JPH0144895Y2 - - Google Patents

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Publication number
JPH0144895Y2
JPH0144895Y2 JP10532584U JP10532584U JPH0144895Y2 JP H0144895 Y2 JPH0144895 Y2 JP H0144895Y2 JP 10532584 U JP10532584 U JP 10532584U JP 10532584 U JP10532584 U JP 10532584U JP H0144895 Y2 JPH0144895 Y2 JP H0144895Y2
Authority
JP
Japan
Prior art keywords
combustion
auxiliary air
air passage
liquid fuel
combustion chamber
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
JP10532584U
Other languages
Japanese (ja)
Other versions
JPS6123067U (en
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 filed Critical
Priority to JP10532584U priority Critical patent/JPS6123067U/en
Publication of JPS6123067U publication Critical patent/JPS6123067U/en
Application granted granted Critical
Publication of JPH0144895Y2 publication Critical patent/JPH0144895Y2/ja
Granted legal-status Critical Current

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  • Air Supply (AREA)
  • Wick-Type Burners And Burners With Porous Materials (AREA)

Description

【考案の詳細な説明】 本考案は燃焼室の筒状壁体に開口する筒状部材
に囲まれて点火栓が配置され、該点火栓周辺に補
助空気を供給して前記筒状部材内に供給される液
体燃料の燃焼を助けて前記点火栓周辺に液体燃料
の未燃焼カーボンが堆積するのを防止する液体燃
料燃焼装置に関する。
[Detailed description of the invention] The present invention is characterized in that an ignition plug is arranged surrounded by a cylindrical member that opens in a cylindrical wall of a combustion chamber, and auxiliary air is supplied around the ignition plug to fill the inside of the cylindrical member. The present invention relates to a liquid fuel combustion device that helps the combustion of supplied liquid fuel and prevents unburned carbon of the liquid fuel from accumulating around the spark plug.

上記構成の液体燃料燃焼装置の従来例を第3図
及び第4図によつて説明すると、符号1は燃焼
室、2は前記燃焼室1の筒状壁体、3は前記燃焼
室1に開口する筒状部材で、鍔部4によつて熱交
換壁体5に固定され、中心部には点火栓6が配置
されている。前記筒状部材3には液体燃料導入管
7、補助空気導入管8が開口している。9は前記
筒状部材3の内周面に取付けられた灯心である。
10は前記燃焼室1の上流側の端部壁体、11は
主燃焼空気導入口、12は燃焼空気用送風機で、
筐体13とインペラ14とかなり、該インペラ1
4は前記筐体13の蓋体15に固定された電動機
16によつて駆動される。17は前記燃焼空気用
送風機12の吐出口で該吐出口17から吹き出さ
れた空気は旋回空気通路18を通つて前記主燃焼
空気導入口11から燃焼室1内に送りこまれる。
19は補助空気取出し管で、前記補助空気導入管
8との間が可撓性パイプ20によつて接続され
る。第4図は前記燃焼空気用送風機12を燃焼室
1から取外して矢印方向から見た図で、第4図
中に示す符号は第3図の場合と同一の部分を示
す。但し筒状部材3、点火栓6及び補助空気導入
管8は補助空気通路の接続関係を示すため仮想線
(鎖線)で示してある。第3図及び第4図に示す
従来構成では補助空気取出し管19が燃焼空気用
送風機12の筐体13の最下位にある吐出口に取
付けられ、補助空気が可撓管20によつて、上方
位置にある補助空気導入管8に導びかれているた
め、燃焼装置の着火ミス、燃焼室内における吹返
しなどによつて、燃料蒸気が補助空気導入管8を
通して逆流露結し、或は液状燃料が直接補助空気
導入管8、可撓管20内に流入し、流下して、補
助空気取出し管19内に溜つて補助空気の流れを
妨げる。その結果筒状部材3の内部、点火栓6の
周辺に未燃焼燃料のカーボンが堆積して、燃料の
点火又は燃焼の継続を困難にする。従来構成の上
記不具合点に鑑みて本考案は補助空気の流れに支
障を来すことがない液体燃料燃焼装置を提供する
ことを目的とし、その要点は前記可撓管20にか
えて補助空気通路を構成する溝を前記燃焼空気用
送風機筐体の下流側端面に設け、主燃焼用空気を
導びく前記旋回空気通路18から上方に向つて上
り勾配で前記旋回空気通路18と一体に分岐形成
させることにある。以下第1図及び第2図によつ
て本考案の液体燃料燃焼装置を詳細説明する。第
1図は本考案の液体燃料燃焼装置の縦断面図で、
符号1乃至18は第3図、第4図の場合と同一の
部分を示し、第2図は第1図の燃焼室1から燃焼
空気用送風機12を取外して矢印方向から見た
図で第1図と同一の符号は第1図の場合と同一の
部分を示すほか、21は補助空気通路を構成する
溝部で隔壁22によつて燃焼空気用送風機12の
吐出口17附近において主燃焼空気の旋回空気通
路18から分岐されている。前記補助空気通路を
構成する溝部21は通路23及24を経て吐出管
25に連通し、該吐出管25と前記補助空気の導
入管8とは短かい可撓管26によつて連結されて
いる。次に本考案の液体燃料燃焼装置の作用を説
明する。
A conventional example of a liquid fuel combustion apparatus having the above structure will be explained with reference to FIGS. 3 and 4. Reference numeral 1 denotes a combustion chamber, 2 a cylindrical wall of the combustion chamber 1, and 3 an opening in the combustion chamber 1. The cylindrical member is fixed to a heat exchange wall 5 by a flange 4, and an ignition plug 6 is disposed in the center. A liquid fuel introduction pipe 7 and an auxiliary air introduction pipe 8 are opened in the cylindrical member 3 . Reference numeral 9 denotes a wick attached to the inner peripheral surface of the cylindrical member 3.
10 is an end wall on the upstream side of the combustion chamber 1, 11 is a main combustion air inlet, 12 is a combustion air blower,
The casing 13 and the impeller 14, the impeller 1
4 is driven by an electric motor 16 fixed to the lid 15 of the housing 13. Reference numeral 17 denotes a discharge port of the combustion air blower 12, and the air blown from the discharge port 17 is sent into the combustion chamber 1 from the main combustion air inlet 11 through the swirling air passage 18.
Reference numeral 19 denotes an auxiliary air take-off pipe, which is connected to the auxiliary air introduction pipe 8 through a flexible pipe 20. FIG. 4 is a view of the combustion air blower 12 removed from the combustion chamber 1 and viewed from the direction of the arrow, and the reference numerals in FIG. 4 indicate the same parts as in FIG. 3. However, the cylindrical member 3, the spark plug 6, and the auxiliary air introduction pipe 8 are shown with imaginary lines (dashed lines) to show the connection relationship of the auxiliary air passage. In the conventional configuration shown in FIGS. 3 and 4, the auxiliary air take-off pipe 19 is attached to the lowest discharge port of the casing 13 of the combustion air blower 12, and the auxiliary air is supplied upward through the flexible pipe 20. Because the fuel vapor is led to the auxiliary air introduction pipe 8 located in the auxiliary air introduction pipe 8, fuel vapor may flow back through the auxiliary air introduction pipe 8 and condense due to ignition errors in the combustion device, blowback in the combustion chamber, or liquid fuel. directly flows into the auxiliary air introduction pipe 8 and the flexible tube 20, flows down, and accumulates in the auxiliary air take-off pipe 19, obstructing the flow of the auxiliary air. As a result, carbon from unburned fuel accumulates inside the cylindrical member 3 and around the ignition plug 6, making it difficult to ignite or continue burning the fuel. In view of the above-mentioned drawbacks of the conventional structure, the present invention aims to provide a liquid fuel combustion device that does not impede the flow of auxiliary air. A groove constituting the combustion air blower housing is provided on the downstream end surface of the combustion air blower housing, and the groove is formed integrally with the swirling air passage 18 with an upward slope upward from the swirling air passage 18 that guides the main combustion air. There is a particular thing. The liquid fuel combustion apparatus of the present invention will be explained in detail below with reference to FIGS. 1 and 2. Figure 1 is a longitudinal sectional view of the liquid fuel combustion device of the present invention.
Reference numerals 1 to 18 indicate the same parts as in FIGS. 3 and 4, and FIG. 2 is a view in which the combustion air blower 12 is removed from the combustion chamber 1 in FIG. The same reference numerals as in the figure indicate the same parts as in the case of FIG. It branches off from the air passage 18. The groove portion 21 constituting the auxiliary air passage communicates with a discharge pipe 25 through passages 23 and 24, and the discharge pipe 25 and the auxiliary air introduction pipe 8 are connected by a short flexible pipe 26. . Next, the operation of the liquid fuel combustion device of the present invention will be explained.

図に示してない燃料ポンプによつて液体燃料が
液体燃料導入管7から筒状部材3内に供給されて
灯心9に支えられ点火栓6に加熱されて点火され
燃焼が継続される。燃焼開始後は点火栓6は通電
が絶たれて、燃料燃焼によつて発生した熱で燃焼
が継続される。灯心9から発生している炎及び燃
料蒸気は主燃焼空気導入口11から燃焼室1内に
旋回流入する主燃焼空気によつて燃焼を完結して
排出されるが、前記筒状部材3の内部に燃料蒸気
と燃焼を完結しない炎が淀んでいると未燃焼カー
ボンが堆積するので補助空気を補助空気導入管8
から筒状部材内に導入して、筒状部材3内におけ
る燃焼を助けると共に、燃焼が完結していない燃
料を燃焼室1内に流出させてカーボン堆積を防止
する。露結した燃料蒸気或は液体燃料が直接に補
助空気導入管8から通路23,24を通つて補助
空気通路21内に流入しても、隔壁22によつて
旋回空気通路18から分岐形成されている該補助
空気通路21は下端部において直接燃焼空気の吐
出口17に通ずる旋回空気通路18から上り勾配
で分岐形成されているので、閉塞されることがな
い。
Liquid fuel is supplied into the cylindrical member 3 from the liquid fuel introduction pipe 7 by a fuel pump (not shown), is supported by the wick 9, is heated by the ignition plug 6, and is ignited to continue combustion. After the combustion starts, the ignition plug 6 is de-energized and the combustion continues using the heat generated by fuel combustion. The flame and fuel vapor generated from the wick 9 complete combustion by the main combustion air swirling into the combustion chamber 1 from the main combustion air inlet 11 and are discharged. If fuel vapor and flame that have not completed combustion stagnate, unburned carbon will accumulate, so auxiliary air is introduced into the auxiliary air introduction pipe 8.
The fuel is introduced into the cylindrical member from above to assist combustion within the cylindrical member 3, and at the same time allows uncombusted fuel to flow out into the combustion chamber 1 to prevent carbon deposition. Even if the condensed fuel vapor or liquid fuel directly flows into the auxiliary air passage 21 from the auxiliary air introduction pipe 8 through the passages 23 and 24, it is branched from the swirling air passage 18 by the partition wall 22. The auxiliary air passage 21 is branched at an upward slope from the swirling air passage 18 which directly communicates with the combustion air discharge port 17 at its lower end, so that it will not be blocked.

上述の構成になる本考案の液体燃料燃焼装置の
利点を列挙すると、 (1) 筒状部材内で一旦蒸発して生じた燃料蒸気が
補助空気通路内に流入露結し、或は燃焼室内に
おける吹返しによつて液体燃料が直接補助空気
通路内に流入しても、補助空気通路を閉塞する
ことがなく、従つて筒状部材3内点火栓6周囲
への補助空気の流通が保証され、燃焼装置の燃
焼開始が困難となつたり、燃焼不良、燃焼中断
を起すことがない。
The advantages of the liquid fuel combustion device of the present invention having the above-mentioned structure are as follows: (1) The fuel vapor that is once evaporated within the cylindrical member flows into the auxiliary air passage and is condensed, or Even if the liquid fuel flows directly into the auxiliary air passage by blowing back, the auxiliary air passage is not blocked, and therefore the circulation of auxiliary air around the ignition plug 6 inside the cylindrical member 3 is guaranteed. There is no difficulty in starting combustion in the combustion device, no combustion failure, and no combustion interruption.

(2) 補助空気通路が燃焼空気用送風機12の筐体
13に形成され、補助空気の吐出口を形成する
吐出管25が筒状部材3の補助空気導入管8と
相対して開口され、短い可撓管26で補助空気
導入管8と接続させることができ、長い可撓管
を燃焼室の外周にそつて迂回させないので形態
がコンパクトになると共に組立作業が簡単にな
る。従つて部品点数に関係なくコスト低減に効
果がある。
(2) An auxiliary air passage is formed in the housing 13 of the combustion air blower 12, and a discharge pipe 25 forming an auxiliary air discharge port is opened opposite the auxiliary air introduction pipe 8 of the cylindrical member 3, and is short. The flexible tube 26 can be connected to the auxiliary air introduction tube 8, and since the long flexible tube does not have to be detoured around the outer periphery of the combustion chamber, the configuration becomes compact and assembly work is simplified. Therefore, it is effective in reducing costs regardless of the number of parts.

などである。etc.

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

第1図は本考案の液体燃料燃焼装置の縦断面
図、第2図は第1図の燃焼室から燃焼空気用送風
機を取外して矢印方向から見た図面、第3図は
液体燃料燃焼装置の従来例の縦断面図、第4図は
第3図の燃焼室から燃焼空気用送風機を取外して
矢印方向から見た図である。 符号の説明:1……燃焼室、2……筒状壁体、
3……筒状部材、4……鍔部、5……熱交換壁
体、6……点火栓、7……液体燃料導入管、8…
…補助空気導入管、9……灯心、10……燃焼室
1の上流側端部壁体、11……主燃焼空気導入
口、12……燃焼空気用送風機、13……燃焼空
気用送風機筐体、14……インペラ、16……電
動機、17……吐出口、18……旋回空気通路、
21……補助空気通路を構成する溝部、22……
隔壁、23,24……通路、25……吐出管、2
6……可撓管。
Figure 1 is a longitudinal cross-sectional view of the liquid fuel combustion apparatus of the present invention, Figure 2 is a view of the combustion air blower removed from the combustion chamber of Figure 1 and viewed from the direction of the arrow, and Figure 3 is a view of the liquid fuel combustion apparatus of the present invention. FIG. 4, which is a vertical cross-sectional view of the conventional example, is a view taken from the direction of the arrow with the combustion air blower removed from the combustion chamber of FIG. Explanation of symbols: 1... Combustion chamber, 2... Cylindrical wall body,
3... Cylindrical member, 4... Flange, 5... Heat exchange wall, 6... Ignition plug, 7... Liquid fuel introduction pipe, 8...
... Auxiliary air introduction pipe, 9 ... Wick core, 10 ... Upstream end wall of combustion chamber 1, 11 ... Main combustion air inlet, 12 ... Combustion air blower, 13 ... Combustion air blower casing body, 14... impeller, 16... electric motor, 17... discharge port, 18... swirling air passage,
21...Groove portion forming an auxiliary air passage, 22...
Partition wall, 23, 24... passage, 25... discharge pipe, 2
6...Flexible tube.

Claims (1)

【実用新案登録請求の範囲】[Scope of utility model registration request] 燃焼室1の筒状壁体2に開口する筒状部材3に
囲まれて点火栓6が配置され、前記筒状部材3に
は液体燃料導入管7と、前記点火栓6周辺の前記
筒状部材3内部における燃料の燃焼を助けてカー
ボン粒子の付着を防止する補助空気の導入管8が
設けられ、前記燃焼室1の燃焼ガス流の上流側端
部壁体10には主燃焼空気導入口11が開口し、
燃焼空気用送風機12の筐体13の下流側端面に
形成された溝18と前記燃焼室1の端部壁体10
とを以て前記燃焼空気用送風機12の吐出口17
と前記主燃焼空気導入口11とを接続する旋回空
気通路18が形成されている液体燃料燃焼装置に
おいて、前記補助空気の通路を構成する溝21
が、前記燃焼空気用送風機12の筐体13の下流
側端面に上り勾配で前記旋回空気通路18から分
岐して該旋回空気通路と一体に形成されているこ
とを特徴とする液体燃料燃焼装置。
An ignition plug 6 is disposed surrounded by a cylindrical member 3 that opens into the cylindrical wall 2 of the combustion chamber 1, and the cylindrical member 3 has a liquid fuel introduction pipe 7 and the cylindrical part around the ignition plug 6. An auxiliary air inlet pipe 8 is provided for assisting the combustion of fuel inside the member 3 and preventing adhesion of carbon particles, and a main combustion air inlet is provided in the end wall 10 on the upstream side of the combustion gas flow of the combustion chamber 1. 11 opens,
A groove 18 formed in the downstream end surface of the housing 13 of the combustion air blower 12 and the end wall 10 of the combustion chamber 1
and the discharge port 17 of the combustion air blower 12.
In a liquid fuel combustion device in which a swirling air passage 18 is formed that connects the main combustion air inlet 11 to the groove 21 that constitutes the auxiliary air passage.
is formed integrally with the swirling air passage 18 by branching from the swirling air passage 18 at an upward slope on the downstream end face of the housing 13 of the combustion air blower 12.
JP10532584U 1984-07-13 1984-07-13 liquid fuel combustion equipment Granted JPS6123067U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP10532584U JPS6123067U (en) 1984-07-13 1984-07-13 liquid fuel combustion equipment

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP10532584U JPS6123067U (en) 1984-07-13 1984-07-13 liquid fuel combustion equipment

Publications (2)

Publication Number Publication Date
JPS6123067U JPS6123067U (en) 1986-02-10
JPH0144895Y2 true JPH0144895Y2 (en) 1989-12-26

Family

ID=30664658

Family Applications (1)

Application Number Title Priority Date Filing Date
JP10532584U Granted JPS6123067U (en) 1984-07-13 1984-07-13 liquid fuel combustion equipment

Country Status (1)

Country Link
JP (1) JPS6123067U (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2538958Y2 (en) * 1991-10-31 1997-06-18 タキロン株式会社 Surface drainage material

Also Published As

Publication number Publication date
JPS6123067U (en) 1986-02-10

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