JPH03106427A - Stirring blade for high delivery flow - Google Patents
Stirring blade for high delivery flowInfo
- Publication number
- JPH03106427A JPH03106427A JP24224689A JP24224689A JPH03106427A JP H03106427 A JPH03106427 A JP H03106427A JP 24224689 A JP24224689 A JP 24224689A JP 24224689 A JP24224689 A JP 24224689A JP H03106427 A JPH03106427 A JP H03106427A
- Authority
- JP
- Japan
- Prior art keywords
- blade
- blades
- stirring
- stirring blade
- fluid
- 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
Links
- 238000003756 stirring Methods 0.000 title claims abstract description 32
- 239000012530 fluid Substances 0.000 claims abstract description 20
- 238000005516 engineering process Methods 0.000 description 2
- 239000002184 metal Substances 0.000 description 2
- 230000000694 effects Effects 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 230000002093 peripheral effect Effects 0.000 description 1
- 238000007789 sealing Methods 0.000 description 1
Landscapes
- Mixers Of The Rotary Stirring Type (AREA)
Abstract
Description
[産業上の利用分野】
本発明は撹拌翼に係り、特に液一液混合に好適な撹拌機
.回転機等に使用される撹拌翼に関するものである.
〔従来の技術1
従来の撹拌翼は文献「混合および撹拌:第9頁第10図
(化学工業社)」に見られるように、径方に向いた平板
羽根(通称:平羽根タービン)、またはこの羽根がわん
曲したもの(通称:わん曲平羽根タービン)等が使用さ
れていた.なお、この種の装置として関連するちのには
例えば特公昭62−50 1 78号が挙げられる.[Industrial Application Field] The present invention relates to a stirring blade, and in particular to a stirring machine suitable for one-liquid mixing. This relates to stirring blades used in rotating machines, etc. [Conventional technology 1] Conventional stirring blades are either radially oriented flat blades (commonly known as flat blade turbines), or Types with curved blades (commonly known as curved flat blade turbines) were used. A related example of this type of device is, for example, Japanese Patent Publication No. 178/1983.
上記従来技術は、流体の均一混合について配慮゜がされ
ておらず、羽根に沿って流れる流体の速度が羽根の各位
置で異なっており,羽根に流体が垂直に当たるように回
転し、径方向への吐出流量が少なく、また羽根近辺でう
すができ易く槽全体の混合が十分に行なえず、撹拌効率
が低いという欠点があった.
本発明の目的は羽根による径方向への吐出流を増やし、
槽内全体の流体の鋺合性を向上させ、単位容積当りの撹
拌動力を低減しl!拌効率を向上させることのできる高
吐出流用撹拌翼を提供することにある.The above conventional technology does not take into account uniform mixing of the fluid, and the speed of the fluid flowing along the blade differs at each position of the blade. The disadvantage was that the discharge flow rate was low, and a thin layer easily formed near the blades, making it difficult to mix the entire tank sufficiently, resulting in low stirring efficiency. The purpose of the present invention is to increase the discharge flow in the radial direction by the blades,
It improves the cohesiveness of the fluid throughout the tank and reduces the stirring power per unit volume! The object of this invention is to provide a stirring blade for high discharge flow that can improve stirring efficiency.
【課題を解決するための手段1
上記目的を達成するために、複数の羽根とディスクとで
撹拌翼を構成すると共に、該撹拌翼の回転方向に対して
各羽根を傾斜させて取り付け,各羽根の各位置で羽根に
沿って流れる流体の速度が同じ値となる様にしたもので
ある.
【作 用】
撹拌翼を構成する従来の羽根の全長の内径側は羽根の回
転による周速は低く、外径側にいくに従って半径に比例
して周速は高くなる.従って、羽根を羽根の内側部での
回転接線方向と並行に設置すれば羽根に沿って流れる流
体の速度を各羽根の各位置で同じ値にすることができる
.
〔実 施 例】
以下,本発明の一実施例を第1図および第2図により説
明する.
図において、撹拌翼1は駆動装置2により、軸封装置3
,撹拌軸4を介して回転し、槽内5の流体6を撹拌する
.槽内5の槽壁側7には邪摩板8が設けられている.撹
拌翼lはボス9、ディスクlO、羽根11、キーl2よ
り成っている.羽根11は羽根内側部11aの回転方向
x−xに対して並行に取り付けられている。このため、
各羽根に沿って流れる流体の速度が羽根の各位置で同じ
値となる.以下,このことを第2図により説明する.羽
根内側部11aの半径なRa、周速をVa、羽根に沿う
流体の流れをUaとすると羽根内側部11aでのUaは
Vaに等しい.また羽根の任意の位置1lbに於ける半
径をRb、周速をVb,羽根に沿う流体の流れをubと
するとubは次式で求まる.
Ub=VbXCOSab −−一−一−−−−−− (
1)Rh
V b = V a x − −−−−−=−−−−−
−−−一− ( 2 )Ra
Ra
COSαb= −−−−−−−−−−−−−−−
−−(3)Rb
ここで、abは羽根の任意の位置1lbと羽根内側部1
1aとの軸心に対する角度である.(1)式に(2)、
(3)式を代入してUbを求ぬる.
=Va
以上により各羽根の任意の位置で羽根に沿って流れる流
体の速度は同一でありその値は羽根内側部11aの回転
周速に等しい.
各羽根11の回転により槽内5の流体6は羽根l1の各
部分に衝突する.衝突した流体は羽根llの表面に沿っ
て外周側に流れる.この流速が各部で同じであるため、
各部分に衝突した流体は非常に円滑に、うすや乱れが無
く外周側に吐出される.
従来の技術である平羽根タービンの場合は、羽根に衝突
した流体の流れは非常に複雑であり,部分的なうずや乱
れが多く発生しており理論的にち解明することがむつか
しく、径方向への吐出流量が少なかったが,本発明の構
造では上述の如く吐出流が理論的にも非常に円滑に行な
われるために径方向への吐出流量が大きく向上する.こ
の吐出された流体は第1図に示すように邪摩板8により
槽内を上下方向に循環させるので槽内金体の混合性を向
上させることができる.また部分的な乱れも少ないため
、撹拌動力ち低くなり、撹拌効率を向上させることがで
きる.
【発明の効果]
本発明によれば、各羽根により径方向への吐出流量を向
上させることができ、槽内金体の混合性が良好となり、
翼部の流れも円滑であるために撹拌動力を低減させるこ
とができ、撹拌効率を大幅に向上させることができる。[Means for Solving the Problems 1] In order to achieve the above object, a stirring blade is constituted by a plurality of blades and a disk, and each blade is attached at an angle with respect to the rotational direction of the stirring blade. The velocity of the fluid flowing along the blade is the same at each position. [Function] The circumferential speed due to the rotation of the blade is low on the inner diameter side of the entire length of the conventional blades that make up the stirring blade, and as it goes to the outer diameter side, the circumferential speed increases in proportion to the radius. Therefore, if the blades are installed parallel to the tangential direction of rotation inside the blade, the velocity of the fluid flowing along the blade can be made the same value at each position of each blade. [Embodiment] An embodiment of the present invention will be explained below with reference to FIGS. 1 and 2. In the figure, the stirring blade 1 is driven by a shaft sealing device 3 by a drive device 2.
, rotates via the stirring shaft 4 and stirs the fluid 6 in the tank 5. A jam plate 8 is provided on the tank wall side 7 of the tank interior 5. The stirring blade l consists of a boss 9, a disk lO, a blade 11, and a key l2. The blade 11 is attached parallel to the rotational direction x-x of the blade inner part 11a. For this reason,
The velocity of the fluid flowing along each blade is the same at each position of the blade. This will be explained below using Figure 2. If Ra is the radius of the inner blade part 11a, Va is the circumferential speed, and Ua is the fluid flow along the blade, Ua at the inner blade part 11a is equal to Va. Further, if the radius at an arbitrary position 1 lb of the blade is Rb, the peripheral speed is Vb, and the fluid flow along the blade is ub, then ub can be found by the following equation. Ub=VbXCOSab ---1-1--(
1) Rh V b = V a x − −−−−−=−−−−−
---1- (2) Ra Ra COSαb= ---
--(3) Rb Here, ab is an arbitrary position 1lb of the blade and the inside part 1 of the blade.
This is the angle with respect to the axis of 1a. (1) and (2),
Find Ub by substituting equation (3). =Va According to the above, the velocity of the fluid flowing along the blade at any arbitrary position of each blade is the same, and its value is equal to the rotational circumferential speed of the blade inner part 11a. As each blade 11 rotates, the fluid 6 in the tank 5 collides with each part of the blade l1. The colliding fluid flows toward the outer circumference along the surface of the blade ll. Since this flow velocity is the same in each part,
The fluid that collides with each part is discharged to the outer periphery very smoothly, without any thinness or turbulence. In the case of conventional flat-blade turbines, the flow of fluid that impinges on the blades is extremely complex, with many local eddies and turbulence occurring, which is difficult to explain theoretically. However, with the structure of the present invention, the discharge flow is theoretically very smooth as described above, so the discharge flow rate in the radial direction is greatly improved. As shown in FIG. 1, this discharged fluid is circulated vertically in the tank by the friction plate 8, so that the mixing properties of the metal bodies in the tank can be improved. In addition, since there is less local turbulence, the stirring power is lower and stirring efficiency can be improved. [Effects of the Invention] According to the present invention, the discharge flow rate in the radial direction can be improved by each blade, and the mixing properties of the metal bodies in the tank are improved.
Since the flow through the blades is smooth, the stirring power can be reduced, and the stirring efficiency can be greatly improved.
Claims (1)
て流れる流体の速度が同じようになるよう、撹拌翼の回
転方向に対して各羽根を傾斜させて取付けたことを特徴
とする高吐出流用撹拌翼。 2、撹拌軸にディスクを固着したボスを取付け、ディス
ク廻りに複数の羽根を固着して撹拌翼を構成すると共に
、各羽根に沿って流れる流体の速度が羽根の各位置で同
じ値となる様、撹拌翼の回転方向に対して各羽根を傾斜
させて取付けたことを特徴とする高吐出流用撹拌翼。[Claims] 1. Each blade is installed at an angle with respect to the rotating direction of the stirring blade so that the speed of the fluid flowing along the blade is the same at each position of the plurality of blades that constitute the stirring blade. A stirring blade for high discharge flow characterized by: 2. Attach a boss with a disk fixed to the stirring shaft, and configure a stirring blade by fixing multiple blades around the disk, so that the velocity of the fluid flowing along each blade is the same at each position of the blade. , a stirring blade for high discharge flow, characterized in that each blade is attached at an angle with respect to the rotating direction of the stirring blade.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP24224689A JPH03106427A (en) | 1989-09-20 | 1989-09-20 | Stirring blade for high delivery flow |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP24224689A JPH03106427A (en) | 1989-09-20 | 1989-09-20 | Stirring blade for high delivery flow |
Publications (1)
Publication Number | Publication Date |
---|---|
JPH03106427A true JPH03106427A (en) | 1991-05-07 |
Family
ID=17086422
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP24224689A Pending JPH03106427A (en) | 1989-09-20 | 1989-09-20 | Stirring blade for high delivery flow |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPH03106427A (en) |
-
1989
- 1989-09-20 JP JP24224689A patent/JPH03106427A/en active Pending
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