GAS TURBINE IN MECHANICAL DRIVE APPLICATIONS AND OPERATING METHODS
A drive system for driving at least one compressor is described. The system comprises a gas turbine configured and arranged for driving the compressor. The gas turbine has a hot end and a cold end. A load coupling for connection of said gas turbine to the compressor is arranged at hot end of the gas...
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| creator | NALDI, Lorenzo SCARPONI, Marco BATTAGLI, Paolo MILANI, Guiliano BIANCHI, Paulo AGOSTINI, Damiano PELAGOTTI, Antonio LIBRASCHI, Mirko LAZZARI, Annunzio DELL'ANNA, Graziano ANTONINI, Claudio |
| description | A drive system for driving at least one compressor is described. The system comprises a gas turbine configured and arranged for driving the compressor. The gas turbine has a hot end and a cold end. A load coupling for connection of said gas turbine to the compressor is arranged at hot end of the gas turbine. An electric motor/generator arranged at the cold end of the gas turbine. The electric motor/generator is electrically connected to an electric power grid and is adapted to function as a generator for converting excess mechanical power from the gas turbine into electrical power and delivering the electrical power to the electric power grid, and as a motor for supplementing driving power to the compressor. |
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The system comprises a gas turbine configured and arranged for driving the compressor. The gas turbine has a hot end and a cold end. A load coupling for connection of said gas turbine to the compressor is arranged at hot end of the gas turbine. An electric motor/generator arranged at the cold end of the gas turbine. The electric motor/generator is electrically connected to an electric power grid and is adapted to function as a generator for converting excess mechanical power from the gas turbine into electrical power and delivering the electrical power to the electric power grid, and as a motor for supplementing driving power to the compressor.</description><language>eng ; fre ; ger</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 ; STEAM ENGINES ; WEAPONS</subject><creationdate>2019</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=20190925&DB=EPODOC&CC=EP&NR=2917504B1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25542,76289</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20190925&DB=EPODOC&CC=EP&NR=2917504B1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>NALDI, Lorenzo</creatorcontrib><creatorcontrib>SCARPONI, Marco</creatorcontrib><creatorcontrib>BATTAGLI, Paolo</creatorcontrib><creatorcontrib>MILANI, Guiliano</creatorcontrib><creatorcontrib>BIANCHI, Paulo</creatorcontrib><creatorcontrib>AGOSTINI, Damiano</creatorcontrib><creatorcontrib>PELAGOTTI, Antonio</creatorcontrib><creatorcontrib>LIBRASCHI, Mirko</creatorcontrib><creatorcontrib>LAZZARI, Annunzio</creatorcontrib><creatorcontrib>DELL'ANNA, Graziano</creatorcontrib><creatorcontrib>ANTONINI, Claudio</creatorcontrib><title>GAS TURBINE IN MECHANICAL DRIVE APPLICATIONS AND OPERATING METHODS</title><description>A drive system for driving at least one compressor is described. The system comprises a gas turbine configured and arranged for driving the compressor. The gas turbine has a hot end and a cold end. A load coupling for connection of said gas turbine to the compressor is arranged at hot end of the gas turbine. An electric motor/generator arranged at the cold end of the gas turbine. The electric motor/generator is electrically connected to an electric power grid and is adapted to function as a generator for converting excess mechanical power from the gas turbine into electrical power and delivering the electrical power to the electric power grid, and as a motor for supplementing driving power to the compressor.</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>STEAM ENGINES</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2019</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZHBydwxWCAkNcvL0c1Xw9FPwdXX2cPTzdHb0UXAJ8gxzVXAMCPABckM8_f2CFRz9XBT8A1yDgFw_d6DaEA9_l2AeBta0xJziVF4ozc2g4OYa4uyhm1qQH59aXJCYnJqXWhLvGmBkaWhuamDiZGhMhBIAldQqrA</recordid><startdate>20190925</startdate><enddate>20190925</enddate><creator>NALDI, Lorenzo</creator><creator>SCARPONI, Marco</creator><creator>BATTAGLI, Paolo</creator><creator>MILANI, Guiliano</creator><creator>BIANCHI, Paulo</creator><creator>AGOSTINI, Damiano</creator><creator>PELAGOTTI, Antonio</creator><creator>LIBRASCHI, Mirko</creator><creator>LAZZARI, Annunzio</creator><creator>DELL'ANNA, Graziano</creator><creator>ANTONINI, Claudio</creator><scope>EVB</scope></search><sort><creationdate>20190925</creationdate><title>GAS TURBINE IN MECHANICAL DRIVE APPLICATIONS AND OPERATING METHODS</title><author>NALDI, Lorenzo ; SCARPONI, Marco ; BATTAGLI, Paolo ; MILANI, Guiliano ; BIANCHI, Paulo ; AGOSTINI, Damiano ; PELAGOTTI, Antonio ; LIBRASCHI, Mirko ; LAZZARI, Annunzio ; DELL'ANNA, Graziano ; ANTONINI, Claudio</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_EP2917504B13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre ; ger</language><creationdate>2019</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>STEAM ENGINES</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>NALDI, Lorenzo</creatorcontrib><creatorcontrib>SCARPONI, Marco</creatorcontrib><creatorcontrib>BATTAGLI, Paolo</creatorcontrib><creatorcontrib>MILANI, Guiliano</creatorcontrib><creatorcontrib>BIANCHI, Paulo</creatorcontrib><creatorcontrib>AGOSTINI, Damiano</creatorcontrib><creatorcontrib>PELAGOTTI, Antonio</creatorcontrib><creatorcontrib>LIBRASCHI, Mirko</creatorcontrib><creatorcontrib>LAZZARI, Annunzio</creatorcontrib><creatorcontrib>DELL'ANNA, Graziano</creatorcontrib><creatorcontrib>ANTONINI, Claudio</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>NALDI, Lorenzo</au><au>SCARPONI, Marco</au><au>BATTAGLI, Paolo</au><au>MILANI, Guiliano</au><au>BIANCHI, Paulo</au><au>AGOSTINI, Damiano</au><au>PELAGOTTI, Antonio</au><au>LIBRASCHI, Mirko</au><au>LAZZARI, Annunzio</au><au>DELL'ANNA, Graziano</au><au>ANTONINI, Claudio</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>GAS TURBINE IN MECHANICAL DRIVE APPLICATIONS AND OPERATING METHODS</title><date>2019-09-25</date><risdate>2019</risdate><abstract>A drive system for driving at least one compressor is described. The system comprises a gas turbine configured and arranged for driving the compressor. The gas turbine has a hot end and a cold end. A load coupling for connection of said gas turbine to the compressor is arranged at hot end of the gas turbine. An electric motor/generator arranged at the cold end of the gas turbine. The electric motor/generator is electrically connected to an electric power grid and is adapted to function as a generator for converting excess mechanical power from the gas turbine into electrical power and delivering the electrical power to the electric power grid, and as a motor for supplementing driving power to the compressor.</abstract><oa>free_for_read</oa></addata></record> |
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| language | eng ; fre ; ger |
| recordid | cdi_epo_espacenet_EP2917504B1 |
| source | esp@cenet |
| 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 STEAM ENGINES WEAPONS |
| title | GAS TURBINE IN MECHANICAL DRIVE APPLICATIONS AND OPERATING METHODS |
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