JPH03151034A - Emulsifying and dispersing device - Google Patents

Emulsifying and dispersing device

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Publication number
JPH03151034A
JPH03151034A JP28769089A JP28769089A JPH03151034A JP H03151034 A JPH03151034 A JP H03151034A JP 28769089 A JP28769089 A JP 28769089A JP 28769089 A JP28769089 A JP 28769089A JP H03151034 A JPH03151034 A JP H03151034A
Authority
JP
Japan
Prior art keywords
turbine
wall surface
conical wall
stator
shaft cylinder
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
JP28769089A
Other languages
Japanese (ja)
Inventor
Toru Taniguchi
徹 谷口
Juichi Watanabe
寿一 渡辺
Minoru Takahashi
稔 高橋
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.)
Tokushu Kika Kogyo Co Ltd
Original Assignee
Tokushu Kika Kogyo Co Ltd
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 Tokushu Kika Kogyo Co Ltd filed Critical Tokushu Kika Kogyo Co Ltd
Priority to JP28769089A priority Critical patent/JPH03151034A/en
Publication of JPH03151034A publication Critical patent/JPH03151034A/en
Pending legal-status Critical Current

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Abstract

PURPOSE:To improve the efficiency of emulsification and dispersion by forming a pump operating chamber in the intermediate part of the spacing part between the shaft cylinder of spiral vane pieces formed on the peripheral surface of a turbine and the circular conical wall surface of a stator and cooperating the respective liquid suction operating parts of a volume substitution type and a centrifugal differential pressure type. CONSTITUTION:The turbine 1 is formed with the liquid suction operating part (a) of the volume substitution type and the liquid suction operating part (b) of the centrifugal differential pressure type by projectingly providing plural spiral vane pieces 4 on the peripheral surface of the shaft cylinder 3 of a prescribed height and projecting the lower parts 4b of the respective vane pieces 4 from the lower part of the shaft cylinder 3. The lower part of the stator 2 is formed as a suction port 5a in the lower part and the peripheral wall in the inner intermediate part thereof is formed as the upper circular conical wall surface 6 of a small diameter circumscribing the rotating locus on the outer periphery of the vane pieces 4 of the turbine; further, plural discharge ports 7 which are expanded upward and are spaced from each other are provided in communication with the circular conical wall surface 6 and the front surface. The stator 2 is fixed and the turbine 1 is rotated while the turbine is inscribed with the inner circular conical wall surface 6. As a result, the dispersing and emulsifying efficiency is improved.

Description

【発明の詳細な説明】 (産業上の利用分野) 本発明は化学製品、食料品、医薬品、化粧品等の分野に
おける液剤の乳化分散装置に関する。
DETAILED DESCRIPTION OF THE INVENTION (Field of Industrial Application) The present invention relates to an emulsifying and dispersing device for liquid agents in the fields of chemical products, foods, pharmaceuticals, cosmetics, and the like.

(従来の技術) この種分野の乳化分散装置において固定したステータと
回転タービンとの組合せによるものはすでに公知である
BACKGROUND OF THE INVENTION Emulsifying and dispersing devices of this kind in combination with a fixed stator and a rotating turbine are already known.

(発明が解決しようとする課題) 従来手段におけるタービンは一般に軸筒(ボス)の周面
に形成される螺旋状翼片は、該軸筒の長さ範囲内に設け
られ、ステータとの接触回転において軸筒と翼片とによ
りステータの内側にポンプ作動域を区画し、該ポンプ作
動域により容積置換式の液体吸引作動部を形成するを一
般とし、このため分散乳化作用にも限度があり、高品位
の製品を得られない点があった。
(Problems to be Solved by the Invention) In conventional turbines, spiral blades are generally formed on the circumferential surface of a shaft cylinder (boss), and are provided within the length range of the shaft cylinder to prevent contact rotation with the stator. In general, a pump operating region is defined inside the stator by a shaft cylinder and blades, and the pump operating region forms a volume displacement type liquid suction operating section, so there is a limit to the dispersion emulsification effect. There was a problem in that it was not possible to obtain high-quality products.

(課題を解決するための手段) 本発明は上記に鑑み、タービン並にステータに改良を加
えて分散乳化作用を促進させ高品位の製品を得ることを
目的とするもので、所定寸法高さの軸筒周面に複数の螺
旋状翼片を一体に突設すると共に、各翼片の下部を軸筒
の下部から突出させて、容積置換式液体吸引作動部と遠
心差圧式液体吸引作動部とを形成したタービンと、下部
を吸込み口とし、その内側中間部周壁をタービン翼片外
周の回転軌跡に外接する上部小径の円錐壁面とし、更に
該円錐壁面と上面とに連通させて上方に拡開した複数の
吐出孔を間隔を存して設けたステータとの組合せから成
り、該ステータを固定し、その内側円錐壁面に内接させ
てタービンを回転させるようにしたことを特徴とする。
(Means for Solving the Problems) In view of the above, the present invention aims to improve the turbine as well as the stator to promote dispersion and emulsification to obtain high-quality products. A plurality of spiral blades are integrally provided on the peripheral surface of the shaft cylinder, and the lower part of each blade is made to protrude from the lower part of the shaft cylinder, thereby forming a volume displacement type liquid suction operating section and a centrifugal differential pressure type liquid suction operation section. The turbine has a suction port at its lower part, its inner intermediate peripheral wall is a conical wall surface with a small diameter at the top circumscribing the rotation locus of the outer periphery of the turbine blade, and the conical wall surface and the upper surface communicate with each other to expand upward. The turbine is characterized in that the stator is fixed and inscribed in the inner conical wall surface of the stator to rotate the turbine.

(作 用) 本発明において処理8器内においてステータ(2)を不
動に固定し、回転軸に結着したタービン(1)を、ステ
ータ(2)の吸込み口(5a)内において円錐壁面(6
)に内接させて回転させる。
(Function) In the present invention, the stator (2) is immovably fixed in the processing unit 8, and the turbine (1) connected to the rotating shaft is connected to the conical wall surface (6) in the suction port (5a) of the stator (2).
) and rotate it.

タービン(1)の周面に形成した螺旋状翼片(4)の上
部(4a)は軸筒(ボス)(3)と一体に連接し、従っ
て各翼片(4)の上部(4a)は、これに外接するステ
ータ(2)の円錐壁面(6)と軸筒(3)との間隔部中
間を区画して、ポンプ作動室を形成し、該ポンプ室によ
る容積置換式による液体吸引作動部aを形成し、更に軸
筒(3)の下部から突出遊離させた各翼片(4)の下部
(4b)の回転により遠心差圧式の液体吸引作動部すを
形成したので、これら両吸引作動部a、bの協動により
乳化分散効率を著しく向上させ得られ、又ステータ(2
)の吐出孔(7)を液の吐出方向において拡開して吐出
口の断面積を逐次大きくしたので、液の流動速度差によ
るキャビティー効果を大にし、且つ多数配設した吐出孔
(7)により形成される半径方向のリブ(8)口縁と翼
片(4)とによる剪断作用も処理効果を宵効にした。
The upper part (4a) of the spiral blade (4) formed on the circumferential surface of the turbine (1) is integrally connected to the axial cylinder (boss) (3), so the upper part (4a) of each blade (4) is A pump operation chamber is formed by dividing the middle of the gap between the conical wall surface (6) of the stator (2) circumscribing the stator (2) and the shaft cylinder (3), and a liquid suction operation section using a volume displacement type by the pump chamber. A, and a centrifugal differential pressure type liquid suction operation part is formed by rotating the lower part (4b) of each wing piece (4) that is released and protrudes from the lower part of the shaft cylinder (3). The cooperation of parts a and b can significantly improve emulsification and dispersion efficiency, and the stator (2)
) is enlarged in the liquid discharge direction to gradually increase the cross-sectional area of the discharge port, thereby increasing the cavity effect due to the difference in liquid flow velocity. ) The shearing action by the rim of the radial rib (8) and the blade (4) also made the treatment effect effective.

(実施例) 本発明の実施例を図面について説明する。(Example) Embodiments of the present invention will be described with reference to the drawings.

タービン(1)とステータ(2)との組合せから成り、
タービン(1)は第2図乃至第4図で示すように所定高
さの軸筒(3)の周縁に複数の螺旋状翼片(4)を一体
に形成し、各翼片(4)の上半部(4a)は軸筒(3)
と連接するが、下半部(4b)は軸筒(3)の下部から
突出遊離させた。
Consists of a combination of a turbine (1) and a stator (2),
As shown in FIGS. 2 to 4, the turbine (1) has a plurality of spiral blades (4) integrally formed on the periphery of a shaft cylinder (3) of a predetermined height. The upper half (4a) is the shaft cylinder (3)
However, the lower half part (4b) was made to protrude and be separated from the lower part of the shaft cylinder (3).

ステータ(2)は第1図および第5図で示すように下部
を吸込み口(5a)とし、上部中心部に吸込み口(5a
)に連通する軸孔(5b)を設けた器筒(5)で構成さ
れ、該器筒(5)の内側中間部の周壁を、第2図で示さ
れるタービン(1)における翼片(4)の外周縁の回転
軌跡円(6′)と合致する円錐壁面(6)とし、且つ該
円錐壁面(6)と器筒(5)の上面に連通ずる吐出孔(
7)の複数を第5図で示すように前記軸孔(5b)を囲
繞して配設し、従ってその間隔部には半径方向のリブ(
8)が形成される。
As shown in FIGS. 1 and 5, the stator (2) has a suction port (5a) at the bottom and a suction port (5a) at the center of the top.
), and the circumferential wall of the inner middle part of the cylinder (5) is connected to the blade (4) of the turbine (1) shown in FIG. ) has a conical wall surface (6) that coincides with the rotation locus circle (6') on the outer periphery of the conical wall surface (6), and a discharge hole (
A plurality of ribs (7) are arranged surrounding the shaft hole (5b) as shown in FIG.
8) is formed.

尚、上記複数の吐出孔(7)は上部に向って漸次拡開し
た。
Note that the plurality of discharge holes (7) gradually expanded toward the top.

以上の構成から成るステータ(2)を第1図で示すよう
処理槽(図示せず)内において固定支持杆(IQに結着
して不動状態とし、ステータ(2)の軸孔(5b)を挿
通した回転軸(9)の下端にキー(Ivでタービン(1
)を固着してその翼片(4)を円錐壁面(6)に内接さ
せた状態で回動させる。
The stator (2) constructed as described above is placed in a processing tank (not shown) as shown in FIG. The turbine (1
) is fixed and rotated with its wing pieces (4) inscribed in the conical wall surface (6).

その回転において各翼片(4)の上部(4a)は、内側
の軸筒(3)と円錐壁面(6)間にポンプ作動室を区画
形成しつつ回転するため容積置換式による液吸引作動部
aによって液を吸引し、同時にその下方においては軸筒
(3)の下面から突出遊離した翼片(4)の下部(4b
)の回転により遠心差圧式の液吸引作動部すによる液の
吸引作動が行われ、両件動部aSbの協動で第1図で矢
示のように下方から上方に向って液を吸引流動させる。
During the rotation, the upper part (4a) of each blade (4) rotates while forming a pump operating chamber between the inner shaft cylinder (3) and the conical wall surface (6), so the liquid suction operating part is a volume displacement type. a, and at the same time, below it, the lower part (4b) of the wing piece (4) protruding from the lower surface of the shaft cylinder (3)
) causes the centrifugal differential pressure type liquid suction operation part to suction the liquid, and by the cooperation of the two movement parts aSb, the liquid is suctioned and flows from the bottom to the top as shown by the arrow in Figure 1. let

又、液は翼片(4)と吐出孔(7)を形成する多数のリ
ブ(8)の下端との接触による剪断作用を受け、更に上
方に向って断面積を大きくした吐出孔(7)によって円
滑に流動する。
In addition, the liquid is subjected to shearing action due to contact between the wing pieces (4) and the lower ends of the many ribs (8) forming the discharge hole (7), and the discharge hole (7) whose cross-sectional area increases upwardly. Flows smoothly.

尚、従来一般にタービン(1)は回転軸(9)に対し結
着した軸筒部分(ボス)が、軸受部との接触で摩耗した
場合にはタービン全体を廃棄せざるを得なかったが、第
1図で示すように軸筒(3)と別個にスリーブ(+21
を組込み、該スリーブ■で軸孔(5b)内周の液中軸受
部材a3で支持させ、摩耗時には該スリーブ(′lbの
みを取換え得るようにし、且つ回転軸に対するタービン
(1)の結合は従来−般のねじ結合によることなく、キ
ー(111)結合として着脱を安易にした。
In addition, conventionally, when the shaft cylinder part (boss) of the turbine (1) that is attached to the rotating shaft (9) wears out due to contact with the bearing part, the entire turbine has to be discarded. As shown in Figure 1, the shaft cylinder (3) and the sleeve (+21
The sleeve (1) is supported by the submerged bearing member a3 on the inner periphery of the shaft hole (5b), so that only the sleeve ('lb) can be replaced when worn, and the connection of the turbine (1) to the rotating shaft is The key (111) connection is used instead of the conventional screw connection for easy attachment and removal.

又、使用において最少の仕込み量時には最低の流動を得
られるように、このときはタービン(1)を逆転させて
これに対処し得るもので、その逆転による流動方向は上
から下となり、液面に浮遊する投入粉末等を下方に吸引
し得る等の作業も可能となる。
In addition, in order to obtain the lowest flow when the minimum amount of charge is used, the turbine (1) can be reversed at this time, and the direction of flow due to the reverse is from top to bottom, and the liquid level is It also becomes possible to perform operations such as suctioning powder, etc. floating in the air downward.

(発明の効果) 本発明によるときは、液体の流動範囲が従来より高粘度
域まで可能となった。
(Effects of the Invention) According to the present invention, the flow range of the liquid can reach a higher viscosity range than before.

キャビテーション領域が拡大され、ミクロ撹拌力が増大
した。
The cavitation area was expanded and the micro-stirring force was increased.

タービンの翼片を薄くすることにより特に軸筒から下方
に突出する翼片下部の微振動により超音波が発生し、こ
れによるミクロ撹拌力が増大した。
By making the blades of the turbine thinner, ultrasonic waves were generated due to micro vibrations in the lower part of the blades that protruded downward from the shaft cylinder, and the resulting micro-agitation force was increased.

使用範囲が更に広汎となった。The range of use has become even wider.

高品質の製品を得られる。You can get high quality products.

等の効果を有する。It has the following effects.

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

図面は本発明の実施例を示すもので、第1図は裁断側面
図、第2図はタービンの正面図、第3図は同平面図、第
4図は同底面図、第5図はステータの平面図である。 (1)・・・タービン (3)・・・軸 筒 (4a) (4b)・・・翼片の上・下部(5a)・・
・吸込み口 (6)・・・円錐壁面 (2)・・・ステータ (4)・・・翼片 (5)・・・器 筒 (5b)・・・軸 孔 (7)・・・吐出孔
The drawings show an embodiment of the present invention, in which Fig. 1 is a cut side view, Fig. 2 is a front view of the turbine, Fig. 3 is a plan view thereof, Fig. 4 is a bottom view of the turbine, and Fig. 5 is a stator. FIG. (1)...Turbine (3)...Shaft cylinder (4a) (4b)...Upper/lower part of blade (5a)...
・Suction port (6)... Conical wall surface (2)... Stator (4)... Wing piece (5)... Vessel cylinder (5b)... Shaft hole (7)... Discharge hole

Claims (1)

【特許請求の範囲】[Claims] 所定寸法高さの軸筒周面に複数の螺旋状翼片を一体に突
設すると共に、各翼片の下部を軸筒の下部から突出させ
て、容積置換式液体吸引作動部と遠心差圧式液体吸引作
動部とを形成したタービンと、下部を吸込み口とし、そ
の内側中間部周壁をタービン翼片外周の回転軌跡に外接
する上部小径の円錐壁面とし、更に該円錐壁面と上面と
に連通させて上方に拡開した複数の吐出孔を間隔を存し
て設けたステータとの組合せから成り、該ステータを固
定し、その内側円錐壁面に内接させてタービンを回転さ
せるようにしたことを特徴とする乳化分散装置。
A plurality of spiral blades are integrally provided on the circumferential surface of the shaft cylinder with a predetermined height, and the lower part of each blade is made to protrude from the lower part of the shaft cylinder. A turbine having a liquid suction operating part, a lower part serving as a suction port, an inner intermediate circumferential wall thereof having an upper small-diameter conical wall surface circumscribing the rotation locus of the outer periphery of the turbine blade, and further communicating with the conical wall surface and the upper surface. The stator is fixed and inscribed in its inner conical wall surface to rotate the turbine. Emulsifying and dispersing equipment.
JP28769089A 1989-11-04 1989-11-04 Emulsifying and dispersing device Pending JPH03151034A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP28769089A JPH03151034A (en) 1989-11-04 1989-11-04 Emulsifying and dispersing device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP28769089A JPH03151034A (en) 1989-11-04 1989-11-04 Emulsifying and dispersing device

Publications (1)

Publication Number Publication Date
JPH03151034A true JPH03151034A (en) 1991-06-27

Family

ID=17720471

Family Applications (1)

Application Number Title Priority Date Filing Date
JP28769089A Pending JPH03151034A (en) 1989-11-04 1989-11-04 Emulsifying and dispersing device

Country Status (1)

Country Link
JP (1) JPH03151034A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR19990049682A (en) * 1997-12-15 1999-07-05 조병욱 High Viscosity and Low Viscosity Stirring Unit of Homogenizer

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR19990049682A (en) * 1997-12-15 1999-07-05 조병욱 High Viscosity and Low Viscosity Stirring Unit of Homogenizer

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