JPH0494485A - Scroll compressor - Google Patents

Scroll compressor

Info

Publication number
JPH0494485A
JPH0494485A JP21108990A JP21108990A JPH0494485A JP H0494485 A JPH0494485 A JP H0494485A JP 21108990 A JP21108990 A JP 21108990A JP 21108990 A JP21108990 A JP 21108990A JP H0494485 A JPH0494485 A JP H0494485A
Authority
JP
Japan
Prior art keywords
blade
fixed
spiral
component
volute
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.)
Granted
Application number
JP21108990A
Other languages
Japanese (ja)
Other versions
JP2850920B2 (en
Inventor
Shuichi Yamamoto
修一 山本
Sadao Kawahara
定夫 河原
Manabu Sakai
学 阪井
Yoshinobu Kojima
小嶋 能宣
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.)
Panasonic Holdings Corp
Original Assignee
Matsushita Electric Industrial 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 Matsushita Electric Industrial Co Ltd filed Critical Matsushita Electric Industrial Co Ltd
Priority to JP21108990A priority Critical patent/JP2850920B2/en
Publication of JPH0494485A publication Critical patent/JPH0494485A/en
Application granted granted Critical
Publication of JP2850920B2 publication Critical patent/JP2850920B2/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Abstract

PURPOSE:To reduce a leakage amount by bringing a point end of either one or the other or both volute blades surely into contact with a groove bottom surface, opposed to the point end, when both volute blade parts are combined. CONSTITUTION:A step difference delta1 is provided between a groove bottom surface 23 of a volute blade 11 of a turning volute blade part 13 and a turning end plate surface 24 in the peripheral part, and a step difference delta2 is provided between volute blade point end surface 25 of a fixed volute blade part 9 and a peripheral surface 26 of a fixed blade frame unit 7. A relation of the step differences delta1, delta2 is set to the relation where delta1<delta2 or delta1>delta2, and when both the volute blade parts 9, 13 are combined, a point end of either one or both the volute blades is surely brought into contact with the groove bottom surface of the volute blade opposed to this point end. In this way, before a turning end plate 12 is brought into contact with the fixed blade frame unit 7 during operation, any of the volute blade point end is surely brought into contact with the groove bottom surface of the volute blade opposed to this volute blade point end. Accordingly, a clearance in the axial direction is decreased to almost 0 to substantially reduce leakage, and performance of a compressor is greatly improved.

Description

【発明の詳細な説明】 産業上の利用分野 本発明は、密閉形のスクロール圧縮機に関するものであ
る。
DETAILED DESCRIPTION OF THE INVENTION Field of the Invention The present invention relates to a hermetic scroll compressor.

従来の技術 第4図(a) (b)は特開昭63−65187  号
公報に示されろ従来のスクロール圧縮機の旋回渦巻羽根
部品および固定渦巻羽根部品の断面図である。第4図(
1)において、旋回渦巻羽根部品5oの中央部の歯溝底
面51は旋回鏡板52の旋回鏡板面53に対してり、の
寸法分だけ低く設定されている。また、第4図(b)に
おいて、固定渦巻羽根部品54の中央部の歯溝底面55
は歯溝外周部56に対してり、の寸法分だけ低く設定さ
れて6−旋回渦巻羽根部品501F)段差寸法り。
BACKGROUND OF THE INVENTION FIGS. 4(a) and 4(b) are cross-sectional views of a rotating spiral vane component and a fixed spiral vane component of a conventional scroll compressor disclosed in Japanese Patent Laid-Open No. 63-65187. Figure 4 (
In 1), the tooth groove bottom surface 51 at the center of the rotating spiral blade component 5o is set lower than the rotating mirror plate surface 53 of the rotating mirror plate 52 by a dimension of . In addition, in FIG. 4(b), a tooth groove bottom surface 55 at the center of the fixed spiral blade component 54 is shown.
is set lower than the tooth groove outer circumferential portion 56 by the dimension of 6-swirling spiral vane part 501F) step dimension.

と固定渦巻羽根部品54の段差寸法り、とは−櫃略り、
mk、の関係にある。
and the step size of the fixed spiral vane part 54, and - omitted from the frame.
It is in the relationship of mk.

また、他の従来例とし”[特開昭62−23588  
号公報のように渦巻羽根先端からの漏ね、を防止するた
めに渦巻羽根の先端部にチップシールを挿入するととも
に、このチップシールの形状により過圧縮をも防止しよ
うとしているものもある。
In addition, as another conventional example,
In some cases, as in the publication, a tip seal is inserted into the tip of the spiral blade in order to prevent leakage from the tip of the spiral blade, and the shape of the tip seal is also used to prevent overcompression.

発明が解決り、ようとする課題 しかし−このような構造のものでは、渦巻羽根先端と対
向する歯溝底面との間に隙間が生じ圧縮機の性能を大き
く低下させろ、、また、この隙間を極力小さくしようと
し段差の寸法をシビアに設定゛すると、広範囲な圧力、
温度の運転条件によっては渦巻羽根の先端部の接触が過
大となり、圧縮性能に人為なばらつきを与えろとともに
、信頼性の低下をもたらす。また、こね、らの欠点を回
避1)ようとして渦巻羽根の先端部にチップシールを挿
入したものでは、チップシール側面とこれに対向する歯
溝底面とに必ず隙間が生じ、この部分での漏れ凰は以外
に大きく、性能の低下をもたらすことが明かとなってい
る。
However, with such a structure, a gap is created between the tip of the spiral blade and the bottom of the opposing tooth groove, which greatly reduces the performance of the compressor. If you set the dimensions of the step to be as small as possible, it will cause a wide range of pressure,
Depending on the temperature operating conditions, the contact between the tips of the spiral vanes becomes excessive, causing artificial variations in compression performance and lowering reliability. In addition, in the case where a tip seal is inserted at the tip of the spiral blade in order to avoid the disadvantages of 1), a gap is always created between the side surface of the tip seal and the bottom surface of the tooth groove that opposes it, and leakage occurs in this area. It is clear that the 凰 is larger than that and causes a decrease in performance.

本発明は上記問題を解決するもので、渦巻羽根の先端部
の接触の適正化8図り、漏れ量を大幅に低減できろスク
ロール圧縮機を提供てろことを目的とするものである。
The present invention solves the above-mentioned problems, and aims to provide a scroll compressor in which the contact between the tips of the spiral blades can be optimized and the amount of leakage can be significantly reduced.

課題を解決オろための手段 課題を解決するために5本発明のスクロ・−ル圧縮機は
、密閉容器の内部に電動機と、この電動機で駆動される
圧縮msを配設し、前記圧縮機lRを固定羽根枠体と一
体に固定あるいは形成した固定渦巻羽根を有する固定渦
巻羽根部品と、前記固定渦巻羽根と噛み合い複数個の圧
縮空間を形成する旋回渦巻羽根を旋回鏡板に固定あるい
は形成したIji回i巻羽根部品と、前記旋回渦巻羽根
部品の自転を拘束する自転拘束部品と、前記電動機によ
り回転駆動されて、旋回渦巻羽根部品を偏心旋回するク
ランク軸と、このクランク軸を支承する軸受は部品を含
んで構成し、前記旋回鏡板の外周部および背面の一部あ
るいは全体に吸入圧力あるいはそね、に近い圧力を作用
させろとともに、旋回鏡板の背面に会少隙rII5をも
うけ、前記旋回渦巻羽根部品の渦巻羽根の溝底面と旋回
鏡板面との間に段差ait設は−かつ前記固定渦巻羽根
部品の渦巻羽根先端面と外B面との間に段差a2を設け
、この段差al 、 12の関係をJl (12あるい
は、Jl ) J2嘉こ構成し、前記1ii渦巻羽根部
品を組み合わせたとき必ずいずれか一方あるいは両方の
渦巻羽根の先端と対向する渦巻羽根の溝底面とが接触す
るようにしたものJ2の・関係をJl < J2あるい
は、Jl)J2とでろことにより、運転中には、旋回鏡
板と固定羽根枠体とが接触する前に必ずいずれかのh巻
羽根先端とこれに対向する溝底面とが接触し一軸方向の
隙間はほぼ0となって、漏れは大幅に低減されろ、その
結果圧縮機の性能は大きく向上する。また、旋回鏡板の
外周部の旋回鏡板面には吸入圧力あるいはそれに近い圧
力が作用しているため、旋回鏡板と固定羽根枠体との隙
間からの漏れは性能を大きく低下させることはない。ま
た、圧力、温度により渦巻羽根の先端が大きく膨張し、
櫛械的接触が過大となる場合は旋回&板の背面に設けち
1だ微少隙間により回避される。したがって、圧縮機の
性能は大幅に向上するとともに信頼性も充分に確保され
る。
Means for Solving the Problems 5 In order to solve the problems, the scroll compressor of the present invention is provided with an electric motor and a compressor ms driven by the electric motor disposed inside a closed container. A fixed spiral vane component having a fixed spiral vane in which the lR is fixed or formed integrally with a fixed vane frame body, and a rotating spiral vane that engages with the fixed spiral vane to form a plurality of compressed spaces is fixed or formed on a rotating mirror plate. A rotating spiral blade component, a rotation restraining component that restrains the rotation of the rotating spiral blade component, a crankshaft that is rotationally driven by the electric motor to eccentrically rotate the rotating spiral blade component, and a bearing that supports this crankshaft. A suction pressure or a pressure close to the pressure is applied to a part or the whole of the outer periphery and back surface of the rotating head plate, and a small gap rII5 is provided at the back surface of the rotating head plate, so that the rotating swirl A step A2 is provided between the groove bottom surface of the spiral vane of the blade component and the rotating mirror plate surface, and a step A2 is provided between the spiral vane tip surface and the outer B surface of the fixed spiral vane component, and this step A1, 12 is provided. Jl (12 or Jl) J2 is constructed so that when the spiral blade parts 1ii are combined, the tip of one or both of the spiral blades is always in contact with the groove bottom surface of the opposing spiral blade. The relationship of J2 is Jl < J2 or Jl)J2. Therefore, during operation, before the rotating head plate and the fixed blade frame come into contact, the tip of one of the H winding blades and the opposite When the groove bottom surface contacts the groove bottom surface, the gap in the uniaxial direction becomes almost zero, and leakage is greatly reduced, resulting in a significant improvement in the performance of the compressor. Furthermore, since the suction pressure or a pressure close to the suction pressure is acting on the rotating head plate surface on the outer periphery of the rotating head plate, leakage from the gap between the rotating head plate and the fixed blade frame does not significantly reduce performance. In addition, the tip of the spiral blade expands greatly due to pressure and temperature.
If the comb-like contact becomes excessive, it can be avoided by providing a very small gap on the back of the turning plate. Therefore, the performance of the compressor is greatly improved and reliability is also sufficiently ensured.

実施例 以下、本発明の一実施例について図面を参照して説明す
る。
EXAMPLE Hereinafter, an example of the present invention will be described with reference to the drawings.

第1図は本発明の一実施例のスクロール圧縮機の縦断面
図である。第1図において、1は密閉容器であり、この
内部下方に圧縮機構2と、圧縮機構2の上方にこれを駆
動する電動機3が設けられ、電動fi3の固定子4は密
閉容器1に固定され、電動機3の回転子5は圧縮機構2
を駆動するクランク軸6と結合されている。圧縮機構2
は、固定羽根枠体7に一体に形成さjた固定渦巻羽根8
を有する固定渦巻羽根部品9と、この固定渦巻羽根部品
9の固定渦巻羽根8とかみ合って複数個の圧縮空間10
を形成する旋回渦巻羽根11を旋回鏡板12の上に形成
された旋回渦巻羽根部品13と、この旋回羽根部品工3
の自転を防止して旋回のみを行わせろ自転拘束部品14
と、この旋回親板12の旋回渦巻羽根11とは反対側に
設けられた旋回駆動軸15と、クランク軸6の主軸16
の内方に設けられ、て、この旋回駆動軸15を駆動でろ
ように構成された偏心軸受け17と、クランク軸6を支
承する主軸受け18を有する軸受は部品19と、この軸
受は部品19に固定さねで旋回鏡板12の背面で、旋回
鏡板12にかかる背圧力を半径方向に仕切る背圧仕切り
環20などを備えている。この背圧仕切り環20の外局
側の空間21には吸入圧力あるいはそれに近い圧力が作
用しており、したがって旋回鏡板13の背面にも吸入圧
力あるいはそれに近い圧力が作用している。また、旋回
鏡板12の背面は軸受は部品19との間に微少隙間22
が設けられている。
FIG. 1 is a longitudinal sectional view of a scroll compressor according to an embodiment of the present invention. In FIG. 1, reference numeral 1 denotes an airtight container, in which a compression mechanism 2 is provided below, an electric motor 3 for driving the compression mechanism 2 is provided above the compression mechanism 2, and a stator 4 of an electric fi 3 is fixed to the airtight container 1. , the rotor 5 of the electric motor 3 is the compression mechanism 2
It is connected to a crankshaft 6 that drives the. Compression mechanism 2
is a fixed spiral blade 8 formed integrally with the fixed blade frame 7.
a fixed spiral vane part 9 having a fixed spiral vane part 9;
A swirling spiral vane component 13 formed on a swirling mirror plate 12 and a swirling spiral vane component 3 forming a swirling spiral vane 11
Rotation restraint component 14 that prevents rotation and allows only rotation.
, a turning drive shaft 15 provided on the opposite side of the turning parent plate 12 from the turning spiral blade 11 , and a main shaft 16 of the crankshaft 6 .
The bearing, which has an eccentric bearing 17 which is provided inwardly and is configured to drive the swing drive shaft 15 and a main bearing 18 which supports the crankshaft 6, is a part 19; A back pressure partition ring 20 is provided on the back side of the rotating mirror plate 12 with a fixed tongue to partition the back pressure applied to the rotating mirror plate 12 in the radial direction. Suction pressure or a pressure close to it acts on the space 21 on the outer side of the back pressure partition ring 20, and therefore suction pressure or a pressure close to it also acts on the back surface of the swiveling mirror plate 13. In addition, on the back side of the rotating mirror plate 12, there is a small gap 22 between the bearing and the component 19.
is provided.

第2図および第3図は固定渦巻羽根部品9と旋回渦巻羽
根部品13がかみ合った場合の詳細な断面図であり、第
2図および第3図に示すように、旋回渦巻羽根部品】3
の渦巻羽根11の溝底面23と外界部の旋回鏡板面24
との間には段差δ1が、また固定渦巻羽根部品9の渦巻
羽根先端m125と固定羽根枠体7の外周面26との間
には段差a2が設けられている。この段差t1 、 J
2の関係は第2図では11〈δ2、第3図ではIN>1
2と設定されており、両渦巻羽根部品を・組み合わゼた
とと、必ずいずれか一方あろいは両方の渦巻羽根の先端
とこれに対向する渦巻羽根の溝底面とが接触するように
なっている。したがって、この場合旋回渦巻羽根部品1
3の旋回鏡板面24と固定渦巻羽根部品9の固定羽根枠
体7の外周面26との間には必ず微少隙間13が存在す
ることになる。
FIGS. 2 and 3 are detailed cross-sectional views when the fixed spiral vane part 9 and the swirling spiral vane part 13 are engaged, and as shown in FIGS.
The groove bottom surface 23 of the spiral blade 11 and the rotating mirror plate surface 24 of the outer part
A step δ1 is provided between the fixed spiral blade component 9 and a step a2 between the spiral blade tip m125 of the fixed spiral blade component 9 and the outer circumferential surface 26 of the fixed blade frame 7. This step t1, J
2 is 11<δ2 in Figure 2, and IN>1 in Figure 3.
2, and when both spiral blade parts are combined, the tip of one or both spiral blades will always come into contact with the groove bottom of the opposite spiral blade. . Therefore, in this case, the swirling spiral vane part 1
There is always a minute gap 13 between the rotating mirror plate surface 24 of No. 3 and the outer peripheral surface 26 of the fixed blade frame 7 of the fixed spiral blade component 9.

その結果、運転中には、旋回鏡板12と固定羽根枠体7
とが接触する前に必ずいずれかの渦巻羽根先端とこれに
対向する渦巻羽根の4底面とが接触し一軸方向の隙間は
ほぼ0となって漏れは大幅に低減され、圧縮機の性能は
大きく向上する。また、旋回鏡板12の外周部には吸入
圧力あるいはそれに近い圧力が作用しているため、旋回
鏡板12の外周部と固定羽根枠体7の外周部との隙間か
らの漏れは性能を大来く低下させろことはない、また、
圧力、温度により渦巻羽根の先端が大きく膨張し、機械
的接融が過大となる場合は旋回鏡板の背面に設Cすらね
た微少隙間22(第1図)により回避されろ。したがっ
て、圧縮機の性能は大幅に向上するばかりでなく信頼性
も充分に確保されることになる。
As a result, during operation, the rotating mirror plate 12 and the fixed blade frame 7
The tip of one of the spiral vanes always comes into contact with the four bottom surfaces of the opposite spiral vane, and the gap in the uniaxial direction becomes almost 0, which greatly reduces leakage and greatly improves the performance of the compressor. improves. In addition, since suction pressure or a pressure close to it is acting on the outer circumference of the swivel head plate 12, leakage from the gap between the outer periphery of the swivel head plate 12 and the outer periphery of the fixed blade frame 7 will greatly impair performance. There is no need to lower the
If the tips of the spiral blades expand greatly due to pressure and temperature, resulting in excessive mechanical welding, this can be avoided by creating a small gap 22 (see FIG. 1) provided on the back of the rotating mirror plate. Therefore, not only the performance of the compressor is greatly improved, but also the reliability is sufficiently ensured.

究明の効果 以上のように、本発明によれば、運転中には、旋回鏡板
と固定羽根枠体とが接触才ろ前に必ずいず旧かの渦巻羽
根先端とこれに対向する渦巻羽根の溝底面とが接触し、
軸方向の隙間はほぼOとなって漏れは大幅に低減され、
圧縮機の性能は大きく向上する。また、旋回鏡板の外周
部には吸入圧力あるいはそれに近い圧力が作用している
ため、旋回鏡板と固定羽根枠体との隙間からの漏れは性
能を大きく低下させることはない、また、圧力、温度に
より渦巻羽根の先端が大きく膨張し、機械的接触が過大
となる場合は旋回鏡板の背面に設けられた微少隙間によ
り回避されろ、したがって、圧縮機の性能は大幅に向上
するばかりでなく信頼性も充分に確保されろことになる
Effects of Investigation As described above, according to the present invention, during operation, before the rotating head plate and the fixed blade frame come into contact with each other, the tip of the spiral blade and the opposite spiral blade are always connected. Contact with the bottom of the groove,
The axial clearance is almost O, and leakage is significantly reduced.
The performance of the compressor will be greatly improved. In addition, since suction pressure or a pressure close to it acts on the outer periphery of the swivel head plate, leakage from the gap between the swivel head plate and the fixed blade frame will not significantly reduce performance. If the tip of the volute vane expands greatly due to this, resulting in excessive mechanical contact, this can be avoided by the small gap provided at the back of the swivel head plate. Therefore, not only the performance of the compressor is greatly improved, but also the reliability is improved. It will also be necessary to ensure sufficient security.

また、さらに従来のように、チップシールを設けること
も不要となり、加工工数、加工コストおよび圧縮機のコ
ストの低減がはかれる。
Moreover, it is no longer necessary to provide a chip seal as in the conventional case, and the number of processing steps, processing cost, and compressor cost can be reduced.

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

第1図は本発明の一実施例のスクロール圧縮機を示す縦
断面図、第2図お↓び第3図はそれぞれ圧縮機構の詳細
例を示す縦断面図、第4図は従来例の圧縮機構を示す縦
断面図である。 l・・・密閉容器、2・−・圧縮機構、3・・・電動機
、6・・・クランク軸、7−・固定羽根枠体、8・・・
固定渦巻羽根、9・・・固定渦巻羽根部品、lO・・・
圧縮空間、11・・・旋回渦巻羽根、12−・旋回鏡板
、13・−旋回渦巻羽根部品、14・・・自転拘束部品
、19・・・軸受は部品、22・−・微少隙間、23・
−・溝底面、24・−・旋回鏡板面、25・・・先端面
、26・・−外局面、il、δ2−・・段差。
Fig. 1 is a vertical cross-sectional view showing a scroll compressor according to an embodiment of the present invention, Figs. 2 and 3 are longitudinal cross-sectional views showing detailed examples of the compression mechanism, and Fig. 4 is a conventional compressor. FIG. 3 is a vertical cross-sectional view showing the mechanism. l...Airtight container, 2--Compression mechanism, 3--Electric motor, 6--Crankshaft, 7--Fixed blade frame, 8...
Fixed spiral vane, 9...Fixed spiral vane part, lO...
Compression space, 11--Swirling spiral vane, 12--Swivel head plate, 13--Swirling spiral vane part, 14--Rotation restraining part, 19--Bearing is a part, 22--Minute gap, 23-
- Groove bottom surface, 24... Turning mirror plate surface, 25... Tip surface, 26... - External surface, il, δ2 -... Step.

Claims (1)

【特許請求の範囲】[Claims] 1.密閉容器の内部に電動機と、この電動機で駆動され
る圧縮機構を配設し、前記圧縮機構を固定羽根枠体と一
体に固定あるいは形成した固定渦巻羽根を有する固定渦
巻羽根部品と、前記固定渦巻羽根と噛み合い複数個の圧
縮空間を形成する旋回渦巻羽根を旋回鏡板に固定あるい
は形成した旋回渦巻羽根部品と、前記旋回渦巻羽根部品
の自転を拘束する自転拘束部品と、前記電動機により回
転駆動されて旋回渦巻羽根部品を偏心旋回するクランク
軸と、このクランク軸を支承する軸受け部品を含んで構
成し、前記旋回鏡板の外周部及び背面の一部あるいは全
体に吸入圧力あるいはそれに近い圧力を作用させるとと
もに、旋回鏡板の背面に微少隙間を設け、前記旋回渦巻
羽根部品の渦巻羽根の溝底面と旋回鏡板面との間に段差
δ1を設け、かつ前記固定渦巻羽根部品の渦巻羽根先端
面と外周面との間に段差δ2を設け、この段差δ1,δ
2の関係をδ1<δ2あるいはδ1>δ2に構成し、前
記両渦巻羽根部品を組み合わせたとき必ずいずれか一方
あるいは両方の渦巻羽根の先端と対向する渦巻羽根の溝
底面とが接触するようにしたスクロール圧縮機。
1. A fixed spiral blade component having a fixed spiral blade in which an electric motor and a compression mechanism driven by the electric motor are disposed inside a closed container, and the compression mechanism is fixed or formed integrally with a fixed blade frame; A swirling spiral vane component in which a swirling spiral vane that engages with the blade and forms a plurality of compressed spaces is fixed or formed on a rotating head plate, a rotation restraining component that restrains the rotation of the swirling spiral vane component, and a rotationally restraining component that is rotationally driven by the electric motor. The rotating spiral vane component is configured to include a crankshaft that rotates eccentrically and a bearing component that supports the crankshaft, and a suction pressure or a pressure close to it is applied to a part or the whole of the outer circumference and back surface of the rotating head plate. , a slight gap is provided on the back surface of the rotating mirror plate, a step δ1 is provided between the bottom surface of the groove of the spiral blade of the rotating spiral blade component and the surface of the rotating mirror plate, and a tip surface and an outer peripheral surface of the spiral blade of the fixed spiral blade component are provided. A step δ2 is provided between the steps δ1, δ
2 is configured to be δ1<δ2 or δ1>δ2, so that when the two spiral blade parts are combined, the tip of one or both of the spiral blades is always in contact with the groove bottom surface of the opposing spiral blade. scroll compressor.
JP21108990A 1990-08-08 1990-08-08 Scroll compressor Expired - Fee Related JP2850920B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP21108990A JP2850920B2 (en) 1990-08-08 1990-08-08 Scroll compressor

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP21108990A JP2850920B2 (en) 1990-08-08 1990-08-08 Scroll compressor

Publications (2)

Publication Number Publication Date
JPH0494485A true JPH0494485A (en) 1992-03-26
JP2850920B2 JP2850920B2 (en) 1999-01-27

Family

ID=16600237

Family Applications (1)

Application Number Title Priority Date Filing Date
JP21108990A Expired - Fee Related JP2850920B2 (en) 1990-08-08 1990-08-08 Scroll compressor

Country Status (1)

Country Link
JP (1) JP2850920B2 (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6494695B1 (en) * 2000-09-19 2002-12-17 Scroll Technologies Orbiting scroll center of mass optimization
KR20030051089A (en) * 2001-12-20 2003-06-25 주식회사 엘지이아이 Structure for preventing the scroll interference of scroll compressor
KR100451228B1 (en) * 2002-02-05 2004-10-02 엘지전자 주식회사 Thrust bearing device for scroll compressor

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6494695B1 (en) * 2000-09-19 2002-12-17 Scroll Technologies Orbiting scroll center of mass optimization
KR20030051089A (en) * 2001-12-20 2003-06-25 주식회사 엘지이아이 Structure for preventing the scroll interference of scroll compressor
KR100451228B1 (en) * 2002-02-05 2004-10-02 엘지전자 주식회사 Thrust bearing device for scroll compressor

Also Published As

Publication number Publication date
JP2850920B2 (en) 1999-01-27

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