount of gas is controlled by means of the adjusting valve as well as the degree of the opening of the dumper and the rotation speed of the fan. Consequently, the air fuel ratio of the gas burner 6 is changed further, so that the condition of combustion changes, thereby further suppressing flame vibration.
  • the present invention is not restricted to this case but can be applied to burners using other fuel such as kerosene, gas oil and the like.
  • the combustion control apparatus is provided with a detecting means for detecting the amount of the flow of combustion air flowing through the duct, the detecting means being placed in the vicinity of the node of the pressure distribution within the duct and determines the amplitude of flame vibration according to the change of the flow amount.
  • the combustion control apparatus comprises a control means for controlling the amount of fuel as well as controlling the amount of the flow of combustion air when flame vibration increases.
  • this combustion control apparatus is capable of detecting a large flame vibration as well as a small flame vibration, and controlling the condition of combustion depending on the amplitude of flame vibration.
  • the combustion control apparatus of the present invention is capable of preventing flame vibration very effectively.

Description

    Field of the Invention
  • The present invention relates to a combustion control apparatus for preventing flame vibration which occurs in a burning appliance, for example, a gas combustion type hot water supply system.
  • Description of the Prior Art
  • Since before, gas combustion type hot water systems have been well known which mixes combustion air supplied from a fan motor, provided on an end of a duct and gas (city gas, propane gas), and burns them in order to obtain hot water through a heat exchanger mounted beside the burner, for example.
  • It is generally known that so-called flame vibration, which means expansion and contraction of flame from the burner, occurs in a hot water supply system which locally heats combustion air flowing within a duct. If flame vibration occurs, uncomfortable noise is generated. Depending on situations, a burner or a heat exchanger may be damaged. There is such a method in order to prevent flame vibration available as determines whether or not flame vibration occurs by detecting vibration of fire current flowing between the surface of a burner and a heat exchanger and controlling the condition of combustion depending on the vibration of the fire current.
  • However, although conventional combustion control apparatus is capable of sufficiently detecting flame vibration when flame vibration is small, if flame vibration increases, fire current is disturbed. Consequently, this conventional combustion control apparatus has such a problem that it cannot detect flame vibration accurately. If a large flame vibration is generated so that noise occurs suddenly after a small flame vibration continues for a short time, it is impossible to detect the frequency of flame vibration based on fire current. Thus, the conventional combustion control apparatus was not capable of controlling combustion depending on the amplitude of flame vibration and therefore was not capable of preventing flame vibration.
  • SUMMARY OF THE INVENTION
  • Accordingly, an object of the present invention is to solve the aforementioned problem and provide a combustion control apparatus capable of effectively preventing flame vibration by controlling the condition of combustion depending on the amplitude of flame vibration.
  • The combustion control apparatus of the present invention is provided with a detecting means for detecting the amount of flow of combustion air flowing through a duct, the detecting means being mounted near the node of pressure distribution within the duct, and is further provided with a control means for determining the amplitude of flame vibration according to the change of air flowing therethrough, controlling the amount of flowing air when flame vibration is small and controlling the amount of flowing fuel as well as the amount of flowing air when flame vibration increases.
  • Because the detecting means mounted near the node of pressure distribution within the duct in the combustion control apparatus of the present invention detects the amount of the combustion air flow, the combustion control apparatus is capable of detecting the amount of the air flow stably and further detecting even slight changes of the amount of the flow to achieve highly accurate detection of the changes of the amount of flowing air. Further, the control means determines the amplitude of flame vibration according to the changes of the air flow, controls the amount of the combustion air when flame vibration is small and further controls the amount of flowing fuel when flame vibration increases in order to effectively prevent flame vibration.
  • BRIEF DESCRIPTION OF THE DRAWINGS
  • Fig. 1 is a partial sectional view of the structure of an embodiment of the present invention.
  • Fig. 2 is a front view of a flow meter applied to the embodiment shown in Fig. 1.
  • Fig. 3 is a perspective view of a flow sensor in the flow meter shown in Fig. 2.
  • Fig. 4(a) is a partial sectional view of a hot water supply system for explaining the mounting positions of a gas burner and a flow sensor.
  • Fig. 4(b) is a characteristic view for showing the pressure distribution of combustion air in a duct.
  • Fig. 4(c) is a characteristic view for showing the flow speed distribution of combustion air in the duct.
  • DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS
  • An embodiment of the present invention will be described with reference to drawings. Fig. 1 is a partial sectional view for showing the structure of an embodiment of the present invention. Referring to Fig. 1, reference numeral 1 denotes a duct having a fan motor 2 which is provided on an end of the duct 1. The fan motor 2 comprises a fan which rotates at a predetermined rotation speed. External air is sucked by the fan and fed into the duct 1. The air outlet of the fan motor 2 is provided with a dumper 3 for adjusting the amount of combustion air flowing into the duct 1. The dumper 3 is rotated around a shaft 5 by a driving unit 4. The degree of the opening of the damper 3 is adjusted so that the air fuel ratio (air: fuel) of a gas burner is approximately 1.2. The reason why the air fuel ratio is fixed to 1.2 is that combustion under this ratio is most excellent.
  • A gas burner 6 is provided in the downstream of the duct 1. The gas burner 6 is supplied with a predetermined amount of gas (city gas, propane gas) from outside the duct. When propane gas is used as fuel gas, the gas is supplied from a gas cylinder 7. A heat exchanger 8 is provided downward of the gas burner 6. The heat exchanger 8 comprises cooling pipes of copper and fins connecting them. Water supplied from an end of the cooling pipe passes through the cooling pipe and then is discharged from the other end. The other end of the duct 1 discharges combustion gas passing through the duct 1, as an exhaust port.
  • For example, a flow sensor 9a is mounted in the center of the fan motor 2 and a flow sensor 9b is mounted adjacent to the gas burner 6, upward of the gas burner 6. The flow sensors 9a, 9b detect the amount of combustion air flowing through the duct 1 and supply a flow signal FS corresponding to the amount of passing air to a control circuit 10. As the flow sensors 9a, 9b, for example, thermal type flow sensors are used. However, only one flow sensor 9 is depicted to facilitate understanding of the following description.
  • Fig. 2 is a front view showing the structure of the thermal type flow sensor. The thermal type flow sensor comprises two cylinders 21, 22 mounted in parallel to each other so that they are perpendicular to the direction of air flowing through the duct 1, a portion in which the ends of the cylinders protruding outside the duct 1 are connected to a through hole 25 of the sensor body 24 by means of tubes 26, 27 and a flow sensor portion 28 provided within the through hole 25.
  • Fig. 3 shows the structure of the flow sensor portion 28. Fig. 3 is a perspective view showing the flow sensor portion 28 of the thermal type flow sensor. As shown in Fig. 3, the flow sensor portion 28 has a diaphragm 32 less than 20 µm in thickness on a semiconductor chip 31 which is 1.7 mm square and further a micro flow sensor placed on the diaphragm, the micro flow sensor containing an exothermic resisting pattern and a heat sensitive resisting pattern.
  • When a predetermined amount of current is supplied to the micro flow sensor, the exothermic resisting pattern becomes to be exothermic. The resistance of the heat sensitive resisting pattern is set to a certain constant value. Combustion air flowing through the duct 1 enters one cylinder 21 through a hole 21a, passes through the tube 26, the through hole 25, and the tube 27, and finally goes out from a hole 22a of the other cylinder 22. At this time, heat on the semiconductor chip changes depending on the amount of air flowing over the micro flow sensor. Consequently, the resistance of the heat sensitive pattern changes. The change of the resistance is detected by the control circuit 10. Because the aforementioned flow sensor portion 28 is constructed with a very small structure, the flow sensor has a very high sensitivity and an excellent responsibility (several meters sec), so that it is always capable of measuring the amount of flow accurately. It is permissible to provide the internal surfaces of the cylinders 21, 22 of the micro flow sensor with minute unevenness in order to collect dust contained in combustion air. Or it is permissible to provide the internal surfaces of the cylinders 21, 22 of the micro flow sensor with a trap, a partition plate coated with adhesive or porous agent or a dust catching plate.
  • The control circuit 10 measures the change of the resistance of the heat sensitive resisting pattern. The change of the resistance of the heat sensitive resisting pattern corresponds to the change of the flow amount of combustion air. Thus, the change of the flow amount of combustion air is measured. When the change of the flow amount of combustion air exceeds a certain constant value (threshold), the control circuit 10 determines that flame vibration occurs and transmits control signals S1, S2. The control signal S1 is supplied to the driving unit 4 and the control signal S2 is supplied to a gas flow adjusting valve 11. The driving unit 4 drives the damper 3 according to the control signal S1 and adjusts the degree of the opening in order to control the flow amount of combustion air flowing through the duct 1. Or it is permissible to control the flow amount of combustion air flowing through the duct 1 by changing the rotation speed of the fan motor 2. On the other hand, the adjusting valve 11 controls the flow amount of gas supplied to the gas burner 6 according to the control signal S2.
  • Next, the mounting positions of the gas burner 6 and the flow sensors 9a, 9b will be described with reference to Figs. 4(a), 4(b), 4(c). Figs. 4(a), 4(b), 4(c) are figures for explaining the method for determining the mounting positions of the gas burner and the flow sensor. Fig. 4(a) is a partial sectional view of the same hot water supply system as shown in Fig. 1. Fig. 4(b) is a characteristic diagram for showing the pressure distribution of combustion air in the duct, and Fig. 4(c) is a characteristic diagram for showing the flow speed distribution of combustion air within the duct. These characteristics are measured by means of a plurality of pressure sensors 41, 42, 43 (three pressures sensors are depicted in the present embodiment) provided in the upstream of the gas burner within the duct 1. The pressure distribution of combustion air is represented in the sinusoidal wave form as shown in Fig. 4(b). On the other hand, the flow speed distribution is represented in cosine wave form approximately 90° off with respect to the pressure distribution.
  • According to the invention, the flow sensors 9a, 9b are mounted in the vicinity of a position in which the amplitude of pressure is minimized or the amplitude of flow speed is maximized. Because the change of pressure is small at this position, it is possible to detect the amount of air flow stably and further it is possible to detect a minute change of air flow. Further, because flame vibration is maximum, it is possible to achieve a high precision detection. Whether or not flame vibration occurs is determined by the change of air flow detected by the flow sensors 9a, 9b, that is, a deflection of the amplitude of pressure or amplitude of flow speed.
  • Next, the operation of the aforementioned embodiment will be described. When the hot water supply system is operated, an almost constant amount of combustion air supplied from the fan motor 2 is mixed with the predetermined amount of gas and then the mixture thereof is burned by means of the gas burner 6. In the heat exchanger 8, water entering therein is heated by flame of the gas burner 6 so that it is hot water and discharged outside. When no flame vibration occurs, there is little change in the amount of flow of combustion air detected by the flow sensors 9a, 9b. Thus, the damper 3 or the adjusting valve 11 is kept as it is.
  • On the other hand, if flame vibration occurs during combustion, the change of flow of combustion air due to flame vibration is detected by means of the flow sensors 9a, 9b. When the change of flow is small or when flame vibration is small, the control circuit 10 drives the driving unit 4 by the control signal S1 depending on the change of flow in order to adjust the degree of the opening of the damper 3 or the rotation speed of the fan. As a result, the air fuel ratio of the gas burner 6 is changed, so that the combustion condition changes, thereby suppressing flame vibration. If flame vibration increases to produce noise, the change of the flow amount thereof detected by the flow sensors 9a, 9b increases. In this case, namely, when flame vibration increases, the control circuit 10 outputs the control signal S2 corresponding to the change of the flow amount as well as the control signal S1. According to the control signal S2, the adjusting valve 11 is driven so as to adjust the amount of the flow of gas. As a result, the amount of the flow amount of gas is controlled by means of the adjusting valve as well as the degree of the opening of the dumper and the rotation speed of the fan. Consequently, the air fuel ratio of the gas burner 6 is changed further, so that the condition of combustion changes, thereby further suppressing flame vibration.
  • Although a burner using gas (city gas, propane gas) was described in the aforementioned embodiment, the present invention is not restricted to this case but can be applied to burners using other fuel such as kerosene, gas oil and the like.
  • As described above, according to the present invention, the combustion control apparatus is provided with a detecting means for detecting the amount of the flow of combustion air flowing through the duct, the detecting means being placed in the vicinity of the node of the pressure distribution within the duct and determines the amplitude of flame vibration according to the change of the flow amount. The combustion control apparatus comprises a control means for controlling the amount of fuel as well as controlling the amount of the flow of combustion air when flame vibration increases. Thus, this combustion control apparatus is capable of detecting a large flame vibration as well as a small flame vibration, and controlling the condition of combustion depending on the amplitude of flame vibration. Thus, the combustion control apparatus of the present invention is capable of preventing flame vibration very effectively.

Claims (3)

  1. A combustion control apparatus characterized by :
    a detecting means (9) for detecting the amount of combustion air flowing through a duct (1), said detecting means being mounted in the vicinity of a node of pressure distribution within said duct; and
    a control means (10) which determines the amplitude of flame vibration according to a change of the flow amount detected by means of said detecting means, controls the amount of the flow of said combustion air when flame vibration is small, and controls the amount of the flow of said combustion air as well as the amount of the flow of fuel when flame vibration increases.
  2. A combustion control apparatus according to claim 1,
       wherein the detecting means comprises a thermal type flow sensor including two cylinders (21,22) mounted in parallel to each other so that they are perpendicular to the direction of air flowing through the duct, a portion in which the ends of the cylinders protruding outside said duct are connected to a through hole (25) of the sensor body (24) by means of tubes (26,27) and a flow sensor portion (28) provided within said through hole.
  3. A combustion control apparatus according to claim 2,
       wherein the control means determines the amplitude of flame vibration according to a change of the resistance of heat sensitive pattern of the thermal type flow sensor.
EP95103639A 1994-03-18 1995-03-14 Combustion control apparatus Expired - Lifetime EP0682210B1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
JP6049004A JP2880398B2 (en) 1994-03-18 1994-03-18 Combustion control device
JP49004/94 1994-03-18

Publications (2)

Publication Number Publication Date
EP0682210A1 EP0682210A1 (en) 1995-11-15
EP0682210B1 true EP0682210B1 (en) 1997-10-29

Family

ID=12819037

Family Applications (1)

Application Number Title Priority Date Filing Date
EP95103639A Expired - Lifetime EP0682210B1 (en) 1994-03-18 1995-03-14 Combustion control apparatus

Country Status (3)

Country Link
EP (1) EP0682210B1 (en)
JP (1) JP2880398B2 (en)
DE (1) DE69500945T2 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9746176B2 (en) 2014-06-04 2017-08-29 Lochinvar, Llc Modulating burner with venturi damper

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE10307131A1 (en) * 2003-02-20 2004-09-02 Robert Bosch Gmbh Heater and associated operating procedure
DE102012024348A1 (en) * 2012-12-13 2014-06-18 Robert Bosch Gmbh Control device with a vibration sensor, method for their operation and heating device with such a control device
EP2829803B1 (en) * 2013-07-25 2017-05-10 Honeywell Technologies Sarl Method of stabilizing gas burner combustion using Fast-Fourier-Transformation (FFT)

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS55110823A (en) * 1979-02-16 1980-08-26 Kobe Steel Ltd Controlling method of air ratio at combustion furnace
JPS59191812A (en) * 1983-04-14 1984-10-31 Nippon Kokan Kk <Nkk> Ignition ascertaining device
FR2645247B2 (en) * 1988-06-22 1991-06-07 Centre Nat Rech Scient METHOD AND DEVICE FOR ACTIVE CONTROL OF COMBUSTION INSTABILITIES
JPH02103312A (en) * 1988-10-12 1990-04-16 Nakayama Steel Works Ltd Hot blast stove
CA2072122A1 (en) * 1989-10-30 1991-05-01 Ulrich Bonne Microbridge-based combustion control

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9746176B2 (en) 2014-06-04 2017-08-29 Lochinvar, Llc Modulating burner with venturi damper
US10161627B2 (en) 2014-06-04 2018-12-25 Lochinvar, Llc Modulating burner with venturi damper

Also Published As

Publication number Publication date
JPH07260140A (en) 1995-10-13
EP0682210A1 (en) 1995-11-15
DE69500945T2 (en) 1998-04-02
DE69500945D1 (en) 1997-12-04
JP2880398B2 (en) 1999-04-05

Similar Documents

Publication Publication Date Title
US6843110B2 (en) Method and apparatus for validating the accuracy of a flowmeter
JP2851960B2 (en) Intake air amount measurement device for internal combustion engine
US9151490B2 (en) Boiler control system
JP2010156537A5 (en)
AU648163B2 (en) Thermoelectric sensor
US4913128A (en) Burner apparatus
EP0682210B1 (en) Combustion control apparatus
US4449569A (en) Method and apparatus for regulating fluid flows in parallel-connected conduits (e.g. in furnace installations having air preheaters and by-pass conduits)
SE9801925L (en) Heart rate burner and boiler for this
JP2002267159A (en) Air-fuel ratio control method and device
US20040020304A1 (en) Differential static pressure measuring device
EP1004856A3 (en) Thermal air flow meter
EP0778448B1 (en) Combustion control system
US20240018921A1 (en) Combustion Apparatus with Mass Flow Sensor
JPH07208734A (en) Flame detecting system
JP2729103B2 (en) Combustion equipment
JP3534865B2 (en) Air-fuel ratio control device for combustor
JP3109718B2 (en) Gas flowmeter flow measurement performance evaluation device
JP2000088620A (en) Engine exhaust gas flow rate measuring system
JP2716347B2 (en) Gas blending equipment
JP3740724B2 (en) Combustion control device
JP2980144B2 (en) Detection method of combustion air volume under furnace
JP2002357362A (en) Hot-water supplier
JPH04327754A (en) Heat exchanger
JPH11108346A (en) Combustor

Legal Events

Date Code Title Description
PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

Free format text: ORIGINAL CODE: 0009012

AK Designated contracting states

Kind code of ref document: A1

Designated state(s): DE FR GB IT

17P Request for examination filed

Effective date: 19951115

GRAG Despatch of communication of intention to grant

Free format text: ORIGINAL CODE: EPIDOS AGRA

17Q First examination report despatched

Effective date: 19970220

GRAH Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOS IGRA

GRAH Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOS IGRA

GRAA (expected) grant

Free format text: ORIGINAL CODE: 0009210

AK Designated contracting states

Kind code of ref document: B1

Designated state(s): DE FR GB IT

REF Corresponds to:

Ref document number: 69500945

Country of ref document: DE

Date of ref document: 19971204

ET Fr: translation filed
ITF It: translation for a ep patent filed

Owner name: ING. C. GREGORJ S.P.A.

PLBE No opposition filed within time limit

Free format text: ORIGINAL CODE: 0009261

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT

26N No opposition filed
REG Reference to a national code

Ref country code: FR

Ref legal event code: CD

REG Reference to a national code

Ref country code: GB

Ref legal event code: IF02

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: FR

Payment date: 20120319

Year of fee payment: 18

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: GB

Payment date: 20120314

Year of fee payment: 18

Ref country code: IT

Payment date: 20120323

Year of fee payment: 18

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: DE

Payment date: 20120411

Year of fee payment: 18

GBPC Gb: european patent ceased through non-payment of renewal fee

Effective date: 20130314

REG Reference to a national code

Ref country code: FR

Ref legal event code: ST

Effective date: 20131129

REG Reference to a national code

Ref country code: DE

Ref legal event code: R119

Ref document number: 69500945

Country of ref document: DE

Effective date: 20131001

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: DE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20131001

Ref country code: FR

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20130402

Ref country code: GB

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20130314

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: IT

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20130314