US20170284663A1 - Premixing Apparatus - Google Patents

Premixing Apparatus Download PDF

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Publication number
US20170284663A1
US20170284663A1 US15/458,156 US201715458156A US2017284663A1 US 20170284663 A1 US20170284663 A1 US 20170284663A1 US 201715458156 A US201715458156 A US 201715458156A US 2017284663 A1 US2017284663 A1 US 2017284663A1
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US
United States
Prior art keywords
air
butterfly valve
supply passage
valve
rotation angle
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.)
Abandoned
Application number
US15/458,156
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English (en)
Inventor
Masao Nonoyama
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.)
Rinnai Corp
Original Assignee
Rinnai 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 Rinnai Corp filed Critical Rinnai Corp
Assigned to RINNAI CORPORATION reassignment RINNAI CORPORATION ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: NONOYAMA, MASAO
Publication of US20170284663A1 publication Critical patent/US20170284663A1/en
Priority to US16/441,172 priority Critical patent/US11105505B2/en
Abandoned legal-status Critical Current

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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23D—BURNERS
    • F23D14/00—Burners for combustion of a gas, e.g. of a gas stored under pressure as a liquid
    • F23D14/02—Premix gas burners, i.e. in which gaseous fuel is mixed with combustion air upstream of the combustion zone
    • F23D14/04—Premix gas burners, i.e. in which gaseous fuel is mixed with combustion air upstream of the combustion zone induction type, e.g. Bunsen burner
    • F23D14/06—Premix gas burners, i.e. in which gaseous fuel is mixed with combustion air upstream of the combustion zone induction type, e.g. Bunsen burner with radial outlets at the burner head
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23D—BURNERS
    • F23D14/00—Burners for combustion of a gas, e.g. of a gas stored under pressure as a liquid
    • F23D14/46—Details, e.g. noise reduction means
    • F23D14/60—Devices for simultaneous control of gas and combustion air
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23D—BURNERS
    • F23D14/00—Burners for combustion of a gas, e.g. of a gas stored under pressure as a liquid
    • F23D14/46—Details, e.g. noise reduction means
    • F23D14/62—Mixing devices; Mixing tubes
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23N—REGULATING OR CONTROLLING COMBUSTION
    • F23N1/00—Regulating fuel supply
    • F23N1/02—Regulating fuel supply conjointly with air supply
    • F23N1/027—Regulating fuel supply conjointly with air supply using mechanical means
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23D—BURNERS
    • F23D2203/00—Gaseous fuel burners
    • F23D2203/007—Mixing tubes, air supply regulation
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23D—BURNERS
    • F23D2900/00—Special features of, or arrangements for burners using fluid fuels or solid fuels suspended in a carrier gas
    • F23D2900/14—Special features of gas burners

Definitions

  • the present invention relates to a premixing apparatus for mixing fuel gas with air to supply thus obtained air-fuel mixture, through a fan, to a burner.
  • Patent Document 1 i.e., JP-A-2015-230113; that is, a downstream end of that gas supply passage for supplying fuel gas which has interposed therein a flow control valve, is connected to a gas suction section disposed in an air supply passage on an upstream side of the fan.
  • the premixing apparatus comprises: an air resistance changeover means for changing over, between high and low, a ventilation resistance in that section of the air supply passage which is on an upstream side of the gas suction section; and a gas resistance changeover means for changing over, between high and low, a ventilation resistance in that section of the gas supply passage which is on the downstream side of the flow control valve.
  • the proportional valve is controlled so that the fuel gas can be supplied in amount depending on the required combustion amount. Further, the rotation speed of the fan is controlled depending on the required combustion amount so that the excess-air ratio of the air-fuel mixture to be supplied to the burner becomes constant.
  • the flow control valve there is a case in which is used a zero governor that maintains the secondary gas pressure at the atmospheric pressure.
  • the amount of fuel gas supply varies with the differential pressure between the atmospheric pressure that is the secondary gas pressure and the negative pressure inside the air supply passage.
  • the amount of fuel gas supply varies with the rotation speed of the fan, i.e., the amount of air supply. Therefore, by controlling the rotation speed of the fan depending on the required combustion amount, the amount of air and fuel gas depending on the required combustion amount will be supplied to the burner.
  • the following arrangement has been employed; i.e., when the required combustion amount has fallen below the predetermined value, the ventilation resistance in the air supply passage is increased by the air flow resistance changeover means and also the ventilation resistance in the gas supply passage is increased by the gas resistance changeover means, thereby attaining a small-capacity state. It is thus made possible to supply the air and the fuel gas in amounts depending on the required combustion amount below the predetermined value. Further, when the required combustion amount has exceeded the predetermined value, the ventilation resistance in the air supply passage is decreased by the air flow resistance changeover means and, at the same time, the ventilation resistance in the gas supply passage is decreased by the gas resistance changeover means, thereby restoring a large-capacity state.
  • the air resistance changeover means is provided in that section of the air supply passage which is on an upstream side of the gas suction section, and is constituted by a butterfly valve which is rotated into an opened posture in parallel with the longitudinal direction of the air supply passage and into a closed posture at right angles to the longitudinal direction of the air supply passage.
  • the gas resistance changeover means is constituted by a changeover valve which is disposed in the gas supply passage in a manner to allow for opening or closing. And there is disposed an interlocking mechanism which is so arranged as to open or close the changeover valve in interlocking with the rotation into an open posture or into a closed posture of the butterfly valve.
  • this invention has a problem of providing a premixing apparatus in which an adjustment can be made without replacing the parts so that the excess air ratio of the air-fuel mixture can be made into an appropriate value in either of the small-capacity state and the large-capacity state.
  • this invention is a premixing apparatus for mixing fuel gas with air to supply thus obtained air-fuel mixture, through a fan, to a burner, in which a downstream end of a gas supply passage having interposed therein a flow control valve for supplying fuel gas is connected to a gas suction section disposed in an air supply passage on an upstream side of the fan.
  • the premixing apparatus comprises: an air resistance changeover means for changing over, between high and low, a ventilation resistance in that section of the air supply passage which is on an upstream side of the gas suction section; and a gas resistance changeover means for changing over, between high and low, a ventilation resistance in that section of the gas supply passage which is on the downstream side of the flow control valve, wherein the air resistance changeover means is constituted by a butterfly valve disposed in that section of the air supply passage which is on an upstream side of the gas suction section so as to be rotatable into an opened posture parallel with a longitudinal direction of the air supply passage or a closed posture at right angles to the longitudinal direction of the air supply passage, and wherein the gas resistance changeover means is constituted by a changeover valve disposed in the gas supply passage in an openable and closable manner, and has an interlocking mechanism to open or close the changeover valve in interlocking with the rotation of the butterfly valve into the opened posture or into the closed posture.
  • the premixing apparatus is characterized in: that the interlocking mechanism maintains the changeover valve in a fully-closed state when the butterfly valve lies in a predetermined first rotation angle range inclusive of the closed posture, and maintains the changeover valve in a fully-opened state when the butterfly valve lies in a predetermined second rotation angle range inclusive of the opened posture; that the rotation angle of the butterfly valve at which the excess air ratio of the air-fuel mixture becomes a predetermined appropriate value within the first rotation angle range is set to be a closing-side stop angle of the butterfly valve; that the rotation angle of the butterfly valve at which the excess air ratio of the air-fuel mixture becomes a predetermined appropriate value within the second rotation angle range is set to be an open-side stop angle of the butterfly valve; and that the butterfly valve is controlled in rotation between the closing-side stop angle and the open-side stop angle.
  • the changeover valve is maintained in the fully-closed state, and only the rotation angle of the butterfly valve changes. Therefore, due to this change, the ventilation resistance in the air supply passage changes and the excess air ratio of the air-fuel mixture also changes. Accordingly, even if the excess air ratio of the air-fuel mixture in the closed posture of the butterfly valve may have been deviated from the appropriate value, the excess air ratio of the air-fuel mixture can be made to be the appropriate value by the rotation of the butterfly valve within the range of the first rotation angle range.
  • the excess air ratio of the air-fuel mixture in the opened posture of the butterfly valve may have been deviated from the appropriate value
  • the excess air ratio of the air-fuel mixture can be made to be the appropriate value by the rotation of the butterfly valve within the range of the second rotation angle range.
  • the butterfly valve is rotated up to the open-side stop angle at which the excess air ratio of the air-fuel mixture becomes the appropriate value within the second rotation angle range.
  • the ignition operation of the burner shall preferably be performed in a state in which the butterfly valve is rotated to the closed posture. According to this arrangement, the ignition takes place in a state in which the excess air ratio of the air-fuel mixture is relatively low and in which the state is gas-rich and easily catching fire. Therefore, ignition failure can be prevented from occurring.
  • FIG. 1 is a side view, partly shown in section, of a premixing apparatus according to an embodiment of this invention.
  • FIG. 2 is a plan view partly cut away along the line II-II in FIG. 1 .
  • FIG. 3 is a sectional view partly cut away along the line III-III in FIG. 1 .
  • FIG. 4 is a sectional view partly cut away along the line IV-IV in FIG. 1 .
  • FIG. 5 is a graph showing the change in excess air ratio of air-fuel mixture accompanied by the change in the rotation angle of the butterfly valve.
  • reference numeral 1 denotes a burner which is made up of a totally aerated combustion type burner (also called “all primary air burner”) and the like having a combustion surface la in which the air-fuel mixture is ejected and combusted.
  • the burner 1 has connected thereto a fan 2 and, by means of a premixing apparatus A according to an embodiment of this invention, the air is mixed with fuel gas and the air-fuel mixture thus obtained is supplied, through a fan 2 , to a burner 11 .
  • the premixing apparatus A is provided with an air supply passage 3 on an upstream side of the fan 2 , and a gas supply passage 4 to supply the fuel gas.
  • a gate valve 5 In an upstream section of the gas supply passage 4 , there are interposed a gate valve 5 , and a flow control valve 6 which is made up of a proportional valve or a zero governor, as shown in FIG. 4 .
  • the downstream end of the gas supply passage 4 is connected to a gas suction section 31 which is disposed in the air supply passage 3 .
  • the premixing apparatus A is provided with: an air resistance changeover means for changing over, between high and low, a ventilation resistance in that section of the air supply passage 3 which is on an upstream side of the gas suction section 31 ; and a gas resistance changeover means for changing over, between high and low, a ventilation resistance in that section of the gas supply passage 4 which is on the downstream side of the flow control valve 6 .
  • an air resistance changeover means for changing over, between high and low, a ventilation resistance in that section of the air supply passage 3 which is on an upstream side of the gas suction section 31 ; and a gas resistance changeover means for changing over, between high and low, a ventilation resistance in that section of the gas supply passage 4 which is on the downstream side of the flow control valve 6 .
  • the amount of air and fuel gas can be supplied depending on the required combustion amount below the required value. Further, when the required combustion amount has exceeded the predetermined value, a large-capacity state is attained in which the ventilation resistance in the air supply passage 3 is made low by the air resistance changeover means, and also in which the ventilation resistance in the gas supply passage 4 is made low by the gas resistance changeover means.
  • an inner tube 33 With a clearance to the inner circumferential wall surface 32 of the air supply passage 3 .
  • a subsidiary passage 3 b which is in parallel with the main passage 3 a inside the inner tube 33 .
  • the flange section 33 a on a downstream end (upper end in FIGS. 1 and 3 ) of the inner tube 33 , there are formed a plurality of arcuate through holes 33 b which serve as outlets to the subsidiary passage 3 b.
  • a butterfly valve 7 which is made up of a disc so as to be rotatable about a shaft 71 .
  • This butterfly valve 7 constitutes the air resistance changeover means.
  • a shaft 71 of the butterfly valve 7 has connected thereto an actuator 72 such as a stepping motor and the like.
  • the butterfly valve 7 is rotated, by the operation of the actuator 72 , from the open posture side, which is in parallel with the longitudinal direction of the air supply passage 3 , as shown by imaginary lines in FIG. 3 to a closed posture side, which is at right angles to the longitudinal direction of the air supply passage 3 , as shown by solid lines in FIGS. 1 through 3 .
  • the butterfly valve 7 is rotated, by the operation of the actuator 72 , from the closed posture side to the open posture side.
  • the butterfly valve 7 is rotated to the closed posture, the main passage 3 a is almost fully closed and the space through which the air flows is substantially limited to the subsidiary passage 3 b , and the ventilation resistance in the air supply passage 3 becomes high.
  • That section of the air supply passage 3 which is adjacent to the upstream side of the gas suction section 31 is provided with a Venturi section 34 which is smaller in diameter than that section of the air supply passage 3 which has disposed therein the inner tube 33 .
  • That section of the air supply passage 3 which is adjacent to the downstream side of the Venturi section 34 is enclosed by a cylindrical section 35 which is larger in diameter than the Venturi section 34 .
  • the downstream end section of the Venturi section 34 is inserted, while leaving an annular clearance, into an upstream end section. It is thus so arranged that this clearance constitutes a gas suction section 31 which is in communication with the gas chamber 41 by this clearance.
  • the inner circumferential wall surface of the air supply passage 3 between the subsidiary passage 3 b and the Venturi section 34 is formed into a tapered surface 36 with a smaller diameter toward the Venturi section 34 .
  • the gas supply passage 4 is provided with a valve chamber 81 which is positioned on an upstream side of that gas chamber 41 on a downstream end of the gas supply passage 4 which is in communication with the gas suction section 31 , the valve chamber being in parallel with a passage section 42 normally communicated with the gas chamber 41 .
  • a changeover valve 8 for opening or closing a valve hole 83 which is in communication with the passage section 42 , the valve hole being formed in a valve seat 82 at the lower end of the valve chamber 81 .
  • the gas resistance changeover means is constituted by this changeover valve 8 .
  • the changeover valve 8 is operated to be opened or closed through an interlocking mechanism 9 accompanied by the rotation of the butterfly valve 7 .
  • This interlocking mechanism 9 is constituted, as shown in FIGS. 1 and 4 , by: a cam 91 which is coupled to the shaft 71 of the butterfly valve 7 ; and a rod 92 which extends upward for connection to the changeover valve 8 and a lower end of which comes into contact with the cam 91 .
  • the rod 92 moves up and down through the cam 91 , whereby the changeover valve 8 is operated to be opened or closed.
  • the cam 91 pushes up the rod 92 .
  • the changeover valve 8 moves up against the urging force of a valve spring 84 , i.e., is operated to be opened.
  • a valve spring 84 When the butterfly valve 8 is rotated to the closed posture side, the upward force of the rod 92 by the cam 91 is released.
  • the changeover valve 8 moves downward by the urging force of the valve spring 84 , i.e., is operated to be closed.
  • the interlocking mechanism 9 is arranged as follows, i.e., when the butterfly valve 7 lies within a predetermined first rotation angle range (e.g., 0° through 15°, where the angle of the butterfly valve 7 at the closed posture is defined to be 0°, and the angle of the butterfly valve 7 is at the opened posture is defined to be 90°), the changeover valve 8 is maintained at the fully-closed state, and when the butterfly valve 7 lies within a predetermined second rotation angle range (e.g., 75° through 90°), the changeover valve 8 is maintained at the fully-opened state.
  • a predetermined first rotation angle range e.g., 0° through 15°, where the angle of the butterfly valve 7 at the closed posture is defined to be 0°, and the angle of the butterfly valve 7 is at the opened posture is defined to be 90°
  • a predetermined first rotation angle range e.g., 0° through 15°, where the angle of the butterfly valve 7 at the closed posture is defined to be 0°, and the angle of the butterfly
  • FIG. 5 shows the relationship between the rotation angle of the butterfly valve 7 and the excess air ratio of the air-fuel mixture.
  • the changeover valve 8 is maintained in the fully-closed state within the first rotation angle range, and only the rotation angle of the butterfly valve 7 will be changed. Therefore, accompanied by the increase in the rotation angle of the butterfly valve 7 , the ventilation resistance in the air supply passage 3 will decrease, and the excess air ratio of the air-fuel mixture will gradually increase.
  • the changeover valve 8 will be started to be subjected to opening operation, and the excess air ratio of the air-fuel mixture will gradually decrease.
  • the excess air ratio of the air fuel mixture becomes minimum.
  • the changeover valve 8 will be maintained in the fully-opened state, and only the rotation angle of the butterfly valve 7 changes. Therefore, accompanied by the increase in the rotation angle of the butterfly valve 7 , the excess air ratio of the air-fuel mixture will gradually increase.
  • the apparatus is generally designed such that, in a state in which the butterfly valve 7 is rotated to the closed posture and to the opened posture, the excess air ratio of the air-fuel mixture becomes an appropriate value (an appropriate value, e.g., 1.3, for stable combustion after ignition).
  • an appropriate value e.g., 1.3, for stable combustion after ignition.
  • the apparatus is designed such that, in a state in which the butterfly valve 7 is rotated to an intermediate angle between the respective first and the second rotation angle ranges, the excess air ratio of the air-fuel mixture becomes an appropriate value.
  • the excess air ratio of the air-fuel mixture becomes the appropriate value when the butterfly valve 7 is rotated to any one of the angles within each of the first and the second rotation angle ranges.
  • the butterfly valve 7 is rotated within the first rotation angle range to thereby find out the rotation angle of the butterfly valve 7 at which the excess air ratio of the air-fuel mixture becomes the appropriate value. Then, this rotation angle is set as the closing-side stop angle. At the time of changing over to the small-capacity state, the butterfly valve 7 is rotated to the opening-side stop angle and then stop there. Similarly, the butterfly valve 7 is rotated within the second rotation angle range to thereby find out the rotation angle of the butterfly valve 7 at which the excess air ratio of the air-fuel mixture becomes the appropriate value. Then, this rotation angle is set as the opening-side stop angle.
  • the butterfly valve 7 is rotated to the opening-side stop angle and then stop there. According to this arrangement, in either of the small-capacity state and the large-capacity state, adjustments can be made without the necessity of replacing the parts so as to attain the appropriate value of the excess air ratio of the air-fuel mixture.
  • the igniting operation of the burner 1 (in order for an ignition electrode, not illustrated, facing the ignition surface 1 a , to cause sparks) must be performed in the small-capacity state.
  • the ignition operation of the burner 1 is arranged to be performed in a state in which the butterfly valve 7 is rotated to the closed posture. According to this arrangement, the ignition operation is performed in a state in which the excess air ratio of the air-fuel mixture is relatively low and in an easily ignitable gas-rich state. The occurrence of ignition failure can thus be prevented.
  • the butterfly valve 7 is rotated to the closing-side stop angle (in case the required combustion amount is small, thereby making the state to a small-capacity state) or to the open-side stop angle (in case the required combustion amount is large, thereby making the state to a large-capacity state).

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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)
  • Gas Burners (AREA)
US15/458,156 2016-04-01 2017-03-14 Premixing Apparatus Abandoned US20170284663A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US16/441,172 US11105505B2 (en) 2016-04-01 2019-06-14 Premixing apparatus and method thereof

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
JP2016073845A JP6654494B2 (ja) 2016-04-01 2016-04-01 予混合装置の制御方法
JP2016-073845 2016-04-01

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US16/441,172 Active 2037-08-07 US11105505B2 (en) 2016-04-01 2019-06-14 Premixing apparatus and method thereof

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US (2) US20170284663A1 (ja)
EP (1) EP3225913B1 (ja)
JP (1) JP6654494B2 (ja)
KR (1) KR102295803B1 (ja)
CN (1) CN107270292B (ja)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20180231243A1 (en) * 2015-08-25 2018-08-16 Rinnai Corporation Premixing Apparatus
JP2019203668A (ja) * 2018-05-25 2019-11-28 リンナイ株式会社 予混合装置
US11105505B2 (en) 2016-04-01 2021-08-31 Rinnai Corporation Premixing apparatus and method thereof
US11287131B2 (en) * 2018-08-28 2022-03-29 Ademco Inc. Method for operating a gas burner appliance

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP6725339B2 (ja) * 2016-03-28 2020-07-15 リンナイ株式会社 予混合装置
JP7088794B2 (ja) * 2018-09-18 2022-06-21 リンナイ株式会社 予混合装置
JP7538759B2 (ja) 2021-03-23 2024-08-22 リンナイ株式会社 予混合装置

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US4752211A (en) * 1986-09-12 1988-06-21 Sabin Darrel B Flow proportioning system
US20150354810A1 (en) * 2014-06-04 2015-12-10 Rinnai Corporation Premixing apparatus

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JP3029570B2 (ja) * 1996-06-17 2000-04-04 川重冷熱工業株式会社 燃焼制御方法及び装置
DE19925567C1 (de) * 1999-06-04 2000-12-14 Honeywell Bv Vorrichtung für Gasbrenner
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KR20110031003A (ko) * 2009-09-18 2011-03-24 하복진 개선된 가스버너용 혼합기 조절장치
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JP5820428B2 (ja) * 2013-04-30 2015-11-24 リンナイ株式会社 予混合装置
JP6050281B2 (ja) * 2014-06-06 2016-12-21 リンナイ株式会社 予混合装置
US10330312B2 (en) * 2016-03-28 2019-06-25 Rinnai Corporation Premixing apparatus
JP6654494B2 (ja) 2016-04-01 2020-02-26 リンナイ株式会社 予混合装置の制御方法

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US4752211A (en) * 1986-09-12 1988-06-21 Sabin Darrel B Flow proportioning system
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Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20180231243A1 (en) * 2015-08-25 2018-08-16 Rinnai Corporation Premixing Apparatus
US10495301B2 (en) * 2015-08-25 2019-12-03 Rinnai Corporation Premixing apparatus
US11105505B2 (en) 2016-04-01 2021-08-31 Rinnai Corporation Premixing apparatus and method thereof
JP2019203668A (ja) * 2018-05-25 2019-11-28 リンナイ株式会社 予混合装置
US11287131B2 (en) * 2018-08-28 2022-03-29 Ademco Inc. Method for operating a gas burner appliance

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Publication number Publication date
EP3225913B1 (en) 2023-05-03
KR102295803B1 (ko) 2021-08-31
KR20170113182A (ko) 2017-10-12
CN107270292A (zh) 2017-10-20
CN107270292B (zh) 2020-07-14
US11105505B2 (en) 2021-08-31
JP6654494B2 (ja) 2020-02-26
US20190293281A1 (en) 2019-09-26
JP2017187177A (ja) 2017-10-12
EP3225913A1 (en) 2017-10-04

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