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JPH0125909B2 - - Google Patents

Info

Publication number
JPH0125909B2
JPH0125909B2 JP57172822A JP17282282A JPH0125909B2 JP H0125909 B2 JPH0125909 B2 JP H0125909B2 JP 57172822 A JP57172822 A JP 57172822A JP 17282282 A JP17282282 A JP 17282282A JP H0125909 B2 JPH0125909 B2 JP H0125909B2
Authority
JP
Japan
Prior art keywords
shaped
spiral
blade
groove
peripheral surface
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
Application number
JP57172822A
Other languages
Japanese (ja)
Other versions
JPS5960086A (en
Inventor
Yasuo Kita
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.)
Shimadzu Corp
Original Assignee
Shimadzu Corp
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 Shimadzu Corp filed Critical Shimadzu Corp
Priority to JP17282282A priority Critical patent/JPS5960086A/en
Publication of JPS5960086A publication Critical patent/JPS5960086A/en
Publication of JPH0125909B2 publication Critical patent/JPH0125909B2/ja
Granted legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04CROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
    • F04C15/00Component parts, details or accessories of machines, pumps or pumping installations, not provided for in groups F04C2/00 - F04C14/00

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Measuring Volume Flow (AREA)
  • Rotary Pumps (AREA)

Description

【発明の詳細な説明】 本発明は、一般に、Cリング式ポンプまたはス
クロール形ポンプ等と称されている容積型の流体
機械に関するものである。
DETAILED DESCRIPTION OF THE INVENTION The present invention relates to a positive displacement fluid machine generally referred to as a C-ring pump or scroll pump.

この種の流体機械としては例えば、前述のCリ
ング式ポンプ等が知られているが、このCリング
式ポンプの場合はケースの端面に、一端が流入口
に連通し他端が流出口に連通するC形溝を設ける
とともに、このC形溝の開口端面に蓋着したデイ
スクから、該C形溝の内側面間に遊嵌し、かつ、
その先端面が前記C形溝の底面に摺接するC形翼
を突設し、このC形翼を、該C形溝の内周面およ
び外周面の少なくとも一方が前記C形溝の内側面
に当接するように前記C形溝の曲率中心から所定
距離だけ偏心させて配置し、このC形翼にその偏
心軌道に沿うみそすり運動を行わせることによつ
て、前記C形溝内に充満する流体を前記流入口側
から前記流出口側へ移動させ得るように構成した
ポンプユニツトを具備している。以下、かかるC
リング式ポンプを中心にして説明を進めるが、こ
のような構成の流体機械によれば、前記ポンプユ
ニツトを複数組直列に接続するとともに、これら
各ユニツトのC形翼を所要角度だけ相互に位相を
異ならせた状態で同期的に作動させ得るようにす
ることによつて、脈動のない容積型のポンプを構
成することが可能であり、また、逆に、流体を前
記各ユニツトに導入して、これら各ユニツトのC
形翼を強制的に作動させ、その作動力を外部に取
り出し得るようにすることによつて、圧力損失の
少ない流量計や高速から低速まで広範囲に亘つて
安定に作動するモータを構成することができるも
のである。
For example, the above-mentioned C-ring type pump is known as this type of fluid machine, but in the case of this C-ring type pump, one end communicates with the inlet and the other end communicates with the outlet on the end face of the case. A C-shaped groove is provided, and a disk fitted with a lid on the open end surface of the C-shaped groove is loosely fitted between the inner surfaces of the C-shaped groove, and
A C-shaped blade whose tip surface slides in sliding contact with the bottom surface of the C-shaped groove is provided, and at least one of the inner circumferential surface and the outer circumferential surface of the C-shaped groove is in contact with the inner surface of the C-shaped groove. The C-shaped groove is filled by placing the C-shaped blade eccentrically by a predetermined distance from the center of curvature of the C-shaped groove so as to make contact therewith, and causing the C-shaped blade to perform a sliding motion along its eccentric trajectory. The pump unit includes a pump unit configured to move fluid from the inlet side to the outlet side. Below, such C
The explanation will focus on a ring type pump, but according to a fluid machine with such a configuration, a plurality of pump units are connected in series, and the C-shaped blades of each unit are shifted in phase from each other by a required angle. By enabling synchronous operation in different states, it is possible to construct a positive displacement pump without pulsation, and conversely, by introducing fluid into each of the units, C of each of these units
By forcibly operating shaped blades and making the operating force available to the outside, it is possible to construct flowmeters with low pressure loss and motors that operate stably over a wide range of speeds from high to low. It is possible.

ところが、従来ものは、前記C形翼の内周面と
外周面および前記C形溝の両内側面をそれぞれ円
柱面にしているので、大量生産が難しいという問
題がある。すなわち、前記内外周面および、前記
内側面をそれぞれユニツトの軸心と平行な母線に
より形成される円柱面とした場合には、抜き勾配
を確保することができないので、前記C形翼や前
記C形溝を有するケースを型加工により製作する
のが非常に難しい。そのため、少なくともかかる
円柱面部分は機械加工により形成せざるを得ない
という面倒さがあり、製作に手間がかかるという
不都合がある。
However, in the conventional type, the inner circumferential surface and outer circumferential surface of the C-shaped blade and both inner circumferential surfaces of the C-shaped groove are respectively cylindrical surfaces, so there is a problem that mass production is difficult. That is, if the inner and outer circumferential surfaces and the inner surface are respectively cylindrical surfaces formed by generatrix lines parallel to the axis of the unit, draft cannot be ensured, so the C-shaped blade or the C It is extremely difficult to manufacture a case with shaped grooves by mold processing. Therefore, at least the cylindrical surface portion has to be formed by machining, which is troublesome, and there is an inconvenience that it takes time and effort to manufacture.

また、このような円柱面の場合には、翼の内外
周面と溝の内側面との接触部分および、翼の先端
面と溝の底面との接触部分がシールを行つて容積
の拡縮する密閉空間を形成するようになつてい
る。ところが、従来のものは、前記翼および溝の
外方端部および内方端部が角ばつているのが一般
的であるため、その角部分でシールの連続性が損
なわれやすいという重大な問題がある。すなわ
ち、面同士の接触部分は、その面加工の精度を向
上させたり、格別なシール部材を設けることによ
つて適切なシール性能を確保することができる
が、凹形の角と凸形の角とを正確に密着させてシ
ールすることは難しい。仮にそのシールができた
としても、使用により角が摩耗してシール性が低
下し易い。そのため、翼および溝の外方端部およ
び内方端部が角ばつた従来のものは、長期に亘つ
て所期の性能を維持するのが難しいという問題が
ある。
In addition, in the case of such a cylindrical surface, the contact area between the inner and outer circumferential surfaces of the blade and the inner surface of the groove, and the contact area between the tip surface of the blade and the bottom surface of the groove perform sealing to expand and contract the volume. It is beginning to form a space. However, in conventional methods, the outer and inner ends of the blades and grooves are generally angular, so there is a serious problem that the continuity of the seal is easily lost at the corners. There is. In other words, it is possible to ensure appropriate sealing performance at the contact area between surfaces by improving the accuracy of surface processing or by providing a special sealing member, but concave corners and convex corners It is difficult to accurately seal the two. Even if such a seal can be achieved, the corners are likely to wear due to use and the sealing performance will deteriorate. For this reason, conventional blades and grooves in which the outer and inner ends are angular have a problem in that it is difficult to maintain desired performance over a long period of time.

本発明は、このような事情に着目してなされた
もので、C形または渦巻形翼の外周面および内周
面を、該C形または渦巻形翼の厚みが先端方向に
漸次減少するように傾斜させると共に、前記C形
または渦巻形溝の各内側面を、その母線が対応す
るC形または渦巻形翼の外周面または、内周面の
母線と平行になるように傾斜させ、さらに、C形
または渦巻形翼およびC形または渦巻形溝のそれ
ぞれの外方端部および内方端部の角部分に、その
曲率半径Rが、t/10≦R≦t/2なる関係を有したア ール部を設けることによつて、前述した不都合を
効果的に解消することができるようにした容積型
流体機械を提供するものである。
The present invention has been made in view of the above-mentioned circumstances, and includes a structure in which the outer circumferential surface and inner circumferential surface of a C-shaped or spiral-shaped blade are formed such that the thickness of the C-shaped or spiral-shaped blade gradually decreases toward the tip. and inclining each inner surface of the C-shaped or spiral-shaped groove so that its generatrix is parallel to the generatrix of the outer circumferential surface or inner circumferential surface of the corresponding C-shaped or spiral-shaped blade; The radius of curvature R has a relationship of t/10≦R≦t/2 at the corner portions of the outer and inner ends of each of the C-shaped or spiral-shaped wing and the C-shaped or spiral groove. An object of the present invention is to provide a positive displacement fluid machine that can effectively eliminate the above-mentioned disadvantages by providing a section.

ここで、tは、翼の先端部の厚みである。アー
ル部の曲率半径Rを前述のように限定した理由
は、次のようである。すなわち、曲率半径Rを
t/10よりも小さくすると、翼および溝の角部分が 実質的に角ばつている場合と同様なものとなり、
摩耗によりその角部分でシールの連続性が損なわ
れ易くなる。一方、曲率半径Rをt/2よりも大き くすると、翼の先端が尖つたものになり好ましく
ない。すなわち、曲率半径Rをt/2にした場合に 翼の先端が横断面半円弧状のものとなる。したが
つて、それよりも曲率半径Rを大きくすると翼の
先端が不連続なものとなり、摩耗し易くなる。
Here, t is the thickness of the tip of the blade. The reason why the radius of curvature R of the rounded portion is limited as described above is as follows. That is, when the radius of curvature R is made smaller than t/10, the corner portions of the blade and the groove become substantially angular;
The continuity of the seal is likely to be lost at the corners due to wear. On the other hand, if the radius of curvature R is made larger than t/2, the tip of the blade becomes sharp, which is not preferable. That is, when the radius of curvature R is set to t/2, the tip of the blade has a semicircular arc shape in cross section. Therefore, if the radius of curvature R is made larger than this, the tip of the blade becomes discontinuous and becomes prone to wear.

以下、本発明をCリング式ポンプに適用した場
合の一実施例につき第1図〜第4図を参照して説
明する。
Hereinafter, an embodiment in which the present invention is applied to a C-ring type pump will be described with reference to FIGS. 1 to 4.

第1のポンプユニツトAと、第2のポンプユニ
ツトBとを直列に接続している。各ポンプユニツ
トA,Bは、ケース1,2の一端面1a,2aに
C形溝3,4を開口させるとともに、このC形溝
3,4を開口させるとともに、このC形溝3,4
の開口端面に蓋着したデイスク5,6から該C形
溝3,4の内側面7と8,9と10間に遊嵌し、
かつ、その先端面11,12が前記C形溝3,4
の底面13,14に液密に摺接するC形翼15,
16を一体的に突設し、このC形翼15,16
を、該C形翼15,16の外周面17,18およ
び内周面19,20の少なくとも一方が前記C形
溝の内側面7,8,9,10に当接するように前
記C形溝3,4の曲率中心0から所定距離だけ偏
心させて配置し、このC形翼15,16にその偏
心軌道に沿う公転円運動を行わせるようになつて
いる。前記C形溝3,4は、それぞれ3/4+α円
弧状のもので、各一端を流入口21,22に連通
させるとともに各他端を流出口23,24に連通
させてある。そして、第1のポンプユニツトAの
流出口23を第2のポンプユニツトBの流入口2
2に接続している。また、前記C形翼15,16
は3/4+α円弧状のものであり、前記C形溝3,
4の所定深さ位置における該C形溝3,4の外側
の内側面7,9の曲率半径をr1、内側の内側面
8,10の曲率半径をr2、該C形翼15,16の
平均曲率半径をr3とした場合、r3=(r1+r2)/2
なる関係式が成立するような形状寸法に設定され
ている。そして、第1のポンプユニツトAのC形
翼15と第2のポンプユニツトBのC形翼16と
を相互に90゜だけ位相を異ならせた状態で同期的
にみそすり運動させるようにしている。なお、こ
こで、みそすり運動とは、前記各C形翼15,1
6の各部が前記C形溝3,4の巾寸法(r2−r1
から該C形翼15,16の巾寸法wを減じた値に
対応する直径の円運動を行うことを意味してい
る。各C形翼15,16にみそすり運動を行わせ
るための具体的な構成は、例えば、前記両ポンプ
ユニツトA,Bを軸心を一致させて背中合せに配
置するとともに、その軸心部に共通の回転軸26
を挿通させ、この回転軸26に一体回転可能に装
着した偏心カム27,28を前記デイスク5,6
に穿設した軸孔29,30に回転可能に嵌合さ
せ、この回転軸26を回転させて前記デイスク
5,6を偏心軌道に沿つて円運動させるようにし
たものである。
A first pump unit A and a second pump unit B are connected in series. Each pump unit A, B has C-shaped grooves 3, 4 opened in one end surface 1a, 2a of the cases 1, 2;
from the disks 5, 6 which are capped on the opening end surfaces of the C-shaped grooves 3, 4, loosely fitting between the inner surfaces 7, 8, 9, 10 of the C-shaped grooves 3, 4;
And, the tip surfaces 11 and 12 are connected to the C-shaped grooves 3 and 4.
C-shaped blades 15, which slide in liquid-tight contact with the bottom surfaces 13, 14 of the
16 are integrally protruded, and these C-shaped wings 15, 16
the C-shaped groove 3 such that at least one of the outer circumferential surfaces 17, 18 and inner circumferential surfaces 19, 20 of the C-shaped blades 15, 16 abuts the inner surfaces 7, 8, 9, 10 of the C-shaped groove. , 4 are arranged eccentrically by a predetermined distance from the center of curvature 0, and the C-shaped blades 15, 16 are made to perform an orbital circular motion along their eccentric orbits. The C-shaped grooves 3 and 4 each have a 3/4+α arc shape, and each one end communicates with the inflow ports 21 and 22, and each other end communicates with the outflow ports 23 and 24. Then, the outflow port 23 of the first pump unit A is connected to the inflow port 2 of the second pump unit B.
Connected to 2. In addition, the C-shaped blades 15, 16
is a 3/4+α circular arc, and the C-shaped groove 3,
The radius of curvature of the outer inner surfaces 7, 9 of the C-shaped grooves 3, 4 at a predetermined depth position of 4 is r 1 , the radius of curvature of the inner inner surfaces 8, 10 of the C-shaped grooves 3, 4 is r 2 , the C-shaped blades 15, 16 If the average radius of curvature of is r 3 , then r 3 = (r 1 + r 2 )/2
The shape and dimensions are set so that the following relational expression holds true. Then, the C-shaped blades 15 of the first pump unit A and the C-shaped blades 16 of the second pump unit B are caused to synchronously move in a synchronous manner with their phases differing by 90 degrees. . In addition, here, the misosuri movement refers to each of the C-shaped blades 15, 1.
Each part of 6 is the width dimension (r 2 - r 1 ) of the C-shaped grooves 3 and 4.
This means performing a circular motion with a diameter corresponding to the value obtained by subtracting the width w of the C-shaped blades 15 and 16 from . A specific configuration for causing each of the C-shaped blades 15 and 16 to perform a sliding motion is, for example, by arranging both the pump units A and B back to back with their axes aligned, and having a common axis at the center of the pump units A and B. axis of rotation 26
The eccentric cams 27 and 28 are inserted into the rotating shaft 26 so as to be integrally rotatable with each other, and the eccentric cams 27 and 28 are attached to the disks 5 and 6.
The disks 5 and 6 are rotatably fitted into shaft holes 29 and 30 drilled in the disks, and the rotating shaft 26 is rotated to cause the disks 5 and 6 to move circularly along eccentric orbits.

また、前記C形翼15,16の外周面17,1
8および内周面19,20を、該C形翼15,1
6の厚みが先端方向に漸次減少するように傾斜さ
せている。また、前記C形溝3,4の内側の内側
面8,10を、その母線が前記C形翼15,16
の内周面19,20の母線と平行になるように傾
斜させるとともに、前記C形溝3,4の外側の内
側面7,9をその母線が前記C形翼の外周面1
7,18の母線と平行になるように傾斜させてい
る。なお、前記各母線は、中央大部分が直線で両
端部が略1/4の円弧線により構成されており、前
記各内側面7,8,9,10、前記外周面17,
18および前記内周面19,20の各外角部分お
よび内角部分にそれぞれアール部7a,8a,9
a,10a,17a,18a,19a,20aが
形成されている。
Further, the outer peripheral surfaces 17, 1 of the C-shaped blades 15, 16
8 and inner circumferential surfaces 19, 20, the C-shaped blades 15, 1
6 is inclined so that the thickness thereof gradually decreases toward the distal end. Further, the inner surfaces 8, 10 on the inside of the C-shaped grooves 3, 4 are arranged such that the generatrix thereof is the C-shaped blade 15, 16.
The outer inner surfaces 7, 9 of the C-shaped grooves 3, 4 are inclined so that the generatrix is parallel to the generatrix of the inner circumferential surfaces 19, 20 of the C-shaped blade.
It is tilted so as to be parallel to the generatrix lines of numbers 7 and 18. Each of the generatrix lines has a straight line at the center and an approximately 1/4 arc line at both ends, and each of the inner surfaces 7, 8, 9, 10, the outer circumferential surface 17,
18, and rounded portions 7a, 8a, 9 at each outer corner portion and inner corner portion of the inner peripheral surfaces 19, 20, respectively.
a, 10a, 17a, 18a, 19a, and 20a are formed.

すなわち、前記C形翼15,16およびC形溝
3,4のそれぞれの外方端部および内方端部の角
部分に、その曲率半径Rがt/10≦R≦t/2なる関係 のアール部7a,8a,9a,10a,17a,
18a,19a,20aを形成している。ここ
で、tは、前記C形翼15,16の先端部の厚み
寸法を示している。
That is, the corners of the outer and inner ends of the C-shaped blades 15, 16 and the C-shaped grooves 3, 4 have a radius of curvature R of t/10≦R≦t/2. Rounded portions 7a, 8a, 9a, 10a, 17a,
18a, 19a, and 20a are formed. Here, t indicates the thickness dimension of the tip portions of the C-shaped blades 15 and 16.

このような構成のものであれば、C形翼15,
16の外周面17,18が外接触部にいてC形
溝3,4の外側の内側面7,9に線接触するとと
もに、C形翼15,16の内周面19,20が内
接触部においてC形溝3,4の内側の内側面
8,10に線接触するため、前記C形溝3,4内
は前記C形翼15,16によつて鎌のような形の
流入口側の空間3a,4aと流出口側の空間3
b,4bとに分断される。そして、この状態から
回転軸26を矢印X方向へ回転移動させて前記C
形翼15,16にみそすり運動を行なわせると、
前記外接触部および前記内接触部がそれぞれ
C形溝3,4の内側面7,8,9,10に沿つて
流入口21,22から流出口23,24側へ移行
するため、前記両空間3a,3b,4a,4bも
同方向に移動することになり、これら両空間3
a,3b,4a,4bに充満している流体が流入
口21,22側から流出口23,24側へ搬送さ
れることになる。なお、前記C形翼15,16が
みそすり運動を行う過程で、前記外接触部が一
時的に無くなる時期(第4図の第1のポンプユニ
ツトAを参照)および前記内接触部が一時的に
無くなる時期(第3図の第2のポンプユニツトB
を参照)が定期的におとずれる。しかしながら、
第1のポンプユニツトAと第2のポンプユニツト
Bとの間でこれらの時期が重なることがないよう
に前記各C形翼15,16のみそすり運動の位相
を異ならせてあるので、第1のポンプユニツトA
の流入口21と第2のポンプユニツトBの流出口
24とがC形溝3,4を介して無抵抗状態で連通
するという事態は一瞬たりとも生じ得ない。その
ため、このようなものであれば、前記流入口21
から吸込まれた流体が前記両C形溝3,4内を順
次に通つて前記流出口24へ確実に導かれ、この
流出口24から逐次吐出されるというポンプ作用
を弁等を一切用いることなしに営ませることがで
きるものである。
If it has such a configuration, the C-shaped blade 15,
The outer circumferential surfaces 17, 18 of the C-shaped blades 15, 16 are in the outer contact portion and are in line contact with the outer inner surfaces 7, 9 of the C-shaped grooves 3, 4, and the inner circumferential surfaces 19, 20 of the C-shaped blades 15, 16 are in the inner contact portion. In order to make line contact with the inner surfaces 8, 10 inside the C-shaped grooves 3, 4, the inside of the C-shaped grooves 3, 4 has a sickle-shaped inlet side formed by the C-shaped blades 15, 16. Spaces 3a, 4a and space 3 on the outlet side
It is divided into 4b and 4b. From this state, the rotating shaft 26 is rotated in the direction of arrow X to
When the shaped wings 15 and 16 are made to perform a misosuri motion,
Since the outer contact portion and the inner contact portion move from the inflow ports 21, 22 to the outflow ports 23, 24 side along the inner surfaces 7, 8, 9, 10 of the C-shaped grooves 3, 4, respectively, the two spaces 3a, 3b, 4a, and 4b will also move in the same direction, and these spaces 3
The fluid filling a, 3b, 4a, and 4b is transported from the inlet ports 21 and 22 side to the outlet ports 23 and 24 side. In addition, in the process of the C-shaped blades 15 and 16 performing a sliding motion, there is a period when the external contact portion temporarily disappears (see the first pump unit A in FIG. 4) and a period when the internal contact portion temporarily disappears. (2nd pump unit B in Figure 3)
) will be visited regularly. however,
Since the phases of the grinding motions of the C-shaped blades 15 and 16 are made different between the first pump unit A and the second pump unit B so that these timings do not overlap, Pump unit A
A situation in which the inlet 21 of the pump unit B and the outlet 24 of the second pump unit B communicate with each other through the C-shaped grooves 3 and 4 without any resistance cannot occur even for a moment. Therefore, if it is like this, the inflow port 21
The fluid sucked in from the C-shaped grooves 3 and 4 is reliably guided to the outlet 24 through the C-shaped grooves 3 and 4, and is sequentially discharged from the outlet 24 without using any valves or the like. It is something that can be operated by

なお、以上の実施例は、本発明に係る流体機械
をポンプとして使用した場合のものであるが、逆
に、流体を前記各ユニツトに貫流させるようにす
れば、本流体機械を流量計やモータとして使用す
ることができるものである。
Note that the above embodiments are for the case where the fluid machine according to the present invention is used as a pump, but conversely, if the fluid is made to flow through each of the units, this fluid machine can be used as a flow meter or a motor. It can be used as

また、前記実施例では、2組のユニツトを直列
に接続した場合について説明したが、本発明に
は、前記ユニツトを1組しか有さないものや、3
組以上のユニツトを備えてなるものも含まれる。
Further, in the above embodiment, a case was explained in which two sets of units were connected in series, but the present invention includes a case having only one set of units, a case having three sets of units, and a case having three sets of units.
It also includes units equipped with more than one set.

さらに、本発明は、前述のとおり渦巻形の翼と
溝の組み合わせからなるユニツトを具備した渦巻
形ポンプ(スクロール形ポンプ)あるいはモータ
にも適用できるものである。この渦巻形流体機械
の一例は、特開昭51―104609号「圧縮性媒体用圧
縮機」に示されている。
Furthermore, the present invention can also be applied to a spiral pump (scroll pump) or a motor equipped with a unit consisting of a combination of spiral blades and grooves, as described above. An example of this spiral fluid machine is shown in JP-A-51-104609, "Compressor for Compressible Media."

以上、説明したように、本発明は、C形または
渦巻形翼およびC形または渦巻形溝のそれぞれの
外方端部および内方端部の角部分に、t/10≦R≦ t/2なる関係を有したアール部を設けているので、 翼と溝との接触シール部分が円滑に連続したもの
になる。しかも、角部分が摩耗により、変形し
て、その部分のシール性が低下するという不具合
も生じ難いものとなる。したがつて、高い効率を
長期に亘つて維持することができるという優れた
効果を得ることができる。
As described above, the present invention provides the corner portions of the outer and inner ends of the C-shaped or spiral-shaped blade and the C-shaped or spiral groove, respectively, with t/10≦R≦t/2. Since the radiused portion has the following relationship, the contact seal portion between the blade and the groove becomes smoothly continuous. Furthermore, the problem that the corner portions are deformed due to wear and the sealing performance of the portions is deteriorated is less likely to occur. Therefore, the excellent effect of being able to maintain high efficiency over a long period of time can be obtained.

さらに、C型または渦巻形翼の内外周面を、該
C型または渦巻形翼の厚みが先端方向に漸次減少
するように傾斜させるとともに、前記C型または
渦巻形溝の各内側面を、その母線が対向するC形
または渦巻形翼の内外周面の母線と平行になるよ
うに傾斜させているので、前記C形または渦巻形
翼を前記C形または渦巻形溝の内側面に線接触さ
せた状態でみそすり運動を行なわせることが可能
であり、原理的には従来のものと同様な機能を発
揮し得るものである。しかも、前記C形または渦
巻形翼の内、外周面および、C形または渦巻形溝
の内側面にそれぞれ前述したような傾斜をつける
と、型加工を行なう場合にその傾斜を抜き勾配と
して利用することができるので、脱型がきわめて
容易となり、前記C形または渦巻形溝を有するケ
ースや前記C形または渦巻形翼を有したデイスク
の製作が簡単なものになる。したがつて、大量生
産を行う場合に、大幅なコストダウンを図ること
ができるものである。また、前記C形または渦巻
形翼を前述のような先細りのテーパ形状にすれ
ば、該C形または渦巻形翼を比較的薄肉なものに
しても必要な剛性を確保することが可能となり、
ユニツトの軽量化を図ることができるという効果
も得られる。
Further, the inner and outer circumferential surfaces of the C-shaped or spiral-shaped blade are inclined such that the thickness of the C-shaped or spiral-shaped blade gradually decreases toward the tip, and each inner surface of the C-shaped or spiral groove is Since the generatrix is inclined so as to be parallel to the generatrix of the inner and outer circumferential surfaces of the opposing C-shaped or spiral-shaped blades, the C-shaped or spiral-shaped blades are brought into line contact with the inner surface of the C-shaped or spiral groove. It is possible to perform a misosuri movement in a state in which the device is held in place, and in principle, it can perform the same functions as conventional devices. Furthermore, if the inner and outer circumferential surfaces of the C-shaped or spiral-shaped blades and the inner surfaces of the C-shaped or spiral grooves are sloped as described above, the slopes can be used as draft angles during mold processing. As a result, demolding becomes extremely easy, and a case having the C-shaped or spiral grooves and a disk having the C-shaped or spiral blades can be manufactured easily. Therefore, when performing mass production, it is possible to significantly reduce costs. Furthermore, by making the C-shaped or spiral-shaped blade into a tapered shape as described above, it is possible to ensure the necessary rigidity even if the C-shaped or spiral-shaped blade is made relatively thin.
Another advantage is that the weight of the unit can be reduced.

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

図面は、本発明の一実施例を示し、第1図は概
略断面図、第2図は要部を示す拡大説明図、第3
図、第4図は原理説明図である。 A,B…ユニツト(ポンプユニツト)、1,2
…ケース、3,4…C形溝、5,6…デイスク、
7,8,9,10…内側壁、11,12…先端
面、13,14…底面、15,16…C形翼、1
7,18…外周面、19,20…内周面、21,
22…流入口、23,24…流出口、7a,8
a,9a,10a,17a,18a,19a,2
0a…アール部。
The drawings show one embodiment of the present invention, with FIG. 1 being a schematic sectional view, FIG. 2 being an enlarged explanatory view showing the main parts, and FIG.
FIG. 4 is a diagram explaining the principle. A, B...Unit (pump unit), 1, 2
...Case, 3, 4...C-shaped groove, 5, 6...Disk,
7, 8, 9, 10... Inner wall, 11, 12... Tip surface, 13, 14... Bottom surface, 15, 16... C-shaped blade, 1
7, 18...outer peripheral surface, 19,20...inner peripheral surface, 21,
22... Inlet, 23, 24... Outlet, 7a, 8
a, 9a, 10a, 17a, 18a, 19a, 2
0a...R section.

Claims (1)

【特許請求の範囲】 1 ケースの端面に、一端が流入口に連通し他端
が流出口に連通するC形または渦巻形溝を設ける
とともに、このC形または渦巻形溝の開口端面に
蓋着したデイスクから、該C形または渦巻形溝の
内側面間に遊嵌しかつその先端面が前記C形また
は渦巻形溝の底面に密接するC形または渦巻形翼
を突設し、このC形または渦巻形翼を、該C形ま
たは渦巻形翼の内周面および外周面の少なくとも
一方が前記C形または渦巻形溝の内側面に当接す
るように前記C形または渦巻形溝の曲率中心から
所定距離だけ偏心させて配置し、このC形または
渦巻形翼にその偏心軌道に沿うみそすり運動を行
わせることによつて、前記C形または渦巻形溝内
に充満する流体を前記流入口側から前記流出口側
へ移動させ得るように構成したユニツトを具備し
てなる容積形の流体機械であつて、前記C形また
は渦巻形翼の外周面および内周面を、該C形また
は渦巻形翼の厚みが先端方向に漸次減少するよう
に傾斜させると共に、前記C形または渦巻形溝の
各内側面を、その母線が対応するC形または渦巻
形翼の外周面または、内周面の母線と平行になる
ように傾斜させ、前記C形または渦巻形翼および
C形または渦巻形溝のそれぞれの外方端部および
内方端部の角部分に、その曲率半径Rが、t/10≦ R≦t/2(tは翼先端部の厚み)なる関係を有し たアール部を形成したことを特徴とする容積型流
体機械。
[Claims] 1. A C-shaped or spiral groove is provided on the end face of the case, one end communicating with the inlet and the other end communicating with the outlet, and a lid is attached to the open end face of the C-shaped or spiral groove. A C-shaped or spiral-shaped wing is protruded from the C-shaped or spiral-shaped disc, and is loosely fitted between the inner surfaces of the C-shaped or spiral-shaped groove, and whose tip surface is in close contact with the bottom surface of the C-shaped or spiral-shaped groove. or a spiral blade from the center of curvature of the C-shape or spiral groove such that at least one of the inner peripheral surface and the outer peripheral surface of the C-shape or spiral blade abuts the inner surface of the C-shape or spiral groove. By arranging the C-shaped or spiral-shaped blades eccentrically by a predetermined distance and causing them to perform a diagonal movement along the eccentric trajectory, the fluid filling the C-shaped or spiral-shaped groove is directed toward the inlet side. A positive displacement fluid machine comprising a unit configured to be able to move from the C-shaped or spiral-shaped blade to the outlet side, the outer peripheral surface and the inner peripheral surface of the C-shaped or spiral-shaped blade The thickness of the blade is inclined so that it gradually decreases toward the tip, and each inner surface of the C-shaped or spiral groove is set so that its generatrix line is the generatrix of the outer peripheral surface or inner peripheral surface of the corresponding C-shaped or spiral blade. and the radius of curvature R is t/10≦at the corner portions of the outer and inner ends of the C-shaped or spiral-shaped blade and the C-shaped or spiral groove, respectively. A positive displacement fluid machine characterized by forming a radiused portion having the relationship R≦t/2 (t is the thickness of a blade tip).
JP17282282A 1982-09-30 1982-09-30 Volume type hydraulic machine Granted JPS5960086A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP17282282A JPS5960086A (en) 1982-09-30 1982-09-30 Volume type hydraulic machine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP17282282A JPS5960086A (en) 1982-09-30 1982-09-30 Volume type hydraulic machine

Publications (2)

Publication Number Publication Date
JPS5960086A JPS5960086A (en) 1984-04-05
JPH0125909B2 true JPH0125909B2 (en) 1989-05-19

Family

ID=15949007

Family Applications (1)

Application Number Title Priority Date Filing Date
JP17282282A Granted JPS5960086A (en) 1982-09-30 1982-09-30 Volume type hydraulic machine

Country Status (1)

Country Link
JP (1) JPS5960086A (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4696084A (en) * 1985-06-14 1987-09-29 Mitsubishi Jukogyo Kabushiki Kaisha Method for forming scroll members used in a scroll type fluid machine

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS51104609A (en) * 1975-02-07 1976-09-16 Aginfor Ag
JPS57146085A (en) * 1981-03-03 1982-09-09 Sanden Corp Scroll type fluid apparatus
JPS58126492A (en) * 1982-01-22 1983-07-27 Sharp Corp Scroll compressor

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS51104609A (en) * 1975-02-07 1976-09-16 Aginfor Ag
JPS57146085A (en) * 1981-03-03 1982-09-09 Sanden Corp Scroll type fluid apparatus
JPS58126492A (en) * 1982-01-22 1983-07-27 Sharp Corp Scroll compressor

Also Published As

Publication number Publication date
JPS5960086A (en) 1984-04-05

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