AIRCRAFT POWERED BY HYBRID POWER
An aircraft with a hybrid power supply, the aircraft comprising: an external structure (12 to 20); electrical equipment (34); internal combustion propulsion means (40); and means for feeding energy to the propulsion means; the aircraft being characterized in that it further comprises: a plurality of...
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creator | ROUSSELIN, STEPHANE FOUCAULT, ALAIN JUCHAULD, ETIENNE PIERROT, ARNAUD |
description | An aircraft with a hybrid power supply, the aircraft comprising: an external structure (12 to 20); electrical equipment (34); internal combustion propulsion means (40); and means for feeding energy to the propulsion means; the aircraft being characterized in that it further comprises: a plurality of converters for directly converting light energy into electrical energy (24), which converters are disposed on at least a fraction of the outside surface of the external structure; means (32) for comparing the electrical energy produced by said converters with the instantaneous consumption of said electrical equipment (34); means (36) for recovering the excess electrical energy, if any; and means (38) for delivering to said propulsion means (40) additional energy taken from said excess electrical energy, if any. |
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and means for feeding energy to the propulsion means; the aircraft being characterized in that it further comprises: a plurality of converters for directly converting light energy into electrical energy (24), which converters are disposed on at least a fraction of the outside surface of the external structure; means (32) for comparing the electrical energy produced by said converters with the instantaneous consumption of said electrical equipment (34); means (36) for recovering the excess electrical energy, if any; and means (38) for delivering to said propulsion means (40) additional energy taken from said excess electrical energy, if any.</description><language>eng ; fre ; ger</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>2012</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=20120201&DB=EPODOC&CC=EP&NR=2296970B1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20120201&DB=EPODOC&CC=EP&NR=2296970B1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>ROUSSELIN, STEPHANE</creatorcontrib><creatorcontrib>FOUCAULT, ALAIN</creatorcontrib><creatorcontrib>JUCHAULD, ETIENNE</creatorcontrib><creatorcontrib>PIERROT, ARNAUD</creatorcontrib><title>AIRCRAFT POWERED BY HYBRID POWER</title><description>An aircraft with a hybrid power supply, the aircraft comprising: an external structure (12 to 20); 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FOUCAULT, ALAIN ; JUCHAULD, ETIENNE ; PIERROT, ARNAUD</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_EP2296970B13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre ; ger</language><creationdate>2012</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>ROUSSELIN, STEPHANE</creatorcontrib><creatorcontrib>FOUCAULT, ALAIN</creatorcontrib><creatorcontrib>JUCHAULD, ETIENNE</creatorcontrib><creatorcontrib>PIERROT, ARNAUD</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>ROUSSELIN, STEPHANE</au><au>FOUCAULT, ALAIN</au><au>JUCHAULD, ETIENNE</au><au>PIERROT, ARNAUD</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>AIRCRAFT POWERED BY HYBRID POWER</title><date>2012-02-01</date><risdate>2012</risdate><abstract>An aircraft with a hybrid power supply, the aircraft comprising: an external structure (12 to 20); electrical equipment (34); internal combustion propulsion means (40); and means for feeding energy to the propulsion means; the aircraft being characterized in that it further comprises: a plurality of converters for directly converting light energy into electrical energy (24), which converters are disposed on at least a fraction of the outside surface of the external structure; means (32) for comparing the electrical energy produced by said converters with the instantaneous consumption of said electrical equipment (34); means (36) for recovering the excess electrical energy, if any; and means (38) for delivering to said propulsion means (40) additional energy taken from said excess electrical energy, if any.</abstract><oa>free_for_read</oa></addata></record> |
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language | eng ; fre ; ger |
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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 POWERED BY HYBRID POWER |
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