MULTISTAGE COMPRESSION TURBINE TYPE COOLING SYSTEM AND MULTISTAGE COMPRESSION TURBINE TYPE COOLING METHOD

To provide a multistage compression turbine type cooling system that can increase/decrease refrigerating capacity without decreasing refrigerating efficiency, and a cooling method thereof.SOLUTION: A multistage compression turbine type cooling system 1A comprises: a main heat exchanger 2; an auxilia...

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Hauptverfasser: HIROKAWA MASAKI, ISHII MASATERU
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creator HIROKAWA MASAKI
ISHII MASATERU
description To provide a multistage compression turbine type cooling system that can increase/decrease refrigerating capacity without decreasing refrigerating efficiency, and a cooling method thereof.SOLUTION: A multistage compression turbine type cooling system 1A comprises: a main heat exchanger 2; an auxiliary heat exchanger 3; a first stage side turbocompressor 4a, a second stage side turbocompressor 4b, and a third stage side turbocompressor 4c that are three units constituting a maximum of three stages; a first stage side driving motor 5a, a second stage side driving motor 5b, and a third stage side driving motor 5c that are three units corresponding to the three stages; an expansion turbine 6; a first stage side water-cooled cooler 7a, a second stage side water-cooled cooler 7b, and a third stage side water-cooled cooler 7c; a valve 8a between the main heat exchanger and the first stage side compressor, a valve 8b between the first stage side and second stage side compressors, and a first stage side compressor bypass valve 8c; a first circulation path L1; and a second circulation path L2.SELECTED DRAWING: Figure 1 【課題】冷凍効率を落とさずに冷凍能力を増減させることができる多段圧縮タービン式冷却システム及びその冷却方法を提供する。【解決手段】主熱交換器2と、副熱交換器3と、最大3段を構成する3基の1段側ターボ圧縮機4a、2段側ターボ圧縮機4b、及び3段側ターボ圧縮機4cと、その3段に対応した3基の1段側駆動モータ5a、2段側駆動モータ5b、及び3段側駆動モータ5cと、膨張タービン6と、1段側水冷クーラー7a、2段側水冷クーラー7b、及び3段側水冷クーラー7cと、主熱交換器/1段側圧縮機間弁8a、1段側/2段側圧縮機間弁8b、及び1段側圧縮機バイパス弁8cと、第1の循環経路L1と、第2の循環経路L2と、を備える多段圧縮タービン式冷却システム1Aを選択する。【選択図】図1
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ISHII MASATERU</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_JP2020060341A3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; jpn</language><creationdate>2020</creationdate><topic>BLASTING</topic><topic>COMBINED HEATING AND REFRIGERATION SYSTEMS</topic><topic>HEAT PUMP SYSTEMS</topic><topic>HEATING</topic><topic>LIGHTING</topic><topic>LIQUEFACTION SOLIDIFICATION OF GASES</topic><topic>MANUFACTURE OR STORAGE OF ICE</topic><topic>MECHANICAL ENGINEERING</topic><topic>REFRIGERATION MACHINES, PLANTS OR SYSTEMS</topic><topic>REFRIGERATION OR COOLING</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>HIROKAWA MASAKI</creatorcontrib><creatorcontrib>ISHII MASATERU</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>HIROKAWA MASAKI</au><au>ISHII MASATERU</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>MULTISTAGE COMPRESSION TURBINE TYPE COOLING SYSTEM AND MULTISTAGE COMPRESSION TURBINE TYPE COOLING METHOD</title><date>2020-04-16</date><risdate>2020</risdate><abstract>To provide a multistage compression turbine type cooling system that can increase/decrease refrigerating capacity without decreasing refrigerating efficiency, and a cooling method thereof.SOLUTION: A multistage compression turbine type cooling system 1A comprises: a main heat exchanger 2; an auxiliary heat exchanger 3; a first stage side turbocompressor 4a, a second stage side turbocompressor 4b, and a third stage side turbocompressor 4c that are three units constituting a maximum of three stages; a first stage side driving motor 5a, a second stage side driving motor 5b, and a third stage side driving motor 5c that are three units corresponding to the three stages; an expansion turbine 6; a first stage side water-cooled cooler 7a, a second stage side water-cooled cooler 7b, and a third stage side water-cooled cooler 7c; a valve 8a between the main heat exchanger and the first stage side compressor, a valve 8b between the first stage side and second stage side compressors, and a first stage side compressor bypass valve 8c; a first circulation path L1; and a second circulation path L2.SELECTED DRAWING: Figure 1 【課題】冷凍効率を落とさずに冷凍能力を増減させることができる多段圧縮タービン式冷却システム及びその冷却方法を提供する。【解決手段】主熱交換器2と、副熱交換器3と、最大3段を構成する3基の1段側ターボ圧縮機4a、2段側ターボ圧縮機4b、及び3段側ターボ圧縮機4cと、その3段に対応した3基の1段側駆動モータ5a、2段側駆動モータ5b、及び3段側駆動モータ5cと、膨張タービン6と、1段側水冷クーラー7a、2段側水冷クーラー7b、及び3段側水冷クーラー7cと、主熱交換器/1段側圧縮機間弁8a、1段側/2段側圧縮機間弁8b、及び1段側圧縮機バイパス弁8cと、第1の循環経路L1と、第2の循環経路L2と、を備える多段圧縮タービン式冷却システム1Aを選択する。【選択図】図1</abstract><oa>free_for_read</oa></addata></record>
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subjects BLASTING
COMBINED HEATING AND REFRIGERATION SYSTEMS
HEAT PUMP SYSTEMS
HEATING
LIGHTING
LIQUEFACTION SOLIDIFICATION OF GASES
MANUFACTURE OR STORAGE OF ICE
MECHANICAL ENGINEERING
REFRIGERATION MACHINES, PLANTS OR SYSTEMS
REFRIGERATION OR COOLING
WEAPONS
title MULTISTAGE COMPRESSION TURBINE TYPE COOLING SYSTEM AND MULTISTAGE COMPRESSION TURBINE TYPE COOLING METHOD
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