MULTIPLE STAGE TURBO-CHARGED ENGINE SYSTEM
An engine system includes an internal combustion engine and a first and second air charge system. The internal combustion engine comprises an air intake system and an exhaust manifold. The first air charge system comprising a first compressor, a turbine, and a generator/motor module. The first compr...
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| creator | Meano, Cesare Maria |
| description | An engine system includes an internal combustion engine and a first and second air charge system. The internal combustion engine comprises an air intake system and an exhaust manifold. The first air charge system comprising a first compressor, a turbine, and a generator/motor module. The first compressor has a first air inlet, a first air outlet, and a first input shaft. The first outlet is connected to the air intake system, the turbine has an exhaust gas inlet, and the exhaust gas inlet is connected to an outlet of the exhaust manifold. The second air charge system includes a second compressor and an electric motor. The second compressor has a second air inlet, a second air outlet, and a second input shaft. The electric motor has an outlet shaft directly coupled for common rotation with the first input shaft of the second compressor. |
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The first air charge system comprising a first compressor, a turbine, and a generator/motor module. The first compressor has a first air inlet, a first air outlet, and a first input shaft. The first outlet is connected to the air intake system, the turbine has an exhaust gas inlet, and the exhaust gas inlet is connected to an outlet of the exhaust manifold. The second air charge system includes a second compressor and an electric motor. The second compressor has a second air inlet, a second air outlet, and a second input shaft. The electric motor has an outlet shaft directly coupled for common rotation with the first input shaft of the second compressor.</description><language>eng</language><subject>AIR INTAKES FOR JET-PROPULSION PLANTS ; BLASTING ; COMBUSTION ENGINES ; COMBUSTION ENGINES IN GENERAL ; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS ; GAS-TURBINE PLANTS ; HEATING ; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS ; INTERNAL-COMBUSTION PISTON ENGINES ; LIGHTING ; MECHANICAL ENGINEERING ; WEAPONS</subject><creationdate>2020</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=20200625&DB=EPODOC&CC=US&NR=2020200074A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,778,883,25547,76298</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20200625&DB=EPODOC&CC=US&NR=2020200074A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>Meano, Cesare Maria</creatorcontrib><title>MULTIPLE STAGE TURBO-CHARGED ENGINE SYSTEM</title><description>An engine system includes an internal combustion engine and a first and second air charge system. The internal combustion engine comprises an air intake system and an exhaust manifold. The first air charge system comprising a first compressor, a turbine, and a generator/motor module. The first compressor has a first air inlet, a first air outlet, and a first input shaft. The first outlet is connected to the air intake system, the turbine has an exhaust gas inlet, and the exhaust gas inlet is connected to an outlet of the exhaust manifold. The second air charge system includes a second compressor and an electric motor. The second compressor has a second air inlet, a second air outlet, and a second input shaft. The electric motor has an outlet shaft directly coupled for common rotation with the first input shaft of the second compressor.</description><subject>AIR INTAKES FOR JET-PROPULSION PLANTS</subject><subject>BLASTING</subject><subject>COMBUSTION ENGINES</subject><subject>COMBUSTION ENGINES IN GENERAL</subject><subject>CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS</subject><subject>GAS-TURBINE PLANTS</subject><subject>HEATING</subject><subject>HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS</subject><subject>INTERNAL-COMBUSTION PISTON ENGINES</subject><subject>LIGHTING</subject><subject>MECHANICAL ENGINEERING</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2020</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZNDyDfUJ8QzwcVUIDnF0d1UICQ1y8td19nAMcnd1UXD1c_f0A0pFBoe4-vIwsKYl5hSn8kJpbgZlN9cQZw_d1IL8-NTigsTk1LzUkvjQYCMDEDQwMDdxNDQmThUA6egliQ</recordid><startdate>20200625</startdate><enddate>20200625</enddate><creator>Meano, Cesare Maria</creator><scope>EVB</scope></search><sort><creationdate>20200625</creationdate><title>MULTIPLE STAGE TURBO-CHARGED ENGINE SYSTEM</title><author>Meano, Cesare Maria</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_US2020200074A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng</language><creationdate>2020</creationdate><topic>AIR INTAKES FOR JET-PROPULSION PLANTS</topic><topic>BLASTING</topic><topic>COMBUSTION ENGINES</topic><topic>COMBUSTION ENGINES IN GENERAL</topic><topic>CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS</topic><topic>GAS-TURBINE PLANTS</topic><topic>HEATING</topic><topic>HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS</topic><topic>INTERNAL-COMBUSTION PISTON ENGINES</topic><topic>LIGHTING</topic><topic>MECHANICAL ENGINEERING</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>Meano, Cesare Maria</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Meano, Cesare Maria</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>MULTIPLE STAGE TURBO-CHARGED ENGINE SYSTEM</title><date>2020-06-25</date><risdate>2020</risdate><abstract>An engine system includes an internal combustion engine and a first and second air charge system. The internal combustion engine comprises an air intake system and an exhaust manifold. The first air charge system comprising a first compressor, a turbine, and a generator/motor module. The first compressor has a first air inlet, a first air outlet, and a first input shaft. The first outlet is connected to the air intake system, the turbine has an exhaust gas inlet, and the exhaust gas inlet is connected to an outlet of the exhaust manifold. The second air charge system includes a second compressor and an electric motor. The second compressor has a second air inlet, a second air outlet, and a second input shaft. The electric motor has an outlet shaft directly coupled for common rotation with the first input shaft of the second compressor.</abstract><oa>free_for_read</oa></addata></record> |
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| language | eng |
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| subjects | AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING COMBUSTION ENGINES COMBUSTION ENGINES IN GENERAL CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS GAS-TURBINE PLANTS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS INTERNAL-COMBUSTION PISTON ENGINES LIGHTING MECHANICAL ENGINEERING WEAPONS |
| title | MULTIPLE STAGE TURBO-CHARGED ENGINE SYSTEM |
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