CIRCUIT D'ALIMENTATION EN ENERGIE ELECTRIQUE DANS UN AERONEF POUR DES EQUIPEMENTS ELECTRIQUES COMPRENANT UN CIRCUIT DE DEGIVRAGE
The circuit has a power distribution system (17) for supplying power to electrical equipment i.e. nacelle load (5b), arranged in an engine (23) i.e. gas turbine engine, of an aircraft e.g. airplane, or in a surrounding of the engine. A power generator (27) is integrated to the engine, and is directl...
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| creator | STUTZ ANTOINE JEAN-BAPTISTE BOUDYAF RACHID |
| description | The circuit has a power distribution system (17) for supplying power to electrical equipment i.e. nacelle load (5b), arranged in an engine (23) i.e. gas turbine engine, of an aircraft e.g. airplane, or in a surrounding of the engine. A power generator (27) is integrated to the engine, and is directly connected to another electrical equipment i.e. nacelle anti-icing system (5a), for supplying alternating current (AC) voltage to the anti-icing system. A permanent magnet generator is mechanically coupled with the power generator. |
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A power generator (27) is integrated to the engine, and is directly connected to another electrical equipment i.e. nacelle anti-icing system (5a), for supplying alternating current (AC) voltage to the anti-icing system. A permanent magnet generator is mechanically coupled with the power generator.</description><language>fre</language><subject>AIRCRAFT ; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT ; AVIATION ; CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTINGELECTRIC POWER ; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER ; COSMONAUTICS ; ELECTRICITY ; EQUIPMENT FOR FITTING IN OR TO AIRCRAFT ; FLYING SUITS ; GENERATION ; PARACHUTES ; PERFORMING OPERATIONS ; SYSTEMS FOR STORING ELECTRIC ENERGY ; TRANSPORTING</subject><creationdate>2009</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=20091225&DB=EPODOC&CC=FR&NR=2911848B1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25542,76290</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20091225&DB=EPODOC&CC=FR&NR=2911848B1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>STUTZ ANTOINE JEAN-BAPTISTE</creatorcontrib><creatorcontrib>BOUDYAF RACHID</creatorcontrib><title>CIRCUIT D'ALIMENTATION EN ENERGIE ELECTRIQUE DANS UN AERONEF POUR DES EQUIPEMENTS ELECTRIQUES COMPRENANT UN CIRCUIT DE DEGIVRAGE</title><description>The circuit has a power distribution system (17) for supplying power to electrical equipment i.e. nacelle load (5b), arranged in an engine (23) i.e. gas turbine engine, of an aircraft e.g. airplane, or in a surrounding of the engine. A power generator (27) is integrated to the engine, and is directly connected to another electrical equipment i.e. nacelle anti-icing system (5a), for supplying alternating current (AC) voltage to the anti-icing system. A permanent magnet generator is mechanically coupled with the power generator.</description><subject>AIRCRAFT</subject><subject>ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT</subject><subject>AVIATION</subject><subject>CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTINGELECTRIC POWER</subject><subject>CONVERSION OR DISTRIBUTION OF ELECTRIC POWER</subject><subject>COSMONAUTICS</subject><subject>ELECTRICITY</subject><subject>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</subject><subject>FLYING SUITS</subject><subject>GENERATION</subject><subject>PARACHUTES</subject><subject>PERFORMING OPERATIONS</subject><subject>SYSTEMS FOR STORING ELECTRIC ENERGY</subject><subject>TRANSPORTING</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2009</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNqNjTEKwkAURNNYiHqH31lZRC1iuW4m8UOyG__u2oYgayUaiAfw6BoQsRQGpnlvZpo8NYsO7ClfqoprGK88W0MYAykZhAraCx8DKFfGUTCkINagoMYGoRyOcAzcYNTdD-9I27oRGGX8qH2_3kso-SSqxDyZXLrrEBefniVUwOvDKvb3Ng59d463-GgLWe_SNNtm-3TzB_IC_CI75g</recordid><startdate>20091225</startdate><enddate>20091225</enddate><creator>STUTZ ANTOINE JEAN-BAPTISTE</creator><creator>BOUDYAF RACHID</creator><scope>EVB</scope></search><sort><creationdate>20091225</creationdate><title>CIRCUIT D'ALIMENTATION EN ENERGIE ELECTRIQUE DANS UN AERONEF POUR DES EQUIPEMENTS ELECTRIQUES COMPRENANT UN CIRCUIT DE DEGIVRAGE</title><author>STUTZ ANTOINE JEAN-BAPTISTE ; BOUDYAF RACHID</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_FR2911848B13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>fre</language><creationdate>2009</creationdate><topic>AIRCRAFT</topic><topic>ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT</topic><topic>AVIATION</topic><topic>CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTINGELECTRIC POWER</topic><topic>CONVERSION OR DISTRIBUTION OF ELECTRIC POWER</topic><topic>COSMONAUTICS</topic><topic>ELECTRICITY</topic><topic>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</topic><topic>FLYING SUITS</topic><topic>GENERATION</topic><topic>PARACHUTES</topic><topic>PERFORMING OPERATIONS</topic><topic>SYSTEMS FOR STORING ELECTRIC ENERGY</topic><topic>TRANSPORTING</topic><toplevel>online_resources</toplevel><creatorcontrib>STUTZ ANTOINE JEAN-BAPTISTE</creatorcontrib><creatorcontrib>BOUDYAF RACHID</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>STUTZ ANTOINE JEAN-BAPTISTE</au><au>BOUDYAF RACHID</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>CIRCUIT D'ALIMENTATION EN ENERGIE ELECTRIQUE DANS UN AERONEF POUR DES EQUIPEMENTS ELECTRIQUES COMPRENANT UN CIRCUIT DE DEGIVRAGE</title><date>2009-12-25</date><risdate>2009</risdate><abstract>The circuit has a power distribution system (17) for supplying power to electrical equipment i.e. nacelle load (5b), arranged in an engine (23) i.e. gas turbine engine, of an aircraft e.g. airplane, or in a surrounding of the engine. A power generator (27) is integrated to the engine, and is directly connected to another electrical equipment i.e. nacelle anti-icing system (5a), for supplying alternating current (AC) voltage to the anti-icing system. A permanent magnet generator is mechanically coupled with the power generator.</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 CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTINGELECTRIC POWER CONVERSION OR DISTRIBUTION OF ELECTRIC POWER COSMONAUTICS ELECTRICITY EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS GENERATION PARACHUTES PERFORMING OPERATIONS SYSTEMS FOR STORING ELECTRIC ENERGY TRANSPORTING |
| title | CIRCUIT D'ALIMENTATION EN ENERGIE ELECTRIQUE DANS UN AERONEF POUR DES EQUIPEMENTS ELECTRIQUES COMPRENANT UN CIRCUIT DE DEGIVRAGE |
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