JPS60244301A - Centrifugal thin film dryer - Google Patents

Centrifugal thin film dryer

Info

Publication number
JPS60244301A
JPS60244301A JP9909884A JP9909884A JPS60244301A JP S60244301 A JPS60244301 A JP S60244301A JP 9909884 A JP9909884 A JP 9909884A JP 9909884 A JP9909884 A JP 9909884A JP S60244301 A JPS60244301 A JP S60244301A
Authority
JP
Japan
Prior art keywords
blade
thin film
wall surface
rotation speed
blades
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
JP9909884A
Other languages
Japanese (ja)
Inventor
Masaaki Sato
佐藤 昌昭
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.)
Hitachi Ltd
Original Assignee
Hitachi 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 Hitachi Ltd filed Critical Hitachi Ltd
Priority to JP9909884A priority Critical patent/JPS60244301A/en
Publication of JPS60244301A publication Critical patent/JPS60244301A/en
Pending legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B01PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
    • B01DSEPARATION
    • B01D1/00Evaporating
    • B01D1/22Evaporating by bringing a thin layer of the liquid into contact with a heated surface
    • B01D1/222In rotating vessels; vessels with movable parts
    • B01D1/223In rotating vessels; vessels with movable parts containing a rotor
    • B01D1/225In rotating vessels; vessels with movable parts containing a rotor with blades or scrapers

Abstract

PURPOSE:To reduce the abrasion of a rotary blade and the inner surface of an external cylinder, by making it possible to adjust the rotary blade in a centrifugal thin film dryer so as to bring the same to the contact or non-contact state with the inner surface of the cylinder corresponding to the number of rotations. CONSTITUTION:A solution to be treated is introduced into a cylinder 2 from a supply port 6 and the powder in the solution is adhered to the inner surface of the cylinder 2 in a thin film form by centrifugal force due to the rapid rotation of a rotary shaft 4. The thin film is dried by the heat of an outside steam jacket 1 and further fallen in a lower hopper 7 while scraped off by the rotation of rotary blades 3 when said thin film is formed, the leading end of each rotary blade 3 is separated from the inner surface of the cylinder by the centrifugal force due to the rotation of the blades 3 and the resultant moment of the springs 10 provided to one ends of the blades 3 and abrasion caused by the contact of both of them is prevented. When the thin film is scraped off from the inner surface of the cylinder, the number of rotations are adjusted to bring the leading ends of the blades 3 into contact with the inner surface of the cylinder to perfectly scrape off the powder thin film. Because the leading ends of the blades are brought into contact with the inner surface of the cylinder only when the membrane is scraped off, abrasion by the friction between both of them is reduced.

Description

【発明の詳細な説明】 〔発明の利用分野〕 本発明は、化学プラントや原子力の廃液処理設備に用い
られる遠心薄膜乾燥機に係シ、特に遠心薄膜乾燥機内壁
に付着する粉体の掻き取シを行なう翼と壁面の摩耗を低
減させる構造に関する。
Detailed Description of the Invention [Field of Application of the Invention] The present invention relates to a centrifugal thin film dryer used in chemical plants and nuclear waste liquid treatment equipment, and in particular to scraping off powder adhering to the inner wall of the centrifugal thin film dryer. This invention relates to a structure that reduces wear on the blades and walls that carry out this process.

〔発明の背景〕[Background of the invention]

遠心薄膜乾燥機は一般に竪型でありで、第2図に示すご
とく、蒸気ジャケット1に覆われた円筒2、円筒2の中
心に取付けられた回転軸4、回転軸4に放射状に取付け
られた翼3、回転軸4を回転させる電動機5、処理液供
給口6、翼3によシ掻取られた粉体を受ける下部ホッパ
7などから構成されている。
A centrifugal thin film dryer is generally vertical, and as shown in Figure 2, there is a cylinder 2 covered with a steam jacket 1, a rotating shaft 4 attached to the center of the cylinder 2, and radially attached to the rotating shaft 4. It is comprised of blades 3, an electric motor 5 that rotates a rotating shaft 4, a processing liquid supply port 6, a lower hopper 7 that receives the powder scraped by the blades 3, and the like.

前記処理液供給口6から供給された処理液(廃液など)
は、回転軸4に取シ付けられた翼3の回転に伴ない、遠
心力によシ壁面2に薄膜状に展延され、蒸気ジャケット
1で加熱されて乾燥粉体化する。乾燥粉体は翼3によシ
円筒壁面2から掻き取られ下部ホッノぐ7へ落下する。
Processing liquid (waste liquid, etc.) supplied from the processing liquid supply port 6
As the blades 3 attached to the rotating shaft 4 rotate, the material is spread in a thin film form on the wall surface 2 by centrifugal force, and is heated in the steam jacket 1 to be dried and powdered. The dry powder is scraped off from the cylindrical wall surface 2 by the blades 3 and falls into the lower hole 7.

翼3と円筒壁面2との関係は水平断面図である第3図、
第4図に示すような2種類が、従来普通である。第3図
は翼3と円筒壁面2との間に間隙を設けて一定量以上付
着した粉体を掻き取るものである。第4図は、軸4が時
計方向に回転するとき、翼3がピン8を支点にして遠心
力によって壁面2に押し付けられ、常時接触回転を行な
って粉体を完全掻き取シ除去するようにしたものである
The relationship between the blade 3 and the cylindrical wall surface 2 is shown in FIG. 3, which is a horizontal sectional view.
Two types as shown in FIG. 4 are conventionally common. In FIG. 3, a gap is provided between the blade 3 and the cylindrical wall surface 2 to scrape off powder that has adhered to a certain amount or more. Fig. 4 shows that when the shaft 4 rotates clockwise, the blades 3 are pressed against the wall surface 2 by centrifugal force using the pin 8 as a fulcrum, and the blades 3 are constantly rotated in contact to completely scrape off the powder. This is what I did.

第3図に示す構造では、翼3と壁面2とは直接に接触し
ないため、翼3及び壁面2の摩耗を防げるという利点が
ある。しかし翼3と壁面2との間隙以下に付着した粉体
又は処理液の除去は行なえず、壁面2からの熱伝達が低
下し、処理液の蒸発速度の低下、つま多処理能力の低下
となる。処理能力を上げるためには、壁面2の加熱温度
を上げることが考えられるが、加熱設備が大きくなる点
及び壁面2の熱変形が大きくなる点等、設備面で不利と
なる。また、翼3と壁面20間に付着した粉体を洗浄除
去する際も、間接的に洗浄液を遠心力によシ粉体へ吹き
つけることになるため、完全除去までの時間がかかると
いう欠点も有している。
In the structure shown in FIG. 3, since the blade 3 and the wall surface 2 do not come into direct contact with each other, there is an advantage that wear of the blade 3 and the wall surface 2 can be prevented. However, it is not possible to remove powder or processing liquid that has adhered below the gap between the blade 3 and the wall surface 2, and the heat transfer from the wall surface 2 is reduced, resulting in a decrease in the evaporation rate of the processing liquid and a reduction in the processing capacity. . In order to increase the processing capacity, it is possible to increase the heating temperature of the wall surface 2, but this is disadvantageous in terms of equipment, such as increasing the size of the heating equipment and increasing thermal deformation of the wall surface 2. In addition, when cleaning and removing the powder adhering between the blade 3 and the wall surface 20, the cleaning liquid is indirectly blown onto the powder by centrifugal force, so there is a drawback that it takes time to completely remove the powder. have.

第4図に示す構造では翼3と壁面2とが常時、接触回転
することによシ前記、熱伝達の低下による処理能力の低
下はほとんど無く、洗浄時も、強制的に翼3によシ洗浄
除去できるため、洗浄時間も少なくてすむ。しかし、常
時接触するため翼3及び壁面2の摩耗が生じ、保守上大
きな問題となる。
In the structure shown in FIG. 4, since the blade 3 and the wall surface 2 constantly rotate in contact with each other, there is almost no decrease in processing capacity due to the decrease in heat transfer, and even during cleaning, the blade 3 is forced to rotate. Since it can be removed by washing, cleaning time is also reduced. However, constant contact causes wear of the blades 3 and wall surface 2, which poses a major maintenance problem.

〔発明の目的〕[Purpose of the invention]

本発明は上記欠点を改善しようとしてなされたもので、
その目的とするところは、通常運転時は翼と壁面の間に
間隙を設けて摩耗の少ない運転を行ない、洗浄時には翼
を壁面に接触させ効率良い洗浄運転をさせることのでき
る遠心薄膜乾燥機を提供することにある。
The present invention has been made in an attempt to improve the above-mentioned drawbacks.
The purpose of this is to create a centrifugal thin film dryer that can operate with less wear by creating a gap between the blades and the wall during normal operation, and that allows the blades to come into contact with the wall during cleaning for efficient cleaning. It is about providing.

〔発明の概要〕[Summary of the invention]

本発明の特徴とするところは、遠心薄膜乾燥機の円筒内
の回転体に翼を回動可能に取付は翼自体の遠心力を利用
し、それと別に作用する制御力との合成モーメントによ
シ、回転数に応じ翼と壁面との接触および非接触状態の
選択を調整可能と′した構造にある。
The feature of the present invention is that the blades are rotatably attached to the rotating body inside the cylinder of the centrifugal thin film dryer, and the blades are rotatably mounted using the centrifugal force of the blade itself. It has a structure in which the selection of contact and non-contact states between the blades and the wall surface can be adjusted depending on the rotational speed.

これによって、翼と壁面の摩耗を低減し寿命を伸ばすこ
とと、効率良い洗浄運転が可能となる。
This reduces wear on the blades and walls, extends their lifespan, and enables efficient cleaning operations.

〔発明の実施例〕[Embodiments of the invention]

以下本発明の詳細な説明する。 The present invention will be explained in detail below.

第1図は、圧縮バネを利用した一実施例に係る遠心薄膜
乾燥機の断面部分上面図である。第5図は第1図の入方
向から見た図である。第6図はその作動説明図である。
FIG. 1 is a cross-sectional top view of a centrifugal thin film dryer according to an embodiment using a compression spring. FIG. 5 is a view seen from the entrance direction of FIG. 1. FIG. 6 is an explanatory diagram of its operation.

従来例と同一構成は同一符号で示す。Components that are the same as those of the conventional example are indicated by the same reference numerals.

これらの図において翼3は回転軸4に取付けた支持フレ
ーム11に対してピ/8を軸にして回転可能に支持され
ておシ、ピン8を境にして内周側に圧縮バネlOを翼3
と支持7レーム11に取付けられたプレート14の間に
取付け、翼3を壁面に押付ける力Fkを与えておく。ま
た翼3のピン8を境に内周側3aの重量と外周側3bの
重量は、それらに働く遠心力によシ翼3を壁面2から離
れる方向に回転させる回転力を生ずるように構成しであ
る。すなわち、回転軸4が回転するに伴ない翼3の内周
側3aに生じる遠心力F1が、外周側3bに生じる遠心
力F;よりも大きくなるように構成しである。そして設
定回転数でこれら遠心力による翼3のピン8を中心にし
た回転力と釣シ合うようバネ10の取付は位置及びその
バネ力Fk1並びに翼3の内周側3aの重量及び重心位
置、外周側3bの重量及び重心位置を決めておく。また
設定回転数以上の回転数で翼3が壁面2よシ離れるため
、翼3と壁面2の間隙を一定に保つためのストッ/ぐ9
をグレート14に設けている。
In these figures, the blade 3 is supported rotatably around pin 8 with respect to a support frame 11 attached to a rotating shaft 4, and a compression spring lO is attached to the inner circumference side of the blade with the pin 8 as the boundary. 3
and the plate 14 attached to the support 7 frame 11 to apply a force Fk to press the wing 3 against the wall surface. Further, the weight of the inner circumferential side 3a and the outer circumferential side 3b of the blade 3 with the pin 8 as a boundary are configured to generate a rotational force that rotates the blade 3 in a direction away from the wall surface 2 due to the centrifugal force acting on them. It is. That is, as the rotating shaft 4 rotates, the centrifugal force F1 generated on the inner peripheral side 3a of the blade 3 is larger than the centrifugal force F; generated on the outer peripheral side 3b. The mounting position of the spring 10 and its spring force Fk1, as well as the weight and center of gravity position of the inner peripheral side 3a of the blade 3, are determined so as to balance the rotational force of the blade 3 around the pin 8 due to the centrifugal force at the set rotation speed. The weight and center of gravity position of the outer peripheral side 3b are determined in advance. In addition, since the blade 3 separates from the wall surface 2 at a rotation speed higher than the set rotation speed, a stopper 9 is required to keep the gap between the blade 3 and the wall surface 2 constant.
is provided in Great 14.

この構成によれば、設定回転数以上を通常運転領域とす
ることによシ、通常運転中は翼3と壁面2は一定間隙を
持って運転することになシ、摩耗を防ぐことができる。
According to this configuration, by setting the rotation speed above the set rotation speed as the normal operating range, the blade 3 and the wall surface 2 are operated with a certain gap during normal operation, and wear can be prevented.

また洗浄運転は設定回転数以下で行なえば、翼3は壁面
2に押し付けられた状態で回転するため、間隙を保った
洗浄運転に比べて、よシ短時間で洗浄が行なえる。
Further, if the cleaning operation is performed at a rotation speed below the set rotation speed, the blades 3 rotate while being pressed against the wall surface 2, so that cleaning can be performed in a much shorter time than in a cleaning operation in which a gap is maintained.

以下、翼3に働らく力関係を第6図をもとに詳細に説明
する。使用する符号は下記のとおシであるO mi 翼3の内周側3aの重量(klil)m; 翼3
の外周側3bの重量(kg)R1翼3の内周側3aの重
心の回転半径(m)R2i 翼3の外周側3bの重心の
回転半径(m)θi 翼3の内周側3aの重心と回転中
心4及びピン8とのなす角(度) θ5翼3の外周側3bの重心と回転中心4及びピン8と
のなす角(度) θ、圧縮バネ10による力の方向と、回転中心4及びピ
ンを結ぶ線とのなす角(度) δ5 翼3の初期角度(翼を壁面2に押し付けた状態)
(度) F、翼3の内周側3&に働らく遠心力(kliJ)F6
 翼3の外周側3bに働らく遠心力(kg)Fb 翼3
の外周端が壁面2を押す力(kg)Fk バネ10によ
シ翼3に加わる力(kg)t、翼3の内周側3aの重心
とぎン8との距離(m) t6 翼3の外周側3bの重心とピン8との距離(m) Lk バネ10の取付位置とピン8との距離(m)tb
 翼3の外周端とピン8との距離(−)K バネ定数(
kg7m ) δにバネ10の変位(初期変位)(m)δ1 バネ10
の変位(ストッp49に[3が治るまでのバネ10の変
位)(m) N 回転数(rpm ) ω 角速度 ω=(2πN)/60 (rad/see
)g 重力加速度(9,8m/s2) M、翼3を壁面2に押し付ける方向のモーメント (R
19・m) ML 翼3を壁面2から離す方向のモーメント(kg・
m) 々お、ストッ/f9に蟲たった状態での各寸法、角度に
は′をつけて示すものとする。
Hereinafter, the force relationship acting on the blade 3 will be explained in detail based on FIG. 6. The codes used are as follows: O mi Weight of inner peripheral side 3a of blade 3 (klil) m; Blade 3
Weight of the outer circumferential side 3b (kg) R1 Radius of rotation of the center of gravity of the inner circumferential side 3a of the blade 3 (m) R2i Radius of rotation of the center of gravity of the outer circumferential side 3b of the blade 3 (m) θi Center of gravity of the inner circumferential side 3a of the blade 3 Angle (degrees) between the center of gravity of the blade 3 and the center of rotation 4 and the pin 8 (degrees) θ5 Angle (degrees) between the center of gravity of the outer circumferential side 3b of the blade 3 and the center of rotation 4 and the pin 8 θ, direction of force by the compression spring 10, and center of rotation 4 and the line connecting the pin (degrees) δ5 Initial angle of blade 3 (when the blade is pressed against wall 2)
(degrees) F, centrifugal force acting on the inner circumferential side 3& of blade 3 (kliJ) F6
Centrifugal force (kg) Fb acting on the outer peripheral side 3b of the blade 3
The force (kg) that the outer peripheral end of the blade pushes against the wall 2 (kg) Fk The force (kg) t exerted on the blade 3 by the spring 10, the distance between the center of gravity of the inner peripheral side 3a of the blade 3 and the pin 8 (m) t6 of the blade 3 Distance between the center of gravity of the outer circumferential side 3b and pin 8 (m) Lk Distance between the mounting position of spring 10 and pin 8 (m) tb
Distance (-)K between the outer peripheral edge of the blade 3 and the pin 8 Spring constant (
kg7m) Displacement (initial displacement) of spring 10 in δ (m) δ1 Spring 10
Displacement (displacement of spring 10 until stop 49 recovers [3]) (m) N Number of rotations (rpm) ω Angular velocity ω = (2πN)/60 (rad/see
) g Gravitational acceleration (9.8 m/s2) M, moment in the direction of pressing the blade 3 against the wall 2 (R
19・m) ML Moment in the direction of separating the blade 3 from the wall 2 (kg・
m) Each dimension and angle in the position of the stop/f9 shall be indicated with a '.

回転数Nの時に翼3の内周側3m、外周側3bの重心位
置にかかる力は、その時の角速度ω=2πN/60とし
て F1=(m17g)R1・ω2.Fδ=(m67g)・
R6・ω2釣シ合い式を考えるのに、ピン8回シのモニ
メントを考え、 MR=Frcotθ6−1−、−cowθb+δに−に
11COsθに+tkIICO8θbML=Fi+co
IIe1−4iacosθbとなる。
When the rotational speed is N, the force applied to the center of gravity of the inner circumferential side 3m and the outer circumferential side 3b of the blade 3 is expressed as F1=(m17g)R1・ω2. Fδ=(m67g)・
To consider the R6・ω2 balance equation, consider the monument of pin 8 times, MR=Frcotθ6−1−, −cowθb+δ−11COsθ+tkIICO8θbML=Fi+co
IIe1-4iacosθb.

回転数Oの場合はFH* FlがOであるから、MR=
δに4KIIcosθに’ tk’ e Ol!θbM
L=0 となシ、翼3はMRに相当するモーメントで壁面2に押
し付けられる。
When the rotation speed is O, FH* Fl is O, so MR=
δ to 4KII cos θ to 'tk' e Ol! θbM
When L=0, the blade 3 is pressed against the wall surface 2 with a moment corresponding to MR.

設定回転数Nの時Mn ” MLとなる様に各寸法重量
を決めれば、すなわちω。=2πN0/ 60として(
m、;/g)・R6φω。”eosθ−・l−・cos
θb 0 +δに+KCO8θに―tkjCOIIθb=(m1/
g)・R1−ω。2・cOaθ1”t1’e08θbを
満足するように決めれば、設定回転数以上ではMR< 
ML、設定回転数以下ではM、 > MLとなる。
If the weight of each dimension is determined so that Mn'' ML at the set rotation speed N, that is, ω.=2πN0/60 (
m,;/g)・R6φω. ``eosθ-・l-・cos
θb 0 +δ to +KCO8θ−tkjCOIIθb=(m1/
g)・R1−ω. If it is determined to satisfy 2・cOaθ1”t1'e08θb, MR<
ML, below the set rotation speed, M > ML.

次に翼3が壁面2から離れ、ストツノ4−9に当だシ停
止した瞬間では、バネの変位はδ、+δ8.とな) (m、/g ) ’R5’−ω2・cosθ5′・を謔
08θb′+(δに十δgt)K*eosθに′・tk
−cosθb′=(町/g)・RI”4”’eo!1I
91’41 Ncosab’なる約9合いとなる。すな
わち Fi′=(m1/g)・R5′・ω2・F5′=(m、
、/g)・R,;′・ω2として MR’=F、;’ aosθo ” t5 ’ (40
8θb′+ (δに十δ8t)・に@cosθに′・t
kaco8θb1ML ’ =F 1 ’ ・c O!
lθI′et1噂cosI9b′で、MR′=ML′と
なりた時である。
Next, at the moment when the wing 3 leaves the wall 2 and stops when it hits the strut 4-9, the displacement of the spring is δ, +δ8. ) (m, /g) 'R5'-ω2・cosθ5′・08θb′+(δ10δgt)K*eosθ′・tk
-cosθb'=(town/g)・RI"4"'eo! 1I
91'41 Ncosab', which is about 9 matches. That is, Fi'=(m1/g)・R5'・ω2・F5'=(m,
, /g)・R, ;′・ω2, MR′=F, ;′ aosθo ” t5 ′ (40
8θb′+ (10δ8t for δ)・@cosθ′・t
kaco8θb1ML' =F 1' ・c O!
This is when MR'=ML' with lθI'et1 rumor cosI9b'.

以上の約9合いから MR≧MLでは、翼3は壁面2に接触。From about 9 matches above When MR≧ML, the blade 3 contacts the wall surface 2.

MR(M、 (M、’では、翼3は壁面2よシ離れ、か
つストツノf −9にも当たらない。
In MR(M, (M,'), the blade 3 is away from the wall 2 and does not hit the strut f -9.

M、’<MLでは、翼3は壁面2よシ離れストッパー9
に当たシ壁面2と一定の間隙を持つ。
When M,'<ML, the wing 3 is separated from the wall 2 by the stopper 9.
There is a certain gap between the contact wall surface 2 and the wall surface 2.

上記の状態を角速度ωすなわち回転数Nで制御すること
によシ、翼3と壁面2の接触または非接触一定間隙の運
転が行なえる。
By controlling the above state using the angular velocity ω, that is, the rotational speed N, it is possible to operate the blade 3 and the wall surface 2 with a constant gap or in contact with each other.

第7図に右回シモーメントMRと回転数の関係、第8図
に左回シモーメントMLと回転数の関係、第9図には右
回シモーメントと左回シモーメントとの差と回転数の関
係を示し、第10図は翼3と壁面2の間隙と回転数との
関係を示す。
Figure 7 shows the relationship between the right-handed moment MR and the rotation speed, Figure 8 shows the relationship between the left-handed moment ML and the number of rotations, and Figure 9 shows the difference between the right-handed moment and the left-handed moment and the number of rotations. FIG. 10 shows the relationship between the gap between the blade 3 and the wall surface 2 and the rotation speed.

第11図は別の実施例を宗す。本実施例は第1図に示し
た圧縮バネ10、ストツノ母9を翼3の外周側に設けた
ものであシ、遠心力による動作は前記実施列と同じであ
って、翼3は、設定回転数以上では壁面2から離れ、設
定回転数以下では壁面2に接する。
FIG. 11 shows another embodiment. In this embodiment, the compression spring 10 and the strut spring 9 shown in FIG. When the rotation speed is higher than the set rotation speed, it separates from the wall surface 2, and when the rotation speed is lower than the set rotation speed, it comes into contact with the wall surface 2.

第12図は他の実施例を示す。第13図は第12図をA
方向から見た図である。1jL3はビン8よシ内周側に
外周に向って昇シ勾配を持つ長孔13を有し、長孔13
にはそれに沿って転=h可能々バランスウェイト12が
組込まれている。また翼3の内周側は、遠心力によl)
 /Jランスウェイト12が外周方向に移動することが
可能な角度で、かつ回転方向と逆向きに折曲げである。
FIG. 12 shows another embodiment. Figure 13 is the same as Figure 12.
It is a figure seen from the direction. 1jL3 has a long hole 13 on the inner circumferential side of the bottle 8 with an ascending slope toward the outer circumference.
A balance weight 12 is incorporated therein so that it can be rotated along it. Also, the inner circumferential side of the blade 3 is affected by centrifugal force.
/J It is bent at an angle that allows the run weight 12 to move in the outer circumferential direction and in the opposite direction to the rotation direction.

支持フレーム11の外周には翼3と壁面2の間隙量を制
限するスト、パ9が設けである。長孔13の角度は、設
定回転数以上で始めてバランスウェイト12が上昇可能
々角度としである。以下、この実施例の作用を第14図
、第15図を用いて詳細説明する。
A stop 9 is provided on the outer periphery of the support frame 11 to limit the amount of gap between the blade 3 and the wall surface 2. The angle of the elongated hole 13 is such that the balance weight 12 can only rise when the number of revolutions exceeds the set rotation speed. The operation of this embodiment will be explained in detail below with reference to FIGS. 14 and 15.

第14図は設定回転数以下で、バランスウェイト12が
長孔13の最下点にある場合の翼3の内周側3aと外周
側3b、及びバランスウェイト12に働く遠心力の状況
を示し、第15図は設定回転数以上でバランスウェイト
12が長孔13の最上点にある場合を示す。設定回転数
以下では第14図のようにバランスウェイト12に生じ
る゛遠心力Fcは、翼3を右回シ、すなわち翼3を壁面
2に押付ける方向の力として作用し、設定回転数以上で
は第15図のように翼3を左回シ、すなわち翼3を壁面
2よシ離す方向の力として作用する。
FIG. 14 shows the situation of centrifugal force acting on the inner circumferential side 3a and outer circumferential side 3b of the blade 3 and the balance weight 12 when the balance weight 12 is at the lowest point of the elongated hole 13 when the rotation speed is below the set rotation speed, FIG. 15 shows a case where the balance weight 12 is at the highest point of the elongated hole 13 when the rotation speed is higher than the set rotation speed. Below the set rotation speed, the centrifugal force Fc generated in the balance weight 12 as shown in Fig. 14 acts as a force in the direction of turning the blade 3 clockwise, that is, pressing the blade 3 against the wall surface 2, and above the set rotation speed. As shown in FIG. 15, it acts as a force in the direction of turning the blade 3 to the left, that is, moving the blade 3 away from the wall surface 2.

これによシ回転軸4の回転数に依存して翼3と壁面2の
接触または非接触一定間隙の運転が行なえる。
As a result, depending on the rotational speed of the rotary shaft 4, the blade 3 and the wall surface 2 can be operated with a constant gap or in contact or non-contact.

次に更に他の実施例を第16図に示す。本図においては
、第1図と異シ、バネ1oは引張バネとして予め伸ばし
て取シ付け、翼3を壁面2から引き離す方向の力Fkを
与えておシ、また1IL3の内周側3aに働く遠心力F
、は外周側3bに働く遠心力F6よシ小さくなるよう構
成されている。したがって第1′図の説明と同一符号を
用いればMR−FrCO8θ、;−2δ8cosθbM
L=p、 HeOJlθ1IIt1・coBθb十δに
・K11coIIθに曾tk轡cosebMR’=F5
′・co@θ、;”z2B’cosθb′ML’=F1
’cosθ、’mAiacosθb′+(δに十δ5t
)K*cosθk” tk’ e Oa 19 b’と
なる。MRI MLは第1図では翼3と壁面2が接触し
た状態を示し、またMB ’ + ML ’は翼3とス
トッパ9が当たりた状態を示すものであったが、本実施
例ではMR,MLは翼3がバネ10によシストツバ9に
当っている状態、そしてMn ’ + ML ’は遠心
力−によシ翼3が壁面2と接触している状態を示す。
Next, still another embodiment is shown in FIG. In this figure, unlike in Figure 1, the spring 1o is stretched and attached in advance as a tension spring, and a force Fk is applied in the direction of separating the blade 3 from the wall surface 2. Centrifugal force F
, are configured to be smaller than the centrifugal force F6 acting on the outer peripheral side 3b. Therefore, using the same symbols as in the explanation of Fig. 1', MR-FrCO8θ, ;-2δ8cosθbM
L=p, HeOJlθ1IIt1・coBθb+δ・K11coIIθ=tkcosebMR'=F5
'・co@θ,;"z2B'cosθb'ML'=F1
'cos θ, 'mAia cos θb' + (10 δ5t for δ
)K*cosθk''tk' e Oa 19 b'. MRI ML shows the state where the blade 3 and the wall surface 2 are in contact in Fig. 1, and MB' + ML' shows the state where the blade 3 and the stopper 9 are in contact. However, in this example, MR and ML are the state where the blade 3 is in contact with the cyst collar 9 due to the spring 10, and Mn' + ML' is the state where the blade 3 is in contact with the wall surface 2 due to centrifugal force. Indicates a state of contact.

したがって ML〉MRでは翼3はストッ・49に当たシ壁面2よシ
一定の間隙を持っている。
Therefore, when ML>MR, the blade 3 hits the stop 49 and has a constant gap from the wall surface 2.

ML<MR<MR′では翼3はストッパ9よシ離れ、か
つ壁面2とも接触しない。
When ML<MR<MR', the blade 3 is away from the stopper 9 and does not come into contact with the wall surface 2 either.

MR′りMRでは翼3は壁面2に接触する。MR' In MR, the blade 3 contacts the wall surface 2.

上記の状態を回転数Nで制御することにょシ、翼3と壁
面2の接触または非接触一定間隙の運転が行なえる。す
なわち、設定回転数以下では非接触一定間隙運転、設定
回転数以上で接触運転が可能と々る。
By controlling the above-mentioned state with the rotational speed N, it is possible to operate the blade 3 and the wall surface 2 with a constant gap or in contact with each other or without contact. That is, non-contact constant gap operation is possible below the set rotation speed, and contact operation is possible above the set rotation speed.

第17図は第16図の変形実施例を示すものである。本
実施例では第16図に示した弾性体である引張バネ10
およびストッパ9を支持フレーム11の外周側に設けた
ものであシ、動作は第16図実施例と同様である。
FIG. 17 shows a modified embodiment of FIG. 16. In this embodiment, a tension spring 10 which is an elastic body shown in FIG.
The stopper 9 is provided on the outer peripheral side of the support frame 11, and the operation is the same as that of the embodiment shown in FIG.

第18図はシフト可能な錘を用いた他の実施例を示す。FIG. 18 shows another embodiment using a shiftable weight.

第19図は第18図をAから見たものである。翼3はピ
ン8よシ内周側から外周側に向い昇シ勾配を持つ長孔1
3を有し、長孔13にはそれに沿って転がシ可能なバラ
ンスウェイト12が組込まれている。また支持フレーム
の外周側には翼3と壁面2の間隙量を一定にするストツ
ノf9が設けである。長孔13の角度は設定回転数以上
で始めてバランスウェイト12が長孔13中を上昇可能
であるような角度としである。
FIG. 19 is a view of FIG. 18 from A. The blade 3 has a long hole 1 which has an upward slope from the inner circumferential side to the outer circumferential side from the pin 8.
3, and a balance weight 12 that can be rolled along the elongated hole 13 is incorporated therein. Further, on the outer circumferential side of the support frame, there is provided a strut horn f9 that keeps the gap between the blade 3 and the wall surface 2 constant. The angle of the elongated hole 13 is such that the balance weight 12 can move up through the elongated hole 13 only when the number of rotations exceeds the set rotation speed.

本実施例は、設定回転数以下ではバランスウェイト12
が溝13の最下点、つt、b最も内周側にあわ、このと
きバランスウェイト12に働く遠心力は翼3を左回シ、
すなわち翼3をストツノ49に押し付け、翼3と壁面2
の間の間隙を一定にする方向に作用し、設定回転数以上
では、バランスウェイ)12が溝13内を上昇して最上
点、すなわち最も外周側に来たシ、このときバランスウ
ェイト12に働く遠心力は翼3を右回シ、すなわち、翼
3を壁面2に押し付ける方向に作用するよう構成されて
いる。これによシ設定回転数以下では非接触一定間隙運
転、設定回転数以上では接触運転が可能となる。
In this embodiment, the balance weight is 12 below the set rotation speed.
is the lowest point of the groove 13, t, b is on the innermost side, and at this time, the centrifugal force acting on the balance weight 12 rotates the blade 3 counterclockwise.
In other words, the wing 3 is pressed against the strut horn 49, and the wing 3 and the wall surface 2 are
When the rotation speed exceeds the set rotation speed, the balance weight 12 rises within the groove 13 and reaches the highest point, that is, the outermost side, and at this time it acts on the balance weight 12. The centrifugal force is configured to act on the blade 3 in a clockwise direction, that is, in a direction that presses the blade 3 against the wall surface 2. This allows non-contact constant gap operation below the set rotation speed, and contact operation above the set rotation speed.

以上説明したように、設定回転数以下で接触、設定回転
数以上で非接触となる実施例、および、逆に、設定回転
数以下で非接触、設定回転数以上で接触となる実施例が
可能であるが、いずれにせよ、通常運転は非接触状態、
洗浄運転は接触状態とすることによって、翼および円筒
壁面の摩耗の防止ならびに効率的な洗□浄が可能とな石
As explained above, it is possible to have an embodiment in which contact occurs below the set rotation speed and non-contact occurs above the set rotation speed, and, conversely, an embodiment in which contact occurs below the set rotation speed and contact occurs above the set rotation speed. However, in any case, normal operation is in a non-contact state,
By keeping the stone in contact during the cleaning operation, it is possible to prevent wear on the blades and the cylindrical wall and to perform efficient cleaning.

〔発明の効果〕〔Effect of the invention〕

本発明によれば、回転数の制御にょシ、遠心薄膜乾燥機
の翼と円筒壁面の摩耗の少ない非接触一定間隙運転と、
翼と壁面が接触した能率的な洗浄運転が可能となシ、寿
命の延長ならびに運転時間の短縮を図ることができる。
According to the present invention, rotation speed control, non-contact constant gap operation with less wear on the blades and cylindrical wall surface of the centrifugal thin film dryer,
Efficient cleaning operation with the blades and wall in contact is possible, extending life and shortening operating time.

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

第1図は本発明の一実施例の横断面部分図、第2図は遠
心薄膜乾燥機の全体的縦断面図、第3図・は固定翼と壁
面との間に一定間隙を有する従来例の横断面図、第4図
は翼可動構造の従来例の横断面図、第5図は第1図のA
方向に見た部分図、第6図は第1図実施例の動作説明図
、第7図ないし第10図は該実施例の動作の様子を示す
グラフ、第11図は本発明の他の実施例の横断面部分図
、第12図は更に他の実施例の部分図、第13図は第1
2図のA方向に見た図、第14図、第15図は第12図
実施例の動作説明図、第16図、第17図、第18図は
夫々異る他の実施例の部分図、第19図は第18図のA
方向に見た図である。 1:蒸気ジャケット 2:円筒壁面 3:翼 4:回転軸 8:ビン 9:ストッパ 10:バネ 11:支持フレーム 12:バランスウェイト 13:長孔 14:プレート 第1図 内p0イ#↑1 タトp0イ鐸11 第3図 第4図 第5図 第6図 第7図 第9図 第10図 IgJ蒙ムを火N 第11図 第12図 第13図 第14図 第16図 第17図
Fig. 1 is a partial cross-sectional view of an embodiment of the present invention, Fig. 2 is an overall vertical cross-sectional view of a centrifugal thin film dryer, and Fig. 3 is a conventional example having a fixed gap between the fixed blade and the wall surface. 4 is a cross sectional view of a conventional example of a movable wing structure, and FIG. 5 is a cross sectional view of A of FIG. 1.
6 is an explanatory diagram of the operation of the embodiment shown in FIG. 1, FIGS. 7 to 10 are graphs showing the operation of the embodiment, and FIG. 11 is a diagram showing another embodiment of the present invention. FIG. 12 is a partial cross-sectional view of the example, FIG. 12 is a partial view of another embodiment, and FIG.
2, as seen in the A direction, FIGS. 14 and 15 are explanatory diagrams of the operation of the embodiment in FIG. 12, and FIGS. 16, 17, and 18 are partial views of other different embodiments. , Figure 19 is A of Figure 18.
It is a view seen in the direction. 1: Steam jacket 2: Cylindrical wall surface 3: Wing 4: Rotating shaft 8: Bottle 9: Stopper 10: Spring 11: Support frame 12: Balance weight 13: Long hole 14: Plate p0 I#↑1 Tato p0 in Figure 1 11 Figure 3 Figure 4 Figure 5 Figure 6 Figure 7 Figure 9 Figure 10 Figure 11 Figure 12 Figure 13 Figure 14 Figure 16 Figure 17

Claims (1)

【特許請求の範囲】 1、 内部に処理液が供給され且つ壁面が加熱される円
筒容器と、円筒容器の中心線の周シに回転する支持フレ
ームと、支持フレームに取付けられ上記壁面の内面に前
記処理液の薄膜の形成・蒸発によって生じた粉末を掻き
取る翼とからなる遠心薄膜乾燥機において、翼を円筒容
器の中心線と平行な軸を中心として回動自在に支持フレ
ームに取付けると共に、翼に制御力を作用させる制御部
材を設け、支持フレームの回転に伴う翼自体に作用する
遠心力と上記制御力との上記軸に関する合モーメントに
よシ、支持フレームの回転速度が設定回転速度以上であ
るか以下であるかに応じて、翼が前記壁面の内面と接触
または離間せしめられ、更に翼の前記壁面からの離間量
を制限するストッ・ぐ−を備えたことを特徴とする遠心
薄膜乾燥機。 2、翼は、支持フレームの回転速度が設定回転速度以上
のとき前記壁面と接触し、以下であるとき前記壁面から
離間する特許請求の範囲第1項記載の遠心薄膜乾燥機。 3、翼は、支持フレームの回転速度が設定回転速度以上
のとき前記壁面から離間し、以下であるとき前記壁面と
接触する特許請求の範囲第1項記載の遠心薄膜乾燥機。 4、制御部材は支持フレームと翼との間に架したバネで
ある特許請求の範囲第1項、第2項又は第3項記載の遠
心薄膜乾燥機。 5、制御部材は、翼に取シ付けられ遠心力によシ翼に対
して相対的に移動可能なバランスウェイトである特許請
求の範囲第1項、第2項、又は第3項記載の遠心薄膜乾
燥機。
[Claims] 1. A cylindrical container into which a processing liquid is supplied and whose wall surface is heated; a support frame that rotates around the center line of the cylindrical container; In a centrifugal thin film dryer comprising blades for scraping powder generated by formation and evaporation of a thin film of the processing liquid, the blades are attached to a support frame so as to be rotatable about an axis parallel to the center line of the cylindrical container, and A control member is provided to apply a control force to the blade, and due to the sum of the centrifugal force acting on the blade itself due to rotation of the support frame and the control force with respect to the axis, the rotation speed of the support frame is equal to or higher than the set rotation speed. The centrifugal thin film is characterized in that the blades are brought into contact with or separated from the inner surface of the wall surface depending on whether the blades are in contact with or separated from the inner surface of the wall surface, and further comprising a stopper for limiting the amount of separation of the blades from the wall surface. Dryer. 2. The centrifugal thin film dryer according to claim 1, wherein the blades contact the wall surface when the rotation speed of the support frame is equal to or higher than a set rotation speed, and are separated from the wall surface when the rotation speed is lower than the set rotation speed. 3. The centrifugal thin film dryer according to claim 1, wherein the blade separates from the wall surface when the rotation speed of the support frame is above a set rotation speed, and comes into contact with the wall surface when the rotation speed is below. 4. The centrifugal thin film dryer according to claim 1, 2 or 3, wherein the control member is a spring suspended between the support frame and the blade. 5. The centrifugal device according to claim 1, 2, or 3, wherein the control member is a balance weight attached to the blade and movable relative to the blade due to centrifugal force. Thin film dryer.
JP9909884A 1984-05-17 1984-05-17 Centrifugal thin film dryer Pending JPS60244301A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP9909884A JPS60244301A (en) 1984-05-17 1984-05-17 Centrifugal thin film dryer

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP9909884A JPS60244301A (en) 1984-05-17 1984-05-17 Centrifugal thin film dryer

Publications (1)

Publication Number Publication Date
JPS60244301A true JPS60244301A (en) 1985-12-04

Family

ID=14238385

Family Applications (1)

Application Number Title Priority Date Filing Date
JP9909884A Pending JPS60244301A (en) 1984-05-17 1984-05-17 Centrifugal thin film dryer

Country Status (1)

Country Link
JP (1) JPS60244301A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2002084189A1 (en) * 2001-04-18 2002-10-24 Giuseppe Bobbiesi Thin film cyclic continuous dryer
JP2013530835A (en) * 2010-07-21 2013-08-01 アクアバック・テクノロジーズ・インコーポレーテッド Distillation equipment
JP2017154046A (en) * 2016-02-29 2017-09-07 株式会社カジワラ Scraping and pressing type heating agitator

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2002084189A1 (en) * 2001-04-18 2002-10-24 Giuseppe Bobbiesi Thin film cyclic continuous dryer
JP2013530835A (en) * 2010-07-21 2013-08-01 アクアバック・テクノロジーズ・インコーポレーテッド Distillation equipment
US9770676B2 (en) 2010-07-21 2017-09-26 Aquaback Technologies, Inc. Distiller
JP2017154046A (en) * 2016-02-29 2017-09-07 株式会社カジワラ Scraping and pressing type heating agitator

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