JPH0688585A - Aerator with large diametral pipe body solid moving blade - Google Patents

Aerator with large diametral pipe body solid moving blade

Info

Publication number
JPH0688585A
JPH0688585A JP3155599A JP15559991A JPH0688585A JP H0688585 A JPH0688585 A JP H0688585A JP 3155599 A JP3155599 A JP 3155599A JP 15559991 A JP15559991 A JP 15559991A JP H0688585 A JPH0688585 A JP H0688585A
Authority
JP
Japan
Prior art keywords
air
flow
water
water flow
diameter
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Pending
Application number
JP3155599A
Other languages
Japanese (ja)
Inventor
正志 ▲土▼田
Masashi Tsuchida
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to JP3155599A priority Critical patent/JPH0688585A/en
Publication of JPH0688585A publication Critical patent/JPH0688585A/en
Pending legal-status Critical Current

Links

Abstract

PURPOSE:To provide an aerator consisting of a stirring simultaneous aerating system for liquid raising the flow velocity and penetration of a water current. CONSTITUTION:A large diametral pipe body connected to a turning shaft in a concentric state is connected to the turning center in the concentric direction, while it is formed into such a structure as submerging the one end in the water even at the lowest, and further it is formed into a construction that installs a spiral or wingy blade part 1 in an inner wall of the large diametral pipe body at the submerged side. Diagonal water currents other than the propulsive direction in the case where moment in time of rotation is added to the blade part are concentrated on the center of the pipe body, and it is also formed into such a structure as amplifying a flow as a water current or muddy stream, etc., structuring the large diametral pipe body on one side as a water current exhaust nozzle, through which a water inlet port 2 is installed in the pipe and simultaneously an air inflow port 15 for letting air flow in is also installed there. Likewise it is also structured to utilize a difference of water currents produced as the blade part produces the water current forcibly, and then a pressure differential is produced and it is structured to draw in air compulsorily.

Description

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

【0001】[0001]

【産業上の利用分野】本発明は、大径管体内の各羽根部
が水切り時に生成させる水流の流方向を拡散させずに中
心部へ集中させて相乗効果を利用しながら水流の流速と
貫通力を強める液体用の攪拌同時曝気方式の曝気装置で
あり、水流の流速によってエアの吸引力をも強める大径
管体一体回転羽根をもつ曝気装置である。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to the flow velocity and penetration of water flow while utilizing the synergistic effect by concentrating the flow direction of the water flow generated at the time of draining water in the large-diameter pipe body to the central part without diffusing it. This is an aerator of the stirring simultaneous aeration system for liquids that strengthens the force, and an aerator with a large-diameter tube-integrated rotary blade that also enhances the suction force of air by the flow velocity of the water flow.

【0002】[0002]

【従 来 技 術】従来、浄化槽へエアを吹き込む場合
にブロワーなどで強制的に気体を圧搾することによって
曝気を行なう方法が存在するが、効率的な曝気という点
では問題があり、圧搾による曝気方法は、ピストン方式
であれロータリー方式であれ、またはダイヤフラムによ
るものであっても、まず、伸縮性が大きい特性をもつ気
体自体を圧縮すること自体に問題があり、特に水圧のか
かった深部へしかも、細いパイプの一端からの圧縮によ
って曝気を行なうこと自体にも問題があり、効率面での
悪さが指摘される。またピストン方式やロータリー方式
はそれ自体の反転または回転運動の際に摩擦熱が発生し
て、そのぶんエネルギー・ロスとなり大変曝気効率の低
い方式であった。
[Prior art] Conventionally, there is a method of performing aeration by forcibly compressing gas with a blower or the like when blowing air into the septic tank, but there is a problem in terms of efficient aeration, and aeration by compression Whether the method is a piston method, a rotary method, or a diaphragm method, first of all, there is a problem in compressing the gas itself, which has the property of large elasticity, and especially to a deep area where water pressure is applied. However, there is also a problem in performing aeration by compressing from one end of a thin pipe, and it is pointed out that the efficiency is poor. Further, the piston system and the rotary system are systems with extremely low aeration efficiency because frictional heat is generated during the reversal or rotary motion of the piston system, resulting in energy loss.

【0003】[0003]

【発明が解決しようとする問題点】そこで、スクリュー
などによるエア吸引方式の曝気装置が存在する。これは
船のスクリューなどの回転を利用して水中で軸方向へ強
制的に水流を発生させて、該軸方向へ生成された水流の
流速なたは渦流を利用して同回転軸の端部よりエアを従
来とは逆に吸引させようとするものであり、この方式に
よれば伸縮性の大きい気体は逆に伸びた状態となって水
中へ吸引されながら同時に水流の流速によって気泡を微
細化させることができる画期的な曝気方式である。
Therefore, there is an aerator of the air suction type using a screw or the like. This is because the rotation of a ship's screw is used to forcibly generate a water flow in the axial direction in water, and the flow velocity or vortex of the water flow generated in the axial direction is used to end the end of the rotation shaft. In this method, the air is sucked in the opposite direction to the conventional one. According to this method, a highly elastic gas is expanded into the opposite state and is sucked into the water, while at the same time, the bubbles are made fine by the flow velocity of the water flow. This is an epoch-making aeration method that can be performed.

【0004】が、しかし本発明者はこの方式を実験する
うちに生成される水流が末広がりに急拡散して弱いもの
となっていくことに気付いた。それはさらに水流中へ噴
出されたエアが混和されることにより一層水流の流速に
ブレーキをかけて、しかもエアが多量に浮上することで
も水流の貫通力を弱める結果となるものであった。そこ
で本発明者は、このような羽根部によって生成される水
流が急激に末広がりに減衰される原因は従来スクリュー
型の羽根部に問題があるものと考えた。つまり羽根部の
回転によって水が切られて軸方向への推進水流と同時に
渦流が生成されるが、この時の羽根部に切られる瞬間の
水には軸芯方向への力モーメントと同時に回転モーメン
トが加わり、この為生成される水流はどうしても斜め方
向水流を発生させる結果、どうしても渦流が放射方向の
末広がり状に拡散される結果になる訳であることが判か
った
However, the inventor of the present invention has found that during the experiment of this system, the water flow generated suddenly spreads toward the end and becomes weak. Further, the air jetted into the water flow further mixes the brakes to the flow velocity of the water flow, and more air floats, resulting in a weaker penetrating force of the water flow. Therefore, the present inventor considered that the reason why the water flow generated by such a blade portion is rapidly and divergently attenuated is that the conventional screw type blade portion has a problem. In other words, the water is cut off by the rotation of the blades and a swirl is generated at the same time as the propelling water flow in the axial direction, but at this moment the water at the moment of being cut by the blades has a rotational moment as well as a force moment in the axial direction. It was found that the resulting water flow inevitably generated an oblique water flow, resulting in the eddy current being diffused in a radial divergent manner.

【0005】[0005]

【問題点を解決しようとする手段】そこで本発明は、従
来船のスクリュー型のような形状の羽根部を配置とは全
く異なる構造にすることで生成する水流を点中心に向か
って集中させるものとしたことにより従来の問題点を解
決するもので、その構造を図面を参照しながら詳述すれ
ば次のとおりとなる。
In view of the above, the present invention concentrates the water flow generated toward the center of the point by making the structure of the blade portion of the screw type of the conventional ship completely different from the arrangement. By doing so, the conventional problems can be solved, and the structure thereof will be described below in detail with reference to the drawings.

【0006】動力につながる回転軸と同軸状態で連結さ
れた大径管体3を設けて、大径管体3は該回転軸の回転
中心と同芯方向で連結される構造として、大径管体3の
最低でも一端を水中へ潜没させる構造として、該潜没側
の大径管体3内壁にはラセン状または翼状の羽根部1を
突設させる構造として、羽根部1へ回転時のモーメント
が加わった場合の推進方向以外の斜め方向水流を大径管
体3中心で集中させる構造として、該水流または渦流な
どの流れを推進方向へ増幅する構造として、大径管体3
の一方を水流噴出口とする構造として、大径管体3の管
内へ水取り入れ口2を設けると同時にエアを流入させる
為のエア流入口4をも設けて、羽根部1が強制的に水流
を発生させる構造としながら、発生した水流の流れの差
を利用する構造とすることで圧力差を発生させて、エア
を強制的に吸引する構造とした。
A large-diameter pipe 3 is provided which is connected coaxially with a rotating shaft connected to power, and the large-diameter pipe 3 is connected to the rotation center of the rotating shaft in a concentric direction. As a structure in which at least one end of the body 3 is submerged in water, a spiral or wing-shaped blade portion 1 is projected on the inner wall of the large-diameter tubular body 3 on the submerged side. As a structure for concentrating a diagonal water flow other than the propulsion direction when a moment is applied at the center of the large diameter pipe body 3, as a structure for amplifying the flow such as the water flow or vortex flow in the propulsion direction, the large diameter pipe body 3
As a structure in which one of them is used as a water jet outlet, a water intake port 2 is provided in the pipe of the large-diameter tubular body 3 and at the same time, an air inlet port 4 for allowing air to flow in is also provided so that the blade portion 1 forcibly flows the water. In addition to the structure for generating air, a structure for utilizing the difference in the generated water flow is used to generate a pressure difference and forcibly suck air.

【0007】大径管体3と羽根部1が回転する構造とす
ることで、大径管体3内へ流入した水を強制的に回転さ
せる構造として同時に、水流が回転することで渦流を発
生させる構造として、大径管体3内の該渦流により発生
する渦巻きをエア通路15に利用する構造として、エア
通路15とエア流入口4とを連通せしめた構造とした。
With the structure in which the large-diameter pipe 3 and the blade portion 1 rotate, the water flowing into the large-diameter pipe 3 is forcibly rotated, and at the same time, the water flow rotates to generate a vortex. As the structure to be used, the structure in which the vortex generated by the vortex in the large-diameter tubular body 3 is used in the air passage 15 is a structure in which the air passage 15 and the air inlet 4 are communicated with each other.

【0008】大径管体3の中心部にエア導入パイプ11
を設ける構造として、導入パイプ11中の中空部はエア
流入口4と連通される構造として、導入パイプ11は大
径管体3中を延設されながら羽根部1付近でエア噴出孔
部10を持つ構造として、水流の流速と渦流または乱流
の働きによる圧力差を利用してエアを吸引させる構造と
した。
An air introduction pipe 11 is provided at the center of the large-diameter pipe body 3.
As a structure in which the hollow portion in the introduction pipe 11 is communicated with the air inlet 4, the introduction pipe 11 is extended in the large-diameter pipe body 3 and has an air ejection hole portion 10 near the blade portion 1. The structure has a structure in which air is sucked by utilizing the pressure difference due to the flow velocity of water flow and the action of vortex or turbulence.

【0009】大径管体3に設けた羽根部1の表面部また
は表面部付近の導入パイプ11などへ噴出孔部10を形
成して、羽根部1が水を切る段階で生じる羽根流れの差
を利用する構造として、該流れの差により圧力差を発生
する構造として、中空状羽根部1の中または該表面部付
近の噴出孔部10までエア通路15を連通させて、噴出
孔部10からエア通路15を介してエア流入口4まで連
通させる構造として、羽根部1が水切り運動を行なう時
点で発生した圧力差を利用する構造として、該噴出孔部
10よりエアを吸引させる構造とした
A difference in blade flow generated when the blade portion 1 drains water by forming the ejection hole portion 10 in the surface of the blade portion 1 provided in the large-diameter tubular body 3 or in the introduction pipe 11 or the like near the surface portion. As a structure for generating a pressure difference due to the flow difference, the air passage 15 is communicated to the ejection hole portion 10 in the hollow blade portion 1 or in the vicinity of the surface portion, and The structure for communicating with the air inlet 4 through the air passage 15 is a structure for utilizing the pressure difference generated at the time when the blade portion 1 performs the draining motion, and the structure for sucking air from the ejection hole portion 10.

【0010】大径管体3に設けた羽根部1へ水流の流方
向に対して立ち上がり部分13形成構造にしながら、立
ち上がり部分13を羽根幅方向へ延設させて、羽根部1
の根元または先端付近に設けた噴出孔部10より水流の
圧力差を利用してエアを羽根幅方向へ吸引させる構造と
して、該エアの吸引方法に立ち上がり部分13による水
流の圧力差発生構造とした。
The rising portion 13 is formed in the blade width direction in the blade portion 1 provided in the large-diameter tubular body 3 while forming the rising portion 13 in the flow direction of the water flow.
As the structure for sucking air in the width direction of the blade by utilizing the pressure difference of the water flow from the jet hole portion 10 provided near the root or the tip of the nozzle, the structure for generating the pressure difference of the water flow by the rising portion 13 is adopted in the air suction method. .

【0011】[0011]

【作 用】本発明は、従来スクリュー型のような、回
転軸の先端へ放射状に羽根部1が突設されることによる
水流の発生方法とは全く異なる生成構造であり、絶対的
に相違する本発明の特徴は、大径管体3の内壁に突設さ
れた羽根部1が互いの間で生成させた水流を中心部へ集
中させることで水流の相乗効果を利用して流速と貫通力
を強めるものであり、とくに羽根部1の回転によって水
流が生成された時のその力成分は、まず水が切られて軸
方向への推進水流と同時に渦流が生成されるが、この時
の羽根部1に切られる瞬間の水には軸芯方向への力モー
メントと同時に回転モーメントが加わり、この為生成さ
れる水流は末広がり状の渦流となる力方向成分である斜
め方向水流が生成されるが、本発明の構造はこの斜め方
向水流を大径管体3の中心部で集めることでラセン状に
生成される水流のうち斜め水流どうしの中心部への押し
合い作用で推進方向への力を取り出すように矯正させる
ものである。またその為の構造上の重要な違いとしては
特に羽根部1を形成させる方向が根本的に異なる。つま
り、羽根部1を形成させる方向をある物体より放射方向
に突設させる従来構造に対して、本発明はある物体より
突設させる方向を点中心方向へ向かう構造としたことの
違いによる。したがって該ある物体が従来では棒(シャ
フト)状回転体であるのに対して、本発明は大径管状回
転体がその構造上から絶対に必要となる。ところで本発
明の羽根部1はラセン状でも翼状でもどのようなもので
もよいし、羽根部1の数も問題でなく、例えばラセン羽
根一枚が大径管体3内側に巻き付くように突設されたも
のでも良い。
[Operation] The present invention has a completely different generation structure from the conventional screw type, which is different from the water flow generation method in which the blade portions 1 are radially projected to the tip of the rotary shaft, and is absolutely different. The feature of the present invention is that the vane portions 1 projecting from the inner wall of the large-diameter tubular body 3 concentrate the water flow generated between them to the central portion to utilize the synergistic effect of the water flow and the flow velocity and the penetration force. In particular, the force component when the water flow is generated by the rotation of the blade portion 1 is that the water is first cut off and the swirling flow is generated at the same time as the propelling water flow in the axial direction. At the moment when the water is cut into the part 1, a rotational moment is applied at the same time as a force moment in the axial direction, and thus the generated water flow is an oblique water flow which is a force direction component that becomes a divergent eddy current. In the structure of the present invention, this diagonal water flow is applied to the large-diameter pipe body 3. Among the water streams generated in a spiral shape by collecting at the central portion, the diagonal water streams are pressed against each other to the central portion to correct the force in the propulsion direction. Further, as an important structural difference for that purpose, the direction in which the blade portion 1 is formed is fundamentally different. In other words, the present invention is different from the conventional structure in which the direction in which the blade portion 1 is formed is projected in the radial direction from a certain object, and the present invention is configured so that the direction in which the blade 1 is projected is directed toward the point center direction. Therefore, while the certain object is conventionally a rod (shaft) -shaped rotating body, the present invention absolutely requires a large-diameter tubular rotating body because of its structure. By the way, the blade portion 1 of the present invention may have any shape such as a spiral shape or a blade shape, and the number of the blade portions 1 does not matter, and for example, one spiral blade is projected so as to wind around the inside of the large-diameter tube body 3. It may be the one that was given.

【0012】さらに本発明は、該発生した水流の流れの
差を利用する構造とすることで圧力差を発生させてエア
を強制的に吸引するものであり、その吸引方法には
Further, according to the present invention, a pressure difference is generated to forcibly suck air by using a structure that utilizes the difference in the generated water flow.

【請求項2】のように大径管体3内へ流入した水を強制
的に回転させる構造として同時に羽根部1が回転するこ
とで水が強制旋回されて渦流が大径管体3内で発生する
が、この時に大径管体3内に渦巻きも発生されて渦の中
心部では水面が吸引されてゆき羽根部1までのエア通路
15が徐々に形成されることになり、羽根部1まで吸引
されたエアはそこで破砕されて大径管体3より噴出され
る。つまり、渦巻きをエア通路15として利用するもの
である。
2. A structure for forcibly rotating the water flowing into the large-diameter pipe body 3 as described above, the water is forcibly swirled by the rotation of the blade portion 1 at the same time, and a vortex flow is generated in the large-diameter pipe body 3. Although generated, at this time, a vortex is also generated in the large-diameter tube body 3, the water surface is sucked at the center of the vortex, and the air passage 15 to the blade portion 1 is gradually formed, and the blade portion 1 The air sucked up to is crushed there and ejected from the large-diameter pipe body 3. That is, the spiral is used as the air passage 15.

【0013】また本発明のAlso according to the present invention

【請求項3】は前記渦巻き利用方法とは別の働きを利用
してエアを供給するものであり、これは渦巻きからの吸
引のような不規則な要素を無くしたものである。つまり
これは 該大径管体3の中心部にエア導入パイプ11を
設けて、その中の中空部をエア通路15として利用する
ものであり、導入パイプ11の太さや長さはどのような
ものでも良く、羽根部1によって強制的に水流を発生さ
せて、該水流の流速または羽根部1廻りに発生した水流
の圧力差と更に生成された渦流中心部の圧力差を利用し
て導入パイプ11の噴出孔部10よりエアを噴出させる
ものであるが、噴出孔部10の数や大きさ、導入パイプ
11に形成させる位置も問題でない。
3. A method for supplying air by utilizing a function different from the method of utilizing a spiral, which eliminates irregular elements such as suction from the spiral. In other words, this is to provide the air introduction pipe 11 in the central portion of the large-diameter pipe body 3 and use the hollow portion therein as the air passage 15. What is the thickness and length of the introduction pipe 11? However, the water flow may be forcibly generated by the blade portion 1, and the introduction pipe 11 may be used by utilizing the flow velocity of the water flow or the pressure difference between the water flow generated around the blade portion 1 and the generated pressure difference at the center of the vortex flow. Although the air is ejected from the ejection hole portion 10, the number and size of the ejection hole portions 10 and the position where the introduction pipe 11 is formed do not matter.

【0014】さらに本発明のFurther of the present invention

【請求項4】のように羽根部1が水を切る時点で発生す
る圧力差を利用して羽根部1の表面部または表面部付近
の導入パイプ11などへ噴出孔部10を形成させて、噴
出孔部10よりエアを吸引させる構造としたものである
が、羽根部1が迎角をもって回転運動する場合に水を切
って水流を発生させる部分は羽根部1腹面部16である
が、背面部17へ廻った水流にも出来るだけ乱れを生じ
させずに再び後縁部18にて腹面部16との流れと合流
させるようにして流れの差を発生させる流線形状とする
ことで船の推進力や飛行機であれば揚力を発生させるも
のであるが、本発明はエア吸引方法に該流線形状物を流
れる流体の原理のように水流をできるだけ整流させるよ
うにして流速を強めてやることで発生する圧力差を増加
させてエア噴出量を増やす方法が一つあり、また該原理
とは全く逆の吸引原理である背面部を流れる水流の流体
抵抗を出来るだけ増加させるようにして乱流を発生させ
て該乱流の持つ不規則な圧力差からエアを吸引させるも
のでもどちらも良いが、乱流による吸引原理はその欠点
として、水流の流速が高まらない特徴をもち、いくら回
転数を高めても乱流が原因で水流の流速が高まらず、圧
力差も増加せず、その分だけエアの吸引力も増加しない
ものとなるがこの方法でも良い。ところで羽根部1表面
部を流れる水流に圧力差を発生させる形状にしながら、
しかも羽根部1が水を切る時点でエアを水流の力で吸引
させる構造としたものであるが、この水切り時でのエア
の吸引方法には・腹面部16へ洗濯板状の段差を設けて
該立ち上がり部分または窪んだ部分にエア噴出孔部10
を設ける方法。・先端縁部18付近へ噴出孔部10を形
成させて従来スクリューの最も圧力差の発生するキャビ
テーション発生部分に噴出孔部10を設ける方法。・後
縁部18に噴出孔部10を設ける方法。・背面部17に
噴出孔部10を設ける方法。・背面部17または後縁部
18の付近に導入パイプ11を突設させてエアを噴出さ
せる方法。などがありどの方法によっても良い。これは
本出願人が従来スクリュー型曝気装置の新曝気方法とし
て出願した特許願62−016634号、同62−11
1366号、同平成2−254693号の羽根面噴出方
式の曝気装置の技術である。
4. The jet hole portion 10 is formed on the surface portion of the blade portion 1 or the introduction pipe 11 or the like near the surface portion by utilizing the pressure difference generated when the blade portion 1 cuts water. Although the structure for sucking air from the ejection hole portion 10 is used, when the blade portion 1 makes a rotational movement at an angle of attack, the portion that cuts off water to generate a water flow is the blade portion 1 ventral surface portion 16, but By creating a streamlined shape that creates a flow difference by causing the water flowing to the part 17 to be turbulent as much as possible and to join the flow with the abdominal part 16 again at the trailing edge 18 The propulsion force or the lift force is generated in the case of an airplane, but the present invention is to increase the flow velocity by rectifying the water flow as much as possible in the air suction method like the principle of the fluid flowing through the streamlined object. The air pressure is increased by increasing the pressure difference generated at There is one way to increase it, and it is a suction principle that is completely opposite to the above principle.The irregular pressure of the turbulent flow is generated by generating turbulent flow by increasing the fluid resistance of the water flow flowing through the back surface as much as possible. Although it is possible to suck air from the difference, the suction principle by turbulence has the disadvantage that the flow velocity of the water flow does not increase, and even if the rotation speed is increased, the flow velocity of the water flow increases due to the turbulence. However, the pressure difference does not increase, and the suction force of the air does not increase correspondingly. However, this method may be used. By the way, while making the water flow flowing on the surface of the blade 1 a pressure difference,
Moreover, the structure is such that the air is sucked by the force of the water flow when the blade portion 1 drains water. The method of sucking the air at the time of draining water is to provide a washing plate-like step on the abdominal surface portion 16. The air ejection hole portion 10 is provided at the rising portion or the depressed portion.
How to provide. A method in which the ejection hole portion 10 is formed near the tip edge portion 18 and the ejection hole portion 10 is provided in the cavitation generation portion of the conventional screw where the pressure difference occurs most. A method of providing the ejection hole portion 10 on the rear edge portion 18. A method of providing the ejection hole portion 10 on the back surface portion 17. A method of ejecting air by projecting the introduction pipe 11 near the back surface portion 17 or the rear edge portion 18. Etc. and any method is acceptable. This is the patent application Nos. 62-016634 and 62-11 filed by the present applicant as a new aeration method for a conventional screw type aeration apparatus.
This is the technology of the blade surface jet aeration device of No. 1366 and No. 2-254693 of Heisei.

【0015】その他エアの噴出方法にはOther methods for ejecting air

【請求項5】のように羽根部1の背面部17を流れる水
流の流方向に対して立ち上がり部分13を形成する構造
にしながら、羽根部1の根元または先端付近に設けた噴
出孔部10より水流の圧力差を利用してエアを羽根幅方
向へ吸引させる構造として、該エアの吸引方法に立ち上
がり部分13による水流の圧力差を発生させる構造とす
ることにより、背面流が立ち上がり部分13を流れる場
合、羽根幅方向に渦を発生するが、該渦の吸引力によっ
て噴出孔部10より強制的にエアを吸引させるものであ
るが、立ち上がり部分13は該渦を発生させるだけでな
く、更に背面流の流速を早めていくと表面剥離現象を発
生させる。この表面剥離現象は立ち上がり部分13に添
って自然に空隙が形成されるものであり、本発明はこの
空隙をエア通路に利用するものでもあるが、該空隙内に
噴出されたエアは水流に吸引されながらも立ち上がり部
分13の先端方向まで吸引されて結果的に背面部17全
面より万遍なくエアを噴出させることになる。この意味
で本発明は立ち上がり部分13を形成させることにより
「羽根幅方向への渦流を利用する構造」であるとも言え
るし、同時に「表面剥離による空隙利用構造」であると
も言えるものである。また本発明は羽根部1の後縁部1
8をクサビ形状として切り立たせて立ち上がり部分13
に相当させて渦発生構造とするもので噴出孔部10より
エアを吸引させるものでも良い。さらに「渦流利用構造
や表面剥離による空隙利用構造」でもある本発明は「圧
力差利用構造」であるということからも例えば「段差を
付けた構造」であっても本発明の「立ち上がり部分」で
あるといえる。これは本出願人が従来スクリュー型曝気
装置の新曝気方法として出願した特許願平成2−417
929号の衝立構造利用方式の曝気装置の技術である。
5. The jet hole portion 10 provided near the root or tip of the blade portion 1 while having the structure in which the rising portion 13 is formed in the flow direction of the water flow flowing through the back surface portion 17 of the blade portion 1 as described above. The back flow flows through the rising portion 13 by using the structure for sucking the air in the width direction of the blade by utilizing the pressure difference of the water flow and the structure for generating the pressure difference of the water flow by the rising portion 13 in the air suction method. In this case, a vortex is generated in the blade width direction, and the suction force of the vortex is used to forcibly suck air from the ejection hole portion 10. However, the rising portion 13 not only generates the vortex, but also the rear surface. The surface separation phenomenon occurs when the flow velocity is increased. This surface peeling phenomenon is that a void is naturally formed along the rising portion 13, and the present invention uses this void as an air passage, but the air jetted into the void is sucked into the water flow. While being carried out, it is sucked up to the front end direction of the rising portion 13 and as a result air is evenly ejected from the entire back surface portion 17. In this sense, the present invention can be said to be a “structure that utilizes a vortex flow in the blade width direction” by forming the rising portion 13, and at the same time a “structure that utilizes voids due to surface separation”. Further, the present invention is directed to the trailing edge portion 1 of the blade portion 1.
8 is cut into a wedge shape to stand up and rise 13
The structure may be a vortex generating structure corresponding to the above, and air may be sucked from the ejection hole portion 10. Furthermore, since the present invention, which is also a “vortex flow utilizing structure or a void utilizing structure due to surface separation”, is a “pressure difference utilizing structure”, for example, even a “stepped structure” is a “rise portion” of the present invention. It can be said that there is. This is a patent application filed by the applicant of the present invention as a new aeration method for a conventional screw type aeration device.
This is the technology for the aeration device of the partition structure type 929.

【0016】[0016]

【実施例】【Example】

【図1】は本発明の第1実施例を示す断面斜視図。本図
FIG. 1 is a sectional perspective view showing a first embodiment of the present invention. This figure is

【請求項1】1.

【請求項2】の特徴を備えた曝気装置であるが、大径管
体3の水取り入れ口2へ耳部12を取り付けてより多く
の水が管内へ流入するものでも良い。また本装置の固定
方法はモーター部9と軸支持部6によっているが軸支持
部6を省略してモーター部9のみで支持するものでも良
い。さらに本図ではモーター部9からの動力をスプリン
グなどの自在継ぎ手7によって大径管体3まで伝達して
いるが、この構造を省略して直接モーター部9からジョ
イント部8を介して大径管体3へ動力を伝えるものでも
良い。また本発明のエア曝気方法には従来、回転軸を中
空構造にしてエア通路15として用いたような通路用の
構造材料を全く必要とせずに、管内で自然に発生する渦
巻きをエア通路15として利用するものでありエア通路
15の為の構造材料が全く不要である。ところで本発明
は羽根部1がラセン状でも翼状でも水流を発生したり圧
力差を発生したりするものであればどのような形状でも
良い。
2. An aeration device having the characteristics of claim 2, but a large amount of water may flow into the pipe by attaching an ear portion 12 to the water intake port 2 of the large diameter pipe body 3. Further, the fixing method of this device depends on the motor portion 9 and the shaft supporting portion 6, but the shaft supporting portion 6 may be omitted and the motor portion 9 alone may be used for supporting. Further, in this figure, the power from the motor unit 9 is transmitted to the large-diameter pipe body 3 by the universal joint 7 such as a spring, but this structure is omitted and the large-diameter pipe body is directly passed from the motor unit 9 through the joint unit 8. It may be one that transmits power to the body 3. In addition, the air aeration method of the present invention does not require any structural material for the passage, which has conventionally been used as the air passage 15 by making the rotating shaft a hollow structure, and uses the vortex naturally generated in the pipe as the air passage 15. Since it is used, no structural material is needed for the air passage 15. By the way, the present invention may have any shape as long as the blade portion 1 has a spiral shape or a blade shape as long as it generates a water flow or a pressure difference.

【0017】さらにFurther

【図1】第1実施例の曝気装置は一部分ごとにさまざま
な展開をさせることができるもので、仕様図A、B、
C、D、E、F図としてそれぞれ展開状態を示したもの
であり、仕様図AおよびB図が導入パイプを設けた場合
の断面斜視図を示し、仕様図C、D、E、F図はそれぞ
れ羽根部1の断面斜視図を示す。
FIG. 1 is an aeration apparatus according to a first embodiment that can be developed in various ways in each part.
C, D, E, and F are developed views, respectively, and the specification diagrams A and B are cross-sectional perspective views when an introduction pipe is provided, and the specification diagrams C, D, E, and F are The cross-sectional perspective view of the blade part 1 is shown, respectively.

【0018】仕様図AはThe specification diagram A is

【請求項3】の特徴を備えたものであり、導入パイプ1
1を大径管体3の中心部に設けたもので、
3. An introduction pipe 1 having the characteristics of claim 3.
1 is provided at the center of the large-diameter tubular body 3,

【請求項2】のような渦巻きをエア通路15として利用
するのでなく専門の導入パイプ11を設けてエア通路1
5として使用し、噴出孔部10より水中へ吸引させるも
のであるが、この場合の導入パイプ11の長さは問題で
ないし、噴出孔部10の位置も問題でない。
2. A special introduction pipe 11 is provided instead of using such a spiral as the air passage 15, and the air passage 1 is provided.
It is used as No. 5 and is sucked into water through the ejection hole portion 10. However, the length of the introduction pipe 11 in this case does not matter, and the position of the ejection hole portion 10 does not matter either.

【0019】仕様図Bは導入パイプ11より供給される
エアは、突設させた羽根部1の裏側にあるエア通路15
を通って羽根部1の根元の噴出孔部10より背面上の水
中へ吸引されるが、羽根部1の構造はラセン状でありな
がら、
In the specification diagram B, the air supplied from the introduction pipe 11 is supplied to the air passage 15 on the back side of the protruding blade portion 1.
Although it is sucked into the water on the back surface from the ejection hole portion 10 at the base of the blade portion 1, though the structure of the blade portion 1 is spiral,

【請求項5】のような羽根部1の立ち上がり部分13を
段差状として背面部17にもち、背面流に乱流や表面剥
離現象を発生させて羽根部1根元に形成させた噴出孔部
10よりエアを吸引させるものである。
5. A jetting hole portion 10 formed at the base of the blade portion 1 by having the rising portion 13 of the blade portion 1 as a stepped shape on the back surface portion 17 and causing turbulent flow or surface separation phenomenon in the back flow. More air is sucked in.

【0020】仕様図CはSpecifications C is

【請求項4】の特徴を備えたものであり、羽根部1の中
を中空状態にしながら該表面部にエア噴出孔部10を形
成することでエア通路15を介してエア流入口4まで連
通させたものであり、 図面は丁度羽根部1の背面部1
7および縁部18に噴出孔部10を形成させたものであ
り、水を切る場合の背面部17に廻り込む水流が再び後
縁部18で合流される時に圧力差の為に流れの差が生ず
るが、本項ではこの流れの差のうち背面部17に発生す
る力には該表面部を上方へ引っ張る力が発生することに
なり、背面部17の噴出孔部10からは効率良くエアが
噴出されるものとなる。また羽根部1の先端縁部18に
噴出孔部10を設けることによってキャビテーションな
どの最も圧力差が発生し易いところに噴出孔部10を設
けてもいる。
4. An air ejection hole portion 10 is formed on the surface of the blade portion 1 while the inside of the blade portion 1 is hollow so as to communicate with the air inlet 4 through an air passage 15. The drawing is just the back part 1 of the blade part 1.
7 and the edge portion 18 are formed with the ejection hole portion 10, and when the water flow that flows around the back surface portion 17 when draining water is merged again at the trailing edge portion 18, a difference in flow is caused by a pressure difference. However, in this section, in this flow difference, the force generated in the rear surface portion 17 is a force that pulls the surface portion upward, so that air is efficiently generated from the ejection hole portion 10 of the rear surface portion 17. It will be ejected. Further, by providing the ejection hole portion 10 at the tip edge portion 18 of the blade portion 1, the ejection hole portion 10 is provided at a place where a pressure difference is most likely to occur such as cavitation.

【0021】仕様図DはC図同様Specification diagram D is the same as C diagram

【請求項4】の特徴を備えながらも、異なる点は請求項
5のような立ち上がり部分13を持つことで背面部17
の表面部を上方へ引っ張る力が発生する以外に乱流や表
面剥離現象を発生させてより一層の圧力差を発生させる
様に働く。しかし本図の基本は請求項4ように噴出孔部
10を羽根部1にもつのである点が唯一異なり、それゆ
えに羽根部1のなかも中空状としてエア通路15として
いる。
4. The rear part 17 is characterized by having the rising portion 13 as in claim 5, while having the features of claim 4.
In addition to the force of pulling the surface portion of the above, the turbulent flow and the surface separation phenomenon are generated to further generate a pressure difference. However, the basic point of this drawing is different only in that the jet hole portion 10 is also connected to the vane portion 1 as in claim 4, and therefore the vane portion 1 is also hollow to form the air passage 15.

【0022】仕様図EはThe specification diagram E is

【請求項5】の特徴を備えたものであり、図面は羽根部
1の構造を翼状としながら、
5. The drawings are characterized by the following:

【請求項5】のような羽根部1の前縁部18を衝立状の
立ち上がり部分13として形成させたもので、背面流の
立ち上がり部分13に渦巻きや表面剥離現象を発生させ
て空隙中の吸引力によって羽根部1根元に形成させた噴
出孔部10よりエアを吸引させるものである。
5. The front edge portion 18 of the vane portion 1 as described above is formed as a partition-shaped rising portion 13, and a vortex or a surface separation phenomenon is generated in the rising portion 13 of the back flow to suck in the gap. Air is sucked from the ejection hole portion 10 formed at the base of the blade portion 1 by a force.

【0023】仕様図FはThe specification diagram F is

【請求項4】の特徴を備えたもので、羽根部1の中は中
空状態ではないが、該表面部の内の背面部17付近にエ
ア噴出孔部10を形成するように導入パイプ11を設け
たものであり、 図面は丁度羽根部1の背面部17およ
び縁部18に噴出孔部10を形成させたものであり、水
を切る場合の背面部17に廻り込む水流が再び後縁部1
8で合流される時に圧力差の為に流れの差が生ずるが、
本項ではこの流れの差のうち背面部17に発生する力に
は該表面部を上方へ引っ張る力が発生することになり、
背面部17の噴出孔部10からは効率良くエアが噴出さ
れるものとなる。また羽根部1の先端縁部18に噴出孔
部10を設けることによってキャビテーションなどの最
も圧力差が発生し易いところに噴出孔部10を設けても
いる。
4. The introduction pipe 11 is provided so as to form the air ejection hole portion 10 near the back surface portion 17 of the surface portion, although the inside of the blade portion 1 is not hollow. In the drawing, the jet holes 10 are just formed in the back surface portion 17 and the edge portion 18 of the blade portion 1, and when the water is drained, the water flow circling around the back surface portion 17 again becomes the rear edge portion. 1
When merged at 8, there is a difference in flow due to the pressure difference,
In this section, the force generated in the back surface portion 17 of the difference in the flow is a force that pulls the surface portion upward,
Air is efficiently ejected from the ejection hole portion 10 of the back surface portion 17. Further, by providing the ejection hole portion 10 at the tip edge portion 18 of the blade portion 1, the ejection hole portion 10 is provided at a place where a pressure difference is most likely to occur such as cavitation.

【0024】ところで本発明は、大深度曝気の為に大径
管体3を更に延長しながら本実施例のような曝気させる
目的の羽根部1を突設させると同時にエアや水流を移送
する為に専門のラセン状羽根部などを設けて水底へ溶存
酸素水を同時に移送させるものでも良し、または本図の
曝気装置の水流噴出口に新たな移送用の管体を近接させ
てラセンによって液体の移送を行なうものでも良い。こ
のようにラセンによる液体の移送方法は既に公知の事実
である。
By the way, according to the present invention, the large-diameter pipe body 3 is further extended for deep aeration, and the blade portion 1 for the purpose of aeration as in this embodiment is projected and at the same time air and water flow are transferred. It is also possible to provide a special spiral blade part etc. at the same time to transfer the dissolved oxygen water to the water bottom at the same time, or to bring a new transfer pipe body close to the water jet outlet of the aeration device of this figure and to transfer the liquid by the spiral. It may be transferred. As described above, the liquid transfer method using the spiral is already known.

【0025】[0025]

【発明の効果】本発明は、大径管体の内壁に突設された
羽根部が互いの間で生成させた水流を中心部へ集中させ
ることによって、水流の相乗効果を利用しながら流速と
貫通力を強めるものである。とくに羽根部1の回転によ
って水流が生成された時のその力成分のうち水流が末広
がり状の渦流となる力方向成分である斜め方向水流を大
径管体の中心部で集めることで水流どうしの中心部への
押し合い作用で推進方向への力を取り出すように矯正さ
せるものである。また、その為の構造上の重要な違いか
らの効果として、特に羽根部1を形成させる方向が根本
的に異なことにより、羽根部1をある物体より放射方向
に突設させる従来構造に対して、本発明はある物体より
突設させる方向を点中心方向へ向かう構造としたことに
より、羽根部の羽根幅が同じものでも中心部で水流を集
中させ合う構造であるぶんだけ生成した渦流を干渉効果
や相互強制効果などで強めながら絞り込むことができ
て、しかも水流の貫通力を強めながら流速を速めことも
できる。このように水流や渦流の流速を強めた分だけ圧
力差も比例して増加する為、エアの吸引力も強めること
ができる。さらに本発明は、従来のスクリュー型曝気装
置と構造も作用も根本的に異なる為に、請求項2のよう
に管体内の渦巻きをエア通路に利用しても発生する渦流
が強力なことと、管体が回転しながらその体内で渦巻き
を発生させる為、途中で途切れることなく発生し続け従
来では不可能であった渦巻きをエア通路として利用でき
る。さらに本発明は本出願人による特許願の新曝気技術
である羽根面噴出方式や羽根部の衝立構造による吸引方
式などの技術をも利用できて、より渦流の断面に対する
エアの分布状態を万遍なく混和させることができてエア
の噴出量もさらに増やすことができる。さらには本発明
の羽根部をラセン状でも翼状でもどのようなものでもよ
いし、羽根部の数も問題でなく、例えばラセン羽根一枚
が大径管体内側に巻き付くように突設されたものでも良
い。ところで、本発明は気泡の微細な発生と同時に何か
の運搬に係るものであるが、本装置の構造上、液体の移
送や何かのものの移送にもこのまま利用できて、例えば
流雪坑の雪の破砕と攪拌を移送と同時に気泡の働きによ
って破砕するものでも良い。
According to the present invention, the vanes projecting from the inner wall of the large-diameter pipe concentrate the water flow generated between them into the central part, thereby utilizing the synergistic effect of the water flow and the flow velocity. It enhances penetration. Especially, when the water flow is generated by the rotation of the blade part 1, the oblique water flow, which is the force direction component of the water flow that becomes a vortex that spreads toward the end, is collected at the center of the large-diameter tubular body, thereby The pressing force to the central portion is corrected so as to extract the force in the propulsion direction. Further, as an effect from an important structural difference for that, in particular, since the direction in which the blade portion 1 is formed is fundamentally different, the blade portion 1 is projected from a certain object in the radial direction, as compared with the conventional structure. , The present invention has a structure in which the direction of projecting from a certain object is directed toward the center of the point, so that even if the blade width is the same, the water flow is concentrated in the central part It is possible to narrow down while strengthening by the effect or mutual compulsion effect, etc., and it is also possible to speed up the flow velocity while strengthening the penetrating force of the water flow. In this way, the pressure difference increases in proportion to the increase in the flow velocity of the water flow or swirl flow, so that the suction force of the air can also be increased. Further, according to the present invention, since the structure and the operation are fundamentally different from the conventional screw type aerator, the vortex flow generated even when the spiral in the pipe body is used for the air passage as in claim 2 is strong, Since the vortex is generated in the body while the tube is rotating, the vortex continues to be generated without interruption and can be used as an air passage, which has been impossible in the past. Further, the present invention can utilize the technology such as the blade surface jetting method, which is the new aeration technology of the applicant's patent application, and the suction method by the partition structure of the blade portion, so that the distribution state of the air to the cross section of the vortex flow is evenly distributed. It is possible to mix without mixing, and the amount of air jetted can be further increased. Further, the blade portion of the present invention may be any shape such as a spiral shape or a blade shape, and the number of blade portions does not matter, and for example, one spiral blade is provided so as to be wound around the inside of the large-diameter pipe body. Anything is fine. By the way, the present invention relates to the transport of something at the same time as the minute generation of bubbles. However, due to the structure of this device, it can be used as it is for the transport of liquids or the transport of something, for example, in a snow mine. It is also possible to crush the snow and agitate it by the action of bubbles at the same time as transferring.

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

【図1】および仕様図A、B、C、D、E、F図は本発
明の第1実施例を示す断面斜視図。 A、B、C、D、E、Fーーー仕様図、1ーー羽根部、
2ーー取り入れ口、3ーー大径管体、4ーーエア流入
口、5ーー管支持部、6ーー軸支持部、7ーー自在継ぎ
手、8ーージョイント部、9ーーモーター部、10ーー
噴出孔部、11ーー導入パイプ、12ーー耳部、13ー
ー立ち上がり部分、14ーーベアリング部、15ーーエ
ア通路、16ーー腹面部、17ーー背面部、18ーー縁
FIG. 1 and specification diagrams A, B, C, D, E, and F are sectional perspective views showing a first embodiment of the present invention. A, B, C, D, E, F --- Specification drawing, 1--blade part,
2--Inlet, 3--Large diameter tube, 4-Air inlet, 5-tube support, 6-shaft support, 7-universal joint, 8-joint, 9-motor, 10-spout hole, 11- Introducing pipe, 12-ears, 13-rising part, 14-bearing part, 15-air passage, 16-belly part, 17-back part, 18-edge part

Claims (5)

【特許請求の範囲】[Claims] 【請求項1】動力につながる回転軸と同軸状態で連結さ
れた大径管体を設けて、該大径管体は該回転軸の回転中
心と同芯方向で連結される構造として、該大径管体の最
低でも一端を水中へ潜没させる構造として、該潜没側の
該大径管体内壁にはラセン状または翼状の羽根部を突設
させる構造として、該羽根部へ回転時のモーメントが加
わった場合の推進方向以外の斜め方向水流を該大径管体
中心で集中させる構造として、該水流または渦流などの
流れを推進方向へ増幅する構造として、該大径管体の一
方を水流噴出口とする構造として、該大径管体の管内へ
水取り入れ口を設けると同時にエアを流入させる為のエ
ア流入口をも設けて、該羽根部が強制的に水流を発生さ
せる構造としながら、発生した水流の流れの差を利用す
る構造とすることで圧力差を発生させて、エアを強制的
に吸引する構造としたことを特徴とする大径管体一体回
転羽根をもつ曝気装置。
1. A large-diameter tube body coaxially connected to a rotating shaft connected to power is provided, and the large-diameter tube body is connected to the center of rotation of the rotating shaft concentrically. As a structure in which at least one end of the diameter pipe body is submerged in water, as a structure in which a spiral or wing-shaped blade portion is projected on the inner wall of the large diameter pipe on the submerged side, As a structure for concentrating a diagonal water flow other than the propulsion direction when a moment is applied at the center of the large-diameter pipe, one of the large-diameter pipes is used as a structure for amplifying a flow such as the water flow or vortex in the propulsion direction. As a structure for making a water jet, a structure is provided in which a water inlet is provided in the pipe of the large-diameter pipe body and at the same time an air inlet for letting in air is also provided so that the vanes forcefully generate a water flow. However, a structure that utilizes the difference in the generated water flow By generating a pressure difference, aerator having a large diameter pipe member integrally rotating blades, characterized in that it has a structure for forcibly sucking air.
【請求項2】前記該大径管体と該羽根部が回転する構造
とすることで、該大径管体内へ流入した水を強制的に回
転させる構造として同時に、水流が回転することで渦流
を発生させる構造として、該大径管体内の該渦流により
発生する渦巻きをエア通路に利用する構造として、該エ
ア通路と該エア流入口とを連通せしめた構造とした特許
請求の範囲第1項記載の大径管体一体回転羽根をもつ曝
気装置。
2. The structure in which the large-diameter pipe body and the vane portion are rotated so that the water flowing into the large-diameter pipe body is forcedly rotated, and at the same time, the water flow is rotated to cause a vortex flow. 2. The structure for generating the above-mentioned structure, wherein the vortex generated by the vortex flow in the large-diameter tubular body is used for the air passage, and the air passage and the air inlet are connected to each other. An aeration device having the large-diameter tubular body-integrated rotary vane described.
【請求項3】前記該大径管体の中心部にエア導入パイプ
を設ける構造として、該導入パイプ中の中空部はエア流
入口と連通される構造として、該導入パイプは該大径管
体中を延設されながら該羽根部付近でエア噴出孔部を持
つ構造として、水流の流速と渦流または乱流の働きによ
る圧力差を利用してエアを吸引させる構造とした特許請
求の範囲第1項記載の大径管体一体回転羽根をもつ曝気
装置。
3. A structure in which an air introduction pipe is provided at the center of the large-diameter pipe body, a hollow portion in the introduction pipe communicates with an air inlet, and the introduction pipe is the large-diameter pipe body. A structure having an air ejection hole portion in the vicinity of the vane portion while being extended, so that air is sucked by utilizing a pressure difference due to a flow velocity of a water flow and a vortex or turbulent flow. An aeration apparatus having a large-diameter tubular body-integrated rotary blade according to the item.
【請求項4】前記大径管体に設けた羽根部の表面部また
は表面部付近の導入パイプなどへ噴出孔部を形成して、
該羽根部が水を切る段階で生じる羽根流れの差を利用す
る構造として、該流れの差により圧力差を発生する構造
として、中空状該羽根部の中または該表面部付近の噴出
孔部までエア通路を連通させて、該噴出孔部からエア通
路を介してエア流入口まで連通させる構造として、該羽
根部が水切り運動を行なう時点で発生した圧力差を利用
する構造として、該噴出孔部よりエアを吸引させる構造
とした特許請求の範囲第1項、第2項または第3項記載
の大径管体一体回転羽根をもつ曝気装置。
4. A jet hole portion is formed in a surface portion of a blade portion provided in the large-diameter tubular body or an introduction pipe in the vicinity of the surface portion,
As a structure that utilizes the difference in the flow of the blades that occurs when the blades cut water, as a structure that generates a pressure difference due to the difference in the flow, up to the ejection holes in the hollow blades or near the surface As a structure in which the air passage is communicated to communicate from the ejection hole portion to the air inlet through the air passage, a structure that utilizes a pressure difference generated when the blade portion performs a draining motion is used. An aeration device having a large-diameter tubular body integrated rotary blade according to claim 1, 2 or 3 having a structure for sucking more air.
【請求項5】前記大径管体に設けた羽根部へ水流の流方
向に対して立ち上がり部分形成構造としながら、該立ち
上がり部分を羽根幅方向へ延設させて、該羽根部の根元
または先端付近に設けた噴出孔部より水流の圧力差を利
用してエアを羽根幅方向へ吸引させる構造として、該エ
アの吸引方法に該立ち上がり部分による水流の圧力差発
生構造とした特許請求の範囲第1項、第2項または第3
項記載の大径管体一体回転羽根をもつ曝気装置。
5. The blade portion provided on the large-diameter tubular body has a structure for forming a rising portion with respect to the flow direction of the water flow, and the rising portion is extended in the blade width direction to form a root or a tip of the blade portion. The structure for sucking air in the width direction of the blade by utilizing the pressure difference of the water flow from a jet hole provided in the vicinity, and the structure for generating the pressure difference of the water flow by the rising portion is adopted in the method of sucking the air. Item 1, Item 2, or Item 3
An aeration apparatus having a large-diameter tubular body-integrated rotary blade according to the item.
JP3155599A 1991-05-31 1991-05-31 Aerator with large diametral pipe body solid moving blade Pending JPH0688585A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP3155599A JPH0688585A (en) 1991-05-31 1991-05-31 Aerator with large diametral pipe body solid moving blade

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP3155599A JPH0688585A (en) 1991-05-31 1991-05-31 Aerator with large diametral pipe body solid moving blade

Publications (1)

Publication Number Publication Date
JPH0688585A true JPH0688585A (en) 1994-03-29

Family

ID=15609549

Family Applications (1)

Application Number Title Priority Date Filing Date
JP3155599A Pending JPH0688585A (en) 1991-05-31 1991-05-31 Aerator with large diametral pipe body solid moving blade

Country Status (1)

Country Link
JP (1) JPH0688585A (en)

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