[go: up one dir, main page]
More Web Proxy on the site http://driver.im/

JPH09324783A - Oil feed type multistage screw compressor and intermediate cooler - Google Patents

Oil feed type multistage screw compressor and intermediate cooler

Info

Publication number
JPH09324783A
JPH09324783A JP14256096A JP14256096A JPH09324783A JP H09324783 A JPH09324783 A JP H09324783A JP 14256096 A JP14256096 A JP 14256096A JP 14256096 A JP14256096 A JP 14256096A JP H09324783 A JPH09324783 A JP H09324783A
Authority
JP
Japan
Prior art keywords
oil
air
pressure stage
stage compressor
separated
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
JP14256096A
Other languages
Japanese (ja)
Inventor
Riichi Uchida
利一 内田
Hidetomo Mori
英智 茂利
Hirochika Kametani
裕敬 亀谷
Akira Suzuki
昭 鈴木
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 JP14256096A priority Critical patent/JPH09324783A/en
Publication of JPH09324783A publication Critical patent/JPH09324783A/en
Pending legal-status Critical Current

Links

Landscapes

  • Applications Or Details Of Rotary Compressors (AREA)

Abstract

PROBLEM TO BE SOLVED: To dispense with injected oil into the working chamber of a high pressure stage compressor so as to reduce oil stirring loss in the high pressure stage compressor by providing an intermediate cooler on the way of an air passage from a low pressure stage compressor to the high pressure stage compressor. SOLUTION: Air is sucked by a low pressure stage compressor 1 through a suction pipe 31, the pressure is raised, oil is injected in the compression process through an oil feed pipe 32b so as to lower the air discharge temperature, and the air is introduced to an intermediate cooler 3 in the condition of containing a large quantity of oil. Air entering from the air inlet 17 of the intermediate cooler 3 collides with the inner wall, and air and oil are separated from each other. Further, the air passes through an air passage 11 and reaches an air outlet 18, a part of separated oil during the time is carried together with air, but the oil is interrupted with a baffle 19. Meanwhile, the separated oil is mixed with air again at the air outlet after being sufficiently cooled by a cooling part 12, so as to lower air temperature. The air is further raised in pressure in a high pressure stage compressor 2, but the air contains oil injected at the low pressure stage compressor 1 in this compression process, and hence it dispenses with oil injection as cooling.

Description

【発明の詳細な説明】Detailed Description of the Invention

【0001】[0001]

【発明の属する技術分野】本発明は作動室内に油を噴射
する給油式スクリュー圧縮機および中間冷却器に関す
る。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to an oil supply type screw compressor and an intercooler for injecting oil into a working chamber.

【0002】[0002]

【従来の技術】従来、給油式2段スクリュー圧縮機で
は、低圧段,高圧段それぞれの圧縮機に圧縮空気の冷
却,ロータの潤滑,すきまのシールのため、作動室に油
を噴射していた。また、低圧段圧縮機と高圧段圧縮機の
間はそれぞれのケーシングで空気通路を形成させただけ
で、中間冷却は行っていなかった。低圧段圧縮機で吸込
まれた空気は圧縮中に油により噴射冷却され、さらに高
圧段でも油により噴射冷却される。
2. Description of the Related Art Conventionally, in a refueling type two-stage screw compressor, oil is injected into the working chamber for cooling the compressed air, lubricating the rotor, and sealing the clearance in each of the low-pressure and high-pressure compressors. . Further, between the low-pressure stage compressor and the high-pressure stage compressor, air passages were formed only in the respective casings, and no intermediate cooling was performed. The air sucked by the low-pressure stage compressor is jet-cooled by oil during compression, and is further jet-cooled by oil even in the high-pressure stage.

【0003】高圧段からの吐出空気には多量の油を含ん
でおり、空気と油を分離するオイルセパレータを設けて
いる。オイルセパレータで油を分離された清浄な空気は
冷却後、種々な用途に利用される。一方、分離された油
は油冷却器で冷却され、それぞれの圧縮機に再噴射され
る。
The air discharged from the high-pressure stage contains a large amount of oil, and an oil separator for separating air from oil is provided. The clean air separated from the oil by the oil separator is cooled and then used for various purposes. On the other hand, the separated oil is cooled by the oil cooler and re-injected into each compressor.

【0004】従来技術の関連として、特開昭57−65895
号公報がある。
As a relation to the prior art, Japanese Patent Laid-Open No. 57-65895.
There is an official gazette.

【0005】[0005]

【発明が解決しようとする課題】低圧段で噴射された油
は圧縮空気の冷却を行うが、吐出空気温度は給油温度よ
り10〜30℃高く、また、低圧段で十分に熱交換が完
了されるため、高圧段では再度油噴射による圧縮空気の
冷却が必要である。油噴射は冷却,潤滑、及びシールの
3作用が行われるが、潤滑及びシールには多量の油は不
必要で、多量の油は空気の冷却だけのものである。多量
の油は空気の冷却という最大の長所を持ち合わせるが、
反面、ロータによる撹拌損失という短所がある。
The oil injected in the low pressure stage cools the compressed air, but the discharge air temperature is 10 to 30 ° C. higher than the oil supply temperature, and heat exchange is sufficiently completed in the low pressure stage. Therefore, it is necessary to cool the compressed air by oil injection again in the high pressure stage. Oil injection has three functions of cooling, lubrication, and sealing, but a large amount of oil is unnecessary for lubrication and sealing, and a large amount of oil is only for cooling air. Large amounts of oil have the greatest advantage of cooling the air,
On the other hand, there is a disadvantage of stirring loss due to the rotor.

【0006】低圧段機で噴射された油は吐出までに十分
に熱交換が完了されており、低圧段機で噴射された油は
高圧段機にとっての圧縮空気の冷却効果はなく、油撹拌
損失の増加になるだけである。
The heat exchange of the oil injected by the low-pressure stage machine has been completed by the time it is discharged, and the oil injected by the low-pressure stage machine has no effect of cooling the compressed air for the high-pressure stage machine, resulting in oil agitation loss. Will only increase.

【0007】[0007]

【課題を解決するための手段】低圧段機と高圧段機の間
に中間冷却器を設け、高圧段機の油噴射を取り止めた。
An intercooler is provided between the low-pressure stage machine and the high-pressure stage machine to stop the oil injection of the high-pressure stage machine.

【0008】[0008]

【発明の実施の形態】以下、本発明の一実施例を図1な
いし図3を参照して説明する。
DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS An embodiment of the present invention will be described below with reference to FIGS.

【0009】図1に本発明の給油式2段スクリュー圧縮
機の系統図を示す。1は低圧段圧縮機、2は高圧段圧縮
機で、その間に中間冷却器3が設けてある。高圧段圧縮
機2の後流には油分離器4,後段冷却器5が設けてあ
る。油分離器4の上部には分離フィルタ6が設けてあ
り、下部には油7が充填してある。油分離器4の下部に
は油配管8が取付けてあり、油冷却器9を介して低圧段
圧縮機1,高圧段圧縮機2の軸受や作動室へ連結してい
る。
FIG. 1 shows a system diagram of a refueling type two-stage screw compressor of the present invention. Reference numeral 1 is a low-pressure stage compressor, 2 is a high-pressure stage compressor, and an intercooler 3 is provided between them. An oil separator 4 and a post-stage cooler 5 are provided downstream of the high-pressure stage compressor 2. A separation filter 6 is provided on the upper part of the oil separator 4, and oil 7 is filled on the lower part. An oil pipe 8 is attached to a lower portion of the oil separator 4, and is connected to a bearing and a working chamber of the low pressure stage compressor 1 and the high pressure stage compressor 2 via an oil cooler 9.

【0010】図2と図3に中間冷却機3を示す。中間冷
却器3は隔壁20によって空気通路部11と油冷却部1
2に分けられている。空気通路部11には隔壁20から
邪魔板19aが突き出しており、油冷却部12には邪魔
板19b,19c,19d,19eが設けてある。中間
冷却器3の両端には水ジャケット13a,13bが設け
てあり、水ジャケット13には水入口14と水出口15
が設けてある。水ジャケット13a,13bとは銅パイ
プ16で連結してあり、冷却水が水ジャケット13aか
ら銅パイプ16を介して水ジャケット13bへ流れる。
中間冷却器3の側面には空気入口17、下面には空気出
口18が設けてある。
The intercooler 3 is shown in FIGS. 2 and 3. The intercooler 3 includes the partition wall 20 and the air passage portion 11 and the oil cooling portion 1.
It is divided into two. A baffle plate 19a projects from the partition wall 20 in the air passage part 11, and baffle plates 19b, 19c, 19d, 19e are provided in the oil cooling part 12. Water jackets 13 a and 13 b are provided at both ends of the intercooler 3, and the water jacket 13 has a water inlet 14 and a water outlet 15.
Is provided. The water jackets 13a and 13b are connected by a copper pipe 16, and cooling water flows from the water jacket 13a through the copper pipe 16 to the water jacket 13b.
An air inlet 17 is provided on the side surface of the intercooler 3 and an air outlet 18 is provided on the lower surface thereof.

【0011】このように構成された給油式2段スクリュ
ー圧縮機の動作について説明する。低圧段圧縮機1は吸
込管31を介して空気を吸込み、1.8kgf/cm2G 程度
に昇圧する。圧縮過程では給油管32bを介して50℃
程度の油が噴射され、低圧段圧縮機1の出口での吐出温
度は60〜80℃となる。低圧段圧縮機1の吐出空気に
は多量の油が含まれており、その状態で中間冷却器3に
導かれる。
The operation of the oil-filled two-stage screw compressor constructed as described above will be described. The low-pressure stage compressor 1 sucks air through the suction pipe 31 and boosts the pressure to about 1.8 kgf / cm 2 G. In the compression process, 50 ° C through the oil supply pipe 32b
A certain amount of oil is injected, and the discharge temperature at the outlet of the low pressure stage compressor 1 becomes 60 to 80 ° C. The air discharged from the low-pressure compressor 1 contains a large amount of oil and is guided to the intercooler 3 in that state.

【0012】中間冷却器3の空気入口17から入った空
気は中間冷却器3の内壁に衝突し、空気と油を分離す
る。さらに空気は空気通路11を通過して空気出口18
に到達するが、その間分離した油33の一部が空気と共
に持ち去るが、邪魔板19aによって遮られる。一方、
分離油33は冷却部12で十分に冷却された後、空気出
口18で再度混合される。空気と油の混合により、空気
温度は数十度低下する。邪魔板19b,19c,19
d,19eは分離油33が銅パイプ16を効率的によぎ
ることで冷却効果を高め、また、邪魔板19eは油溜の
効果をも持ち合わせる。
The air entering from the air inlet 17 of the intercooler 3 collides with the inner wall of the intercooler 3 and separates air and oil. Further, the air passes through the air passage 11 and the air outlet 18
A part of the oil 33 separated during this time is carried away with the air, but is blocked by the baffle plate 19a. on the other hand,
The separated oil 33 is sufficiently cooled in the cooling unit 12 and then mixed again at the air outlet 18. Mixing air and oil lowers the air temperature by tens of degrees. Baffles 19b, 19c, 19
d and 19e enhance the cooling effect by the separated oil 33 efficiently crossing the copper pipe 16, and the baffle plate 19e also has the effect of the oil sump.

【0013】高圧段圧縮機2ではさらに昇圧され7kgf
/cm2G程度になる。この圧縮過程では低圧段圧縮機1
で噴射された冷却油が含まれており、冷却としての油噴
射は不要である。高圧段圧縮機2での吐出空気は低圧段
圧縮機1と同様60〜80℃になる。この吐出空気は油
分離器4での空気と油の分離、さらには後段冷却器5で
の空気の冷却を行った後、工場空気源として使用され
る。
In the high pressure stage compressor 2, the pressure is further increased to 7 kgf.
/ Cm 2 G In this compression process, the low pressure stage compressor 1
Since the cooling oil injected in the above is included, the oil injection for cooling is unnecessary. The discharge air in the high-pressure stage compressor 2 becomes 60 to 80 ° C. as in the low-pressure stage compressor 1. The discharged air is used as a factory air source after the air and oil are separated in the oil separator 4 and the air is cooled in the post-stage cooler 5.

【0014】油分離器5で分離された油は下部に落下
し、油分離器5内の圧力と圧縮機1,2の内の圧力差で
給油、再循環される。油冷却器9で冷却された油は低圧
段圧縮機1の軸受への給油32a,32cと作動室への
給油32b、並びに高圧段圧縮機の軸受32d,32e
へ供給される。
The oil separated by the oil separator 5 falls to the lower part, and is refueled and recirculated due to the pressure difference between the oil separator 5 and the compressors 1 and 2. The oil cooled by the oil cooler 9 is supplied with oil 32a, 32c to the bearings of the low-pressure compressor 1 and oil 32b to the working chamber, and bearings 32d, 32e of the high-pressure compressor.
Supplied to

【0015】図4と図5に中間冷却器の他の実施例を示
す。中間冷却器内筒の内側には螺旋板21と円周上に銅
パイプ16が設けられている。螺旋板19の内側にはガ
イド22が設けてある。空気入口17と空気出口18は
内筒軸心からオフセットされている。
4 and 5 show another embodiment of the intercooler. A spiral plate 21 and a copper pipe 16 are provided on the circumference of the inner tube of the intercooler. A guide 22 is provided inside the spiral plate 19. The air inlet 17 and the air outlet 18 are offset from the inner cylinder axis.

【0016】図4の中間冷却器で、空気入口17から油
を含んだ空気が入ると空気と油が旋回し、密度の大きい
油が外周側に流れる。螺旋板21のガイド22は一部の
分離油33が内側に流れることを防ぎ、螺旋板の上面に
伝い流れ銅パイプ16を介して分離油33を積極的に冷
却される。そして冷却された分離油33は空気出口18
で空気と混合冷却される。
In the intercooler of FIG. 4, when air containing oil enters from the air inlet 17, the air and the oil swirl, and oil having a high density flows to the outer peripheral side. The guide 22 of the spiral plate 21 prevents a part of the separated oil 33 from flowing inward, and the separated oil 33 is positively cooled via the copper pipe 16 that flows along the upper surface of the spiral plate. Then, the cooled separated oil 33 is supplied to the air outlet 18
It is mixed with air and cooled.

【0017】[0017]

【発明の効果】本発明によれば従来高圧段圧縮機の作動
室に噴射していた油が不要になり、高圧段圧縮機での油
撹拌損失が低減される。また従来、油冷却器を循環して
いた油量は低,高圧段圧縮機1,2の軸受と作動室への
和であったが、高圧段圧縮機への油噴射がなくなるた
め、油冷却器9を小形化できる。
According to the present invention, the oil that has been conventionally injected into the working chamber of the high-pressure compressor becomes unnecessary, and the oil agitation loss in the high-pressure compressor is reduced. In the past, the amount of oil circulating in the oil cooler was low, and was the sum of the bearings and working chambers of the high-pressure compressors 1 and 2, but since oil injection to the high-pressure compressor was eliminated, oil cooling The container 9 can be miniaturized.

【0018】さらに中間冷却器は中で空気と油を分離
し、容積当たりの熱容量の大きい油だけを冷却している
ので、中間冷却器の小形,高性能化が図れる。
Further, since the intercooler separates air and oil from each other and cools only the oil having a large heat capacity per volume, the intercooler can be made compact and have high performance.

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

【図1】本発明の給油式2段スクリュー圧縮機の系統
図。
FIG. 1 is a system diagram of a refueling type two-stage screw compressor of the present invention.

【図2】中間冷却器の縦断面図。FIG. 2 is a vertical sectional view of an intercooler.

【図3】図2のA−A断面図。FIG. 3 is a sectional view taken along line AA of FIG. 2;

【図4】中間冷却器の他の実施例の断面図。FIG. 4 is a cross-sectional view of another embodiment of the intercooler.

【図5】図4のB−B断面図。FIG. 5 is a sectional view taken along line BB of FIG. 4;

【符号の説明】[Explanation of symbols]

1…低圧段圧縮機、2…高圧段圧縮機、3…中間冷却
器、11…空気通路部、12…油冷却部。
DESCRIPTION OF SYMBOLS 1 ... Low-pressure stage compressor, 2 ... High-pressure stage compressor, 3 ... Intercooler, 11 ... Air passage part, 12 ... Oil cooling part.

───────────────────────────────────────────────────── フロントページの続き (72)発明者 鈴木 昭 静岡県清水市村松390番地 株式会社日立 製作所空調システム事業部内 ─────────────────────────────────────────────────── ─── Continuation of the front page (72) Inventor Akira Suzuki 390 Muramatsu, Shimizu City, Shizuoka Prefecture Hitachi Ltd. Air Conditioning Systems Division

Claims (4)

【特許請求の範囲】[Claims] 【請求項1】低圧圧縮機から高圧圧縮機へと空気通路で
連結された給油式多段スクリュー圧縮機において、前記
空気通路の途中に中間冷却器を設けたことを特徴とする
給油式多段スクリュー圧縮機。
1. A refueling multi-stage screw compressor in which a low pressure compressor is connected to a high pressure compressor by an air passage, and an intercooler is provided in the middle of the air passage. Machine.
【請求項2】前記中間冷却器はガスと油の二相流の油だ
けを選択的に冷却する機能を有し、さらに入口近くでガ
スと油の分離機能、並びに出口近くでガスと油の混合機
能を有する請求項1に記載の給油式多段スクリュー圧縮
機。
2. The intercooler has a function of selectively cooling only oil in a two-phase flow of gas and oil, and further has a function of separating gas and oil near an inlet and a function of separating gas and oil near an outlet. The refueling multi-stage screw compressor according to claim 1, which has a mixing function.
【請求項3】重力によってガスと油の分離を行う請求項
2に記載の中間冷却器。
3. The intercooler according to claim 2, wherein the gas and the oil are separated by gravity.
【請求項4】遠心力によってガスと油の分離を行う請求
項2に記載の中間冷却器。
4. The intercooler according to claim 2, wherein gas and oil are separated by centrifugal force.
JP14256096A 1996-06-05 1996-06-05 Oil feed type multistage screw compressor and intermediate cooler Pending JPH09324783A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP14256096A JPH09324783A (en) 1996-06-05 1996-06-05 Oil feed type multistage screw compressor and intermediate cooler

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP14256096A JPH09324783A (en) 1996-06-05 1996-06-05 Oil feed type multistage screw compressor and intermediate cooler

Publications (1)

Publication Number Publication Date
JPH09324783A true JPH09324783A (en) 1997-12-16

Family

ID=15318183

Family Applications (1)

Application Number Title Priority Date Filing Date
JP14256096A Pending JPH09324783A (en) 1996-06-05 1996-06-05 Oil feed type multistage screw compressor and intermediate cooler

Country Status (1)

Country Link
JP (1) JPH09324783A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
BE1014461A3 (en) * 2001-11-08 2003-10-07 Atlas Copco Airpower Nv Oil injected screw compressor, has separate oil supply system with cooler for lubricating rotor bearings
CN100425839C (en) * 2006-11-15 2008-10-15 烟台冰轮股份有限公司 Single-unit two-stage screw refrigeration compressor set and using method therefor
CN103175346A (en) * 2011-12-26 2013-06-26 株式会社神户制钢所 Oil-cooling type secondary compressor and heat pump
CN110939570A (en) * 2018-09-25 2020-03-31 阿特拉斯·科普柯空气动力股份有限公司 Oil-injected multistage compressor arrangement and method for controlling the compressor arrangement

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
BE1014461A3 (en) * 2001-11-08 2003-10-07 Atlas Copco Airpower Nv Oil injected screw compressor, has separate oil supply system with cooler for lubricating rotor bearings
CN100425839C (en) * 2006-11-15 2008-10-15 烟台冰轮股份有限公司 Single-unit two-stage screw refrigeration compressor set and using method therefor
CN103175346A (en) * 2011-12-26 2013-06-26 株式会社神户制钢所 Oil-cooling type secondary compressor and heat pump
CN110939570A (en) * 2018-09-25 2020-03-31 阿特拉斯·科普柯空气动力股份有限公司 Oil-injected multistage compressor arrangement and method for controlling the compressor arrangement
KR20210047352A (en) * 2018-09-25 2021-04-29 아틀라스 캅코 에어파워, 남로체 벤누트삽 Oil-injected multi-stage compressor arrangement and method for controlling such compressor arrangement
CN110939570B (en) * 2018-09-25 2021-09-28 阿特拉斯·科普柯空气动力股份有限公司 Oil-injected multistage compressor arrangement and method for controlling the compressor arrangement
TWI748246B (en) * 2018-09-25 2021-12-01 比利時商亞特拉斯可波克氣動股份有限公司 Oil-injected multistage compressor device and method for controlling such a compressor device

Similar Documents

Publication Publication Date Title
US3291385A (en) Receiver-separator unit for liquidinjected compressor
US8187370B2 (en) Horizontal bulk oil separator
TWI509207B (en) Refrigeration circuit using a vapor compression cycle
JP6670196B2 (en) Gas-liquid separator for compression refrigerators
US4780061A (en) Screw compressor with integral oil cooling
CN105090041B (en) Helical-lobe compressor and water cooler with oil eliminator
CN1071999A (en) Integral oil separator and baffler
US3684412A (en) Oil separator for rotary compressor
JPH06173873A (en) Oil injection type screw compressor
CA2258944A1 (en) Core-in-shell heat exchangers for multistage compressors
US6991443B2 (en) Oil injected screw compressor
US3822567A (en) Refrigerating apparatus
JP2003201964A (en) Gas compressor
CN107120879A (en) Air conditioning equipment, centrifugal unit and flash tank thereof
JPH09324783A (en) Oil feed type multistage screw compressor and intermediate cooler
JP2003083272A (en) Screw compressor
WO2014000671A1 (en) Oil return device and scroll compressor having the same
CN211345950U (en) Oil separator, condenser and refrigerating system
CN105332912A (en) Scroll compressor and air conditioner comprising same
KR100776075B1 (en) Condenser in one form with oil separator
CN100348867C (en) Method and structure for improving efficiency and reliability of vertical vortex compressor
CN111810407A (en) Oil-gas separation structure of compressor, compressor and air conditioner
JP7554254B2 (en) Helium compressor system with unmodified scroll compressor
JP2518455B2 (en) Compressor for cryogenic refrigerator
CN117386585A (en) Combined gas-liquid separator