JPH08128609A - Fan equipped with fuel gas mixing mechanism - Google Patents

Fan equipped with fuel gas mixing mechanism

Info

Publication number
JPH08128609A
JPH08128609A JP6292433A JP29243394A JPH08128609A JP H08128609 A JPH08128609 A JP H08128609A JP 6292433 A JP6292433 A JP 6292433A JP 29243394 A JP29243394 A JP 29243394A JP H08128609 A JPH08128609 A JP H08128609A
Authority
JP
Japan
Prior art keywords
fuel gas
chamber
impeller
combustion air
motor
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.)
Pending
Application number
JP6292433A
Other languages
Japanese (ja)
Inventor
Toshihiro Kayahara
敏広 茅原
Noboru Takubo
昇 田窪
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.)
Miura Co Ltd
Original Assignee
Miura Co Ltd
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 Miura Co Ltd filed Critical Miura Co Ltd
Priority to JP6292433A priority Critical patent/JPH08128609A/en
Publication of JPH08128609A publication Critical patent/JPH08128609A/en
Pending legal-status Critical Current

Links

Classifications

    • 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
    • F23D14/34Burners specially adapted for use with means for pressurising the gaseous fuel or the combustion air
    • F23D14/36Burners specially adapted for use with means for pressurising the gaseous fuel or the combustion air in which the compressor and burner form a single unit
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/40Casings; Connections of working fluid
    • F04D29/42Casings; Connections of working fluid for radial or helico-centrifugal pumps
    • F04D29/4206Casings; Connections of working fluid for radial or helico-centrifugal pumps especially adapted for elastic fluid pumps
    • F04D29/4213Casings; Connections of working fluid for radial or helico-centrifugal pumps especially adapted for elastic fluid pumps suction ports
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/40Casings; Connections of working fluid
    • F04D29/42Casings; Connections of working fluid for radial or helico-centrifugal pumps
    • F04D29/4206Casings; Connections of working fluid for radial or helico-centrifugal pumps especially adapted for elastic fluid pumps
    • F04D29/4226Fan casings

Abstract

PURPOSE: To provide a fan, equipped with a fuel gas mixing mechanism, preventing the leakage of fuel gas surely and very high in safety property, in a fuel gas mixing mechanism, in which combustion air and fuel gas are mixed in the casing of the fan. CONSTITUTION: An air chamber 2, having a suction port 1, a fuel gas chamber 4, having a fuel gas supplying port 3, an impeller chamber 6, having a discharging port, are arranged sequentially and these air chamber 2, fuel gas chamber 4 and impeller chamber 6 are communicated through a communicating hole 7, formed at the center of the impeller chamber substantially, while a fuel gas inflow unit 8 from the fuel gas chamber 4 to the communicating hole 7 is constituted of an ejector nozzle structure. The motor shaft 10 of a motor 9 is inserted into the communicating hole 7 while forming a predetermined gap between the fuel gas inflow unit 8 while an impeller 11 is connected to the tip end of the motor shaft 10 in the impeller chamber 6.

Description

【発明の詳細な説明】Detailed Description of the Invention

【0001】[0001]

【産業上の利用分野】この発明は、予混合式のバーナに
用いる送風機の改良に関するものである。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to an improvement of a blower used in a premix type burner.

【0002】[0002]

【従来の技術】一般に、予混合式のバーナは、燃焼部の
上流位置において燃焼用空気に燃料ガスを混合する構成
になっているため、燃料ガスの供給圧が比較的高くなけ
ればならない。燃料ガスの供給圧が低くても混合可能と
する方式としては、送風機の吸込口に燃料ガスを供給し
て、送風機のケーシング内に燃焼用空気と燃料ガスを混
合しつつ吸い込ませるものがある。しかしながら、この
構造のものは、インペラを連結したモータ軸の軸受部か
ら燃料ガスが漏れやすいという問題点がある。燃料ガス
が漏れるのを防止するためには、軸受部として非常に機
密性の高いものを使用しなければならず、そうすると送
風機全体のコストが高くなってしまう。
2. Description of the Related Art Generally, a premixing burner has a structure in which a fuel gas is mixed with combustion air at a position upstream of a combustion section, and therefore the supply pressure of the fuel gas must be relatively high. As a method of allowing the fuel gas to be mixed even when the supply pressure is low, there is a method in which the fuel gas is supplied to the suction port of the blower so that the combustion air and the fuel gas are mixed and sucked into the casing of the blower. However, this structure has a problem that fuel gas easily leaks from the bearing portion of the motor shaft to which the impeller is connected. In order to prevent the fuel gas from leaking, it is necessary to use a bearing unit having very high airtightness, which increases the cost of the blower as a whole.

【0003】[0003]

【発明が解決しようとする課題】この発明は、送風機の
ケーシング内で燃焼用空気と燃料ガスとを混合する方式
のものにおいて、燃料ガスの漏れを確実に防止し、非常
に安全性の高い、燃料ガス混合機構を備えた送風機を提
供することを目的としている。
SUMMARY OF THE INVENTION The present invention relates to a system for mixing combustion air and fuel gas in the casing of a blower, which surely prevents the fuel gas from leaking and has a very high safety. An object is to provide a blower provided with a fuel gas mixing mechanism.

【0004】[0004]

【課題を解決するための手段】この発明は、上述の課題
に鑑みてなされたもので、吸込口を有する空気室と、燃
料ガス供給口を有する燃料ガス室と、吐出口を有するイ
ンペラ室を順に配置し、これら空気室、燃料ガス室およ
びインペラ室を、その略中央部に形成した流通孔で連通
させ、前記燃料ガス室から前記流通孔への燃料ガス流入
部をエゼクターノズル構造とし、前記流通孔に、前記燃
料ガス流入部との間に所定の隙間を形成してモータのモ
ータ軸を挿入し、このモータ軸の先端に前記インペラ室
内においてインペラを連結したことを特徴としている。
SUMMARY OF THE INVENTION The present invention has been made in view of the above-mentioned problems, and provides an air chamber having a suction port, a fuel gas chamber having a fuel gas supply port, and an impeller chamber having a discharge port. Arranged in order, these air chamber, the fuel gas chamber and the impeller chamber are communicated with each other through a flow hole formed in a substantially central portion thereof, and a fuel gas inflow portion from the fuel gas chamber to the flow hole has an ejector nozzle structure, The motor shaft of the motor is inserted into the flow hole with a predetermined gap between the fuel gas inflow portion and the fuel gas inflow portion, and the impeller is connected to the tip of the motor shaft in the impeller chamber.

【0005】[0005]

【作用】上述の構成において、吸込口より流入した燃焼
用空気は、流通孔を通ってインペラ室に流入するが、そ
の際、燃料ガス室から流通孔への燃料ガス流入部がエゼ
クターノズル構造となっているため、燃焼用空気の流れ
に燃料ガス室内の燃料ガスが吸引され、燃焼用空気と燃
料ガスとが混合されつつ、インペラ室内に流入する。イ
ンペラ室内に流入した、燃焼用空気と燃料ガスとの混合
気体は、吐出口より予混合バーナに供給される。
In the above structure, the combustion air flowing in from the suction port flows into the impeller chamber through the flow hole. At this time, the fuel gas inflow portion from the fuel gas chamber to the flow hole has the ejector nozzle structure. Therefore, the fuel gas in the fuel gas chamber is sucked into the flow of the combustion air, and the combustion air and the fuel gas are mixed and flow into the impeller chamber. The mixed gas of the combustion air and the fuel gas, which has flowed into the impeller chamber, is supplied to the premix burner through the discharge port.

【0006】[0006]

【実施例】以下、この発明の好ましい実施例について説
明する。図1,図2において、吸込口1を有する空気室
2と、燃料ガス供給口3を有する燃料ガス室4と、吐出
口5を有するインペラ室6を順に配置し、これら空気室
2、燃料ガス室4およびインペラ室6を、その略中央部
に形成した流通孔7で連通させている。前記空気室2の
吸込口1は、図示した実施例では、空気室2の周面部に
形成し、この吸込口1にはフィルタ12を装填してあ
る。前記燃料ガス供給口3は、外部の燃料ガス供給管
(図示せず)に接続している。前記インペラ室6の吐出
口5は、インペラ室6の周側壁部に形成してあり、接線
方向に開口させている。この吐出口5はバーナ(図示せ
ず)に連通させている。
The preferred embodiments of the present invention will be described below. 1 and 2, an air chamber 2 having a suction port 1, a fuel gas chamber 4 having a fuel gas supply port 3, and an impeller chamber 6 having a discharge port 5 are arranged in this order. The chamber 4 and the impeller chamber 6 are communicated with each other through a flow hole 7 formed in a substantially central portion thereof. In the illustrated embodiment, the suction port 1 of the air chamber 2 is formed in the peripheral surface portion of the air chamber 2, and the suction port 1 is equipped with a filter 12. The fuel gas supply port 3 is connected to an external fuel gas supply pipe (not shown). The discharge port 5 of the impeller chamber 6 is formed in the peripheral side wall of the impeller chamber 6 and is opened in the tangential direction. The discharge port 5 communicates with a burner (not shown).

【0007】前記燃料ガス室4から前記流通孔7への燃
料ガス流入部8は、エゼクターノズル構造をしており、
前記吸込口1より流入した燃焼用空気が、流通孔7を通
って空気室2からインペラ室6へ向かって流れる際、燃
料ガスを吸引する構成になっている。前記流通孔7の断
面積は比較的小さく、燃焼用空気はその流速を高められ
て高速で流れ、その流れの作用により、エゼクターノズ
ル構造をした前記燃料ガス流入部8が負圧になり、燃焼
用空気の流れに燃料ガスが吸引されるようになってい
る。従って、燃料ガスの供給圧が比較的低くても、燃料
ガスを燃焼用空気に対して効率よく混合させることがで
きるとともに、燃料ガスが空気室2側へ逆流することも
ない。
The fuel gas inflow portion 8 from the fuel gas chamber 4 to the flow hole 7 has an ejector nozzle structure,
When the combustion air flowing in through the suction port 1 flows from the air chamber 2 toward the impeller chamber 6 through the flow hole 7, the fuel gas is sucked. The cross-sectional area of the flow hole 7 is relatively small, and the flow rate of the combustion air is increased at a high speed, and the action of the flow causes the fuel gas inflow portion 8 having the ejector nozzle structure to have a negative pressure, resulting in combustion. Fuel gas is sucked into the flow of air for use. Therefore, even if the supply pressure of the fuel gas is relatively low, the fuel gas can be efficiently mixed with the combustion air, and the fuel gas does not flow back to the air chamber 2 side.

【0008】前記流通孔7には、モータ9のモータ軸1
0を空気室2側より挿入している。このモータ軸10と
前記燃料ガス流入部8との間には、所定の寸法の隙間、
即ち燃焼用空気および燃料ガスが流れるのに支障がない
寸法を有する隙間を形成している。前記モータ軸10の
先端には、前記インペラ室6内においてインペラ11を
連結している。モータ9を空気室2を介して固定した構
成であるので、燃料ガスがモータ軸10の軸受部から外
部に漏れることがなく、比較的機密性の低い、即ち安価
な軸受を用いることができる。また、万が一、不測の事
態が生じてバーナから火炎が逆火してきても、空気室2
を設けてあるので、防爆性が高い。
A motor shaft 1 of a motor 9 is provided in the through hole 7.
0 is inserted from the air chamber 2 side. Between the motor shaft 10 and the fuel gas inflow portion 8, a gap of a predetermined size,
That is, a gap having a size that does not hinder the flow of combustion air and fuel gas is formed. An impeller 11 is connected to the tip of the motor shaft 10 in the impeller chamber 6. Since the motor 9 is fixed via the air chamber 2, the fuel gas does not leak from the bearing portion of the motor shaft 10 to the outside, and a relatively low airtight bearing, that is, an inexpensive bearing can be used. In addition, even if an unexpected situation occurs and the flame comes back from the burner, the air chamber 2
Since it has been installed, it is highly explosion-proof.

【0009】前記燃料ガス流入部8には、圧力センサ1
3を設けてあり、この圧力センサ13からの検出信号に
基づいて、この燃料ガス流入部8が負圧状態になってい
ること、即ち送風機が正常に作動していることを確認し
て、燃料ガスの供給(燃料ガス供給用電磁弁の開閉)を
行うようにしている。そうすることにより、燃料ガスの
漏れをより確実に防止することができる。
A pressure sensor 1 is installed in the fuel gas inflow portion 8.
3 is provided, and based on the detection signal from the pressure sensor 13, it is confirmed that the fuel gas inflow portion 8 is in a negative pressure state, that is, the blower is operating normally, Gas is supplied (opening and closing of a solenoid valve for supplying fuel gas). By doing so, leakage of the fuel gas can be prevented more reliably.

【0010】次に、上記の構成についてその作用を説明
する。モータ9を作動させることによりインペラ11を
回転させて、吸込口1より燃焼用空気を流入させる。吸
込口1より流入した燃焼用空気は、モータ軸10に沿っ
て流れ、流通孔7を通ってインペラ室6に流入するが、
その際、燃料ガス室6から流通孔7への燃料ガス流入部
8がエゼクターノズル構造となっているため、燃料ガス
室6内の燃料ガスが燃焼用空気の流れに吸引される。吸
引された燃料ガスは、燃焼用空気と混合されつつインペ
ラ室6内に流入する。そして、このインペラ室6内で燃
焼用空気と燃料ガスの混合が促進され、しかる後、燃焼
用空気と燃料ガスとの混合気体は、吐出口5より下流位
置の予混合バーナに供給される。
Next, the operation of the above configuration will be described. By operating the motor 9, the impeller 11 is rotated and the combustion air is flown in through the suction port 1. The combustion air flowing in through the suction port 1 flows along the motor shaft 10 and flows into the impeller chamber 6 through the flow hole 7,
At that time, since the fuel gas inflow portion 8 from the fuel gas chamber 6 to the flow hole 7 has an ejector nozzle structure, the fuel gas in the fuel gas chamber 6 is sucked into the flow of combustion air. The sucked fuel gas flows into the impeller chamber 6 while being mixed with the combustion air. Then, the mixing of the combustion air and the fuel gas is promoted in the impeller chamber 6, and then the mixed gas of the combustion air and the fuel gas is supplied to the premix burner located downstream of the discharge port 5.

【0011】また、その他の実施例としては、モータ9
を空気室2内にすっぽりと収納し、吸込口1をモータ9
の端面側に設けて、燃焼用空気がモータ9の周囲を流れ
るように構成することもできる。この構成によれば、モ
ータ9の周囲を流れる燃焼用空気が、モータ9を冷却す
る作用をなす。
In another embodiment, the motor 9
Is completely stored in the air chamber 2, and the suction port 1 is connected to the motor 9
Can be provided on the end face side of the motor so that the combustion air flows around the motor 9. According to this configuration, the combustion air flowing around the motor 9 serves to cool the motor 9.

【0012】[0012]

【発明の効果】この発明は、以上のような構成であるの
で、低供給圧の燃料ガスを用いることが可能であり、送
風機のケーシング内で燃焼用空気と燃料ガスとを混合す
る際、燃料ガスの漏れを確実に防止することができ、非
常に安全性が高い。即ち、燃焼用空気がモータ軸に沿っ
て流通孔を流れる際、燃焼用空気はその流速を高められ
て高速で流れ、その流れの作用により、エゼクターノズ
ル構造をした燃料ガス流入部から燃料ガスを吸引する構
成であるので、燃料ガスの供給圧が比較的低くても、燃
料ガスを燃焼用空気に対して効率よく混合させることが
できるとともに、燃料ガスが空気室側へ逆流することが
ない。また、モータを空気室を介して固定した構成であ
るので、燃料ガスがモータ軸の軸受部から外部に漏れる
ことがなく安価な軸受を用いることができる。
EFFECTS OF THE INVENTION Since the present invention is constructed as described above, it is possible to use a fuel gas having a low supply pressure, and when the combustion air and the fuel gas are mixed in the casing of the blower, the fuel gas is used. It is very safe because it can surely prevent gas leakage. That is, when the combustion air flows through the flow hole along the motor shaft, the flow speed of the combustion air is increased and the combustion air flows at high speed, and the action of the flow causes the fuel gas to flow from the fuel gas inflow portion having the ejector nozzle structure. Because of the suction structure, even if the supply pressure of the fuel gas is relatively low, the fuel gas can be efficiently mixed with the combustion air, and the fuel gas does not flow back to the air chamber side. Further, since the motor is fixed via the air chamber, the fuel gas does not leak from the bearing portion of the motor shaft to the outside, and an inexpensive bearing can be used.

【図面の簡単な説明】[Brief description of drawings]

【図1】この発明の一実施例を示す縦断面図である。FIG. 1 is a vertical sectional view showing an embodiment of the present invention.

【図2】図1の右側面図である。FIG. 2 is a right side view of FIG.

【符号の説明】[Explanation of symbols]

1 吸込口 2 空気室 3 燃料ガス供給口 4 燃料ガス室 5 吐出口 6 インペラ室 7 流通孔 8 燃料ガス流入部 9 モータ 10 モータ軸 11 インペラ 1 Suction Port 2 Air Chamber 3 Fuel Gas Supply Port 4 Fuel Gas Chamber 5 Discharge Port 6 Impeller Chamber 7 Distribution Hole 8 Fuel Gas Inlet 9 Motor 10 Motor Shaft 11 Impeller

Claims (1)

【特許請求の範囲】[Claims] 【請求項1】 吸込口1を有する空気室2と、燃料ガス
供給口3を有する燃料ガス室4と、吐出口5を有するイ
ンペラ室6を順に配置し、これら空気室2、燃料ガス室
4およびインペラ室6を、その略中央部に形成した流通
孔7で連通させ、前記燃料ガス室4から前記流通孔7へ
の燃料ガス流入部8をエゼクターノズル構造とし、前記
流通孔7に、前記燃料ガス流入部8との間に所定の隙間
を形成してモータ9のモータ軸10を挿入し、このモー
タ軸10の先端に前記インペラ室6内においてインペラ
11を連結したことを特徴とする燃料ガス混合機構を備
えた送風機。
1. An air chamber 2 having a suction port 1, a fuel gas chamber 4 having a fuel gas supply port 3, and an impeller chamber 6 having a discharge port 5 are arranged in order, and these air chamber 2 and fuel gas chamber 4 are arranged. Further, the impeller chamber 6 is communicated with the flow hole 7 formed in the substantially central portion thereof, and the fuel gas inflow portion 8 from the fuel gas chamber 4 to the flow hole 7 has an ejector nozzle structure. A fuel characterized in that a motor shaft 10 of a motor 9 is inserted into the fuel gas inflow portion 8 with a predetermined gap formed therein, and an impeller 11 is connected to the tip of the motor shaft 10 in the impeller chamber 6. Blower equipped with gas mixing mechanism.
JP6292433A 1994-10-31 1994-10-31 Fan equipped with fuel gas mixing mechanism Pending JPH08128609A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP6292433A JPH08128609A (en) 1994-10-31 1994-10-31 Fan equipped with fuel gas mixing mechanism

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP6292433A JPH08128609A (en) 1994-10-31 1994-10-31 Fan equipped with fuel gas mixing mechanism

Publications (1)

Publication Number Publication Date
JPH08128609A true JPH08128609A (en) 1996-05-21

Family

ID=17781734

Family Applications (1)

Application Number Title Priority Date Filing Date
JP6292433A Pending JPH08128609A (en) 1994-10-31 1994-10-31 Fan equipped with fuel gas mixing mechanism

Country Status (1)

Country Link
JP (1) JPH08128609A (en)

Cited By (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR20040052099A (en) * 2002-12-13 2004-06-19 엘지전선 주식회사 Device of pre-mixture for pre-mixture type gas burner
WO2005080871A1 (en) * 2004-02-17 2005-09-01 Fasco Industries, Inc. Gas delivery system with pre-mix blower
KR20060024881A (en) * 2004-09-15 2006-03-20 (주)지알텍 Apparatus for upgrading of burning efficiency of the boiler
EP1657489A1 (en) 2004-11-12 2006-05-17 Robert Bosch Gmbh Mixing device for a premix burner
JP2007509273A (en) * 2003-10-23 2007-04-12 イービーエム−パプスト ラントシュット ゲーエムベーハー Fan with a laminar flow element in front of the suction port
ITPD20090215A1 (en) * 2009-07-22 2011-01-23 Ln 2 Srl Socio Unico AIR-GAS MIXER DEVICE, PARTICULARLY FOR PRE-MIXING BURNER APPLIANCES.
JP2012026715A (en) * 2010-07-26 2012-02-09 Hovalwerk Ag Premixing combustion device
WO2011051462A3 (en) * 2009-10-29 2012-03-01 Resmed Ltd. Patient ventilation device and components thereof
DE102010048626A1 (en) * 2010-10-15 2012-04-19 Friedrich Boysen Gmbh & Co. Kg Mixing device for mixing two fluid streams, particularly for exhaust system of internal combustion engine, comprises primary pipeline for primary fluid stream, and secondary pipeline for secondary fluid stream
DE102004004062B4 (en) * 2003-01-27 2012-11-22 Vaillant Gmbh Mixing device for fuel gas and air, preferably for heaters
JP2013514517A (en) * 2009-12-16 2013-04-25 インターガス・ヒーティング・アセッツ・ベスローテン・フェンノートシャップ Fan housing for a fan for supplying a fuel / oxidant mixture to a burner, insert and supply device therefor
JP2014503781A (en) * 2010-12-17 2014-02-13 インターガス・ヒーティング・アセッツ・ベスローテン・フェンノートシャップ Mixture supply system for hot water apparatus, hot water apparatus including such mixture supply system, and method for mixing fuel and oxidant
CN105972596A (en) * 2016-07-06 2016-09-28 王鸿川 Low-nitrogen burner
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JP2013514517A (en) * 2009-12-16 2013-04-25 インターガス・ヒーティング・アセッツ・ベスローテン・フェンノートシャップ Fan housing for a fan for supplying a fuel / oxidant mixture to a burner, insert and supply device therefor
JP2012026715A (en) * 2010-07-26 2012-02-09 Hovalwerk Ag Premixing combustion device
DE102010048626A1 (en) * 2010-10-15 2012-04-19 Friedrich Boysen Gmbh & Co. Kg Mixing device for mixing two fluid streams, particularly for exhaust system of internal combustion engine, comprises primary pipeline for primary fluid stream, and secondary pipeline for secondary fluid stream
JP2014503781A (en) * 2010-12-17 2014-02-13 インターガス・ヒーティング・アセッツ・ベスローテン・フェンノートシャップ Mixture supply system for hot water apparatus, hot water apparatus including such mixture supply system, and method for mixing fuel and oxidant
CN105972596A (en) * 2016-07-06 2016-09-28 王鸿川 Low-nitrogen burner
JP2019174016A (en) * 2018-03-28 2019-10-10 株式会社サムソン Premixing gas burner

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