JPH0124963B2 - - Google Patents

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Publication number
JPH0124963B2
JPH0124963B2 JP58023497A JP2349783A JPH0124963B2 JP H0124963 B2 JPH0124963 B2 JP H0124963B2 JP 58023497 A JP58023497 A JP 58023497A JP 2349783 A JP2349783 A JP 2349783A JP H0124963 B2 JPH0124963 B2 JP H0124963B2
Authority
JP
Japan
Prior art keywords
combustion
flame
mixing tube
air
tube
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
Application number
JP58023497A
Other languages
Japanese (ja)
Other versions
JPS59147914A (en
Inventor
Akihiko Hisamatsu
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.)
Inax Corp
Original Assignee
Inax 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 Inax Corp filed Critical Inax Corp
Priority to JP2349783A priority Critical patent/JPS59147914A/en
Publication of JPS59147914A publication Critical patent/JPS59147914A/en
Publication of JPH0124963B2 publication Critical patent/JPH0124963B2/ja
Granted legal-status Critical Current

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Description

【発明の詳細な説明】[Detailed description of the invention]

本発明は噴霧ノズルの前方に設けた混合管へ燃
焼ガスを循環させて空気と燃料の混合体をガス化
燃焼させるようにした燃焼装置を備えてなる熱交
換装置に関する。 従来、石油給湯機等の燃焼装置には、ガンタイ
プバーナーと称するものがある。これは、送風機
より送り出される新鮮空気と、電磁ポンプ等で加
圧されて噴霧ノズルから噴出される霧状燃料の混
合霧を、高圧電気放電等にて着火し、燃焼させる
ものである。ところが、この従来のものでは、混
合霧中の空気量が多い黄炎燃焼となり、燃焼効率
が悪いと共に、黄炎燃焼により発生したカーボン
粒子が罐体内部の伝熱面に付着して熱交換効率を
低下させ、更に炎の振動による燃焼音が大きいと
いう欠点があつた。 また最近では、省エネルギー及び環境上の観点
から高燃焼効率化、低騒音化及び清浄排ガス化の
要求があり、燃料油をガス化させて青炎燃焼させ
る、所謂ロータリーガス化バーナあるいはヒータ
ーガス化式バーナといつたものが開発されてい
る。ところが、前者のものは着火の立上がり時と
消火時に、燃料油のガス化が不十分となつて臭気
が発生するという欠点があつた。また後者のもの
はヒーターの予熱に長時間を必要とするため、使
用上の不便さがあり、しかもヒーターのコントロ
ール等に複雑な制御を要する欠点があつた。更
に、両者は燃料油のガス化構造が複雑で、保守点
検に際し、特殊な技能を必要とする欠点があつ
た。 本出願人は上述の欠点を解決するものとして、
特願昭57―83799号において熱交換装置を出願済
みである。即ち、該熱交換装置29は、第1図に
示す如く、罐体32の内部に筒状の燃焼室33が
形成され、該燃焼室33に臨んで設けられた送風
管35の内部に噴霧ノズル34が設置され、前記
燃焼室33内で且つ該噴霧ノズル34の前方位置
に、保炎板31を内部に備そた混合管30が、該
混合管30と前記送風管35との間に燃焼ガス流
入口36を形成し且つ該混合管30の燃焼炎延長
中心線Gと前記燃焼室の長手中心線Hとが直交す
るように設置されたものである。 しかし、前記熱交換装置29では、混合管の燃
焼炎延長中心線Gと燃焼室33の長手中心線Hと
を直交させてあるので、混合管30から噴出した
燃焼ガス(図示省略)は、混合管30と対向する
内周壁面32a上へ吹付けられた後、内周壁面3
2aの長手方向に沿つて排気側へ上昇するガス
と、内周壁面32aの周方向に沿つて流れるガス
とに分散される。内周壁面32aの周方向へ沿つ
て右回り及び左回りに分散されたガスは、混合管
30が設置されている側の内周壁面32a上で衝
突した後、混合管30に吸引されたガスを除いた
その余のガス内周壁面32aの長手方向に沿つて
排出側へ上昇する。このように、装置全体的にみ
れば、燃焼ガスの大部分は、内周壁面32aの周
方向への運動力成分より内周壁面32aの長手方
向への運動力成分のほうが大きいので、燃焼ガス
と内周壁面32aとの接触移動距離が短くなり、
燃焼ガスと伝熱面である内周壁面32aとの接触
を十分にとることなく外部へ排出される。その結
果、前記従来の熱交換装置29は熱交換率の低い
欠点があつた。 本発明は、従来の前記欠点に鑑み、本出願人が
先に出願した前記未公知の燃焼装置に関する技術
を更に改良し、高燃焼効率、低騒音且つ清浄排ガ
スを維持させつつ、燃焼ガスと伝熱面である内周
壁面との接触を十分にとることのできる熱交換効
率の高い熱交換装置の提供を目的とする。 以下、本発明を図面に示す実施例に基づいて説
明する。第2図及び第3図は本発明の実施例の熱
交換装置1を示すものである。該熱交換装置1の
主たる改良点となつたのは、混合管20を経て噴
出される燃焼炎の延長中心線Bが、燃焼室3の中
心部を通つて排気側へ延びる縦中心線Aと直交す
る任意の横断面Cに沿うように混合管20の姿勢
を位置づけし、且つ混合管20の燃焼炎延長中心
線Bが該縦中心線Aに対して適宜寸法Dだけ燃焼
室3の外側寄りへ偏心するようになされている点
である。罐体2は、外周壁2bと内周壁2aとの
間に水室2cを形成した二重管構造からなり、内
周壁2aで囲まれた断面円形状、断面多角形状等
の適宜断面形状からなる筒状の燃焼室3が形成さ
れている。該罐体2の外周は保温材5で覆われて
いる。なお、前記罐体2は、筒状に限定するもの
でなく、図示省略したが、球状又は錐状の如く横
断面形状が長手方向に沿つて変化するものであつ
たもよい。更に、前記罐体2は前記二重管構造に
限定するものではなく、図示省略したが、長尺小
径パイプを螺旋状に巻付ける等して内部に燃焼室
を形成した構造とすることも勿論可能であり、燃
焼室を形成する内周壁面が熱交換用の伝熱面であ
ればその構造は問わない。前記燃焼室3内で且つ
後述する送風管10の前面位置には、所定間隙W
(例えば、15mm)をもつて混合管20が、燃焼室
3の中心部を通り、排気側(図示実施例では上
方)へ延びる縦中心線Aと直交する横断面Cに沿
うように燃焼炎延長中心線Bを位置させ、且つ燃
焼炎延長中心線Bを該縦中心線Aに対して適宜寸
法D(例えば、燃焼室3の半径の1/3乃至1/2)だ
け燃焼室3の外側寄りへ偏心させて設置されてい
る。この間隙Wにより、混合管20と送風筒10
との間には、循環ガスの流入口(以下、循環流入
口という)16が前記燃焼室3を形成する罐体2
の内周壁2a近傍に形成されている。前記混合管
20を有する多重管構造の保炎部15は、第4図
に示す如く、その中心寄りにステンレス鋼製パン
チングメタル等からなる保炎板17が設置されて
おり、その外周に下流方向へ拡開するテーパーコ
ーン状の保炎筒18が設置されている。そして、
この保炎筒18の外周にはステンレス鋼製パンチ
ングメタル等からなる副保炎筒19が設置され、
更に、これの外周には混合管20が設置されてい
る。該保炎板17、保炎筒18、副保炎筒19及
び混合管20は、支持脚21,21……により連
結されていると共に、混合管20が送風管10に
脚22,22……で懸架されている。なお、前記
保炎筒18及び副保炎筒19は必要に応じて設置
されるものであり、必ず必要とするものではな
い。前記保炎部15の後方には、前記燃焼炎延長
中心線Bと略々同芯で噴霧ノズル8が設置されて
おり、油圧ポンプ7(第2図参照)で加圧された
燃料油を霧状の微粒子にして噴出するように構成
されている。該噴霧ノズル8の外周には、送風機
9(第2図参照)では起風された新鮮空気を前記
混合管20へ噴出するための送風管10が設置さ
れている。該送風管10の先端開口部には、高速
空気噴出板11が設置される。この噴出板11
は、霧状燃料と新鮮空気を噴出する中央噴出孔1
2と、その中心から所定距離をもつて適宜周ピツ
チに穿設された複数個の空気噴出孔13とを有し
ている。この空気噴出孔13は、それぞれが周方
向に所定角度傾斜しており、噴出空気に旋回流を
起こして燃料粒子を更に微細化すると共に、霧状
燃料と新鮮空気の混合を均一に分布せしめるよう
にしている。14は、噴霧ノズル8の先端近傍で
高圧電気によるスパークを発生させ、噴出された
燃料油の微粒子に点火を行なう電極棒である。第
1図中25は燃焼筒、24は排気煙突、26は給
水口、27は給湯口である。 次に、以上のように構成された燃交換装置1の
動作を、被熱交換流体を水とし、燃料油を灯油と
し、更に供給灯油量と供給新鮮空気量を一定とし
たときに基づいて説明する。 噴霧ノズル8より噴出された霧状の灯油粒子
は、電極棒16のスパークによつて点火され、最
初のうちは、噴出板11の先端近傍で黄炎燃焼を
始める。この状態では、空気が過剰である。その
後、この燃焼炎は次第に噴霧方向へ移動し、副保
炎筒19に伝播され、更に保炎板17に移動し、
この保炎板17に至る途中で整流されて、該保炎
板17で安定し、保炎筒18に案内されて定常燃
焼が維持される。このように副保炎筒19は、燃
焼炎が保炎板17へ移動するに際し、その伝播を
スムーズにさせる働きをする。なお、噴出板1
1、保炎筒18及び副保炎筒19を設置していな
いときは、保炎板17近傍でのスパーク点火によ
つて、保炎板17で安定燃焼が開始維持される。 燃焼ガスは、第3図に示す如く、燃焼炎延長中
心線Bと罐体2の内周壁2aとの交差点の周囲へ
吹付けられ、燃焼ガスの有する運動エネルギーに
よりその一部分が罐体2の内周壁面2a′に沿つて
矢符Fに流れ、水室2c内の水と熱交換を行いつ
つ循環流入口16に至る。そして、燃焼ガスは、
間隙Wを送風管10から混合管20へ高速状態で
通過する旋回空気流によつて発生する負圧により
混合管20内へ強制吸引され、灯油粒子と新鮮空
気の混合霧へ瞬時に混和する。他方、矢符E方向
へ分散した燃焼ガスは、燃焼ガスの有する運動エ
ネルギーにより罐体2の内周壁面2a′の周方向に
沿つて螺旋状に循環しながら上方へ流れ、内周壁
面2a′と長時間接触する間に水室2c内の水と熱
交換を十分に行いつつ燃焼筒25及び排気煙突2
4を介して外部へ排出される。すなわち、混合管
20の燃焼炎延長中心線Bが燃焼室3の縦中心線
Aに対して適宜寸法Dだけ燃焼室3の外側寄りへ
偏心するように向けられているので、燃焼ガスの
大部分が罐体2の内周壁面2aの周方向に沿つて
螺旋状に循環しながら上方へ流れる。従つて、罐
体2の内周壁面2aに対する燃焼ガスの接触機会
が大幅に増加し、長時間接触するようになり、そ
の間に熱交換が十分に行われる。それ故、飛躍的
な熱交換効率の向上を図ることが可能である。 前記混合管20内に吸引された循環燃焼ガス
は、旋回空気流によつて非常に微細化された灯油
粒子と新鮮空気との混合霧を暖め、灯油粒子を瞬
時にガス化若しくはこれに近い状態にする。この
ため、燃焼状態は、ガス化燃焼若しくはこれに近
い状態となり、保炎板17からの青炎燃焼が得ら
れる。即ち、灯油粒子と新鮮空気と循環燃焼ガス
の三者が混合管20内で混和された後に整流さ
れ、過剰空気で燃焼していたものが理論空気比に
近い、しかも整流された理想の燃焼となる。した
がつて、燃焼音は低く熱交換率に優れた燃焼が得
られる。以後はこの青炎燃焼が維持される。 而して、上述の青炎燃焼を得るためには、新鮮
空気と灯油粒子の混合霧に燃焼ガスを適当量だけ
混合させることが必要であり、循環流入口16に
発生する負圧(吸引作用)の大きさが問題にな
る。そこで、本実施例では、上記負圧に最も影響
を与える噴出空気の流速を変えて実験を行つた結
果、理想の空気比に必要な燃焼ガス量を吸引する
に足る流速を設定するに到つた。噴出空気の流速
に影響を及ぼす因子は、送風機9の出力及び送風
管10の内径(この場合、直径を80mm)を一定と
すると、中央噴出孔12と空気噴出孔13の孔径
及び両噴出孔12と13の面積比である。なお、
空気噴出孔13の数及び中央噴出孔12と空気噴
出孔13の距離は、噴出空気の流速にはほとんど
影響を与えず、無視できるものである。ただし、
両噴出孔12と13間の距離は、それが最適値を
越えると、灯油粒子と空気の良好な混合が得られ
なくなる。送風管10の直径を80mmとした本実施
例(燃焼出力が35000Kcal/Hr)の場合は、中
央噴出孔12と空気噴出孔13の距離は32mmが適
当であつた。 表−1及び表−2は、噴出孔12,13の孔径
と噴出孔12,13から自然大気中へ噴出したと
きの空気流速及び供給空気量との関係を示す実験
結果である。
The present invention relates to a heat exchanger equipped with a combustion device that gasifies and burns a mixture of air and fuel by circulating combustion gas through a mixing tube provided in front of a spray nozzle. BACKGROUND ART Conventionally, combustion devices such as oil water heaters include a type called a gun-type burner. This involves igniting and burning a mixture of fresh air sent from a blower and atomized fuel pressurized by an electromagnetic pump or the like and sprayed from a spray nozzle using a high-pressure electric discharge or the like. However, with this conventional method, the amount of air in the mixed mist is large, resulting in yellow flame combustion, resulting in poor combustion efficiency, and the carbon particles generated by yellow flame combustion adhere to the heat transfer surface inside the casing, reducing heat exchange efficiency. In addition, there was a drawback that the combustion noise caused by the vibration of the flame was loud. Recently, there has been a demand for high combustion efficiency, low noise, and clean exhaust gas from the viewpoint of energy conservation and the environment, and so-called rotary gasification burners or heater gasification systems that gasify fuel oil and combust it with blue flame have recently been introduced. A burner has been developed. However, the former method had the disadvantage that the gasification of the fuel oil was insufficient at the time of ignition and extinguishment, resulting in odor. Moreover, the latter method requires a long time to preheat the heater, which is inconvenient in use, and has the disadvantage that it requires complicated control of the heater. Furthermore, both had the disadvantage that their fuel oil gasification structures were complicated and required special skills for maintenance and inspection. As a solution to the above-mentioned drawbacks, the applicant has
We have applied for a heat exchange device in Japanese Patent Application No. 57-83799. That is, as shown in FIG. 1, the heat exchange device 29 includes a cylindrical combustion chamber 33 formed inside a housing 32, and a spray nozzle installed inside a blow pipe 35 facing the combustion chamber 33. 34 is installed in the combustion chamber 33 and in front of the spray nozzle 34, a mixing pipe 30 having a flame stabilizing plate 31 inside is installed between the mixing pipe 30 and the blower pipe 35. It forms a gas inlet 36 and is installed so that the combustion flame extension center line G of the mixing tube 30 and the longitudinal center line H of the combustion chamber are perpendicular to each other. However, in the heat exchange device 29, the combustion flame extension center line G of the mixing tube and the longitudinal center line H of the combustion chamber 33 are perpendicular to each other, so that the combustion gas (not shown) ejected from the mixing tube 30 is mixed. After being sprayed onto the inner peripheral wall surface 32a facing the pipe 30, the inner peripheral wall surface 3
The gas is dispersed into gas that rises toward the exhaust side along the longitudinal direction of the inner peripheral wall surface 32a, and gas that flows along the circumferential direction of the inner peripheral wall surface 32a. The gas dispersed clockwise and counterclockwise along the circumferential direction of the inner circumferential wall surface 32a collides on the inner circumferential wall surface 32a on the side where the mixing tube 30 is installed, and then the gas is sucked into the mixing tube 30. The remaining gas rises toward the discharge side along the longitudinal direction of the inner circumferential wall surface 32a. In this way, when looking at the device as a whole, most of the combustion gas is caused by the kinetic force component in the longitudinal direction of the inner peripheral wall surface 32a being larger than the kinetic force component in the circumferential direction of the inner peripheral wall surface 32a. The contact movement distance between the inner peripheral wall surface 32a and the inner peripheral wall surface 32a becomes shorter,
The combustion gas is discharged to the outside without sufficient contact with the inner circumferential wall surface 32a, which is a heat transfer surface. As a result, the conventional heat exchange device 29 has a drawback of low heat exchange efficiency. In view of the above-mentioned drawbacks of the conventional technology, the present invention further improves the technology related to the above-mentioned unknown combustion device, which was previously filed by the present applicant. It is an object of the present invention to provide a heat exchange device with high heat exchange efficiency that can sufficiently make contact with an inner circumferential wall surface which is a hot surface. Hereinafter, the present invention will be explained based on embodiments shown in the drawings. FIGS. 2 and 3 show a heat exchange device 1 according to an embodiment of the present invention. The main improvement of the heat exchange device 1 is that the extension center line B of the combustion flame ejected through the mixing tube 20 is different from the longitudinal center line A extending through the center of the combustion chamber 3 toward the exhaust side. Position the mixing tube 20 so that it follows an arbitrary cross section C that intersects perpendicularly, and position the combustion flame extension center line B of the mixing tube 20 toward the outside of the combustion chamber 3 by an appropriate dimension D with respect to the vertical center line A. The point is that it is eccentric to the center. The housing 2 has a double pipe structure in which a water chamber 2c is formed between an outer circumferential wall 2b and an inner circumferential wall 2a, and has an appropriate cross-sectional shape surrounded by the inner circumferential wall 2a, such as a circular cross-section or a polygonal cross-section. A cylindrical combustion chamber 3 is formed. The outer periphery of the housing 2 is covered with a heat insulating material 5. Note that the housing 2 is not limited to a cylindrical shape, and may have a cross-sectional shape that changes along the longitudinal direction, such as a spherical or conical shape, although not shown. Further, the housing 2 is not limited to the double pipe structure, and although not shown, it may of course have a structure in which a long small diameter pipe is wound spirally to form a combustion chamber inside. It is possible, and any structure may be used as long as the inner circumferential wall surface forming the combustion chamber is a heat transfer surface for heat exchange. A predetermined gap W is provided within the combustion chamber 3 and at a front position of the blow pipe 10, which will be described later.
(for example, 15 mm), the mixing tube 20 passes through the center of the combustion chamber 3 and extends the combustion flame along a cross section C perpendicular to the vertical center line A extending toward the exhaust side (upward in the illustrated embodiment). Position the center line B, and move the combustion flame extension center line B toward the outside of the combustion chamber 3 by an appropriate dimension D (for example, 1/3 to 1/2 of the radius of the combustion chamber 3) with respect to the vertical center line A. It is installed eccentrically to. This gap W allows the mixing pipe 20 and the blower pipe 10 to
A circulating gas inlet (hereinafter referred to as a circulating inlet) 16 is located between the housing 2 and the combustion chamber 3.
It is formed near the inner peripheral wall 2a of. As shown in FIG. 4, the flame stabilizing section 15 having a multi-tube structure including the mixing tube 20 has a flame stabilizing plate 17 made of punched stainless steel metal or the like installed near the center thereof, and a flame stabilizing plate 17 made of punched metal made of stainless steel or the like is installed on the outer periphery of the flame stabilizing plate 17 in the downstream direction. A tapered cone-shaped flame-holding tube 18 that expands is installed. and,
A sub-flame-holding tube 19 made of stainless steel punched metal or the like is installed on the outer periphery of this flame-holding tube 18.
Furthermore, a mixing tube 20 is installed around the outer periphery of this. The flame stabilizing plate 17, the flame stabilizing tube 18, the sub flame stabilizing tube 19, and the mixing tube 20 are connected by support legs 21, 21..., and the mixing tube 20 is connected to the blower tube 10 by legs 22, 22... It is suspended in Note that the flame-holding tube 18 and the sub-flame-holding tube 19 are installed as necessary, and are not necessarily required. A spray nozzle 8 is installed behind the flame holding section 15 so as to be substantially coaxial with the combustion flame extension center line B, and sprays fuel oil pressurized by a hydraulic pump 7 (see FIG. 2). It is configured to eject in the form of fine particles. A blow pipe 10 is installed around the outer periphery of the spray nozzle 8 for blowing fresh air blown by a blower 9 (see FIG. 2) to the mixing pipe 20. A high-speed air jetting plate 11 is installed at the opening at the tip of the blast pipe 10 . This ejection plate 11
is the central nozzle 1 that spouts out atomized fuel and fresh air.
2, and a plurality of air jet holes 13 which are formed at appropriate circumferential pitches at a predetermined distance from the center. Each of the air ejection holes 13 is inclined at a predetermined angle in the circumferential direction, and creates a swirling flow in the ejected air to further refine the fuel particles and uniformly distribute the mixture of atomized fuel and fresh air. I have to. Reference numeral 14 denotes an electrode rod that generates a spark using high-voltage electricity near the tip of the spray nozzle 8 and ignites the fine particles of fuel oil that are ejected. In FIG. 1, 25 is a combustion tube, 24 is an exhaust chimney, 26 is a water supply port, and 27 is a hot water supply port. Next, the operation of the fuel exchange device 1 configured as described above will be explained based on the case where the fluid to be heat exchanged is water, the fuel oil is kerosene, and the amount of kerosene supplied and the amount of fresh air supplied are constant. do. The atomized kerosene particles ejected from the spray nozzle 8 are ignited by the spark of the electrode rod 16, and at first start yellow flame combustion near the tip of the ejection plate 11. In this condition there is an excess of air. After that, this combustion flame gradually moves in the spray direction, propagates to the sub-flame stabilizing cylinder 19, and further moves to the flame stabilizing plate 17,
The flow is rectified on the way to the flame stabilizing plate 17, stabilized at the flame stabilizing plate 17, and guided to the flame stabilizing tube 18 to maintain steady combustion. In this way, the auxiliary flame stabilizing cylinder 19 functions to smooth the propagation of the combustion flame when it moves to the flame stabilizing plate 17. In addition, the ejection plate 1
1. When the flame-holding tube 18 and the sub-flame-holding tube 19 are not installed, stable combustion is started and maintained on the flame-holding plate 17 by spark ignition near the flame-holding plate 17. As shown in FIG. 3, the combustion gas is blown around the intersection of the combustion flame extension center line B and the inner circumferential wall 2a of the casing 2, and a part of it is blown inside the casing 2 due to the kinetic energy of the combustion gas. It flows along the peripheral wall surface 2a' in the direction of arrow F and reaches the circulation inlet 16 while exchanging heat with the water in the water chamber 2c. And the combustion gas is
The negative pressure generated by the swirling airflow that passes through the gap W from the blast pipe 10 to the mixing pipe 20 at high speed forces the air into the mixing pipe 20 and instantly mixes it into a mixed mist of kerosene particles and fresh air. On the other hand, the combustion gas dispersed in the direction of the arrow E flows upward while circulating spirally along the circumferential direction of the inner peripheral wall surface 2a' of the housing 2 due to the kinetic energy of the combustion gas, and flows upward toward the inner peripheral wall surface 2a'. The combustion tube 25 and the exhaust chimney 2 while sufficiently exchanging heat with the water in the water chamber 2c during the long period of contact with the combustion tube 25 and the exhaust chimney 2.
4 and is discharged to the outside. That is, since the combustion flame extension center line B of the mixing tube 20 is oriented eccentrically toward the outside of the combustion chamber 3 by an appropriate dimension D with respect to the longitudinal center line A of the combustion chamber 3, most of the combustion gas is flows upward while circulating spirally along the circumferential direction of the inner peripheral wall surface 2a of the housing 2. Therefore, the chances of the combustion gas coming into contact with the inner circumferential wall surface 2a of the casing 2 are greatly increased, and the contact occurs for a long time, during which heat exchange is sufficiently performed. Therefore, it is possible to dramatically improve heat exchange efficiency. The circulating combustion gas sucked into the mixing tube 20 warms the mixed mist of very fine kerosene particles and fresh air due to the swirling airflow, and instantly gasifies the kerosene particles or into a state close to this. Make it. Therefore, the combustion state becomes gasification combustion or a state close to this, and blue flame combustion from the flame stabilizing plate 17 is obtained. In other words, kerosene particles, fresh air, and circulating combustion gas are mixed in the mixing tube 20 and then rectified, and what used to be combustion with excess air becomes an ideal combustion that is close to the stoichiometric air ratio and is rectified. Become. Therefore, combustion with low combustion noise and excellent heat exchange efficiency can be obtained. From then on, this blue flame combustion is maintained. In order to obtain the above-mentioned blue flame combustion, it is necessary to mix an appropriate amount of combustion gas into the mixed mist of fresh air and kerosene particles. ) is the problem. Therefore, in this example, we conducted experiments by changing the flow rate of the ejected air, which has the greatest effect on the negative pressure, and as a result, we were able to set a flow rate that was sufficient to suck in the amount of combustion gas required for the ideal air ratio. . The factors that affect the flow velocity of the ejected air are the diameters of the central ejection hole 12 and the air ejection hole 13 and the diameters of both the air ejection holes 12 and The area ratio is 13. In addition,
The number of air ejection holes 13 and the distance between the central ejection hole 12 and the air ejection hole 13 have little effect on the flow velocity of the ejected air and can be ignored. however,
If the distance between the two nozzles 12 and 13 exceeds an optimum value, good mixing of kerosene particles and air will not be achieved. In the case of this embodiment in which the diameter of the blast pipe 10 was 80 mm (combustion output was 35000 Kcal/Hr), the distance between the central nozzle 12 and the air nozzle 13 was appropriately 32 mm. Tables 1 and 2 are experimental results showing the relationship between the diameter of the ejection holes 12 and 13 and the air flow velocity and amount of air supplied when ejected from the ejection holes 12 and 13 into the natural atmosphere.

【表】 表−1から明らかなように、空気噴出孔13の
孔径を小さくすれば、噴出空気の流速は速くな
り、循環流入口16で発生する負圧は大きくな
る。ところが、供給空気量は空気噴出孔13の径
が小さくなると減少する傾向にある。このため、
供給空気量が十分にとれ、且つ流速の速い孔の直
径としては8mmが必要である。
[Table] As is clear from Table 1, if the diameter of the air ejection holes 13 is made smaller, the flow velocity of the ejected air becomes faster and the negative pressure generated at the circulation inlet 16 becomes larger. However, the amount of supplied air tends to decrease as the diameter of the air jet hole 13 becomes smaller. For this reason,
A hole diameter of 8 mm is required to ensure a sufficient amount of supplied air and a high flow rate.

【表】 但し、上記孔12の開口率とは、中央噴出孔1
2の開口面積を中央噴出孔12及び空気噴出孔1
3の開口面積の総和で除した値に100を乗した値
である。 また、表−2から明らかなように、中央噴出孔
12もその孔径を小さくすれば流速は速くなる
が、供給空気量は少なくなる。しかも、中央噴出
孔12と空気噴出孔13の全体の開口面積に対す
る中央噴出孔12の開口面積の割合は、空気量に
比例した値を取る。そこで供給空気量と、噴出空
気流速のバランスを考慮すれば、中央噴出孔12
の直径は、18乃至20mmが最適である。 中央噴出孔12の直径を18mm、空気噴出孔13
の直径を8mm、空気噴出孔13の直径を8mm、送
風管10の直径を80mmとして、実際の空気流速を
測定したところ21m/secであつた。参考までに、
従来市販されている燃焼装置の空気流速は、通常
12.5m/sec程度であつた。 要するに、保炎部15は、混合管20内におい
て、灯油粒子を循環燃焼ガスで暖めることによ
り、ガス化若しくはこれに近い状態にすると共
に、空気と灯油粒子の混合霧に燃焼ガスを加えて
理論空気比に近い空気比で青炎燃焼させているの
で、一定量の燃料に対する発生熱量が多く、優れ
た熱効率が得られる。更には、整流された青炎燃
焼であるため、燃焼音も低いという利点もある。 以上説明したように本発明に係る熱交換装置
は、次の如き優れた効果を有する。 混合管を経て噴出される燃焼炎の延長中心線
が、燃焼室の中心部を通つて排気側へ延びる縦
中心線と直交する任意の横断面に沿うように、
混合管の姿勢を位置づけ、且つ混合管の燃焼炎
延長中心線が前記縦中心線に対して適宜寸法だ
け前記燃焼室の外側寄りに偏心するように向け
られているので、燃焼ガスの大部分が、罐体の
内周壁面の周方向に沿つて螺旋状に循環しなが
ら上方へ流れ、内周壁面と長時間接触する間に
熱交換を十分に行つた後、外部へ排出されるか
ら熱交換効率を向上させることが出来る。 また、燃焼ガスを混合管に循環させて燃料粒
子を暖めることにより、ガス化若しくはこれに
近い状態にすると共に、新鮮空気と燃料粒子と
の混合物に燃焼ガスを加えて理論空気比に近い
空気比で燃焼させることにより、青炎燃焼させ
ることができ、一定量の燃料に対する発生熱量
が多く、装置の熱効率に優れている。 更には、燃焼炎が定常の青炎であることと、
混合管による整流効果により、燃焼音が低いと
いう利点がある。
[Table] However, the opening ratio of the hole 12 above refers to the opening ratio of the central nozzle 1.
The opening area of 2 is the center nozzle 12 and the air nozzle 1.
It is the value obtained by multiplying the value divided by the sum of the opening areas of 3 by 100. Further, as is clear from Table 2, if the hole diameter of the central jet hole 12 is made smaller, the flow velocity becomes faster, but the amount of supplied air decreases. Furthermore, the ratio of the opening area of the central jetting hole 12 to the total opening area of the central jetting hole 12 and the air jetting hole 13 takes a value proportional to the amount of air. Therefore, if we consider the balance between the amount of supplied air and the flow rate of the ejected air, the center ejection hole 12
The optimum diameter is 18 to 20 mm. The diameter of the central nozzle 12 is 18 mm, and the air nozzle 13 is
The actual air flow velocity was measured to be 21 m/sec, assuming that the diameter of the air blowing hole 13 was 8 mm, the diameter of the air blowing pipe 10 was 80 mm, and the actual air flow velocity was 21 m/sec. For your reference,
The air flow velocity of conventional commercially available combustion equipment is usually
It was about 12.5m/sec. In short, the flame stabilizing section 15 warms the kerosene particles in the mixing tube 20 with circulating combustion gas to turn them into a gasified state or a state close to this, and also adds combustion gas to the mixed mist of air and kerosene particles. Since blue flame combustion is performed at an air-to-air ratio, a large amount of heat is generated for a given amount of fuel, resulting in excellent thermal efficiency. Furthermore, since it is a rectified blue flame combustion, it also has the advantage of low combustion noise. As explained above, the heat exchange device according to the present invention has the following excellent effects. so that the extended center line of the combustion flame ejected through the mixing tube is along any cross section perpendicular to the longitudinal center line extending through the center of the combustion chamber to the exhaust side;
Since the posture of the mixing tube is positioned so that the center line of the combustion flame extension of the mixing tube is eccentric to the outside of the combustion chamber by an appropriate amount with respect to the vertical center line, most of the combustion gas is , flows upward while circulating spirally along the circumferential direction of the inner peripheral wall of the casing, and after sufficiently exchanging heat while in contact with the inner peripheral wall for a long time, it is discharged to the outside. Efficiency can be improved. In addition, by circulating the combustion gas through the mixing tube to warm the fuel particles, it is brought to a state close to gasification, and by adding combustion gas to the mixture of fresh air and fuel particles, the air ratio is close to the stoichiometric air ratio. By burning with a blue flame, a large amount of heat is generated for a given amount of fuel, and the device has excellent thermal efficiency. Furthermore, the combustion flame is a steady blue flame,
The rectifying effect of the mixing tube has the advantage of low combustion noise.

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

第1図は従来の熱交換装置の横断面図、第2図
は本発明に係る熱交換装置の実施例を示す縦断面
図、第3図は同上の横断面図、第4図は混合管及
び送風管等を示す部分切欠き斜視図である。 2……罐体、3……燃焼室、8……噴霧ノズ
ル、10……送風管、16……循環流入口、20
……混合管、A……縦中心線、B……燃焼炎延長
中心線、C……横断面。
Fig. 1 is a cross-sectional view of a conventional heat exchange device, Fig. 2 is a longitudinal cross-sectional view showing an embodiment of the heat exchange device according to the present invention, Fig. 3 is a cross-sectional view of the same, and Fig. 4 is a mixing tube. FIG. 2... Housing, 3... Combustion chamber, 8... Spray nozzle, 10... Air pipe, 16... Circulation inlet, 20
... Mixing tube, A ... Vertical center line, B ... Combustion flame extension center line, C ... Cross section.

Claims (1)

【特許請求の範囲】[Claims] 1 円筒状罐体内に形成された筒状の燃焼室に臨
んで先端を開口させた燃焼用空気の送風管と、該
送風管の先端開口部を覆うべく配設され、中央噴
出孔及び円周部の空気噴出孔を有する高速空気噴
出板と、前記送風管の内部に配設された噴霧ノズ
ル及び点火用電極と、前記送風管の先端開口より
噴霧方向前方にあつて、この送風管と軸芯を一致
させるようにして連結配置されたテーパーコーン
状の混合管と、該混合管の中心部にあつて前記噴
霧ノズルの噴霧方向に正対面して設けられた多孔
若しくは網目状の保炎板とを備え、前記送風管と
混合管との連結部には、円筒状の燃焼室内壁に沿
つて循環する燃焼ガスを混合管の後端開口へ流入
できる大きさの環状流入口が設けられている燃焼
装置を有する熱交換装置において、前記混合管の
設置姿勢は、この混合管を経て噴出される燃焼炎
の延長中心線が、前記燃焼室の中心部を通つて排
気側へ延びる縦中心線と直交する任意の横断面に
沿うように位置づけられ、且つ前記縦中心線に対
して適宜寸法だけ前記燃焼室の外側寄りに偏心す
るように向けられていることを特徴とする熱交換
装置。
1. A combustion air blowing pipe whose tip is open facing a cylindrical combustion chamber formed in a cylindrical housing, and a central blowing hole and a circumferential blowing pipe arranged to cover the tip opening of the blowing tube. a high-speed air ejection plate having air ejection holes at the top; a spray nozzle and an ignition electrode disposed inside the blast pipe; Tapered cone-shaped mixing tubes connected and arranged so that their cores match, and a porous or mesh-shaped flame stabilizing plate provided at the center of the mixing tube and facing directly in the spraying direction of the spray nozzle. and an annular inlet having a size that allows the combustion gas circulating along the wall of the cylindrical combustion chamber to flow into the rear end opening of the mixing tube is provided at the connecting portion between the blower tube and the mixing tube. In the heat exchange device having a combustion device, the mixing tube is installed in such a manner that the extension center line of the combustion flame ejected through the mixing tube is a vertical center line extending through the center of the combustion chamber toward the exhaust side. A heat exchange device characterized in that the heat exchange device is positioned along an arbitrary cross section orthogonal to the vertical center line, and is oriented eccentrically toward the outside of the combustion chamber by an appropriate dimension with respect to the longitudinal centerline.
JP2349783A 1983-02-14 1983-02-14 Heat exchanger Granted JPS59147914A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP2349783A JPS59147914A (en) 1983-02-14 1983-02-14 Heat exchanger

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP2349783A JPS59147914A (en) 1983-02-14 1983-02-14 Heat exchanger

Publications (2)

Publication Number Publication Date
JPS59147914A JPS59147914A (en) 1984-08-24
JPH0124963B2 true JPH0124963B2 (en) 1989-05-15

Family

ID=12112122

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2349783A Granted JPS59147914A (en) 1983-02-14 1983-02-14 Heat exchanger

Country Status (1)

Country Link
JP (1) JPS59147914A (en)

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5520123A (en) * 1978-07-17 1980-02-13 Nippon Pirooburotsuku Seizou K Crack detector for bottle head
JPS5616008A (en) * 1979-07-12 1981-02-16 Combustion Eng Steam generator

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5520123A (en) * 1978-07-17 1980-02-13 Nippon Pirooburotsuku Seizou K Crack detector for bottle head
JPS5616008A (en) * 1979-07-12 1981-02-16 Combustion Eng Steam generator

Also Published As

Publication number Publication date
JPS59147914A (en) 1984-08-24

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