GAS TURBINE EQUIPMENT AND GAS TURBINE POWER GENERATING EQUIPMENT
PROBLEM TO BE SOLVED: To provide gas turbine equipment and gas turbine power generating equipment for reducing heat transmission from a gas turbine to a compressor with simple structure. SOLUTION: Between the gas turbine 2 and the compressor 1, for example, an air through passage AF making part of c...
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| creator | HAYASAKA YASUSHI SEKIHARA TAKASHI |
| description | PROBLEM TO BE SOLVED: To provide gas turbine equipment and gas turbine power generating equipment for reducing heat transmission from a gas turbine to a compressor with simple structure. SOLUTION: Between the gas turbine 2 and the compressor 1, for example, an air through passage AF making part of compressed air of a compressor 1 flow to a gas turbine 2 side is formed as a heat transmission reducing means. By the simple structure where the air through passage AF as the heat transmission reducing means is formed, the heat transmitted from the gas turbine 2 to a compressor 1 side is cooled by the transmission heat reducing means, or is kept out and reduced. Therefore, a high temperature is not transmitted to the compressor 1 side and degradation in performance of the compressor 1 is prevented. COPYRIGHT: (C)2005,JPO&NCIPI |
| format | Patent |
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SOLUTION: Between the gas turbine 2 and the compressor 1, for example, an air through passage AF making part of compressed air of a compressor 1 flow to a gas turbine 2 side is formed as a heat transmission reducing means. By the simple structure where the air through passage AF as the heat transmission reducing means is formed, the heat transmitted from the gas turbine 2 to a compressor 1 side is cooled by the transmission heat reducing means, or is kept out and reduced. Therefore, a high temperature is not transmitted to the compressor 1 side and degradation in performance of the compressor 1 is prevented. COPYRIGHT: (C)2005,JPO&NCIPI</description><edition>7</edition><language>eng</language><subject>AIR INTAKES FOR JET-PROPULSION PLANTS ; BLASTING ; COMBUSTION ENGINES ; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS ; ENGINE PLANTS IN GENERAL ; GAS-TURBINE PLANTS ; HEATING ; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS ; LIGHTING ; MACHINES OR ENGINES IN GENERAL ; MECHANICAL ENGINEERING ; NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES ; NON-POSITIVE DISPLACEMENT PUMPS ; POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS ; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS ; STEAM ENGINES ; WEAPONS</subject><creationdate>2005</creationdate><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktohtml>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20050609&DB=EPODOC&CC=JP&NR=2005147079A$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76419</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20050609&DB=EPODOC&CC=JP&NR=2005147079A$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>HAYASAKA YASUSHI</creatorcontrib><creatorcontrib>SEKIHARA TAKASHI</creatorcontrib><title>GAS TURBINE EQUIPMENT AND GAS TURBINE POWER GENERATING EQUIPMENT</title><description>PROBLEM TO BE SOLVED: To provide gas turbine equipment and gas turbine power generating equipment for reducing heat transmission from a gas turbine to a compressor with simple structure. SOLUTION: Between the gas turbine 2 and the compressor 1, for example, an air through passage AF making part of compressed air of a compressor 1 flow to a gas turbine 2 side is formed as a heat transmission reducing means. By the simple structure where the air through passage AF as the heat transmission reducing means is formed, the heat transmitted from the gas turbine 2 to a compressor 1 side is cooled by the transmission heat reducing means, or is kept out and reduced. Therefore, a high temperature is not transmitted to the compressor 1 side and degradation in performance of the compressor 1 is prevented. COPYRIGHT: (C)2005,JPO&NCIPI</description><subject>AIR INTAKES FOR JET-PROPULSION PLANTS</subject><subject>BLASTING</subject><subject>COMBUSTION ENGINES</subject><subject>CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS</subject><subject>ENGINE PLANTS IN GENERAL</subject><subject>GAS-TURBINE PLANTS</subject><subject>HEATING</subject><subject>HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS</subject><subject>LIGHTING</subject><subject>MACHINES OR ENGINES IN GENERAL</subject><subject>MECHANICAL ENGINEERING</subject><subject>NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES</subject><subject>NON-POSITIVE DISPLACEMENT PUMPS</subject><subject>POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS</subject><subject>PUMPS FOR LIQUIDS OR ELASTIC FLUIDS</subject><subject>STEAM ENGINES</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2005</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZHBwdwxWCAkNcvL0c1VwDQz1DPB19QtRcPRzUUCWCfAPdw1ScHf1cw1yDPH0c0co5WFgTUvMKU7lhdLcDEpuriHOHrqpBfnxqcUFicmpeakl8V4BRgYGpoYm5gbmlo7GRCkCAAkHKz0</recordid><startdate>20050609</startdate><enddate>20050609</enddate><creator>HAYASAKA YASUSHI</creator><creator>SEKIHARA TAKASHI</creator><scope>EVB</scope></search><sort><creationdate>20050609</creationdate><title>GAS TURBINE EQUIPMENT AND GAS TURBINE POWER GENERATING EQUIPMENT</title><author>HAYASAKA YASUSHI ; SEKIHARA TAKASHI</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_JP2005147079A3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng</language><creationdate>2005</creationdate><topic>AIR INTAKES FOR JET-PROPULSION PLANTS</topic><topic>BLASTING</topic><topic>COMBUSTION ENGINES</topic><topic>CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS</topic><topic>ENGINE PLANTS IN GENERAL</topic><topic>GAS-TURBINE PLANTS</topic><topic>HEATING</topic><topic>HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS</topic><topic>LIGHTING</topic><topic>MACHINES OR ENGINES IN GENERAL</topic><topic>MECHANICAL ENGINEERING</topic><topic>NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES</topic><topic>NON-POSITIVE DISPLACEMENT PUMPS</topic><topic>POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS</topic><topic>PUMPS FOR LIQUIDS OR ELASTIC FLUIDS</topic><topic>STEAM ENGINES</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>HAYASAKA YASUSHI</creatorcontrib><creatorcontrib>SEKIHARA TAKASHI</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>HAYASAKA YASUSHI</au><au>SEKIHARA TAKASHI</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>GAS TURBINE EQUIPMENT AND GAS TURBINE POWER GENERATING EQUIPMENT</title><date>2005-06-09</date><risdate>2005</risdate><abstract>PROBLEM TO BE SOLVED: To provide gas turbine equipment and gas turbine power generating equipment for reducing heat transmission from a gas turbine to a compressor with simple structure. SOLUTION: Between the gas turbine 2 and the compressor 1, for example, an air through passage AF making part of compressed air of a compressor 1 flow to a gas turbine 2 side is formed as a heat transmission reducing means. By the simple structure where the air through passage AF as the heat transmission reducing means is formed, the heat transmitted from the gas turbine 2 to a compressor 1 side is cooled by the transmission heat reducing means, or is kept out and reduced. Therefore, a high temperature is not transmitted to the compressor 1 side and degradation in performance of the compressor 1 is prevented. COPYRIGHT: (C)2005,JPO&NCIPI</abstract><edition>7</edition><oa>free_for_read</oa></addata></record> |
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| subjects | AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS ENGINE PLANTS IN GENERAL GAS-TURBINE PLANTS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES NON-POSITIVE DISPLACEMENT PUMPS POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PUMPS FOR LIQUIDS OR ELASTIC FLUIDS STEAM ENGINES WEAPONS |
| title | GAS TURBINE EQUIPMENT AND GAS TURBINE POWER GENERATING EQUIPMENT |
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