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JPH09303287A - Gas compressor - Google Patents

Gas compressor

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Publication number
JPH09303287A
JPH09303287A JP12016496A JP12016496A JPH09303287A JP H09303287 A JPH09303287 A JP H09303287A JP 12016496 A JP12016496 A JP 12016496A JP 12016496 A JP12016496 A JP 12016496A JP H09303287 A JPH09303287 A JP H09303287A
Authority
JP
Japan
Prior art keywords
coolant
gas
flows
passage
easing
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
JP12016496A
Other languages
Japanese (ja)
Inventor
Seiichi Tanabe
清一 田辺
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.)
Mitsubishi Heavy Industries Ltd
Original Assignee
Mitsubishi Heavy Industries 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 Mitsubishi Heavy Industries Ltd filed Critical Mitsubishi Heavy Industries Ltd
Priority to JP12016496A priority Critical patent/JPH09303287A/en
Publication of JPH09303287A publication Critical patent/JPH09303287A/en
Pending legal-status Critical Current

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  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

PROBLEM TO BE SOLVED: To provide an excellent effect including the reduction of facility cost, the improvement of reliability and the reduction of a facility area, compared with a system for utilizing an external inter-cooler, by installing a gas cooling device inside at least one of a easing and a stationary blade so as to cool gases at a pressure rise process. SOLUTION: A coolant having pressure boosted with a pump 11 flows in the part of a casing 1A between the first-stage and the second-stage moving blades 13a and 13b, and a coolant passage 6a formed inside a stationary blade 3a via a pipeline 12. Also, the coolant after the coolant passage 6a first flows in an upper pipe passage 14a laid outside the easing 1A and then flows to the next coolant passage 6b. Furthermore, the coolant after the passage 6b flows in an upper pipeline 14b similarly formed outside the casing 1A and then flows in the next coolant passage 6c, thereby being discharged from an upper pipeline 12a. As a result, gases having pressure raised with the moving blades 13a to 13d are effectively cooled with the coolant flowing in the coolant passages 6a to 6c formed within the easing 1A and the stationary blades 3a to 3d.

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、所要動力を低減す
ることができるようにしたガス圧縮機に関する。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a gas compressor capable of reducing required power.

【0002】[0002]

【従来の技術】ガス圧縮機の所要動力は、入口ガス温度
に大きく依存している。従って、従来の多段ガス圧縮機
においては、図4に示すように、ガス圧縮機を低圧圧縮
機01aと高圧圧縮機01bで構成し、この両者間に昇
圧されるガスを冷却する中間冷却器011を併せ持った
設備が一部では実用化されている。なお、図4中02は
圧縮機を駆動するモータであり、白抜きの矢印は被昇圧
ガスの流れを示す。
2. Description of the Related Art The required power of a gas compressor largely depends on the inlet gas temperature. Therefore, in the conventional multi-stage gas compressor, as shown in FIG. 4, the gas compressor is composed of a low-pressure compressor 01a and a high-pressure compressor 01b, and an intercooler 011 for cooling the gas pressurized between the two. Some facilities that have both have been put to practical use. Reference numeral 02 in FIG. 4 denotes a motor for driving the compressor, and a white arrow indicates a flow of the gas to be pressurized.

【0003】しかし、コスト、信頼性及びスペース等の
点で、軸流ガス圧縮機ではこの方式のものは殆ど採用さ
れていない。
However, in terms of cost, reliability and space, this type of axial flow gas compressor is hardly adopted.

【0004】[0004]

【発明が解決しようとする課題】前述の図4に示す従来
の技術では、中間冷却による所要動力の低減という長所
はあるが、次のような短所が長所を大きく上回ってい
た。即ち、中間冷却器の前後でガス圧縮機を分けること
となり、部品点数増による設備費の上昇、信頼性の低下
及び設置面積の増加という問題点が長所を大きく上回っ
ていた。
The above-mentioned conventional technique shown in FIG. 4 has an advantage that the required power is reduced by the intercooling, but the following disadvantages greatly exceed the advantages. That is, the gas compressor is divided before and after the intercooler, and the problems such as an increase in equipment cost due to an increase in the number of parts, a decrease in reliability, and an increase in installation area greatly exceed the advantages.

【0005】本発明は、以上の問題点を解決することが
できるガス圧縮機を提供しようとするものである。
The present invention is intended to provide a gas compressor capable of solving the above problems.

【0006】[0006]

【課題を解決するための手段】本発明のガス圧縮機は、
昇圧途中のガスを冷却するガス冷却装置を車室及び静翼
の少くともいずれかの内部に設けたことを特徴とする。
The gas compressor of the present invention comprises:
It is characterized in that a gas cooling device for cooling the gas in the middle of pressurization is provided inside at least one of the passenger compartment and the vanes.

【0007】本発明は、前記の構成を有しているので、
昇圧途中のガスはガス圧縮機外へ抽気することなく冷却
される。
Since the present invention has the above structure,
The gas in the middle of pressurization is cooled without being extracted to the outside of the gas compressor.

【0008】[0008]

【発明の実施の形態】本発明の実施の第1の形態を、図
1によって説明する。1は、モータ2によって第1段な
いし第4段のその動翼13a,13b,13c,13d
が駆動される4段の軸流ガス圧縮機であり、車室1Aに
は、隣接する動翼の間に位置するように静翼3a,3
b,3c,3dが固定されている。
DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS A first embodiment of the present invention will be described with reference to FIG. The motor 1 uses the motor 2 to move the moving blades 13a, 13b, 13c, 13d of the first to fourth stages.
Is a four-stage axial flow gas compressor driven by a stationary vane 3a, 3
b, 3c and 3d are fixed.

【0009】10は、軸流ガス圧縮機1外に設けられた
液体の冷媒溜めであり、同冷媒溜め10にはポンプ11
が接続されている。各静翼3a,3b,3c及び車室1
Aの各静翼が取付けられている部分の内部には、それぞ
れ冷媒通路6a,6b,6cが設けられている。ポンプ
11によって昇圧された冷媒は、管路12を経て第1段
と第2段の動翼13a,13bの間の車室1Aの部分と
静翼3aの内部に設けられた冷媒通路6a内を流れ、同
冷媒通路6aを出た冷媒は一旦車室1A外へ排出された
上管路14aを通って次の冷媒通路6b内に流入し、ま
た、同冷媒通路6bを出た冷媒は上と同様に車室1A外
に排出された上管路14bを通って次の冷媒通路6cを
流れた上管路12aに排出されるようになっている。
Reference numeral 10 is a liquid refrigerant reservoir provided outside the axial flow gas compressor 1, and a pump 11 is provided in the refrigerant reservoir 10.
Is connected. Each stationary vane 3a, 3b, 3c and the passenger compartment 1
Refrigerant passages 6a, 6b, and 6c are provided inside the portion of A where each vane is attached. The refrigerant whose pressure is increased by the pump 11 passes through the pipe 12 and flows through the portion of the casing 1A between the first and second moving blades 13a and 13b and the inside of the refrigerant passage 6a provided inside the stationary blade 3a. The refrigerant that has flowed out of the refrigerant passage 6a flows into the next refrigerant passage 6b through the upper pipeline 14a that has been once discharged to the outside of the vehicle compartment 1A, and the refrigerant that has exited the refrigerant passage 6b is above. Similarly, it is designed to be discharged to the upper pipeline 12a flowing through the next refrigerant passage 6c through the upper pipeline 14b discharged to the outside of the vehicle interior 1A.

【0010】なお、図1中、1aはガス圧縮機1の被昇
圧ガスの低圧ガス入口1bはガス圧縮機1の被昇圧ガス
の高圧ガス出口であり、白抜き矢印は、被昇圧ガスの流
れを示している。
In FIG. 1, 1a is a low-pressure gas inlet 1b of the gas to be boosted in the gas compressor 1 and 1b is a high-pressure gas outlet of the gas to be boosted in the gas compressor 1, and the white arrow indicates the flow of the gas to be boosted. Is shown.

【0011】本実施の形態では、動翼13a,13b,
13c,13dによって昇圧される途中のガスは、車室
1A及び静翼3a,3b,3c,3dの内部に設けられ
た冷媒通路6a,6b,6c内を流れる冷媒によって冷
却されることとなり、外おきの中間冷却器を設けること
なく、従って被昇圧ガスをガス圧縮機1外へ抽気するこ
となく、昇圧途中のガスを冷却してガス圧縮機1の所要
動力を低減させることができる。
In this embodiment, the moving blades 13a, 13b,
The gas which is being pressurized by 13c and 13d is cooled by the refrigerant flowing in the refrigerant passages 6a, 6b and 6c provided inside the casing 1A and the vanes 3a, 3b, 3c and 3d, and the outside gas is cooled. It is possible to reduce the required power of the gas compressor 1 by cooling the gas in the middle of pressurization without providing an intercooler every other time and therefore without extracting the gas to be boosted out of the gas compressor 1.

【0012】なお、前記の液体の冷媒としては、低温ボ
イラ給水、脱気器給水等を用いることができる。また、
液体の冷媒に代えて、ガスの冷媒、例えば低温の被昇圧
ガス、低温の水素ガス等を用いることもできる。
As the liquid refrigerant, low temperature boiler feed water, deaerator feed water or the like can be used. Also,
Instead of the liquid refrigerant, a gas refrigerant, for example, a low temperature boosted gas, a low temperature hydrogen gas, or the like can be used.

【0013】本発明の実施の第2の形態を、図2及び図
3によって説明する。本実施の形態は、前記本発明の第
1の形態において、各静翼3a,3b,3cのシュラウ
ド4a,4b,4c,及び車室1Aの隣接する静翼間の
部分の内表面に多数の吸熱フィン5を設けている。ま
た、車室1Aと静翼3a,3b,3cの内部に連続した
冷媒通路6を設けており、各冷媒通路6は、図3(a)
に示すように冷却パイプにより構成し、又は図3(b)
に示すように車室1Aの内壁が冷媒通路6の一つの壁と
なるように構成されている。
A second embodiment of the present invention will be described with reference to FIGS. This embodiment is different from the first embodiment of the present invention in that a large number of shrouds 4a, 4b, 4c of the respective vanes 3a, 3b, 3c and a large number of inner surfaces of a portion between the adjacent vanes of the vehicle interior 1A are provided. A heat absorbing fin 5 is provided. Further, a continuous refrigerant passage 6 is provided inside the casing 1A and the stationary vanes 3a, 3b, 3c, and each refrigerant passage 6 is shown in FIG.
As shown in Fig. 3, it is configured by a cooling pipe, or Fig. 3 (b).
As shown in (1), the inner wall of the vehicle interior 1A is configured to be one wall of the refrigerant passage 6.

【0014】本実施の形態においても、前記本発明の実
施の第1の形態におけると同様に昇圧途中のガスを冷却
してガス圧縮機の所要動力を低減させることができる
が、フィン5によって前記昇圧途中のガスの冷却を更に
効果的に行なうことが可能である。
Also in this embodiment, as in the first embodiment of the present invention, the gas in the middle of pressurization can be cooled to reduce the required power of the gas compressor. It is possible to more effectively cool the gas during pressurization.

【0015】なお、前記の本発明の第1及び第2の形態
は、多段の軸流圧縮機に係るが、本発明は多段のガス圧
縮機に広く適用することができる。
The first and second embodiments of the present invention described above relate to a multi-stage axial compressor, but the present invention can be widely applied to multi-stage gas compressors.

【0016】[0016]

【発明の効果】以上説明したように、本発明において
は、ガス圧縮機の車室及び静翼の少くともいずれかの内
部に昇圧途中のガスを冷却する冷却装置を設けているの
で、外おきの中間冷却器を用いる方式に比べて設備費削
減、信頼性向上及び設置面積削減という効果が得られ、
経済的なガス圧縮機を提供することができる。
As described above, according to the present invention, since the cooling device for cooling the gas in the middle of pressurization is provided inside at least one of the passenger compartment and the stationary blades of the gas compressor, it is kept outside. Compared with the method that uses the intercooler, the effects of reduced equipment costs, improved reliability, and reduced installation area can be obtained.
An economical gas compressor can be provided.

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

【図1】本発明の実施の第1の形態の概略図である。FIG. 1 is a schematic diagram of a first embodiment of the present invention.

【図2】本発明の実施の第2の形態の概略図である。FIG. 2 is a schematic diagram of a second embodiment of the present invention.

【図3】図3(a)及び図3(b)は、前記本発明の実
施の第2の形態に用いられる冷媒通路を示す図2のA−
A矢視断面図である。
3 (a) and 3 (b) are A- of FIG. 2 showing a refrigerant passage used in the second embodiment of the present invention.
FIG.

【図4】従来のガス圧縮機の概念図である。FIG. 4 is a conceptual diagram of a conventional gas compressor.

【符号の説明】[Explanation of symbols]

1 軸流ガス圧縮機 1a 低圧ガス入口 1b 高圧ガス出口 1A 車室 2 モータ 3a,3b,3c,3d 静翼 4a,4b,4c シュラウド 5 フィン 6,6a,6b,6c 冷媒通路 10 冷媒溜め 11 ポンプ 12,12a 管路 13a,13b,13c,13d 動翼 14a,14b 管路 1 Axial Flow Gas Compressor 1a Low Pressure Gas Inlet 1b High Pressure Gas Outlet 1A Cabin 2 Motors 3a, 3b, 3c, 3d Stator Blades 4a, 4b, 4c Shroud 5 Fins 6, 6a, 6b, 6c Refrigerant Passage 10 Refrigerant Reservoir 11 Pump 12, 12a pipelines 13a, 13b, 13c, 13d moving blades 14a, 14b pipelines

Claims (1)

【特許請求の範囲】[Claims] 【請求項1】 昇圧途中のガスを冷却するガス冷却装置
を車室及び静翼の少くともいずれかの内部に設けたこと
を特徴とするガス圧縮機。
1. A gas compressor, characterized in that a gas cooling device for cooling gas in the middle of pressurization is provided inside at least one of a vehicle compartment and a vane.
JP12016496A 1996-05-15 1996-05-15 Gas compressor Pending JPH09303287A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP12016496A JPH09303287A (en) 1996-05-15 1996-05-15 Gas compressor

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP12016496A JPH09303287A (en) 1996-05-15 1996-05-15 Gas compressor

Publications (1)

Publication Number Publication Date
JPH09303287A true JPH09303287A (en) 1997-11-25

Family

ID=14779539

Family Applications (1)

Application Number Title Priority Date Filing Date
JP12016496A Pending JPH09303287A (en) 1996-05-15 1996-05-15 Gas compressor

Country Status (1)

Country Link
JP (1) JPH09303287A (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2012033744A3 (en) * 2010-09-09 2012-06-14 Southwest Research Institute Internally-cooled centrifugal compressor with cooling jacket formed in the diaphragm
WO2014134266A1 (en) * 2013-02-27 2014-09-04 Dresser-Rand Company Method of construction for internally cooled diaphragms for centrifugal compressor
CN106989066A (en) * 2017-05-25 2017-07-28 华能国际电力股份有限公司 Indirect cooling type multistage axial flow compressor and working method thereof
US10012107B2 (en) 2011-05-11 2018-07-03 Dresser-Rand Company Compact compression system with integral heat exchangers
US11519426B2 (en) 2020-02-14 2022-12-06 Mitsubishi Heavy Industries, Ltd. Pressurizing device, carbon dioxide cycle plant, and combined cycle plant

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2012033744A3 (en) * 2010-09-09 2012-06-14 Southwest Research Institute Internally-cooled centrifugal compressor with cooling jacket formed in the diaphragm
US10012107B2 (en) 2011-05-11 2018-07-03 Dresser-Rand Company Compact compression system with integral heat exchangers
WO2014134266A1 (en) * 2013-02-27 2014-09-04 Dresser-Rand Company Method of construction for internally cooled diaphragms for centrifugal compressor
CN106989066A (en) * 2017-05-25 2017-07-28 华能国际电力股份有限公司 Indirect cooling type multistage axial flow compressor and working method thereof
US11519426B2 (en) 2020-02-14 2022-12-06 Mitsubishi Heavy Industries, Ltd. Pressurizing device, carbon dioxide cycle plant, and combined cycle plant
DE102021200405B4 (en) 2020-02-14 2024-09-26 Mitsubishi Heavy Industries, Ltd. Pressure generating device, carbon dioxide cycle plant and combined cycle plant

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