VERTICAL TAKEOFF AND LANDING (VTOL) AIR VEHICLE
A flight control apparatus for fixed-wing aircraft includes a first port wing (115) and first starboard wing (120), a first port swash plate (145) coupled between a first port rotor 155) and first port electric motor (135), the first port electric 5 motor (135) coupled to the first port wing (115),...
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| creator | MUKHERJEE, JASON SIDHARTHADEV KING, JOSEPH FREDERICK TOKUMARU, PHILLIP T TAYLOR, DANA J GANZER, DAVID WAYNE FISHER, CHRISTOPHER EUGENE PARKS, WILLIAM MARTIN HIBBS, BART DEAN |
| description | A flight control apparatus for fixed-wing aircraft includes a first port wing (115) and first starboard wing (120), a first port swash plate (145) coupled between a first port rotor 155) and first port electric motor (135), the first port electric 5 motor (135) coupled to the first port wing (115), and a first starboard swash plate (150) coupled between a first starboard rotor (130) and first starboard electric motor (140), the first starboard electric motor (140) coupled to the first starboard wing (120).
Un appareil de commande de vol destiné à un aéronef à voilure fixe comprend : une première voilure gauche (115) ; une première voilure droite (120) ; un premier plateau oscillant gauche (145) couplé entre un premier rotor gauche (155) et un premier moteur électrique gauche (135), le premier moteur électrique gauche (135) étant couplé à la première voilure gauche (115) ; et un premier plateau oscillant droit (150) couplé entre un premier rotor droit (130) et un premier moteur électrique droit (140), le premier moteur électrique droit (140) étant couplé à la première voilure droite (120). |
| format | Patent |
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Un appareil de commande de vol destiné à un aéronef à voilure fixe comprend : une première voilure gauche (115) ; une première voilure droite (120) ; un premier plateau oscillant gauche (145) couplé entre un premier rotor gauche (155) et un premier moteur électrique gauche (135), le premier moteur électrique gauche (135) étant couplé à la première voilure gauche (115) ; et un premier plateau oscillant droit (150) couplé entre un premier rotor droit (130) et un premier moteur électrique droit (140), le premier moteur électrique droit (140) étant couplé à la première voilure droite (120).</description><language>eng ; fre</language><subject>AEROPLANES ; AIRCRAFT ; AVIATION ; CONTROLLING ; COSMONAUTICS ; HELICOPTERS ; PERFORMING OPERATIONS ; PHYSICS ; REGULATING ; SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES ; TRANSPORTING</subject><creationdate>2021</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=20210608&DB=EPODOC&CC=CA&NR=2947672C$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20210608&DB=EPODOC&CC=CA&NR=2947672C$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>MUKHERJEE, JASON SIDHARTHADEV</creatorcontrib><creatorcontrib>KING, JOSEPH FREDERICK</creatorcontrib><creatorcontrib>TOKUMARU, PHILLIP T</creatorcontrib><creatorcontrib>TAYLOR, DANA J</creatorcontrib><creatorcontrib>GANZER, DAVID WAYNE</creatorcontrib><creatorcontrib>FISHER, CHRISTOPHER EUGENE</creatorcontrib><creatorcontrib>PARKS, WILLIAM MARTIN</creatorcontrib><creatorcontrib>HIBBS, BART DEAN</creatorcontrib><title>VERTICAL TAKEOFF AND LANDING (VTOL) AIR VEHICLE</title><description>A flight control apparatus for fixed-wing aircraft includes a first port wing (115) and first starboard wing (120), a first port swash plate (145) coupled between a first port rotor 155) and first port electric motor (135), the first port electric 5 motor (135) coupled to the first port wing (115), and a first starboard swash plate (150) coupled between a first starboard rotor (130) and first starboard electric motor (140), the first starboard electric motor (140) coupled to the first starboard wing (120).
Un appareil de commande de vol destiné à un aéronef à voilure fixe comprend : une première voilure gauche (115) ; une première voilure droite (120) ; un premier plateau oscillant gauche (145) couplé entre un premier rotor gauche (155) et un premier moteur électrique gauche (135), le premier moteur électrique gauche (135) étant couplé à la première voilure gauche (115) ; et un premier plateau oscillant droit (150) couplé entre un premier rotor droit (130) et un premier moteur électrique droit (140), le premier moteur électrique droit (140) étant couplé à la première voilure droite (120).</description><subject>AEROPLANES</subject><subject>AIRCRAFT</subject><subject>AVIATION</subject><subject>CONTROLLING</subject><subject>COSMONAUTICS</subject><subject>HELICOPTERS</subject><subject>PERFORMING OPERATIONS</subject><subject>PHYSICS</subject><subject>REGULATING</subject><subject>SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES</subject><subject>TRANSPORTING</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2021</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZNAPcw0K8XR29FEIcfR29XdzU3D0c1HwARKefu4KGmEh_j6aCo6eQQphrh6ezj6uPAysaYk5xam8UJqbQd7NNcTZQze1ID8-tbggMTk1L7Uk3tnRyNLE3MzcyNmYsAoAPtckog</recordid><startdate>20210608</startdate><enddate>20210608</enddate><creator>MUKHERJEE, JASON SIDHARTHADEV</creator><creator>KING, JOSEPH FREDERICK</creator><creator>TOKUMARU, PHILLIP T</creator><creator>TAYLOR, DANA J</creator><creator>GANZER, DAVID WAYNE</creator><creator>FISHER, CHRISTOPHER EUGENE</creator><creator>PARKS, WILLIAM MARTIN</creator><creator>HIBBS, BART DEAN</creator><scope>EVB</scope></search><sort><creationdate>20210608</creationdate><title>VERTICAL TAKEOFF AND LANDING (VTOL) AIR VEHICLE</title><author>MUKHERJEE, JASON SIDHARTHADEV ; KING, JOSEPH FREDERICK ; TOKUMARU, PHILLIP T ; TAYLOR, DANA J ; GANZER, DAVID WAYNE ; FISHER, CHRISTOPHER EUGENE ; PARKS, WILLIAM MARTIN ; HIBBS, BART DEAN</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_CA2947672C3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre</language><creationdate>2021</creationdate><topic>AEROPLANES</topic><topic>AIRCRAFT</topic><topic>AVIATION</topic><topic>CONTROLLING</topic><topic>COSMONAUTICS</topic><topic>HELICOPTERS</topic><topic>PERFORMING OPERATIONS</topic><topic>PHYSICS</topic><topic>REGULATING</topic><topic>SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES</topic><topic>TRANSPORTING</topic><toplevel>online_resources</toplevel><creatorcontrib>MUKHERJEE, JASON SIDHARTHADEV</creatorcontrib><creatorcontrib>KING, JOSEPH FREDERICK</creatorcontrib><creatorcontrib>TOKUMARU, PHILLIP T</creatorcontrib><creatorcontrib>TAYLOR, DANA J</creatorcontrib><creatorcontrib>GANZER, DAVID WAYNE</creatorcontrib><creatorcontrib>FISHER, CHRISTOPHER EUGENE</creatorcontrib><creatorcontrib>PARKS, WILLIAM MARTIN</creatorcontrib><creatorcontrib>HIBBS, BART DEAN</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>MUKHERJEE, JASON SIDHARTHADEV</au><au>KING, JOSEPH FREDERICK</au><au>TOKUMARU, PHILLIP T</au><au>TAYLOR, DANA J</au><au>GANZER, DAVID WAYNE</au><au>FISHER, CHRISTOPHER EUGENE</au><au>PARKS, WILLIAM MARTIN</au><au>HIBBS, BART DEAN</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>VERTICAL TAKEOFF AND LANDING (VTOL) AIR VEHICLE</title><date>2021-06-08</date><risdate>2021</risdate><abstract>A flight control apparatus for fixed-wing aircraft includes a first port wing (115) and first starboard wing (120), a first port swash plate (145) coupled between a first port rotor 155) and first port electric motor (135), the first port electric 5 motor (135) coupled to the first port wing (115), and a first starboard swash plate (150) coupled between a first starboard rotor (130) and first starboard electric motor (140), the first starboard electric motor (140) coupled to the first starboard wing (120).
Un appareil de commande de vol destiné à un aéronef à voilure fixe comprend : une première voilure gauche (115) ; une première voilure droite (120) ; un premier plateau oscillant gauche (145) couplé entre un premier rotor gauche (155) et un premier moteur électrique gauche (135), le premier moteur électrique gauche (135) étant couplé à la première voilure gauche (115) ; et un premier plateau oscillant droit (150) couplé entre un premier rotor droit (130) et un premier moteur électrique droit (140), le premier moteur électrique droit (140) étant couplé à la première voilure droite (120).</abstract><oa>free_for_read</oa></addata></record> |
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| subjects | AEROPLANES AIRCRAFT AVIATION CONTROLLING COSMONAUTICS HELICOPTERS PERFORMING OPERATIONS PHYSICS REGULATING SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES TRANSPORTING |
| title | VERTICAL TAKEOFF AND LANDING (VTOL) AIR VEHICLE |
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