AIRCRAFT COMPRISING A REVERSIBLE ROTARY ELECTRICAL MACHINE
The invention concerns an aircraft comprising a reversible rotary electrical machine 30), a wheel (35) for imparting movement to a stream of air, linked to said machine (30), a first ventilation duct (10, 15) configured to supply said wheel (35) with air, an electricity distribution network (70), a...
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| creator | MAVIER, JEROME LANDO, JEAN-LOUIS FOCH, ETIENNE ROBOAM, XAVIER BARKOWSKY, JAN |
| description | The invention concerns an aircraft comprising a reversible rotary electrical machine 30), a wheel (35) for imparting movement to a stream of air, linked to said machine (30), a first ventilation duct (10, 15) configured to supply said wheel (35) with air, an electricity distribution network (70), a reversible power converter (40) connected to said machine (30) and to said network (70), and a control circuit (50) configured to control said converter (40) for, in a motor operating mode of said machine (30), taking a supply current from said network (70) to supply said machine (30) and drive said wheel (35), and, in an alternator operating mode of said machine (30), in which a stream of air flows in said first ventilation duct (15) and imparts movement to said wheel (35), to provide supply power to said network (70) which is generated by said machine (30) driven by said wheel (35).
Linvention porte sur un aéronef comprenant une machine électrique rotative réversible (30), une roue (35) visant à imprimer un mouvement à un flux dair, raccordée à ladite machine (30), un premier conduit de ventilation (10, 15) configuré pour fournir de lair à ladite roue (35), un réseau de distribution délectricité (70), un convertisseur de puissance réversible (40) relié à ladite machine (30) et audit réseau (70), et un circuit de commande (50) configuré en vue de commander ledit convertisseur (40) pour, dans un mode de fonctionnement de moteur de ladite machine (30), prélever un courant dalimentation dudit réseau (70) afin dalimenter ladite machine (30) et entraîner ladite roue (35) et, à un mode de fonctionnement dalternateur de ladite machine (30), dans lequel un flux dair sécoule dans ledit premier conduit de ventilation (15) et imprime un mouvement à ladite roue (35), pour fournir un courant dalimentation audit réseau (70) qui est généré par ladite machine (30) entraînée par ladite roue (35). |
| format | Patent |
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Linvention porte sur un aéronef comprenant une machine électrique rotative réversible (30), une roue (35) visant à imprimer un mouvement à un flux dair, raccordée à ladite machine (30), un premier conduit de ventilation (10, 15) configuré pour fournir de lair à ladite roue (35), un réseau de distribution délectricité (70), un convertisseur de puissance réversible (40) relié à ladite machine (30) et audit réseau (70), et un circuit de commande (50) configuré en vue de commander ledit convertisseur (40) pour, dans un mode de fonctionnement de moteur de ladite machine (30), prélever un courant dalimentation dudit réseau (70) afin dalimenter ladite machine (30) et entraîner ladite roue (35) et, à un mode de fonctionnement dalternateur de ladite machine (30), dans lequel un flux dair sécoule dans ledit premier conduit de ventilation (15) et imprime un mouvement à ladite roue (35), pour fournir un courant dalimentation audit réseau (70) qui est généré par ladite machine (30) entraînée par ladite roue (35).</description><language>eng ; fre</language><subject>AIRCRAFT ; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT ; AVIATION ; COSMONAUTICS ; EQUIPMENT FOR FITTING IN OR TO AIRCRAFT ; FLYING SUITS ; PARACHUTES ; PERFORMING OPERATIONS ; TRANSPORTING</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=20190115&DB=EPODOC&CC=CA&NR=2758211C$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20190115&DB=EPODOC&CC=CA&NR=2758211C$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>MAVIER, JEROME</creatorcontrib><creatorcontrib>LANDO, JEAN-LOUIS</creatorcontrib><creatorcontrib>FOCH, ETIENNE</creatorcontrib><creatorcontrib>ROBOAM, XAVIER</creatorcontrib><creatorcontrib>BARKOWSKY, JAN</creatorcontrib><title>AIRCRAFT COMPRISING A REVERSIBLE ROTARY ELECTRICAL MACHINE</title><description>The invention concerns an aircraft comprising a reversible rotary electrical machine 30), a wheel (35) for imparting movement to a stream of air, linked to said machine (30), a first ventilation duct (10, 15) configured to supply said wheel (35) with air, an electricity distribution network (70), a reversible power converter (40) connected to said machine (30) and to said network (70), and a control circuit (50) configured to control said converter (40) for, in a motor operating mode of said machine (30), taking a supply current from said network (70) to supply said machine (30) and drive said wheel (35), and, in an alternator operating mode of said machine (30), in which a stream of air flows in said first ventilation duct (15) and imparts movement to said wheel (35), to provide supply power to said network (70) which is generated by said machine (30) driven by said wheel (35).
Linvention porte sur un aéronef comprenant une machine électrique rotative réversible (30), une roue (35) visant à imprimer un mouvement à un flux dair, raccordée à ladite machine (30), un premier conduit de ventilation (10, 15) configuré pour fournir de lair à ladite roue (35), un réseau de distribution délectricité (70), un convertisseur de puissance réversible (40) relié à ladite machine (30) et audit réseau (70), et un circuit de commande (50) configuré en vue de commander ledit convertisseur (40) pour, dans un mode de fonctionnement de moteur de ladite machine (30), prélever un courant dalimentation dudit réseau (70) afin dalimenter ladite machine (30) et entraîner ladite roue (35) et, à un mode de fonctionnement dalternateur de ladite machine (30), dans lequel un flux dair sécoule dans ledit premier conduit de ventilation (15) et imprime un mouvement à ladite roue (35), pour fournir un courant dalimentation audit réseau (70) qui est généré par ladite machine (30) entraînée par ladite roue (35).</description><subject>AIRCRAFT</subject><subject>ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT</subject><subject>AVIATION</subject><subject>COSMONAUTICS</subject><subject>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</subject><subject>FLYING SUITS</subject><subject>PARACHUTES</subject><subject>PERFORMING OPERATIONS</subject><subject>TRANSPORTING</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2019</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZLBy9AxyDnJ0C1Fw9vcNCPIM9vRzV3BUCHINcw0K9nTycVUI8g9xDIpUcPVxdQ4J8nR29FHwdXT28PRz5WFgTUvMKU7lhdLcDPJuriHOHrqpBfnxqcUFicmpeakl8c6ORuamFkaGhs7GhFUAABqjKCQ</recordid><startdate>20190115</startdate><enddate>20190115</enddate><creator>MAVIER, JEROME</creator><creator>LANDO, JEAN-LOUIS</creator><creator>FOCH, ETIENNE</creator><creator>ROBOAM, XAVIER</creator><creator>BARKOWSKY, JAN</creator><scope>EVB</scope></search><sort><creationdate>20190115</creationdate><title>AIRCRAFT COMPRISING A REVERSIBLE ROTARY ELECTRICAL MACHINE</title><author>MAVIER, JEROME ; LANDO, JEAN-LOUIS ; FOCH, ETIENNE ; ROBOAM, XAVIER ; BARKOWSKY, JAN</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_CA2758211C3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre</language><creationdate>2019</creationdate><topic>AIRCRAFT</topic><topic>ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT</topic><topic>AVIATION</topic><topic>COSMONAUTICS</topic><topic>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</topic><topic>FLYING SUITS</topic><topic>PARACHUTES</topic><topic>PERFORMING OPERATIONS</topic><topic>TRANSPORTING</topic><toplevel>online_resources</toplevel><creatorcontrib>MAVIER, JEROME</creatorcontrib><creatorcontrib>LANDO, JEAN-LOUIS</creatorcontrib><creatorcontrib>FOCH, ETIENNE</creatorcontrib><creatorcontrib>ROBOAM, XAVIER</creatorcontrib><creatorcontrib>BARKOWSKY, JAN</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>MAVIER, JEROME</au><au>LANDO, JEAN-LOUIS</au><au>FOCH, ETIENNE</au><au>ROBOAM, XAVIER</au><au>BARKOWSKY, JAN</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>AIRCRAFT COMPRISING A REVERSIBLE ROTARY ELECTRICAL MACHINE</title><date>2019-01-15</date><risdate>2019</risdate><abstract>The invention concerns an aircraft comprising a reversible rotary electrical machine 30), a wheel (35) for imparting movement to a stream of air, linked to said machine (30), a first ventilation duct (10, 15) configured to supply said wheel (35) with air, an electricity distribution network (70), a reversible power converter (40) connected to said machine (30) and to said network (70), and a control circuit (50) configured to control said converter (40) for, in a motor operating mode of said machine (30), taking a supply current from said network (70) to supply said machine (30) and drive said wheel (35), and, in an alternator operating mode of said machine (30), in which a stream of air flows in said first ventilation duct (15) and imparts movement to said wheel (35), to provide supply power to said network (70) which is generated by said machine (30) driven by said wheel (35).
Linvention porte sur un aéronef comprenant une machine électrique rotative réversible (30), une roue (35) visant à imprimer un mouvement à un flux dair, raccordée à ladite machine (30), un premier conduit de ventilation (10, 15) configuré pour fournir de lair à ladite roue (35), un réseau de distribution délectricité (70), un convertisseur de puissance réversible (40) relié à ladite machine (30) et audit réseau (70), et un circuit de commande (50) configuré en vue de commander ledit convertisseur (40) pour, dans un mode de fonctionnement de moteur de ladite machine (30), prélever un courant dalimentation dudit réseau (70) afin dalimenter ladite machine (30) et entraîner ladite roue (35) et, à un mode de fonctionnement dalternateur de ladite machine (30), dans lequel un flux dair sécoule dans ledit premier conduit de ventilation (15) et imprime un mouvement à ladite roue (35), pour fournir un courant dalimentation audit réseau (70) qui est généré par ladite machine (30) entraînée par ladite roue (35).</abstract><oa>free_for_read</oa></addata></record> |
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| subjects | AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS PARACHUTES PERFORMING OPERATIONS TRANSPORTING |
| title | AIRCRAFT COMPRISING A REVERSIBLE ROTARY ELECTRICAL MACHINE |
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