JPS5960093A - Scroll compressor - Google Patents

Scroll compressor

Info

Publication number
JPS5960093A
JPS5960093A JP57171736A JP17173682A JPS5960093A JP S5960093 A JPS5960093 A JP S5960093A JP 57171736 A JP57171736 A JP 57171736A JP 17173682 A JP17173682 A JP 17173682A JP S5960093 A JPS5960093 A JP S5960093A
Authority
JP
Japan
Prior art keywords
blade
discharging port
scroll
discharge port
fixed scroll
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
JP57171736A
Other languages
Japanese (ja)
Inventor
Mitsuo Hatori
羽鳥 三男
Shigemi Nagatomo
長友 繁美
Kanji Sakata
坂田 寛二
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.)
Toshiba Corp
Original Assignee
Toshiba 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 Toshiba Corp filed Critical Toshiba Corp
Priority to JP57171736A priority Critical patent/JPS5960093A/en
Publication of JPS5960093A publication Critical patent/JPS5960093A/en
Pending 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
    • F04C18/00Rotary-piston pumps specially adapted for elastic fluids
    • F04C18/02Rotary-piston pumps specially adapted for elastic fluids of arcuate-engagement type, i.e. with circular translatory movement of co-operating members, each member having the same number of teeth or tooth-equivalents
    • F04C18/0207Rotary-piston pumps specially adapted for elastic fluids of arcuate-engagement type, i.e. with circular translatory movement of co-operating members, each member having the same number of teeth or tooth-equivalents both members having co-operating elements in spiral form
    • F04C18/0246Details concerning the involute wraps or their base, e.g. geometry
    • F04C18/0253Details concerning the base
    • F04C18/0261Details of the ports, e.g. location, number, geometry
    • 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
    • F04C18/00Rotary-piston pumps specially adapted for elastic fluids
    • F04C18/02Rotary-piston pumps specially adapted for elastic fluids of arcuate-engagement type, i.e. with circular translatory movement of co-operating members, each member having the same number of teeth or tooth-equivalents
    • F04C18/0207Rotary-piston pumps specially adapted for elastic fluids of arcuate-engagement type, i.e. with circular translatory movement of co-operating members, each member having the same number of teeth or tooth-equivalents both members having co-operating elements in spiral form
    • F04C18/0246Details concerning the involute wraps or their base, e.g. geometry
    • F04C18/0269Details concerning the involute wraps

Abstract

PURPOSE:To enlarge the hole diameter of a discharging port and reduce the hydraulic loss of high-pressure gas passing through the discharging port by a method wherein a notched groove, communicating with the discharging port and extending from the discharging port into the direction of the height of a blade, is formed on the side of a fixed scroll blade. CONSTITUTION:The discharging port 24 is enlarged to the side of the fixed scroll blade 23 and the port diameter is enlarged to the size (d2) compared with the port diameter (d1) of the conventional discharging port shown by an one- dot chain line. Further, the notched groove 23a, communicating with the discharging port 24, is formed on the side surface of the fixed scroll blade 23 while the bottom surface thereof has an arced surface having the same curvature with a part of the discharging port 24 and the groove extends from the discharging port 24 into the direction of the height of the blade thereby arriving at the end of the blade. According to this method, the hydraulic loss of the gas, pressurized in the compression chamber, may be reduced when it is passing through the discharging port 24, whose hole diameter is enlarged, thus, a compression efficiency may be improved and a high compression ratio may be maintained.

Description

【発明の詳細な説明】 〔発明の技術分野〕 本発明はスクロール・コンプレッサに係す、特に吐出ボ
ートの孔径を拡大して圧縮効率を向上しうるようにした
スクロール・コンプレッサに関する。
DETAILED DESCRIPTION OF THE INVENTION [Technical Field of the Invention] The present invention relates to a scroll compressor, and particularly to a scroll compressor in which the pore diameter of the discharge boat is enlarged to improve compression efficiency.

〔発明の技術的背景と問題点〕[Technical background and problems of the invention]

一般に、スクロール・コンプレッサは、ウス巻状の固定
スクロール翼に対してうず巻状の旋回スクロール翼をか
み合せ、吸込口から吸入したガスを固定スクロール翼と
旋回スクロール翼との間に形成された圧縮室内に閉じ込
め、旋回スクロール翼の旋回動に伴って圧縮室の容積を
漸次減少させ。
In general, a scroll compressor has spiral-shaped orbiting scroll blades engaged with spiral-shaped fixed scroll blades, and the gas sucked in from the suction port is compressed between the fixed scroll blade and the orbiting scroll blade. Confined in a chamber, the volume of the compression chamber is gradually reduced as the orbiting scroll blades rotate.

この間にガスを圧縮して高圧がスとし、固定スクロール
翼のうず巻の中心近くに設けられた吐出口より吐出室内
に高圧ガスを吐出するようにしたものであり、原理自体
は公知のものである。
During this time, the gas is compressed to release high pressure, and the high pressure gas is discharged into the discharge chamber from the discharge port provided near the center of the spiral of the fixed scroll blade.The principle itself is well known. be.

と(Dmのコンプレッサにおいては、圧縮工程中。(In the Dm compressor, during the compression process.

固定スクロール翼と旋回スクロール翼とが常に2か所の
翼腹で接触し、この間に圧縮室を画成し。
The fixed scroll blade and the orbiting scroll blade are always in contact at two blade bellies, and a compression chamber is defined between them.

最終的には、前記圧縮室の容積はかなり、小さくなり、
がスの高圧化を図ることができるようになっている。し
たがって前記吐出ボートは、最終圧縮段階の圧縮室内に
開口している必要があるため、その大きさは、極めて小
さいものに制限されていた。このように吐出ポートが小
さいと、ガスに大きな流体損失が発生して運転効率が低
下してしまう上に、騒音が大きく、振動が発生すること
もしばしげある。
Eventually, the volume of the compression chamber becomes considerably smaller,
This makes it possible to increase the pressure of the gas. Therefore, since the discharge boat must open into the compression chamber of the final compression stage, its size has been limited to an extremely small one. When the discharge port is small in this way, a large fluid loss occurs in the gas, which reduces operational efficiency, and often causes noise and vibration.

〔発明の目的〕[Purpose of the invention]

そこで本発明の目的は、従来の欠点を解消し。 SUMMARY OF THE INVENTION It is therefore an object of the present invention to overcome the drawbacks of the prior art.

がスが吐出ポートを通過する際の流体」H失、騒音およ
び振動を低減すると同時に、圧縮比を高く維持すること
ができるスクロール・コンプレッサを提供することにあ
る。
An object of the present invention is to provide a scroll compressor that can reduce fluid loss, noise, and vibration when gas passes through a discharge port, and at the same time maintain a high compression ratio.

〔発明の概要〕[Summary of the invention]

上記目的を達成するため1本発明は、固定スクロール翼
の翼腹面に吐出前−トから翼高さ方向に延びる切欠溝を
形成して、of Re吐出ポートの孔径を拡大しつるよ
うにしたことを特徴としている。
In order to achieve the above object, 1 the present invention is to form a notched groove extending in the blade height direction from the discharge front on the blade vent surface of a fixed scroll blade so as to enlarge the hole diameter of the of Re discharge port. It is characterized by

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

以下本発明によるスクロール・コンプレッサの実施例を
図面を参照して説明する。
Embodiments of a scroll compressor according to the present invention will be described below with reference to the drawings.

第1図において、符号1は密閉したケーシングヲ示し、
このケーシング1の内側には取付フレーム2が圧入固定
されている。この取付フレーム2内には、収容室3、ヘ
ッド受孔4および軸受孔5が段階的に形成されている。
In FIG. 1, reference numeral 1 indicates a closed casing;
A mounting frame 2 is press-fitted into the inside of the casing 1. In this mounting frame 2, a housing chamber 3, a head receiving hole 4, and a bearing hole 5 are formed in stages.

上記軸受孔5内には駆動軸6が回転可能に嵌挿され、こ
の駆動軸6の上端の軸ヘッド7が上記ヘッド受孔4内に
遊嵌され、軸ヘッド7の下端面7aが取付フレーム2に
よって支承されている。また、駆動軸6はケーシング1
の下方に向って延出し、その下端がケーシング1の底部
に貯溜された潤滑油8内に没入されている。
A drive shaft 6 is rotatably fitted into the bearing hole 5, a shaft head 7 at the upper end of the drive shaft 6 is loosely fitted into the head receiving hole 4, and a lower end surface 7a of the shaft head 7 is attached to the mounting frame. It is supported by 2. In addition, the drive shaft 6 is connected to the casing 1
The lubricating oil 8 extends downward, and its lower end is immersed in lubricating oil 8 stored at the bottom of the casing 1 .

また、上記駆動軸6の軸上には、駆動電動機を構成する
ロータ9が固着されており、一方、上記ロータ9の外側
にはステータ10が同心的に配置され、ステータ10は
ケーシング1の側に保持されている。
Further, a rotor 9 constituting a drive motor is fixed on the axis of the drive shaft 6. On the other hand, a stator 10 is arranged concentrically on the outside of the rotor 9, and the stator 10 is placed on the side of the casing 1. is maintained.

一方、上記軸ヘッド7には、駆動軸6の軸心か(込ゝ ら中心を偏籍させた偏心穴11が形成されている。On the other hand, the shaft head 7 has an axial center (included) of the drive shaft 6. An eccentric hole 11 is formed with its center offset from the center.

この偏心穴11には、全体を符号12で示した旋回(3
) スクロールの被駆動軸13が遊嵌しておし、被駆動軸1
3には翼支持円盤14が一体的に連設され、さらにその
上面にはうず巻状の旋回スクロール翼15(第2図参照
)が一体的に形成されている。上記旋回スクロール翼1
5は、その横断面が矩形をなし、翼端面15aと、平行
関係にある翼腹面15 b 、 15 cとを有してい
る。上記翼支持円盤14は、その下面をオルダムリング
16によって支承されており、このオルダムリング16
は、横断面が矩形状のリングであって、第3図から明ら
かなように、その両端面には、互に直交関係にあるキー
溝17および18が形成されている。このうちキー溝1
8は、上記収容室3の底面に設けられた直径線上のキー
19と嵌合する一方、他方のキー溝17は、上記翼支持
円盤14の下面に取付けられ、かつ上記キー19と直交
関係にあるキー20と嵌合している。したがって、駆動
軸60回転によって被駆動軸13は円運動をするが、旋
回スクロール12はオルダムリング160作用によって
旋回運動することになる。
This eccentric hole 11 has a pivot (3
) The driven shaft 13 of the scroll is loosely fitted, and the driven shaft 1
A blade support disk 14 is integrally connected to the blade support disk 3, and a spiral scroll blade 15 (see FIG. 2) is integrally formed on the upper surface of the blade support disk 14. The above orbiting scroll blade 1
5 has a rectangular cross section and has a wing tip surface 15a and wing ventral surfaces 15b and 15c that are parallel to each other. The wing support disk 14 is supported on its lower surface by an Oldham ring 16.
is a ring having a rectangular cross section, and as is clear from FIG. 3, key grooves 17 and 18 are formed on both end faces thereof in a perpendicular relationship to each other. Of these, keyway 1
8 is fitted with a diametrical key 19 provided on the bottom surface of the accommodation chamber 3, while the other key groove 17 is attached to the lower surface of the wing support disk 14 and is perpendicular to the key 19. It is fitted with a certain key 20. Therefore, the driven shaft 13 moves in a circular motion due to the rotation of the driving shaft 60, but the orbiting scroll 12 moves in an orbiting motion due to the action of the Oldham ring 160.

しかして、上記取付フレーム2の上方には、シ(4) ニラウド21が旋回スクロール12を挾むようにして固
着され、このンユラウド21は、内方外側に環状の吸込
室22を備え、さらにその内側に固定スクロール翼23
を有し、第2図に示すように、この固定スクロール翼2
3のうず巻の中心には吐出、N−)24が開口している
。上記固定スクロール翼23は、前記旋回スクロール翼
15と同形同大に製作され、翼の高さも正確に同一高さ
を与えられるように加工されている。
Thus, above the mounting frame 2, a (4) Niroud 21 is fixed so as to sandwich the orbiting scroll 12, and this Niroud 21 has an annular suction chamber 22 on the inner and outer sides, and is further fixed on the inside thereof. scroll wing 23
As shown in FIG.
A discharge outlet (N-) 24 is opened at the center of the spiral 3. The fixed scroll blade 23 is manufactured to have the same shape and size as the orbiting scroll blade 15, and is processed so that the height of the blade is exactly the same.

また、上記吐出ポート24は、特に第4図および第5図
に示すように、固定スクロール翼23の翼腹側に拡大さ
れており、一点鎖線で示す従来の吐出yie−)の口径
dユに対して本発明による前記吐出ポート240口径は
、d2まで広げられている。さらに、前記固定スクロー
ル翼23の翼腹面には、前記24の一部と同じ曲率の円
弧面を有しており、前記吐出ポート24から翼の高さ方
向に延び、翼端まで達している。
In addition, as shown in FIGS. 4 and 5, the discharge port 24 is enlarged toward the blade vent side of the fixed scroll blade 23, and has a diameter d of the conventional discharge port yie-) shown by the dashed line. On the other hand, the diameter of the discharge port 240 according to the present invention is widened to d2. Furthermore, the blade vent surface of the fixed scroll blade 23 has an arcuate surface having the same curvature as a part of the blade 24, extending from the discharge port 24 in the height direction of the blade and reaching the blade tip.

すように全面を傾斜させて設けてもよく、さらに第8図
および第9図のように一部のみを傾斜させてもよい。こ
のような傾斜溝を設けると、固定スクロールR23の強
度を増大することができる利点が生ずる。
The entire surface may be inclined as shown in FIG. 8 and FIG. 9, or only a portion may be inclined as shown in FIGS. Providing such an inclined groove has the advantage of increasing the strength of the fixed scroll R23.

なお、上記吸込室22にはケーシング1を側方から貫通
した吸込パイプ25が接続されており、また。
A suction pipe 25 passing through the casing 1 from the side is connected to the suction chamber 22.

上記シュラウl’21とケーシング1の天板との間には
吐出室26が形成され、この吐出室26に吐出管27が
接続されている。
A discharge chamber 26 is formed between the shroud l'21 and the top plate of the casing 1, and a discharge pipe 27 is connected to this discharge chamber 26.

また、上記駆動軸6内には送油路28が形成されており
、この送油路28は入口油路29と連絡油路30と出口
油路31とからなり、入口油路29の入口I−ト29 
aは駆動軸6の軸心位置で開口し、出口ポート29bは
上記軸受孔5の下方位置に関している。
Further, an oil passage 28 is formed in the drive shaft 6, and this oil passage 28 is composed of an inlet oil passage 29, a communication oil passage 30, and an outlet oil passage 31, and an inlet I of the inlet oil passage 29 is formed. -G29
a opens at the axial center position of the drive shaft 6, and the outlet port 29b is located below the bearing hole 5.

また出口油路31はかぎ形に形成され、入口ポート31
aが軸受孔5の」二部位置に開口し、出口ポート31b
は、上記駆動軸6の軸心より偏心した位置に開口してお
り、被駆動軸13の軸端の下方には油溜り室32が形成
されている。したがって、駆動軸6が回転すると、出口
=1? = 1−31 bが偏心位置にあるために遠心
力の作用下で潤滑油が送油路z3を通して油溜り室32
内に供給されるようになっている。
Further, the outlet oil passage 31 is formed in a hook shape, and the inlet port 31
a opens at the second position of the bearing hole 5, and the outlet port 31b
is opened at a position eccentric from the axial center of the drive shaft 6, and an oil reservoir chamber 32 is formed below the shaft end of the driven shaft 13. Therefore, when the drive shaft 6 rotates, the exit=1? = 1-31 Since b is in an eccentric position, lubricating oil passes through the oil feed path z3 and into the oil reservoir chamber 32 under the action of centrifugal force.
It is designed to be supplied internally.

このような構成からなるスクロール・コンプレッサにお
いては、駆動軸6の回転によって被駆動軸13を前記駆
動軸6の軸心回りに円運動をさせると2旋回スクロール
12が、オルダムリング16の作用によって、旋回運動
をする。そして、吸入ノ9イゾ25より吸込室22内へ
吸引されたガスは、旋回スクロール翼15と固定スクロ
ール翼23の翼間に形成された2個所の圧縮室34 、
34内にとじ込められ、旋回スクロールg15の旋回運
動に伴って圧縮室の容積が漸次減少され、ガスは圧縮さ
れ圧縮工程の終期で吐出ポート24より吐出室が内へ吐
き出される。第2図は圧縮工程中の固定スクロール翼2
3と旋回スクロール翼15の関係位置を示し、(a)か
ら(d)へ移行するに従い圧縮室Cエ 、C3の容積が
漸次変化していることがわかる。
In the scroll compressor having such a configuration, when the driven shaft 13 is caused to make a circular motion around the axis of the drive shaft 6 by the rotation of the drive shaft 6, the two orbiting scrolls 12 are moved by the action of the Oldham ring 16. make a rotating movement. Then, the gas sucked into the suction chamber 22 from the suction nozzle 25 is compressed into two compression chambers 34 formed between the orbiting scroll blade 15 and the fixed scroll blade 23.
The volume of the compression chamber is gradually reduced as the orbiting scroll g15 rotates, and the gas is compressed and discharged into the discharge chamber from the discharge port 24 at the end of the compression process. Figure 2 shows the fixed scroll blade 2 during the compression process.
3 and the orbiting scroll blade 15, and it can be seen that the volumes of the compression chambers C and C3 gradually change as they move from (a) to (d).

そして、吐出z −1−24の孔径は、従来のものよ抄
拡大されているため、この吐出ポート24を高圧ガスが
通過する際に生ずる流体損失は、非常に小さくなってい
る。しかも、最終段階の圧縮室の容積は、従来のものと
ほとんど変らないため、ガスの圧縮比はそのまま維持さ
れる。
Since the hole diameter of the discharge port z-1-24 is enlarged compared to the conventional one, the fluid loss that occurs when high-pressure gas passes through the discharge port 24 is extremely small. Moreover, since the volume of the compression chamber at the final stage is almost the same as in the conventional case, the compression ratio of the gas is maintained as is.

〔発明の効果〕〔Effect of the invention〕

以上述べたように1本発明は、固定スクロール翼の翼腹
に吐出ポートに連通しかつこの吐出ポートから翼の高さ
方向に延びる切欠溝を形成して。
As described above, one aspect of the present invention is to form a notched groove in the blade belly of a fixed scroll blade that communicates with a discharge port and extends from the discharge port in the height direction of the blade.

前記吐出ポートの孔径を拡大したから、圧縮室で高圧に
されたガスが吐出ポートを通過する際の流体損失を非常
に小さくすることができ、圧縮効率を向上させることが
できる。しかも、圧縮室の容積変化はほとんどないため
、高圧縮比をその捷ま維持することができるという大き
な効果が得られる。
Since the hole diameter of the discharge port is enlarged, fluid loss when the high-pressure gas in the compression chamber passes through the discharge port can be extremely reduced, and compression efficiency can be improved. Moreover, since there is almost no change in the volume of the compression chamber, a great effect can be obtained in that a high compression ratio can be maintained.

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

第1図は、本発明によるスクロール・コンデンサーの一
実゛施例を示す縦断面図、第2図(a) 、 (b) 
。 における吐出ポート形成部分を示す底面図、B −B線
断面図、底面図およびC−C線断面図である。 12・・・旋回スクロール、15・・・旋回スクロール
翼、21・・・シュラウド、23・・・固定スクロール
翼、23a・・・切欠溝、24・・・吐出ポート。 出願人代理人  猪  股   清 80゛図 5I3W 躬7F] 第pH
FIG. 1 is a longitudinal sectional view showing an embodiment of a scroll capacitor according to the present invention, and FIGS. 2(a) and (b)
. FIG. 2 is a bottom view, a cross-sectional view taken along the line B-B, a bottom view, and a cross-sectional view taken along the line CC, showing a discharge port forming portion in FIG. DESCRIPTION OF SYMBOLS 12... Orbiting scroll, 15... Orbiting scroll wing, 21... Shroud, 23... Fixed scroll wing, 23a... Notch groove, 24... Discharge port. Applicant's representative Kiyoshi Inomata 80゛Figure 5I3W 7F] No. pH

Claims (1)

【特許請求の範囲】 シュラウドの内側に突設されたうず巻状の固定スクロー
ル翼に対して旋回スクロール翼をかみ合せ、上記旋回ス
クロール翼に対して旋回駆動させ。 両方のスクロール翼間に形成された圧縮室の容積変化を
利用してガスを圧縮し、上記クユラウげに形成された吐
出ポートより高圧ガスを吐出するようにしたスクロール
・コンプレッサにおいテ;前記固定スクロール翼の翼腹
に前記吐出ポートに連通しかつこの吐出ボートから翼高
さ方向に延びる切欠溝を形成して、前記吐出ポートの孔
径を拡大したことを特徴とするスクロール・コンプレッ
サ。
[Scope of Claims] An orbiting scroll vane is engaged with a spiral fixed scroll vane protruding from the inside of a shroud, and the orbiting scroll vane is driven to orbit. A scroll compressor that compresses gas by utilizing a change in volume of a compression chamber formed between both scroll blades, and discharges high-pressure gas from a discharge port formed in the above-mentioned shape; the fixed scroll blade; A scroll compressor characterized in that a notch groove is formed in the blade belly of the blade to communicate with the discharge port and extend from the discharge boat in the blade height direction, thereby enlarging the hole diameter of the discharge port.
JP57171736A 1982-09-30 1982-09-30 Scroll compressor Pending JPS5960093A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP57171736A JPS5960093A (en) 1982-09-30 1982-09-30 Scroll compressor

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP57171736A JPS5960093A (en) 1982-09-30 1982-09-30 Scroll compressor

Publications (1)

Publication Number Publication Date
JPS5960093A true JPS5960093A (en) 1984-04-05

Family

ID=15928725

Family Applications (1)

Application Number Title Priority Date Filing Date
JP57171736A Pending JPS5960093A (en) 1982-09-30 1982-09-30 Scroll compressor

Country Status (1)

Country Link
JP (1) JPS5960093A (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS60230585A (en) * 1984-04-27 1985-11-16 Matsushita Electric Ind Co Ltd Scroll compressor
JPH04214979A (en) * 1990-01-16 1992-08-05 Carrier Corp Scroll compressor
US5242283A (en) * 1991-03-15 1993-09-07 Kabushiki Kaisha Toyoda Jidoshokki Seisakusho Scroll type compressor with elongated discharge port
WO2006019010A1 (en) * 2004-08-17 2006-02-23 Matsushita Electric Industrial Co., Ltd. Scroll compressor
WO2019008875A1 (en) 2017-07-07 2019-01-10 ダイキン工業株式会社 Scroll compressor

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS60230585A (en) * 1984-04-27 1985-11-16 Matsushita Electric Ind Co Ltd Scroll compressor
JPH04214979A (en) * 1990-01-16 1992-08-05 Carrier Corp Scroll compressor
US5242283A (en) * 1991-03-15 1993-09-07 Kabushiki Kaisha Toyoda Jidoshokki Seisakusho Scroll type compressor with elongated discharge port
WO2006019010A1 (en) * 2004-08-17 2006-02-23 Matsushita Electric Industrial Co., Ltd. Scroll compressor
WO2019008875A1 (en) 2017-07-07 2019-01-10 ダイキン工業株式会社 Scroll compressor
JP2019015246A (en) * 2017-07-07 2019-01-31 ダイキン工業株式会社 Scroll compressor
CN110603381A (en) * 2017-07-07 2019-12-20 大金工业株式会社 Scroll compressor having a discharge port
CN110603381B (en) * 2017-07-07 2020-06-30 大金工业株式会社 Scroll compressor having a discharge port
US20200224658A1 (en) * 2017-07-07 2020-07-16 Daikin Industries, Ltd. Scroll compressor
US11067078B2 (en) 2017-07-07 2021-07-20 Daikin Industries, Ltd. Scroll compressor having single discharge port open at starting end of fixed-side wrap

Similar Documents

Publication Publication Date Title
CA2147644C (en) Scroll apparatus with reduced inlet pressure drop
EP2581605B1 (en) Scroll compressor with bypass hole
KR100338266B1 (en) Rotary compressor
JP3024743B2 (en) Rotary compressor
KR100688671B1 (en) Noise reducing structure for scroll compressor
US4571164A (en) Vane compressor with vane back pressure adjustment
JPH01163401A (en) Scroll type machine
JPS58135396A (en) Movable-blade compressor
US6203301B1 (en) Fluid pump
KR102409675B1 (en) Compressor having enhanced discharge structure
JP5195774B2 (en) Scroll compressor
JPS5960093A (en) Scroll compressor
KR102553485B1 (en) High-pressure type scroll compressor
US6764288B1 (en) Two stage scroll vacuum pump
KR20190106275A (en) Rotary compressor
JPH11247761A (en) Hermetic compressor
KR20060030767A (en) A double-acting orbiting vane compressor
JPS58170876A (en) Scroll compressor
KR100343727B1 (en) Structure for supporting crankshaft of scroll compressor
JPS58170883A (en) Scroll compressor
KR102548470B1 (en) Compressor having oldham's ring
JP4232705B2 (en) Swing compressor
JPS58170871A (en) Scroll compressor
JPS5960098A (en) Scroll compressor
JPS58170878A (en) Scroll compressor