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JP4098463B2 - Liquid fuel combustion equipment - Google Patents
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JP4098463B2 - Liquid fuel combustion equipment - Google Patents

Liquid fuel combustion equipment Download PDF

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Publication number
JP4098463B2
JP4098463B2 JP2000208520A JP2000208520A JP4098463B2 JP 4098463 B2 JP4098463 B2 JP 4098463B2 JP 2000208520 A JP2000208520 A JP 2000208520A JP 2000208520 A JP2000208520 A JP 2000208520A JP 4098463 B2 JP4098463 B2 JP 4098463B2
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Prior art keywords
combustion
liquid fuel
cylinder
vaporization
air
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JP2002022114A (en
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高志 桑子
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Yamaha Living Tech Co Ltd
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Yamaha Living Tech Co Ltd
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Description

【0001】
【発明の属する技術分野】
本発明は、液体燃料燃焼装置に係り、更に詳しくは、噴霧燃焼開始時において、燃焼室の側壁部のうち平面視で略長手方向に沿う側壁部側からの空気の噴出量を抑制する液体燃料燃焼装置に関する。
【0002】
【従来の技術】
従来より、給湯機等に用いられる液体燃料燃焼装置として、燃焼室が平面視で略円形状となるバーナーが知られている。しかしながら、このようなバーナーでは、その周囲に配置される熱交換器が平面視略長方形状であった場合に、当該熱交換器への伝熱が不充分となる等の不都合がある。そこで、このような不都合を改善すべく、本出願人は、図6及び図7に例示されるように、燃焼室が平面視で略偏平状すなわち略長方形状となるバーナー50を提案した(特願2000−180041号等)。このバーナー50は、外側に位置する燃焼室外筒52と、この燃焼室外筒52の内側に隙間を隔てて設けられた有底筒状の燃焼盤53と、当該燃焼盤53の内側略中央に設けられた気化筒55と、この気化筒55の下方に微細な隙間Cを隔てて設けられた飛散リング56と、気化筒の55の近傍に延びる点火装置57と、気化筒55の内部に空気を供給する送風機58とを備えて構成されている。ここにおいて、気化筒55を除く燃焼盤53の内部空間が液体燃料を燃焼させる燃焼室60として機能する。また、燃焼室外筒52と燃焼盤53との間に形成される隙間は、気化筒55の内部で気化した液体燃料と送風機58からの空気とが混合した混合気が通過するガス室62となる。なお、燃焼盤53の底壁53Aの略中央には、穴部63が形成されており、この穴部63は、気化筒55の内部からの前記混合気をガス室62に通すことができるようになっている。更に、燃焼盤53の底壁53A、並びに、平面視長手方向に沿う長辺側側壁部53B及び同短手方向に沿う短辺側側壁部53Cには、多数の炎孔65A,65B,65Cが形成され、これら炎孔65A〜65Cからガス室62を経た前記混合気が燃焼室60内に噴出される。
【0003】
前記バーナー50は、回転する気化筒55の内部に燃料供給管67から液体燃料が供給されると、当該液体燃料が気化筒55と飛散リング56との間の隙間Cから燃焼室60に向かって飛散され、この飛散された液体燃料を点火装置57で着火することによって噴霧燃焼が行われる。そして、この噴霧燃焼の燃焼熱で気化筒55が加熱され、これにより、当該気化筒55の内部の液体燃料が気化される。この気化された液体燃料は、送風機58に連なる送風筒69から気化筒55内に噴出された空気と混合される。この混合気は、ガス室62を経て燃焼盤53の各炎孔65A〜65Cから燃焼室60内に噴出され、前記噴霧燃焼の火炎により気化燃焼が行われる。
【0004】
【発明が解決しようとする課題】
しかしながら、前記バーナー50にあっては、燃焼室60が平面視で略長方形状となっていることから、気化筒55の近傍で形成された噴霧燃焼の火炎が拡散し易く、気化筒55内の液体燃料の気化に時間がかかってしまうという問題がある。すなわち、噴霧燃焼開始時においては、気化筒55内の液体燃料がまだ気化しておらず、送風機58からの空気は、燃料を含まずにそのままガス室62を経て各炎孔65A〜65Cから噴出されることとなる。ところが、燃焼室60の長辺側側壁部53Bにおける気化筒55の近傍領域は、短辺側側壁部53Cよりも送風筒69からの距離が短いため、長辺側側壁部53Bの気化筒55近傍領域の炎孔65Bからの空気噴出量が多くなり、これによって、気化筒55の近傍で形成された噴霧燃焼の火炎が拡散されてしまう。その結果、気化筒55が加熱されにくくなり、その内部に供給される液体燃料の気化の促進を妨げ、噴霧燃焼から気化燃焼までの移行に時間がかかるという問題がある。
【0005】
【発明の目的】
本発明は、既提案の構造上の問題に鑑みて更にこれを改良したものであり、その目的は、気化筒近傍で形成された噴霧燃焼時の火炎の拡散を防止し、噴霧燃焼から気化燃焼への移行時間を短縮することができる液体燃料燃焼装置を提供することにある。
【0006】
【課題を解決するための手段】
前記目的を達成するため、本発明は、平面視で長手方向と短手方向とを有する略偏平状の燃焼室内に設けられた気化筒から前記燃焼室に飛散された液体燃料を着火して噴霧燃焼を行い、この噴霧燃焼の燃焼熱で前記気化筒を加熱することで、当該気化筒内の液体燃料を気化し、当該気化した燃料を、有底筒状の燃焼盤の外側に形成されたガス室を経て前記燃焼盤の側壁部に形成された多数の炎孔から燃焼盤内に噴出させて気化燃焼を行う液体燃料燃焼装置であって、
前記ガス室には、噴霧燃焼時に通過する空気の略短手方向の流れを阻害する邪魔部材が設けられる、という構成を採っている。このような構成によれば、邪魔部材で、噴霧燃焼時に通過する空気の平面視略短手方向の流れが阻害されるため、燃焼室の平面視長手方向に沿う側壁部に形成された炎孔のうち気化筒近傍に位置する炎孔から燃焼室内に噴出される噴霧燃焼時の空気量を低減することができ、気化筒周囲に形成された噴霧燃焼の火炎の拡散を防止することができる。従って、噴霧燃焼開始時において気化筒を短時間で加熱することができ、当該気化筒内部の液体燃料の気化を促進して噴霧燃焼から気化燃焼への移行時間を短縮することができる。
【0007】
【発明の実施の形態】
本発明において、前記邪魔部材を、噴霧燃焼時に通過する空気の流れ方向を略長手方向に整えることができる構成としてもよい。
【0008】
なお、本明細書において、「噴霧燃焼」とは、液体燃料を着火することによって行われる燃焼を意味し、「気化燃焼」とは、気化した液体燃焼を空気と混合することにより得られる混合気を着火することによって行われる燃焼を意味する。
【0009】
また、本明細書において、「偏平状」とは、平面視長方形状、同楕円状、同小判状、同菱形状、同瓢箪形状等に例示される形状を含む概念として用いられ、平面視真円状、同正n角形状等の形状を除く概念として用いられる。
【0010】
【実施例】
以下、本発明の実施例について図面を参照しながら説明する。
【0011】
図1には、本実施例に係る液体燃料燃焼装置としてのバーナーの概略斜視図が示され、図2には、図1の概略平面図が示されている。また、図3には、図2のA−A線矢視断面図が示されている。これらの図において、バーナー10は、灯油等の液体燃料を燃焼させる燃焼部11と、燃焼部11の下方に設けられ、当該燃焼部11に空気を供給する送風機12とを備えて構成されている。
【0012】
前記燃焼部11は、外側に位置する有底状の燃焼室外筒14と、この燃焼室外筒14の内側に設けられた有底筒状の燃焼盤15と、燃焼盤15の内側略中央に設けられた釣鐘型の気化筒16と、この気化筒16の下方に設けられた飛散リング18と、気化筒16の近傍に延びる点火装置20とを備えて構成されている。ここにおいて、気化筒16を除く燃焼盤15の内部空間が液体燃料を燃焼させる燃焼室22として機能し、この燃焼室22は、平面視において、長手方向と短手方向を有する略長方形状となっている。
【0013】
前記燃焼室外筒14の底壁14Aの略中央には、気化筒16の内部に向かって延びる送風筒24が連設され、当該送風筒24の下側に連なる送風機12からの空気を気化筒16の内側に送り込めるようになっている。前記燃焼盤15は、燃焼室外筒14の底壁14A及び周壁14Bよりも若干に内方に隙間を隔てて配置され、この隙間は、後述するように気化した液体燃料と空気との混合気が通過するガス室25となる。また、燃焼盤15は、底壁15Aと、平面視長手方向に沿う長辺側側壁部15Bと、平面視短手方向に沿う短辺側側壁部15Cとによって構成され、これら底壁15A及び各側壁部15B,15Cには、それぞれ多数の炎孔26A,26B,26Cが形成されている。これら各炎孔26A〜26Cは、ガス室25からの前記混合気を燃焼室22内に噴出可能に設けられている。なお、図1及び図3においては、図面の錯綜を回避するために、各炎孔26A〜26Cの記載を部分的或いは全体的に省略することを了解されたい。また、燃焼盤15の底壁15Aの略中央には、前記送風筒24が通過するとともに、気化筒16の内部からの混合気等をガス室25に送り込む穴部27が形成されている。
【0014】
前記ガス室25には、前記燃焼盤15の底壁15Aと燃焼室外筒14の底壁14Aとの間に、噴霧燃焼時に通過する空気Aの平面視略短手方向の流れを阻害する邪魔部材としての邪魔板28が部分的に設けられている。この邪魔板28は、図2に示されるように、前記気化筒16の外周面に略沿った円弧状となる湾曲形状に設けられており、ガス室25内における送風筒24と前記各長辺側側壁部15B,15Bとの間に一対配設されている。また、邪魔板28の上下両端は、図3に示されるように、前記各底壁15A,14Aにそれぞれ連なっており、送風筒24を経て気化筒16の内部から邪魔板28に向かう空気Aは、その外側すなわち長辺側側壁部15B側に直接流れないようになっている。なお、本実施例では、邪魔板28を円弧状の湾曲形状としたが、噴霧燃焼時に通過する空気Aの平面視略長手方向の流れを阻害すなわち流路抵抗を付与できる限りにおいて、直線状に延びる形状等の他の板状体、或いは、ブロック状等の他の邪魔部材を用いることもできる。
【0015】
前記気化筒16は、下方が開放する向きで、燃焼盤15の底壁15Aに対して隙間を隔てて配置されており、その内側上方には、燃料供給管32から液体燃料が供給される燃料拡散体33が設けられている。これら気化筒16及び燃料拡散体33は、共通の回転軸35によって支持されており、当該回転軸35に連なるモータ36によって共に回転可能となっている。燃料拡散体33は、その下端側に液体燃料の受け部33Aが設けられており、当該受け部33Aで燃料供給管32からの液体燃料を一旦受け取るようになっている。なお、燃料拡散体33の上端と気化筒16との間には、微細な隙間C1が形成されており、これによって、燃料拡散体33が回転すると、燃料拡散体33の内側の液体燃料が隙間C1を通って外側に噴出するようになっている。前記飛散リング18は、気化筒16の下側に微細な隙間C2を隔てて配置されており、当該隙間C2から、気化筒16内の液体燃料が燃焼室22に向かって噴出可能となっている。
【0016】
前記送風機12は、ここでは詳細構造を省略するが、図示しないスイッチを投入すると、前記モータ36の駆動によってファン38が回転し、吸入した空気を気化筒16の内部等に直接送り込めるようになっている。なお、送風機としては、前述した軸流式のものに限定されずに、遠心式、斜流式、或いは横流式のもの等を採用してもよい。また、本実施例においては、ファン38及び気化筒16は、共通のモータ36によって回転駆動されるが、別個のモータでそれぞれを回転させてもよい。
【0017】
次に、本実施例に係るバーナー10の作用について説明する。
【0018】
先ず、図示しないスイッチを投入すると、モータ36が駆動し、送風機12のファン38が回転して、燃焼部11側への空気の供給が開始するとともに、気化筒16及び燃料拡散体33が同時に回転する。すると、燃料拡散体33の回転によって、燃料供給管32から燃料拡散体33の受け部33Aに供給された液体燃料が、その上端と気化筒16との間に形成された微細な隙間C1から噴出され、気化筒16の内周を伝って飛散リング18との間に形成される隙間C2から燃焼室22に飛散される。この飛散された液体燃料は、点火装置20で着火されて、噴霧燃焼が開始する。この噴霧燃焼開始時においては、気化筒16の内部の液体燃料がまだ気化していないため、図3中一点鎖線で示されるように、送風機12から供給された空気Aがそのまま気化筒16の内部を通ってガス室25に流れ、各炎孔26A〜26Cから噴出する。この際、ガス室25に流れる空気Aは、邪魔板28によって、平面視略短手方向の流れが阻害され、図2中破線で示されるように、空気Aの流れ方向が略長手方向に整えられる。このため、平面視略短手方向に向かう空気Aの流量が同略長手方向に向かう空気Aの流量よりも少なくなって、燃焼盤15における長辺側側壁部15Bのうち送風筒24からの距離の短い領域に形成された炎孔26Bからの空気Aの噴出量が従来よりも少なくなる。
【0019】
そして、噴霧燃焼の燃焼熱によって気化筒16が加熱され、気化筒16の内部の液体燃料が気化する。当該気化した燃料は、送風機12から気化筒16の内部に供給された空気と混合して混合気となり、当該混合気がガス室25を通って燃焼盤15の各炎孔26A〜26Cから燃焼室22に噴出され、既に発生している噴霧燃焼の火炎によって気化燃焼が行われる。ここで、気化燃焼時には、その燃焼熱で気化筒16の内部の液体燃料が気化される。
【0020】
従って、このような実施例によれば、噴霧燃焼開始時において、気化筒16の周囲に形成される噴霧燃焼の火炎が長辺側側壁部15Bに形成された炎孔26Bからの空気Aによって拡散されずに、気化筒16を短時間で加熱することができる。その結果、気化筒16内の液体燃料の気化を促進し、噴霧燃焼から気化燃焼への移行を早めることができるという効果を得る。
【0021】
なお、前記実施例においては、燃焼室22の形状を平面視略長方形状としたが、本発明はこれに限らず、平面視略小判状、同楕円状、同菱形状、同瓢箪形状等に例示される他の平面視偏平状の燃焼室を有するバーナーに適用してもよい。
【0022】
また、図4、図5に示されるように、邪魔板28は、燃焼盤15の底壁15A、或いは、燃焼室外筒14の底壁14Aの何れか一方にのみ連なるようにし、下側又は上側を貫通可能としてもよい。また、前記邪魔板28は、正面視で帯状となっているが、櫛歯状にしてもよいし、網目状或いは多孔質状にしてもよい。要するに、燃焼盤15の下方のガス室25内において、前記空気Aの平面視略短手方向の流れに対し、所定の抵抗を付与できる限り、種々の形状の邪魔板を採用することができる。
【0023】
更に、本発明における装置各部の構成は図示構成例に限定されるものではなく、実質的に同様の作用を奏する限りにおいて、種々の変更が可能である。
【0024】
【発明の効果】
以上説明したように、本発明によれば、ガス室に噴霧燃焼時に通過する空気の前記略短手方向の流れを阻害する邪魔部材を設けたから、燃焼室の平面視略長手方向に沿う側壁部側から燃焼室内に噴出される空気量を低減することができ、気化筒16の周囲に形成された噴霧燃焼の火炎の拡散を防止することができ、噴霧燃焼から気化燃焼への移行時間を短縮することができる。
【図面の簡単な説明】
【図1】 実施例におけるバーナーの概略斜視図。
【図2】 図1の概略平面図。
【図3】 図2における矢視A−A線縦断面図。
【図4】 図1のバーナーに対して邪魔板の配置を変えた変形例に係る部分拡大断面図。
【図5】 図4の他の変形例に係る部分拡大断面図。
【図6】 従来例に係るバーナーの概略断面正面図。
【図7】 従来例に係るバーナーの概略平面図。
【符号の説明】
10・・・バーナー(液体燃料燃焼装置)、15・・・燃焼盤、16・・・気化筒、22・・・燃焼室、25・・・ガス室、26B・・・炎孔、26C・・・炎孔、28・・・邪魔板(邪魔部材)
[0001]
BACKGROUND OF THE INVENTION
The present invention relates to a liquid fuel combustion apparatus, and more particularly, a liquid fuel that suppresses the amount of air jetted from the side wall portion side along the substantially longitudinal direction in a plan view among the side wall portions of the combustion chamber at the start of spray combustion. The present invention relates to a combustion apparatus.
[0002]
[Prior art]
2. Description of the Related Art Conventionally, as a liquid fuel combustion apparatus used for a water heater or the like, a burner having a combustion chamber having a substantially circular shape in plan view is known. However, such a burner has a disadvantage that heat transfer to the heat exchanger becomes insufficient when the heat exchanger arranged around the burner has a substantially rectangular shape in plan view. Therefore, in order to improve such inconvenience, the present applicant has proposed a burner 50 in which the combustion chamber has a substantially flat shape, that is, a substantially rectangular shape in plan view, as illustrated in FIGS. Application No. 2000-180041). The burner 50 is provided on the outer side of the combustion chamber outer cylinder 52, a bottomed cylindrical combustion disk 53 provided inside the combustion chamber outer cylinder 52 with a gap therebetween, and substantially in the center of the combustion disk 53. The vaporization cylinder 55 formed, a scattering ring 56 provided below the vaporization cylinder 55 with a minute gap C therebetween, an ignition device 57 extending in the vicinity of the vaporization cylinder 55, and air inside the vaporization cylinder 55 And a blower 58 to be supplied. Here, the internal space of the combustion disc 53 excluding the vaporizing cylinder 55 functions as a combustion chamber 60 for burning liquid fuel. Further, the gap formed between the combustion chamber outer cylinder 52 and the combustion disk 53 becomes a gas chamber 62 through which the air-fuel mixture obtained by mixing the liquid fuel vaporized inside the vaporization cylinder 55 and the air from the blower 58 passes. . In addition, a hole 63 is formed in the approximate center of the bottom wall 53 </ b> A of the combustion disk 53, and this hole 63 allows the air-fuel mixture from the inside of the vaporizing cylinder 55 to pass through the gas chamber 62. It has become. Furthermore, a large number of flame holes 65A, 65B, 65C are formed in the bottom wall 53A of the combustion plate 53, the long side wall 53B along the longitudinal direction in plan view, and the short side wall 53C along the short side. The air-fuel mixture that is formed and passes through the gas chamber 62 from these flame holes 65 </ b> A to 65 </ b> C is ejected into the combustion chamber 60.
[0003]
When the liquid fuel is supplied from the fuel supply pipe 67 into the rotating vaporization cylinder 55, the burner 50 is directed toward the combustion chamber 60 from the gap C between the vaporization cylinder 55 and the scattering ring 56. Spray combustion is performed by igniting the scattered liquid fuel by the ignition device 57. Then, the vaporizing cylinder 55 is heated by the combustion heat of this spray combustion, whereby the liquid fuel inside the vaporizing cylinder 55 is vaporized. The vaporized liquid fuel is mixed with air ejected from the blower cylinder 69 connected to the blower 58 into the vaporization cylinder 55. This air-fuel mixture is ejected from the flame holes 65A to 65C of the combustion disc 53 into the combustion chamber 60 through the gas chamber 62, and vaporization combustion is performed by the spray combustion flame.
[0004]
[Problems to be solved by the invention]
However, in the burner 50, the combustion chamber 60 has a substantially rectangular shape in plan view, so that the spray combustion flame formed in the vicinity of the vaporizing cylinder 55 is easily diffused, and the inside of the vaporizing cylinder 55 There is a problem that it takes time to vaporize the liquid fuel. That is, at the start of spray combustion, the liquid fuel in the vaporizing cylinder 55 is not yet vaporized, and the air from the blower 58 is ejected from the flame holes 65A to 65C through the gas chamber 62 without containing fuel. Will be. However, the area near the vaporizing cylinder 55 in the long side wall part 53B of the combustion chamber 60 is near the vaporizing cylinder 55 in the long side wall part 53B because the distance from the blower cylinder 69 is shorter than the short side wall part 53C. The amount of air ejected from the flame hole 65B in the region increases, and as a result, the spray combustion flame formed in the vicinity of the vaporizing cylinder 55 is diffused. As a result, there is a problem that the vaporization cylinder 55 is difficult to be heated, the vaporization of the liquid fuel supplied to the vaporization cylinder 55 is prevented from being accelerated, and it takes time to shift from spray combustion to vaporization combustion.
[0005]
OBJECT OF THE INVENTION
The present invention is a further improvement in view of the previously proposed structural problems, and its purpose is to prevent the diffusion of flames during spray combustion formed in the vicinity of the vaporization cylinder, from vapor combustion to vaporization combustion. An object of the present invention is to provide a liquid fuel combustion apparatus that can shorten the transition time to.
[0006]
[Means for Solving the Problems]
In order to achieve the above object, the present invention ignites and sprays liquid fuel scattered in a combustion chamber from a vaporization cylinder provided in a substantially flat combustion chamber having a longitudinal direction and a short direction in a plan view. By performing combustion and heating the vaporization cylinder with the combustion heat of this spray combustion, the liquid fuel in the vaporization cylinder was vaporized, and the vaporized fuel was formed outside the bottomed cylindrical combustion disk. A liquid fuel combustion apparatus for performing vaporization combustion by ejecting into a combustion disk from a number of flame holes formed in a side wall of the combustion disk through a gas chamber,
The gas chamber has a configuration in which a baffle member that obstructs the flow of air that passes during spray combustion in a generally short direction is provided. According to such a configuration, the baffle member inhibits the flow of the air that passes during spray combustion in a substantially short direction in a plan view, so that the flame hole formed in the side wall portion along the longitudinal direction in the plan view of the combustion chamber Among these, the amount of air at the time of spray combustion ejected from the flame hole located in the vicinity of the vaporization cylinder into the combustion chamber can be reduced, and the diffusion of the flame of the spray combustion formed around the vaporization cylinder can be prevented. Accordingly, the vaporization cylinder can be heated in a short time at the start of spray combustion, and the vaporization of the liquid fuel inside the vaporization cylinder can be promoted to shorten the transition time from spray combustion to vaporization combustion.
[0007]
DETAILED DESCRIPTION OF THE INVENTION
In this invention, it is good also as a structure which can arrange the flow direction of the air which passes the said baffle member at the time of spray combustion in a substantially longitudinal direction.
[0008]
In the present specification, “spray combustion” means combustion performed by igniting liquid fuel, and “vaporization combustion” refers to an air-fuel mixture obtained by mixing vaporized liquid combustion with air. It means the combustion performed by igniting.
[0009]
Further, in this specification, the “flat shape” is used as a concept including shapes exemplified by a rectangular shape in plan view, an elliptical shape, an oval shape, a rhombus shape, a cognate shape, and the like. It is used as a concept excluding shapes such as a circular shape and the same n-square shape.
[0010]
【Example】
Embodiments of the present invention will be described below with reference to the drawings.
[0011]
FIG. 1 is a schematic perspective view of a burner as a liquid fuel combustion apparatus according to this embodiment, and FIG. 2 is a schematic plan view of FIG. 3 is a cross-sectional view taken along line AA in FIG. In these drawings, the burner 10 includes a combustion unit 11 that burns liquid fuel such as kerosene, and a blower 12 that is provided below the combustion unit 11 and supplies air to the combustion unit 11. .
[0012]
The combustion section 11 is provided at the outer side of the bottomed combustion chamber outer cylinder 14 located on the outer side, the bottomed cylindrical combustion disk 15 provided inside the combustion chamber outer cylinder 14, and the substantially inner center of the combustion disk 15. The bell-shaped vaporizing cylinder 16 is provided, a scattering ring 18 provided below the vaporizing cylinder 16, and an ignition device 20 extending in the vicinity of the vaporizing cylinder 16. Here, the internal space of the combustion disc 15 excluding the vaporizing cylinder 16 functions as a combustion chamber 22 for burning liquid fuel, and the combustion chamber 22 has a substantially rectangular shape having a longitudinal direction and a short direction in plan view. ing.
[0013]
A blower cylinder 24 extending toward the inside of the vaporization cylinder 16 is connected to a substantially center of the bottom wall 14 </ b> A of the combustion chamber outer cylinder 14, and air from the blower 12 connected to the lower side of the blower cylinder 24 is supplied to the vaporization cylinder 16. It can be sent to the inside. The combustion disc 15 is disposed with a gap slightly inwardly from the bottom wall 14A and the peripheral wall 14B of the combustion chamber outer cylinder 14, and this gap is a mixture of vaporized liquid fuel and air as will be described later. The gas chamber 25 passes through. The combustion plate 15 includes a bottom wall 15A, a long side wall 15B along the longitudinal direction of the plan view, and a short side wall 15C along the short side of the plan view. A large number of flame holes 26A, 26B, and 26C are formed in the side wall portions 15B and 15C, respectively. Each of the flame holes 26 </ b> A to 26 </ b> C is provided so that the air-fuel mixture from the gas chamber 25 can be ejected into the combustion chamber 22. In FIGS. 1 and 3, it should be understood that the description of each of the flame holes 26 </ b> A to 26 </ b> C is partially or wholly omitted in order to avoid complication of the drawings. Further, a hole 27 through which the air blowing cylinder 24 passes and an air-fuel mixture or the like from the inside of the vaporizing cylinder 16 is fed into the gas chamber 25 is formed substantially at the center of the bottom wall 15A of the combustion plate 15.
[0014]
The gas chamber 25 has a baffle member that hinders the flow of the air A that passes during spray combustion between the bottom wall 15A of the combustion disc 15 and the bottom wall 14A of the combustion chamber outer cylinder 14 in a generally short direction in plan view. The baffle plate 28 is partially provided. As shown in FIG. 2, the baffle plate 28 is provided in a curved shape having an arc shape substantially along the outer peripheral surface of the vaporizing cylinder 16, and the air blowing cylinder 24 in the gas chamber 25 and each of the long sides. A pair is provided between the side wall portions 15B and 15B. Further, the upper and lower ends of the baffle plate 28 are connected to the bottom walls 15A and 14A, respectively, as shown in FIG. 3, and the air A traveling from the inside of the vaporizing cylinder 16 to the baffle plate 28 through the blower cylinder 24 is The outer side, that is, the long side side wall portion 15B is prevented from flowing directly. In this embodiment, the baffle plate 28 has an arcuate curved shape. However, the baffle plate 28 has a linear shape as long as the flow of the air A passing during spray combustion is obstructed, that is, the flow path resistance can be imparted. Other plate-like bodies such as extending shapes, or other baffle members such as block shapes can also be used.
[0015]
The vaporization cylinder 16 is disposed with a gap with respect to the bottom wall 15A of the combustion disk 15 in a direction in which the lower part opens, and a fuel to which liquid fuel is supplied from a fuel supply pipe 32 is provided on the inner upper side thereof. A diffuser 33 is provided. The vaporizing cylinder 16 and the fuel diffuser 33 are supported by a common rotating shaft 35 and can be rotated together by a motor 36 connected to the rotating shaft 35. The fuel diffuser 33 is provided with a liquid fuel receiving portion 33A on the lower end side thereof, and the liquid fuel from the fuel supply pipe 32 is once received by the receiving portion 33A. Note that a fine gap C1 is formed between the upper end of the fuel diffuser 33 and the vaporizing cylinder 16, so that when the fuel diffuser 33 rotates, the liquid fuel inside the fuel diffuser 33 becomes a gap. It is designed to spray outward through C1. The scattering ring 18 is disposed on the lower side of the vaporizing cylinder 16 with a minute gap C2 therebetween, and the liquid fuel in the vaporizing cylinder 16 can be ejected toward the combustion chamber 22 from the gap C2. .
[0016]
Although the detailed structure of the blower 12 is omitted here, when a switch (not shown) is turned on, the fan 38 is rotated by driving the motor 36 and the sucked air can be directly sent into the vaporizing cylinder 16 or the like. ing. The blower is not limited to the above-described axial flow type, but may be a centrifugal type, a diagonal flow type, or a cross flow type. In the present embodiment, the fan 38 and the vaporizing cylinder 16 are rotationally driven by the common motor 36, but each may be rotated by a separate motor.
[0017]
Next, the operation of the burner 10 according to the present embodiment will be described.
[0018]
First, when a switch (not shown) is turned on, the motor 36 is driven, the fan 38 of the blower 12 is rotated, the supply of air to the combustion unit 11 side is started, and the vaporizing cylinder 16 and the fuel diffuser 33 are simultaneously rotated. To do. Then, by the rotation of the fuel diffuser 33, the liquid fuel supplied from the fuel supply pipe 32 to the receiving portion 33A of the fuel diffuser 33 is ejected from a minute gap C1 formed between the upper end of the fuel diffuser 33 and the vaporizing cylinder 16. Then, the gas is scattered into the combustion chamber 22 through a gap C2 formed between the vaporizing cylinder 16 and the scattering ring 18 along the inner circumference. The scattered liquid fuel is ignited by the ignition device 20 and spray combustion starts. At the start of spray combustion, since the liquid fuel inside the vaporizing cylinder 16 has not yet been vaporized, the air A supplied from the blower 12 remains as it is inside the vaporizing cylinder 16 as indicated by the one-dot chain line in FIG. The gas flows through the gas chamber 25 and ejects from each of the flame holes 26A to 26C. At this time, the air A flowing into the gas chamber 25 is obstructed by the baffle plate 28 in a substantially short direction in plan view, and the flow direction of the air A is adjusted to a substantially longitudinal direction as shown by a broken line in FIG. It is done. For this reason, the flow rate of the air A toward the generally short direction in plan view is smaller than the flow rate of the air A toward the approximately longitudinal direction, and the distance from the blower cylinder 24 in the long side wall portion 15B in the combustion plate 15. The amount of air A ejected from the flame hole 26 </ b> B formed in the short region is smaller than that in the prior art.
[0019]
The vaporizing cylinder 16 is heated by the combustion heat of the spray combustion, and the liquid fuel inside the vaporizing cylinder 16 is vaporized. The vaporized fuel is mixed with the air supplied from the blower 12 to the inside of the vaporizing cylinder 16 to become an air-fuel mixture, and the air-fuel mixture passes through the gas chamber 25 through the flame holes 26 </ b> A to 26 </ b> C of the combustion plate 15. Evaporation combustion is performed by the spray combustion flame which has been ejected to 22 and has already occurred. Here, at the time of vaporization combustion, the liquid fuel inside the vaporization cylinder 16 is vaporized by the combustion heat.
[0020]
Therefore, according to such an embodiment, at the start of spray combustion, the spray combustion flame formed around the vaporizing cylinder 16 is diffused by the air A from the flame hole 26B formed in the long side wall portion 15B. Instead, the vaporizing cylinder 16 can be heated in a short time. As a result, it is possible to promote the vaporization of the liquid fuel in the vaporizing cylinder 16 and to accelerate the transition from the spray combustion to the vaporized combustion.
[0021]
In the above embodiment, the shape of the combustion chamber 22 is a substantially rectangular shape in plan view. However, the present invention is not limited to this, and the shape of the combustion chamber 22 is not limited to this. You may apply to the burner which has the combustion chamber of the other planar view flat shape illustrated.
[0022]
4 and 5, the baffle plate 28 is connected to only one of the bottom wall 15A of the combustion plate 15 or the bottom wall 14A of the combustion chamber outer cylinder 14, and the lower or upper side May be penetrable. In addition, the baffle plate 28 has a band shape when viewed from the front, but may also have a comb shape, a mesh shape, or a porous shape. In short, various shapes of baffle plates can be employed in the gas chamber 25 below the combustion plate 15 as long as a predetermined resistance can be given to the flow of the air A in a generally short direction in plan view.
[0023]
Furthermore, the configuration of each part of the apparatus according to the present invention is not limited to the illustrated configuration example, and various modifications are possible as long as substantially the same operation is achieved.
[0024]
【The invention's effect】
As described above, according to the present invention, since the baffle member that obstructs the flow in the substantially short direction of the air that passes during spray combustion is provided in the gas chamber, the side wall portion along the substantially longitudinal direction in a plan view of the combustion chamber. The amount of air ejected from the side into the combustion chamber can be reduced, the diffusion of the spray combustion flame formed around the vaporization cylinder 16 can be prevented, and the transition time from spray combustion to vaporization combustion can be shortened can do.
[Brief description of the drawings]
FIG. 1 is a schematic perspective view of a burner in an embodiment.
FIG. 2 is a schematic plan view of FIG.
3 is a longitudinal sectional view taken along line AA in FIG.
4 is a partial enlarged cross-sectional view according to a modified example in which the arrangement of baffle plates is changed with respect to the burner of FIG. 1;
5 is a partially enlarged cross-sectional view according to another modification of FIG.
FIG. 6 is a schematic sectional front view of a burner according to a conventional example.
FIG. 7 is a schematic plan view of a burner according to a conventional example.
[Explanation of symbols]
DESCRIPTION OF SYMBOLS 10 ... Burner (liquid fuel combustion apparatus), 15 ... Combustion board, 16 ... Vaporization cylinder, 22 ... Combustion chamber, 25 ... Gas chamber, 26B ... Flame hole, 26C ... -Flame hole, 28 ... baffle plate (baffle member)

Claims (2)

平面視で長手方向と短手方向とを有する略偏平状の燃焼室内に設けられた気化筒から前記燃焼室に飛散された液体燃料を着火して噴霧燃焼を行い、この噴霧燃焼の燃焼熱で前記気化筒を加熱することで、当該気化筒内の液体燃料を気化し、当該気化した燃料を、有底筒状の燃焼盤の外側に形成されたガス室を経て前記燃焼盤の側壁部に形成された多数の炎孔から燃焼盤内に噴出させて気化燃焼を行う液体燃料燃焼装置であって、
前記ガス室には、噴霧燃焼時に通過する空気の略短手方向の流れを阻害する邪魔部材が設けられていることを特徴とする液体燃料燃焼装置。
The liquid fuel scattered in the combustion chamber is ignited from a vaporization cylinder provided in a substantially flat combustion chamber having a longitudinal direction and a short direction in a plan view, and spray combustion is performed. By heating the vaporization cylinder, the liquid fuel in the vaporization cylinder is vaporized, and the vaporized fuel passes through a gas chamber formed outside the bottomed cylindrical combustion disk to the side wall portion of the combustion disk. A liquid fuel combustion apparatus for performing vaporization combustion by ejecting into a combustion disk from a number of formed flame holes,
The liquid fuel combustion apparatus according to claim 1, wherein the gas chamber is provided with a baffle member that inhibits the flow of air that passes during spray combustion in a substantially short direction.
平面視で長手方向と短手方向とを有する略偏平状の燃焼室内に設けられた気化筒から前記燃焼室に飛散された液体燃料を着火して噴霧燃焼を行い、この噴霧燃焼の燃焼熱で前記気化筒を加熱することで、当該気化筒内の液体燃料を気化し、当該気化した燃料を、有底筒状の燃焼盤の外側に形成されたガス室を経て前記燃焼盤の側壁部に形成された多数の炎孔から燃焼盤内に噴出させて気化燃焼を行う液体燃料燃焼装置であって、
前記ガス室には、噴霧燃焼時に通過する空気の流れ方向を略長手方向に整える邪魔部材が設けられていることを特徴とする液体燃料燃焼装置。
The liquid fuel scattered in the combustion chamber is ignited from a vaporization cylinder provided in a substantially flat combustion chamber having a longitudinal direction and a short direction in a plan view, and spray combustion is performed. By heating the vaporization cylinder, the liquid fuel in the vaporization cylinder is vaporized, and the vaporized fuel passes through a gas chamber formed outside the bottomed cylindrical combustion disk to the side wall portion of the combustion disk. A liquid fuel combustion apparatus for performing vaporization combustion by ejecting into a combustion disk from a number of formed flame holes,
The gas chamber is provided with a baffle member for adjusting the flow direction of air passing during spray combustion in a substantially longitudinal direction.
JP2000208520A 2000-07-10 2000-07-10 Liquid fuel combustion equipment Expired - Fee Related JP4098463B2 (en)

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JP4098463B2 true JP4098463B2 (en) 2008-06-11

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