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JP4380889B2 - Reciprocating stirring blade - Google Patents
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JP4380889B2 - Reciprocating stirring blade - Google Patents

Reciprocating stirring blade Download PDF

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Publication number
JP4380889B2
JP4380889B2 JP2000170090A JP2000170090A JP4380889B2 JP 4380889 B2 JP4380889 B2 JP 4380889B2 JP 2000170090 A JP2000170090 A JP 2000170090A JP 2000170090 A JP2000170090 A JP 2000170090A JP 4380889 B2 JP4380889 B2 JP 4380889B2
Authority
JP
Japan
Prior art keywords
stirring blade
blade
reciprocating
wing body
stirring
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 - Lifetime
Application number
JP2000170090A
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Japanese (ja)
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JP2001347151A (en
Inventor
茂 西岡
好一 加藤
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.)
Satake Chemical Equipment Mfg Ltd
Original Assignee
Satake Chemical Equipment Mfg 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 Satake Chemical Equipment Mfg Ltd filed Critical Satake Chemical Equipment Mfg Ltd
Priority to JP2000170090A priority Critical patent/JP4380889B2/en
Publication of JP2001347151A publication Critical patent/JP2001347151A/en
Application granted granted Critical
Publication of JP4380889B2 publication Critical patent/JP4380889B2/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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Description

【0001】
【発明の属する技術分野】
本発明は医薬、化粧、食品やバイオ等の各種工業における液等の撹拌に好適な往復反転用の撹拌翼に関する。
【0002】
【従来の技術】
従来の往復反転用の撹拌翼として、図10の如くボスaの外周から4本の長方形の板状の翼体bを放射状に突設した撹拌翼c、又は図11の如くボスdの外周から4本の断面が三角形の柱状の翼体eを放射状に突設した撹拌翼fが知られている。
【0003】
【発明が解決しようとする課題】
従来の前者の撹拌翼cを図12の如く回転軸gに固定して撹拌槽h内の液中に垂下して該回転軸gを往復回転させると、図13の如く翼体bも背面に渦流が生じ、この渦流によって大きな剪断力を生ずると共に図12の如く撹拌槽h内の液に上下の互いに逆方向のフローパターンが形成され、槽内の流れは二分される。又、従来の後者の撹拌翼fを図14の如く回転軸gに固定して撹拌槽h内の液中に垂下して該回転軸gを往復回転させると、図15の如く翼体eの背面に渦流が生じ、この渦流によって大きな剪断力を生ずると共に図14の如く撹拌槽h内の液にショートパスする循環流と上下の互いに逆方向のフローパターンが形成され、かくてこれら従来の撹拌翼は槽内かきみだし形の撹拌しか行なえず、撹拌効率が低いという問題があった。
【0004】
本発明はこれらの問題点を解消し、撹拌において低剪断力で有効な軸方向を作り出して槽内に上下循環流が得られるような撹拌効率の良い往復反転用撹拌翼を提供することを目的とする。
【0005】
【課題を解決するための手段】
本発明は上記の目的を達成すべく、横断面において、その中心線の左右の形状が対称であり、且つ上面が上方に向かって凸の湾曲状に形成されていると共に、下面が水平か又は上方に向って凹の湾曲状に形成されている翼体よりなり、該翼体は下面の左右端部に間隔を存して左右対称の横断面形状の補助翼を付設したことを特徴とする。
【0006】
【発明の実施の形態】
本発明の往復反転用撹拌翼の一実施の形態を図1乃至図9により説明する。
【0007】
図1は本発明の往復反転用撹拌翼1を組込んだ撹拌装置の斜視図であり、該往復反転用撹拌翼1は図示していない駆動装置によって矢印R1又は矢印R2の方向へ往復反転可能に撹拌槽3内に垂設されている。
【0008】
4は撹拌槽内の液面を示す。
【0009】
前記往復反転用撹拌翼1は、回転軸1aの下端部のボス1bに複数の翼体2を放射状に固定して有している。
【0010】
図2は翼体2の横断面図を示し、該翼体2の断面は上面2aが上方に向かって凸で下面2bが水平な左右対称の翼形に形成されている。
【0011】
図3は前記翼体2の平面図を示し、翼体2は平面において、根部から先端部に向かって幅が狭くなる略尖塔状に形成されている。
【0012】
次に本実施の形態の往復反転用撹拌翼1の作動及び効果について説明する。
【0013】
撹拌槽3内の往復反転用撹拌翼1を回転方向R1、又はR2の方向へ、所定のインターバルで切り換えながら交互に回転させる。
【0014】
翼体2の断面形状を上方に凸の湾曲状としたため、図4の(a)、(b)に示す如く、往復反転運転時の両方向において翼後縁における剥離を防ぎ、且つ、翼上下面における圧力差により揚力Fが生じて下向きの軸方向流を作り出している。
【0015】
即ち、往復反転撹拌翼1は前述の如く翼後縁における剥離が防止されると共に図1の矢印Aで示す循環流を生じて剪断力の小さな撹拌効率の高い撹拌装置とすることができた。
【0016】
尚、本実施の形態では、翼体2の平面形状を根部から先端部に向かって幅が狭くなる略尖塔状としたが、これは図5に示す如く、翼体2の平面形状を根部から先端部に向かって幅が一定の略長方形状としたり、又は図6に示す如く、翼体2の平面形状を根部から先端部に向かって幅が広くなる略扇状としてもよい。
【0017】
又、本実施の形態では、翼体2の横断面形状を上面が上方に向かって凸で下面が水平な左右対称の翼形としたが、これは図7で示す如く、上面が上方に向かって凸で下面が上方に向かって凹の左右対称の薄い板状の翼体2´としてもよく、又は図8に示す如く、上面が上方に向かって凸で下面が上方に向かって凹の前記翼体2´よりも厚肉とした左右対称の翼形を有する翼体2´´としてもよく、或いは又、図9に示す如く、前記翼体2´´の下面の左右端部に間隔を存して左右対称の横断面形状の補助翼2cをステー2dを介して付設して、2重翼方式の翼体2´´´としてもよい。
【0018】
【発明の効果】
このように本発明によれば、往復反転をしながら撹拌を行なう撹拌装置の往復反転用撹拌翼において、低剪断力で有効な軸方向流を作り出して、槽内に良好な上下循環流が得られる効果を有する。
【図面の簡単な説明】
【図1】本発明の往復反転用撹拌翼を組み込んだ撹拌装置の斜視図である。
【図2】前記往復反転用撹拌翼の翼体の横断面図である。
【図3】前記往復反転用撹拌翼の翼体の平面図である。
【図4】前記翼体の作動を示す説明図である。
【図5】
【図6】
【図7】
【図8】
【図9】それぞれ前記翼体の別の実施形態を示す説明図である。
【図10】従来の往復反転用撹拌翼の一例の斜視図である。
【図11】従来の往復反転用撹拌翼の他の例の斜視図である。
【図12】図10に示す従来の往復反転用撹拌翼の一例の作動状態を示す説明図である。
【図13】同上往復反転用撹拌翼の一例の翼体の作動状態を示す説明図である。
【図14】図11に示す従来の往復反転用撹拌翼の他の例の作動状態を示す説明図である。
【図15】同上往復反転用撹拌翼の他の例の翼体の作動状態を示す説明図である。
【符号の説明】
1 往復反転用撹拌翼
2、2´、2´´、2´´´ 翼体
2c 補助翼
[0001]
BACKGROUND OF THE INVENTION
The present invention relates to a reciprocating stirring blade suitable for stirring liquids in various industries such as medicine, cosmetics, food, and biotechnology.
[0002]
[Prior art]
As a conventional agitating blade for reciprocal reversal, a stirring blade c in which four rectangular plate-like blade bodies b project radially from the outer periphery of the boss a as shown in FIG. 10, or from the outer periphery of the boss d as shown in FIG. There is known a stirring blade f in which four wings e having a triangular cross section are radially provided.
[0003]
[Problems to be solved by the invention]
When the former former agitating blade c is fixed to the rotating shaft g as shown in FIG. 12 and suspended in the liquid in the agitating tank h to rotate the rotating shaft g back and forth, the blade body b is also moved to the back as shown in FIG. A vortex flow is generated, and a large shearing force is generated by the vortex flow, and flow patterns in opposite directions are formed in the liquid in the stirring tank h as shown in FIG. 12, and the flow in the tank is divided into two. Further, when the latter latter stirring blade f is fixed to the rotating shaft g as shown in FIG. 14 and suspended in the liquid in the stirring vessel h and the rotating shaft g is reciprocally rotated, the blade body e of FIG. A vortex flow is generated on the back surface, and a large shearing force is generated by the vortex flow, and a circulating flow short-passing the liquid in the stirring tank h and a flow pattern in the opposite directions are formed as shown in FIG. There was a problem that the blades could only be stirred in the tank and the stirring efficiency was low.
[0004]
An object of the present invention is to solve these problems and to provide an agitating blade for reciprocating reversal with good agitation efficiency so as to create an effective axial direction with low shearing force in agitation and to obtain a vertical circulation flow in a tank. And
[0005]
[Means for Solving the Problems]
In order to achieve the above object, in the present invention, in the cross section, the left and right shapes of the center line are symmetrical, and the upper surface is formed in a convex curved shape upward, and the lower surface is horizontal or It consists of a wing body that is formed in a concave curved shape toward the upper side, and the wing body is provided with auxiliary wings having a symmetrical cross-sectional shape at intervals on the left and right ends of the lower surface. .
[0006]
DETAILED DESCRIPTION OF THE INVENTION
An embodiment of a reciprocating stirring blade according to the present invention will be described with reference to FIGS.
[0007]
FIG. 1 is a perspective view of a stirring device incorporating a reciprocating stirring blade 1 according to the present invention. The reciprocating stirring blade 1 can be reciprocated in the direction of arrow R1 or arrow R2 by a driving device (not shown). Is suspended in the stirring tank 3.
[0008]
4 shows the liquid level in the stirring tank.
[0009]
The reciprocating stirring blade 1 has a plurality of blade bodies 2 radially fixed to the boss 1b at the lower end of the rotating shaft 1a.
[0010]
FIG. 2 shows a cross-sectional view of the wing body 2. The wing body 2 has a cross section formed into a symmetrical airfoil shape in which the upper surface 2 a is convex upward and the lower surface 2 b is horizontal.
[0011]
FIG. 3 shows a plan view of the wing body 2, and the wing body 2 is formed in a substantially spire shape with a width narrowing from the root portion toward the tip portion in the plane.
[0012]
Next, the operation and effect of the reciprocating stirring blade 1 of this embodiment will be described.
[0013]
The reciprocating stirring blades 1 in the stirring tank 3 are rotated alternately while switching at a predetermined interval in the direction of rotation R1 or R2.
[0014]
Since the cross-sectional shape of the wing body 2 is convex upward, as shown in FIGS. 4 (a) and 4 (b), it is possible to prevent separation at the trailing edge of the wing in both directions during reciprocating reversal operation, and A lift F is generated by the pressure difference at, creating a downward axial flow.
[0015]
In other words, the reciprocating reversing stirring blade 1 was prevented from peeling at the trailing edge of the blade as described above, and a circulating flow indicated by the arrow A in FIG.
[0016]
In the present embodiment, the planar shape of the wing body 2 is a substantially spire shape whose width decreases from the root portion toward the tip portion. However, as shown in FIG. The plane shape of the wing body 2 may be substantially fan-shaped with the width increasing from the root portion toward the tip portion as shown in FIG. 6.
[0017]
Further, in the present embodiment, the cross-sectional shape of the wing body 2 is a symmetrical wing shape in which the upper surface is convex upward and the lower surface is horizontal. However, as shown in FIG. It may be a symmetric thin plate-like wing body 2 ′ having a convex surface and a bottom surface concave upward, or, as shown in FIG. 8, the top surface is convex upward and the bottom surface is concave upward. A wing body 2 ″ having a symmetric airfoil that is thicker than the wing body 2 ′ may be used. Alternatively, as shown in FIG. 9, there is a gap between the left and right ends of the lower surface of the wing body 2 ″. Alternatively, a double wing type wing body 2 "'may be provided by attaching auxiliary blades 2c having a symmetrical cross-sectional shape via a stay 2d.
[0018]
【The invention's effect】
As described above, according to the present invention, in the stirring blade for reciprocal reversal of the stirring device that performs stirring while performing reciprocal reversal, an effective axial flow is created with a low shear force, and a good vertical circulation flow is obtained in the tank. Has the effect.
[Brief description of the drawings]
FIG. 1 is a perspective view of a stirring apparatus incorporating a reciprocating stirring blade of the present invention.
FIG. 2 is a cross-sectional view of a blade body of the reciprocating reversing stirring blade.
FIG. 3 is a plan view of a blade body of the reciprocating stirring blade.
FIG. 4 is an explanatory view showing the operation of the wing body.
[Figure 5]
[Fig. 6]
[Fig. 7]
[Fig. 8]
FIG. 9 is an explanatory view showing another embodiment of the wing body.
FIG. 10 is a perspective view of an example of a conventional reciprocating stirring blade.
FIG. 11 is a perspective view of another example of a conventional reciprocating stirring blade.
12 is an explanatory view showing an operating state of the example of the conventional reciprocating stirring blade shown in FIG.
FIG. 13 is an explanatory view showing an operating state of a blade body as an example of a reciprocating stirring blade.
14 is an explanatory view showing an operating state of another example of the conventional reciprocating stirring blade shown in FIG.
FIG. 15 is an explanatory view showing an operating state of a blade body of another example of the above-described reciprocating reversing stirring blade.
[Explanation of symbols]
1 Reciprocating stirring blade 2, 2 ′, 2 ″, 2 ″ ″ Wing body 2c Auxiliary blade

Claims (1)

横断面において、その中心線の左右の形状が対称であり、且つ上面が上方に向かって凸の湾曲状に形成されていると共に、下面が水平か又は上方に向って凹の湾曲状に形成されている翼体よりなり、該翼体は下面の左右端部に間隔を存して左右対称の横断面形状の補助翼を付設したことを特徴とする往復反転用撹拌翼。In the cross section, the left and right shapes of the center line are symmetrical, and the upper surface is formed in a convex curved shape upward, and the lower surface is formed in a curved shape that is horizontal or concave upward. and which Ri Na than wing body, the wing body reciprocating reversing stirring blade, characterized in that annexed aileron cross-sectional shape symmetrical with intervals in the right and left end portions of the lower surface.
JP2000170090A 2000-06-07 2000-06-07 Reciprocating stirring blade Expired - Lifetime JP4380889B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP2000170090A JP4380889B2 (en) 2000-06-07 2000-06-07 Reciprocating stirring blade

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP2000170090A JP4380889B2 (en) 2000-06-07 2000-06-07 Reciprocating stirring blade

Publications (2)

Publication Number Publication Date
JP2001347151A JP2001347151A (en) 2001-12-18
JP4380889B2 true JP4380889B2 (en) 2009-12-09

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Country Status (1)

Country Link
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Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
BR112015031637B1 (en) * 2013-06-28 2022-01-18 Saint-Gobain Performance Plastics Corporation MIXING ASSEMBLIES INCLUDING MAGNETIC IMPELLERS
US11944946B2 (en) 2013-06-28 2024-04-02 Saint-Gobain Performance Plastics Corporation Mixing assemblies including magnetic impellers
US11497692B2 (en) * 2019-10-15 2022-11-15 Rea Innovations, Inc. Systems and methods for blending solid-shell cosmetic ingredient capsules and blendable cosmetic ingredient capsules
CN115024073B (en) * 2022-06-19 2024-04-05 河南省禾安氏生态科技有限公司 Agricultural water and fertilizer irrigation device and method

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