JPH0229394Y2 - - Google Patents

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Publication number
JPH0229394Y2
JPH0229394Y2 JP14234984U JP14234984U JPH0229394Y2 JP H0229394 Y2 JPH0229394 Y2 JP H0229394Y2 JP 14234984 U JP14234984 U JP 14234984U JP 14234984 U JP14234984 U JP 14234984U JP H0229394 Y2 JPH0229394 Y2 JP H0229394Y2
Authority
JP
Japan
Prior art keywords
tube
rotating disk
evaporator coil
centrifugal pressure
coil 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
JP14234984U
Other languages
Japanese (ja)
Other versions
JPS6158524U (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 JP14234984U priority Critical patent/JPH0229394Y2/ja
Publication of JPS6158524U publication Critical patent/JPS6158524U/ja
Application granted granted Critical
Publication of JPH0229394Y2 publication Critical patent/JPH0229394Y2/ja
Expired legal-status Critical Current

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  • Spray-Type Burners (AREA)
  • Feeding And Controlling Fuel (AREA)

Description

【考案の詳細な説明】 (産業上利用分野) 本考案は各種用途に供される回転加圧式石油バ
ーナーに関する。
[Detailed Description of the Invention] (Industrial Application Field) The present invention relates to a rotary pressurized oil burner used for various purposes.

(従来の技術およびその問題点) 従来、石油バーナーとして種々の形式のものが
開発、提供されているが、石油を完全に近い状態
まで気化させて燃焼させる、あるいは充分に空気
を補給して完全燃焼させるという点では、解決す
べき問題点が多い。
(Prior art and its problems) Conventionally, various types of oil burners have been developed and provided. There are many problems that need to be solved in terms of combustion.

(考案の目的) 本考案は、気化された石油のみを燃焼させ、し
かも燃焼力の増大に伴つて自動的に潤滑な給油を
なしつつ、燃焼部への給気を増加させて完全燃焼
を促進するとともに、燃焼部の冷却度をも大とす
ることが可能、そのうえ簡易な機構で製作費が低
廉で済む、回転加圧式石油バーナーを提供するこ
とを目的とする。
(Purpose of the invention) This invention burns only vaporized oil, and as the combustion power increases, it automatically provides lubricant oil supply and increases air supply to the combustion part to promote complete combustion. It is also an object of the present invention to provide a rotary pressurized oil burner which can increase the degree of cooling of the combustion section and which has a simple mechanism and is inexpensive to manufacture.

(考案の構成) 上記目的を達するため、本考案は以下に示す構
成とする。
(Structure of the invention) In order to achieve the above object, the invention has the following structure.

回転円板と、回転円板の一側に枢着される元軸
と、元軸に固定されてその外周を複数巻回する遠
心圧力管と、回転円板の他側に巻回中心線を上記
遠心圧力管と同一水平レベルとして配置された複
数巻回の蒸発コイル管と、遠心圧力管・蒸発コイ
ル管間を接続する連通管とを具えている。上記遠
心圧力管は回転円板反対方向端が給油源に連通可
能とされている。遠心圧力管と蒸発コイル管と
は、回転円板を回転させた場合の遠心力で生ずる
それぞれの管内の圧力が均衡して相殺されるよう
に、互いに逆方向巻きとするとともに、それぞれ
の管径、巻径および巻回数を所定に設定してあ
る。上記蒸発コイル管の回転円板に近接した端部
は内側へ曲げて巻回軸線に至らしめ、その先端に
口を軸線上他側に向けたノズルを設ける。上記連
通管は遠心圧力管の回転円板側端部と接続し、回
転円板の一側表面沿いに元軸の半径方向へU字を
描いて伸延、折曲したうえ所定位置で回転円板を
貫通して蒸発コイル管のノズル反対端まで伸びて
接続される。
A rotating disk, a base shaft pivotally mounted on one side of the rotating disk, a centrifugal pressure tube fixed to the base shaft and wound around its outer circumference multiple times, and a winding center line on the other side of the rotating disk. The evaporator coil tube includes a plurality of turns of an evaporator coil tube arranged on the same horizontal level as the centrifugal pressure tube, and a communication tube connecting the centrifugal pressure tube and the evaporator coil tube. The end of the centrifugal pressure pipe in the direction opposite to the rotating disk can communicate with the oil supply source. The centrifugal pressure tube and the evaporator coil tube are wound in opposite directions, and the diameters of each tube are , the winding diameter and the number of windings are set to predetermined values. The end of the evaporator coil tube close to the rotating disk is bent inward to reach the winding axis, and a nozzle with its mouth facing the other side on the axis is provided at its tip. The communication pipe is connected to the end of the centrifugal pressure tube on the rotating disk side, extends and bends in a U-shape along one surface of the rotating disk in the radial direction of the base shaft, and then connects the rotating disk at a predetermined position. It extends through the evaporator coil tube to the opposite end of the nozzle and is connected to the evaporator coil tube.

また、上記回転円板の一側表面の周部には所定
間隔をへだてて羽根を装着し、さらに回転円板の
周縁に沿つて中空状の送風ケースを設け、上記送
風ケースを導風管を介して蒸発コイル管を巻回す
る中空環状の風気室に接続し、上記風気室に風気
孔を設ける。
In addition, blades are attached to the periphery of one side surface of the rotating disk at a predetermined interval, and a hollow air blowing case is provided along the periphery of the rotating disk, and the air blowing case is connected to an air guide pipe. It is connected to a hollow annular air chamber around which the evaporator coil tube is wound, and an air hole is provided in the air chamber.

(実施例) 上記構成を第1図ないし第3図に示す実施例に
従つてさらに詳述する。
(Embodiment) The above configuration will be further explained in detail according to the embodiment shown in FIGS. 1 to 3.

図における1は軸受け2,2で支持される元軸
で、その一端は回転円板9の一側に枢着されてい
る。30は元軸1を回転させるための駆動プーリ
であり、図示しない無段変速機を介して駆動源の
駆動力を伝達する。元軸1の同図における右方部
は中実、左方部は中空に構成され、当該中空部は
給油孔3となつている。給油孔3の一端は給油座
4を介して後述する遠心圧力管の一端と連通し、
他端は給油接手20内の給油座19に連通し、上
記給油接手20はバルブ21に接続されている。
バルブ21は管22を介して補助ンク23に接続
されている。26は主給油タンク、25はポン
プ、24はオーバーフロー管である。
1 in the figure is a base shaft supported by bearings 2, 2, one end of which is pivoted to one side of a rotating disk 9. 30 is a drive pulley for rotating the main shaft 1, and transmits the driving force of the drive source via a continuously variable transmission (not shown). The right side portion of the base shaft 1 in the figure is solid, and the left side portion is hollow, and the hollow portion serves as the oil supply hole 3. One end of the oil supply hole 3 communicates with one end of a centrifugal pressure pipe, which will be described later, via the oil supply seat 4.
The other end communicates with a fuel seat 19 in a fuel fitting 20, and the fuel fitting 20 is connected to a valve 21.
Valve 21 is connected to auxiliary tank 23 via pipe 22 . 26 is a main oil supply tank, 25 is a pump, and 24 is an overflow pipe.

5は一端が上記給油座4と連通するコイル状の
遠心圧力管であり、元軸1の外周に複数巻回され
て元軸1に固定され、その他端は後述する連通管
6に接続・連通している。
Reference numeral 5 denotes a coiled centrifugal pressure tube whose one end communicates with the oil supply seat 4, which is wound around the outer circumference of the base shaft 1 in multiple turns and fixed to the base shaft 1, and whose other end is connected and communicated with a communication pipe 6 to be described later. are doing.

連通管6は回転円板9の一側表面沿いに元軸1
の半径方向へ伸延したのち、61として示す如く
折曲して元軸1方向へ戻り、所定位置で回転円板
9、およびその他側に装着された断熱円板13を
貫通して水平方向に延長されている。
The communication pipe 6 is connected to the base shaft 1 along one side surface of the rotating disk 9.
After extending in the radial direction of has been done.

7はコイル状に複数巻回された蒸発コイル管
で、遠心圧力管5と同一水平レベルとなる如く配
置されていて、巻方向が遠心圧力管5とは逆であ
る。実施例では、管径、巻回径および巻回数を遠
心圧力管5と同一に設定してある。蒸発コイル管
7の回転円板9に近接した先端部は巻中心方向へ
曲げ、その巻回軸線上に位置する先端には、図示
右方向へ口が指向するノズル8が装着されてい
る。蒸発コイル管7のノズル8側反対方向端は上
記連通管6の水平方向に延長された端部と接続・
連通している。
Reference numeral 7 denotes an evaporator coil tube which is wound in a plurality of coils, and is arranged so as to be on the same horizontal level as the centrifugal pressure tube 5, and its winding direction is opposite to that of the centrifugal pressure tube 5. In the embodiment, the tube diameter, winding diameter, and number of windings are set to be the same as those of the centrifugal pressure tube 5. The distal end of the evaporator coil tube 7 close to the rotating disk 9 is bent toward the center of the winding, and a nozzle 8 whose mouth is oriented toward the right in the figure is attached to the distal end located on the winding axis. The opposite end of the evaporator coil tube 7 on the nozzle 8 side is connected to the horizontally extended end of the communication tube 6.
It's communicating.

上記回転円板9の一側表面の周縁近傍には所定
間隔をへだてて送風用の羽根10が設けられる。
Near the periphery of one side surface of the rotating disk 9, air blowing blades 10 are provided at a predetermined interval.

11は回転円板9の周縁に沿うように形成され
た中空状の送風ケースで、回転円板9の一側方向
は周縁を突出させて開口部12としてあり、開口
部12から中空部11′内に挿入状態とされてい
る回転円板9、連通管6およびその折曲部61が
支障なく回転可能である。また、中空部11′は
回転円板9の回転方向に従う一方側から他方側へ
向かつてその径が漸増する設定である。
Reference numeral 11 denotes a hollow air blowing case formed along the periphery of the rotary disk 9. On one side of the rotary disk 9, the periphery protrudes to form an opening 12. From the opening 12, the hollow portion 11' The rotating disk 9, the communicating tube 6, and its bent portion 61, which are inserted therein, can rotate without any trouble. Further, the diameter of the hollow portion 11' gradually increases from one side to the other side according to the rotational direction of the rotary disk 9.

送風ケース11の最大径中空部11′の蒸発コ
イル管7方向側には、これと連通する導風管14
が設けられ、導風管14は蒸発コイル管7と同心
的に設けた中空環状の風気室15に連通してい
る。風気室15の蒸発コイル管7側環壁には複数
の一次空気孔17が、また前方環壁には複数の二
次空気孔16がそれぞれ形成されている。
On the side of the maximum diameter hollow part 11' of the blower case 11 in the direction of the evaporator coil pipe 7, there is an air guide pipe 14 that communicates with the evaporator coil pipe 7.
The air guide pipe 14 communicates with a hollow annular air chamber 15 provided concentrically with the evaporator coil pipe 7. A plurality of primary air holes 17 are formed in the ring wall on the side of the evaporator coil tube 7 of the air chamber 15, and a plurality of secondary air holes 16 are formed in the front ring wall.

なお、18はガスバーナ、27は軸受2,2と
給油座19を支持する支持部材、28はボイラー
本体、29は燃焼カバー、31はエアーダンパー
である。
In addition, 18 is a gas burner, 27 is a support member that supports the bearings 2, 2 and the oil supply seat 19, 28 is a boiler main body, 29 is a combustion cover, and 31 is an air damper.

上記構成からなる実施例装置の動作を以下に説
明する。
The operation of the embodiment device having the above configuration will be explained below.

公知の如く、補助ンク23内の石油の上面レベ
ルは、主給油タンク26、ポンプ25およびオー
バーフロー管24からなる構成により常時所定に
維持されている。
As is well known, the upper surface level of oil in the auxiliary tank 23 is always maintained at a predetermined level by the main oil supply tank 26, pump 25, and overflow pipe 24.

駆動プーリ30の駆動源を駆動することによつ
て元軸1が回転し、これに伴つて回転円板9、遠
心圧力管5、連通管6および蒸発コイル管7も一
体的に回転する。その状態でバルブ21を開とす
る。補助ンク23の石油は管22、給油接手2
0、元軸1の給油孔3を介して遠心圧力管5へと
流入する。遠心圧力管5に流入した石油は、遠心
圧力管5の回転に伴つて生ずる遠心力により順次
回転円板9方向へと送られ、次いで連通管6を介
して蒸発コイル管7内をも満たす。ところで、前
述したように遠心圧力管5および蒸発コイル管7
は巻方向を相逆とするとともに、管径、巻径、お
よび巻回数を同一に設定してあるので、両者の遠
心力から生ずるの管内の圧力は均衡・相殺される
こととなり、ノズル8から石油が洩れることはな
い。
By driving the drive source of the drive pulley 30, the main shaft 1 is rotated, and accordingly, the rotating disk 9, the centrifugal pressure tube 5, the communication tube 6, and the evaporator coil tube 7 are also rotated integrally. In this state, the valve 21 is opened. The oil in the auxiliary tank 23 is connected to the pipe 22 and the oil supply fitting 2.
0, flows into the centrifugal pressure pipe 5 through the oil supply hole 3 of the main shaft 1. The oil flowing into the centrifugal pressure tube 5 is sequentially sent toward the rotating disk 9 by the centrifugal force generated as the centrifugal pressure tube 5 rotates, and then fills the evaporator coil tube 7 via the communication tube 6. By the way, as mentioned above, the centrifugal pressure tube 5 and the evaporator coil tube 7
Since the winding directions are opposite to each other and the pipe diameter, winding diameter, and number of windings are set to be the same, the pressure inside the pipe resulting from the centrifugal force of both is balanced and cancelled, and the pressure from the nozzle 8 is No oil will leak.

この状態でガスバーナ18を点火する。それに
よつてノズル8近傍の蒸発コイル管7巻部分は加
熱され、管内の石油の気化が始まる。石油は気化
して体積が膨脹し、拡散しようとする。しかし、
その拡散は石油の充満している蒸発コイル管7の
図示右方向へ向かうことが許容されないのでノズ
ル8から排出され、燃焼が開始される。
In this state, the gas burner 18 is ignited. As a result, the seven turns of the evaporator coil tube near the nozzle 8 are heated, and the oil in the tube begins to vaporize. Oil vaporizes, expands in volume, and tries to spread out. but,
Since the diffusion of the oil is not allowed to proceed to the right in the drawing of the evaporator coil tube 7 filled with oil, the oil is discharged from the nozzle 8 and combustion begins.

一方、石油が気化、燃焼して消費されると蒸発
コイル管7内の圧力が低下し、遠心圧力管5・蒸
発コイル管7間の圧力の均衡が破れ、それを補償
する形で、遠心圧力管5内の石油が遠心力により
連通管6を介して蒸発コイル管7方向へと流動す
る。
On the other hand, when oil is vaporized and consumed by combustion, the pressure inside the evaporator coil tube 7 decreases, and the pressure balance between the centrifugal pressure tube 5 and the evaporator coil tube 7 is broken, and in order to compensate for this, the centrifugal pressure Petroleum in the tube 5 flows toward the evaporator coil tube 7 via the communication tube 6 due to centrifugal force.

他方、燃焼が開始されると、その熱により蒸発
コイル管7の全長は加熱され、管内の石油の気化
が進んで全長に気化ガスが充満する状態となる
が、蒸発コイル管7に接続する連通管6は断熱円
板13および回転円板9を隔てた位置で元軸の半
径方向へ充分に伸延折曲し、かつ回転して空冷状
態下にあり、従つて当該管内の冷却状態下にある
石油が蒸発コイル管7方向へ向かつて流動してい
るので、気化ガスが連通管6を介して遠心圧力管
5まで逆流する虞はない。
On the other hand, when combustion starts, the entire length of the evaporator coil tube 7 is heated by the heat, and the petroleum inside the tube progresses to vaporization, and the entire length is filled with vaporized gas. The tube 6 is sufficiently extended and bent in the radial direction of the original axis at a position separated by the heat insulating disk 13 and the rotating disk 9, and is rotated and is under an air-cooled condition, so that the inside of the tube is under a cooling condition. Since the oil is flowing in the direction of the evaporator coil tube 7, there is no possibility that the vaporized gas will flow back through the communication tube 6 to the centrifugal pressure tube 5.

かくて、蒸発コイル管7へは石油の補給が円滑
に継続し、補給された石油は蒸発コイル管7内で
完全に気化し、従つてノズル8から気化した石油
のみが排出されることとなり、気化した石油のみ
による燃焼が継続される。
In this way, the supply of oil to the evaporator coil tube 7 continues smoothly, the supplied oil is completely vaporized within the evaporator coil tube 7, and therefore only the vaporized oil is discharged from the nozzle 8. Combustion continues using only vaporized oil.

而して、無段変速機を介して回転する元軸1の
回転速度を変化させれば、当該変化は一体的に回
転する回転円板9、遠心圧力管5および蒸発コイ
ル管7の回転速度を変化させる。回転速度の速め
れば、遠心力の増大、蒸発コイル管7への石油の
補給増大とこれに伴う気化の促進との相関関係、
またノズル8から気化した石油の噴射量の増大と
遠心圧力管5・蒸発コイル管7間の圧力差の増大
という相関関係から燃焼力が大となり、逆に回転
速度を遅くすれば燃焼力が小となる。
Therefore, if the rotational speed of the main shaft 1 that rotates via the continuously variable transmission is changed, the change in the rotational speed of the rotating disk 9, the centrifugal pressure tube 5, and the evaporator coil tube 7 that rotate integrally will change. change. There is a correlation between increasing the rotational speed, increasing centrifugal force, increasing replenishment of oil to the evaporator coil tube 7, and promoting vaporization accordingly.
Furthermore, due to the correlation between an increase in the amount of vaporized oil injected from the nozzle 8 and an increase in the pressure difference between the centrifugal pressure tube 5 and the evaporator coil tube 7, the combustion power increases, and conversely, if the rotation speed is slowed down, the combustion force decreases. becomes.

一方、回転円板9が回転すると、羽根10の働
きで生じた風が送風ケース11の中空部11′に
おける小径部から大径部へと送られ、導風管1
4、風気室15を介して一次空気孔17および二
次空気孔16から噴出し、一次空気孔17から噴
出する風は蒸発コイル管7を冷却したのち燃焼部
への給気となり、二次空気孔16から噴出する風
は燃焼カバー29内を冷却したのち燃焼部の給気
を補完する。従つて蒸発コイル管7の異常昇温が
防止されるとともに、燃焼に必要な給気が充分で
完全燃焼を促進する。而して、回転円板9の回転
速度が速くなればなるほど、即ち燃焼力が増大す
ればするほど、送風ケース11からの送風量が増
大し、燃焼部への給気量および蒸発コイル管7に
対する冷却力が増大する。
On the other hand, when the rotary disk 9 rotates, the wind generated by the action of the blades 10 is sent from the small diameter part to the large diameter part in the hollow part 11' of the blower case 11, and the air guide pipe 1
4. The wind blows out from the primary air hole 17 and the secondary air hole 16 through the air chamber 15, and the wind blows out from the primary air hole 17 cools the evaporator coil tube 7, and then becomes the supply air to the combustion section, and becomes the secondary air. The air blowing out from the air holes 16 cools the inside of the combustion cover 29 and then supplements the air supply to the combustion section. Therefore, abnormal temperature rise of the evaporator coil tube 7 is prevented, and the supply air necessary for combustion is sufficient to promote complete combustion. Therefore, as the rotational speed of the rotating disk 9 becomes faster, that is, as the combustion power increases, the amount of air blown from the air blowing case 11 increases, and the amount of air supplied to the combustion section and the evaporator coil tube 7 increase. cooling power increases.

(考案の作用) 本考案は遠心力を利用し、燃焼開始前には元
軸1、回転円板9、遠心圧力管5、および蒸発コ
イル管7を回転させても、遠心圧力管5管内と蒸
発コイル管7管内の圧力が均衡状態にあつてノズ
ル8から石油を漏らさず、燃焼開始にあたり、
ノズル8からは気化した石油のみを排出して燃焼
を開始し、燃焼中は蒸発コイル管7側の石油の
消費による圧力均衡の破れから、これを補償せん
とする動作によつて蒸発コイル管7側への石油の
潤滑な補給を確保し、かつ燃焼力の増大と補給量
とを連動させる作用がある。また、蒸発コイル管
7とノズル8との位置関係は完全に気化した石
油のみをノズル8から排出して燃焼させる作用が
ある。さらに連通管6の形状ならびに配置構成は
気化した石油の遠心圧力管5方向への逆流防止
とハンチング発生を阻止して石油の円滑な流
動、供給を確保する作用がある。そのうえ、回転
円板9の回転の速さと燃焼力とに相関関係をもた
せているので燃焼部への給気量および蒸発コイ
ル管7に対する冷却力が回転の速さに対応して確
保されるなど、本考案構成が齎す作用は極めて多
様である。
(Function of the invention) The present invention utilizes centrifugal force, and even if the main shaft 1, rotating disk 9, centrifugal pressure tube 5, and evaporator coil tube 7 are rotated before combustion starts, the inside of the centrifugal pressure tube 5 remains When the pressure inside the evaporator coil tube 7 is in a balanced state and no oil leaks from the nozzle 8, combustion starts.
Only vaporized oil is discharged from the nozzle 8 to start combustion, and during combustion, the pressure balance is broken due to oil consumption on the evaporator coil tube 7 side, so the evaporator coil tube 7 is operated to compensate for this. It has the effect of ensuring a lubricated supply of oil to the side and linking the increase in combustion power and the amount of supply. Further, the positional relationship between the evaporator coil tube 7 and the nozzle 8 has the effect of discharging only completely vaporized oil from the nozzle 8 and burning it. Furthermore, the shape and arrangement of the communication pipe 6 have the effect of preventing the backflow of vaporized petroleum in the direction of the centrifugal pressure pipe 5 and preventing the occurrence of hunting, thereby ensuring smooth flow and supply of petroleum. Furthermore, since there is a correlation between the rotational speed of the rotating disk 9 and the combustion power, the amount of air supplied to the combustion section and the cooling power for the evaporator coil tube 7 can be secured in accordance with the rotational speed. The effects of the configuration of the present invention are extremely diverse.

(他の実施例) 上記実施例では、回転円板9を回転させた場合
に遠心力から生ずる遠心圧力管5および蒸発コイ
ル管7の管内の圧力が均衡・相殺されるように、
それぞれの巻回方向を相逆とするとともに、両者
の管径、巻径および巻回数を同一設定としたが、
巻回方向を相逆としたうえで、少なくとも両管内
の圧力が均衡・相殺される条件を満たすならば、
管径、巻径および巻回数を異なる設定としてもよ
く、実施例同様な作用が齎される。
(Other Embodiments) In the above embodiments, when the rotating disk 9 is rotated, the pressure inside the centrifugal pressure tube 5 and the evaporator coil tube 7 caused by centrifugal force is balanced and canceled out.
The respective winding directions were set to be opposite to each other, and the pipe diameter, winding diameter, and number of windings were set to be the same for both.
If the winding directions are reversed and at least the pressure in both tubes is balanced and cancelled, then
The tube diameter, winding diameter, and number of windings may be set differently, and the same effect as that of the embodiment is brought about.

(考案の効果) 本考案によれば、気化した石油のみによる燃焼
が可能であり、かつ給気が充分であるので、不完
全燃焼を生ずることがなく、極めて効率のよい衛
生的な燃焼が確保される。しかも、燃焼力の増
減、およびそれに伴う燃焼部への給気量は無段階
的に自動連動制御可能であり、蒸発コイル管の昇
温は昇温度に応じて自動的に抑えることができる
等、その実用的効果は顕著である。
(Effects of the invention) According to the invention, combustion is possible using only vaporized oil, and since there is sufficient air supply, incomplete combustion does not occur, ensuring highly efficient and sanitary combustion. be done. Moreover, the increase/decrease in combustion power and the accompanying amount of air supplied to the combustion section can be automatically controlled in a stepless manner, and the temperature rise in the evaporator coil tube can be automatically suppressed according to the temperature rise. Its practical effect is remarkable.

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

第1図は本考案の一実施例装置の縦断面図、第
2図は実施例装置の右側面図、第3図は第1図に
おける回転円板と遠心圧力管と連通管との機構的
関係を示す側面図である。 1……元軸、5……遠心圧力管、6……連通
管、7……蒸発コイル管、8……ノズル、9……
回転円板、10……羽根、11……送風ケース、
14……導風管、15……風気室、16,17…
…空気孔。
FIG. 1 is a longitudinal sectional view of an embodiment of the device of the present invention, FIG. 2 is a right side view of the embodiment device, and FIG. 3 is a mechanical diagram of the rotating disk, centrifugal pressure tube, and communication tube in FIG. 1. FIG. 3 is a side view showing the relationship. 1... Base shaft, 5... Centrifugal pressure tube, 6... Communication tube, 7... Evaporation coil tube, 8... Nozzle, 9...
Rotating disk, 10...Blade, 11...Blower case,
14... Air guide pipe, 15... Air chamber, 16, 17...
...Air hole.

Claims (1)

【実用新案登録請求の範囲】[Scope of utility model registration request] 回転円板と、回転円板の一側に枢着される元軸
と、元軸に固定されてその外周を複数巻回する遠
心圧力管と、回転円板の他側に巻回中心線を遠心
圧力管と同一水平レベルとして配置され、かつ遠
心圧力管の巻方向とは逆巻に複数巻回した蒸発コ
イル管と、遠心圧力管・蒸発コイル管間を接続す
る連通管とを具え、上記遠心圧力管は回転円板反
対方向端を給油源に連通可能に構成し、上記蒸発
コイル管は回転円板近接側の端部を巻回中心方向
へ曲げて巻回軸線に至らしめ、その先端に軸線上
他側方向へ口を向けるノズルを装着し、上記連通
管は遠心圧力管の回転円板側端部との接続部から
回転円板の表面沿いに元軸の半径方向へU字を描
いて伸延、折曲したうえ所定位置で回転円板を貫
通して蒸発コイル管におけるノズル反対端に接続
し、上記回転円板の一側表面の周部に所定間隔を
へだてて羽根を装着し、回転円板の周縁に沿つて
中空状の送風ケースを設け、上記送風ケースを導
風管を介して蒸発コイル管を巻回する中空環状の
風気室に接続し、上記風気室に風気孔を設けてな
り、回転円板を回転した際、回転する遠心圧力管
および蒸発コイル管それぞれの管内の遠心力に起
因して生ずる圧力が均衡・相殺される如く、それ
ぞれ管径、巻径および巻回数を所定に設定したこ
とを特徴とする回転加圧式石油バーナー。
A rotating disk, a base shaft pivotally mounted on one side of the rotating disk, a centrifugal pressure tube fixed to the base shaft and wound around its outer circumference multiple times, and a winding center line on the other side of the rotating disk. The above-mentioned method comprises an evaporator coil tube arranged on the same horizontal level as the centrifugal pressure tube and wound in a plurality of turns in a direction opposite to the winding direction of the centrifugal pressure tube, and a communication tube connecting the centrifugal pressure tube and the evaporator coil tube. The centrifugal pressure tube is configured such that the end opposite to the rotating disk can communicate with the oil supply source, and the evaporator coil tube has its end near the rotating disk bent toward the winding center to reach the winding axis, and the end thereof is bent toward the winding center. A nozzle with its mouth directed toward the other side on the axis is attached, and the communicating tube is formed in a U-shape along the surface of the rotating disk from the connection point with the end of the centrifugal pressure tube on the rotating disk side in the radial direction of the original axis. After drawing, stretching, and bending, the blade is passed through the rotating disk at a predetermined position and connected to the opposite end of the nozzle in the evaporator coil tube, and blades are attached at a predetermined interval to the circumference of one side of the rotating disk. A hollow air blowing case is provided along the periphery of the rotating disk, and the air blowing case is connected to a hollow annular air chamber around which an evaporator coil tube is wound through an air guide pipe, and air is supplied to the air chamber. The tube diameter, winding diameter and A rotary pressurized oil burner characterized by a predetermined number of turns.
JP14234984U 1984-09-21 1984-09-21 Expired JPH0229394Y2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP14234984U JPH0229394Y2 (en) 1984-09-21 1984-09-21

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP14234984U JPH0229394Y2 (en) 1984-09-21 1984-09-21

Publications (2)

Publication Number Publication Date
JPS6158524U JPS6158524U (en) 1986-04-19
JPH0229394Y2 true JPH0229394Y2 (en) 1990-08-07

Family

ID=30700673

Family Applications (1)

Application Number Title Priority Date Filing Date
JP14234984U Expired JPH0229394Y2 (en) 1984-09-21 1984-09-21

Country Status (1)

Country Link
JP (1) JPH0229394Y2 (en)

Also Published As

Publication number Publication date
JPS6158524U (en) 1986-04-19

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