SYSTEMS AND METHODS FOR VERTICAL TAKEOFF AND LANDING VEHICLE
A vertical takeoff and landing (VTOL) vehicle includes a first housing comprising a first compartment; a drive system comprising a rotor and a stator, the drive system arranged around the first housing; a second housing comprising a second compartment separated from the first compartment, the second...
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| creator | LEMBKE, Torbjörn RANDALL, Ian Morris RANDALL, Roderick K CONCIA, Bernardo Martin O'REGAN, Peter ELVANDER, Josh |
| description | A vertical takeoff and landing (VTOL) vehicle includes a first housing comprising a first compartment; a drive system comprising a rotor and a stator, the drive system arranged around the first housing; a second housing comprising a second compartment separated from the first compartment, the second compartment comprising one or more control systems for the controlling the drive system, the second housing spaced from the first housing and the drive system to form a gap between second housing and the drive system; and a beam extending between the first housing and the second housing across the gap.
Un véhicule à décollage et atterrissage verticaux (VTOL) comprend un premier logement comprenant un premier compartiment ; un système d'entraînement comprenant un rotor et un stator, le système d'entraînement étant agencé autour du premier logement ; un second logement comprenant un second compartiment séparé du premier compartiment, le second compartiment comprenant un ou plusieurs systèmes de commande à des fins de commande du système d'entraînement, le second logement étant espacé du premier logement et du système d'entraînement pour former un espace entre le second logement et le système d'entraînement ; et un rayon s'étendant entre le premier logement et le second logement à travers l'espace. |
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Un véhicule à décollage et atterrissage verticaux (VTOL) comprend un premier logement comprenant un premier compartiment ; un système d'entraînement comprenant un rotor et un stator, le système d'entraînement étant agencé autour du premier logement ; un second logement comprenant un second compartiment séparé du premier compartiment, le second compartiment comprenant un ou plusieurs systèmes de commande à des fins de commande du système d'entraînement, le second logement étant espacé du premier logement et du système d'entraînement pour former un espace entre le second logement et le système d'entraînement ; et un rayon s'étendant entre le premier logement et le second logement à travers l'espace.</description><language>eng ; fre</language><subject>AEROPLANES ; AIRCRAFT ; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT ; AVIATION ; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER ; COSMONAUTICS ; DYNAMO-ELECTRIC MACHINES ; ELECTRICITY ; EQUIPMENT FOR FITTING IN OR TO AIRCRAFT ; FLYING SUITS ; GENERATION ; HELICOPTERS ; PARACHUTES ; PERFORMING OPERATIONS ; TRANSPORTING</subject><creationdate>2024</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=20241219&DB=EPODOC&CC=WO&NR=2024259331A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25542,76290</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20241219&DB=EPODOC&CC=WO&NR=2024259331A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>LEMBKE, Torbjörn</creatorcontrib><creatorcontrib>RANDALL, Ian Morris</creatorcontrib><creatorcontrib>RANDALL, Roderick K</creatorcontrib><creatorcontrib>CONCIA, Bernardo Martin</creatorcontrib><creatorcontrib>O'REGAN, Peter</creatorcontrib><creatorcontrib>ELVANDER, Josh</creatorcontrib><title>SYSTEMS AND METHODS FOR VERTICAL TAKEOFF AND LANDING VEHICLE</title><description>A vertical takeoff and landing (VTOL) vehicle includes a first housing comprising a first compartment; a drive system comprising a rotor and a stator, the drive system arranged around the first housing; a second housing comprising a second compartment separated from the first compartment, the second compartment comprising one or more control systems for the controlling the drive system, the second housing spaced from the first housing and the drive system to form a gap between second housing and the drive system; and a beam extending between the first housing and the second housing across the gap.
Un véhicule à décollage et atterrissage verticaux (VTOL) comprend un premier logement comprenant un premier compartiment ; un système d'entraînement comprenant un rotor et un stator, le système d'entraînement étant agencé autour du premier logement ; un second logement comprenant un second compartiment séparé du premier compartiment, le second compartiment comprenant un ou plusieurs systèmes de commande à des fins de commande du système d'entraînement, le second logement étant espacé du premier logement et du système d'entraînement pour former un espace entre le second logement et le système d'entraînement ; et un rayon s'étendant entre le premier logement et le second logement à travers l'espace.</description><subject>AEROPLANES</subject><subject>AIRCRAFT</subject><subject>ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT</subject><subject>AVIATION</subject><subject>CONVERSION OR DISTRIBUTION OF ELECTRIC POWER</subject><subject>COSMONAUTICS</subject><subject>DYNAMO-ELECTRIC MACHINES</subject><subject>ELECTRICITY</subject><subject>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</subject><subject>FLYING SUITS</subject><subject>GENERATION</subject><subject>HELICOPTERS</subject><subject>PARACHUTES</subject><subject>PERFORMING OPERATIONS</subject><subject>TRANSPORTING</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2024</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZLAJjgwOcfUNVnD0c1HwdQ3x8HcJVnDzD1IIcw0K8XR29FEIcfR29XdzAyvwARKefu5ASQ9PZx9XHgbWtMSc4lReKM3NoOzmGuLsoZtakB-fWlyQmJyal1oSH-5vZGBkYmRqaWxs6GhoTJwqAJdbKkE</recordid><startdate>20241219</startdate><enddate>20241219</enddate><creator>LEMBKE, Torbjörn</creator><creator>RANDALL, Ian Morris</creator><creator>RANDALL, Roderick K</creator><creator>CONCIA, Bernardo Martin</creator><creator>O'REGAN, Peter</creator><creator>ELVANDER, Josh</creator><scope>EVB</scope></search><sort><creationdate>20241219</creationdate><title>SYSTEMS AND METHODS FOR VERTICAL TAKEOFF AND LANDING VEHICLE</title><author>LEMBKE, Torbjörn ; RANDALL, Ian Morris ; RANDALL, Roderick K ; CONCIA, Bernardo Martin ; O'REGAN, Peter ; ELVANDER, Josh</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_WO2024259331A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre</language><creationdate>2024</creationdate><topic>AEROPLANES</topic><topic>AIRCRAFT</topic><topic>ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT</topic><topic>AVIATION</topic><topic>CONVERSION OR DISTRIBUTION OF ELECTRIC POWER</topic><topic>COSMONAUTICS</topic><topic>DYNAMO-ELECTRIC MACHINES</topic><topic>ELECTRICITY</topic><topic>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</topic><topic>FLYING SUITS</topic><topic>GENERATION</topic><topic>HELICOPTERS</topic><topic>PARACHUTES</topic><topic>PERFORMING OPERATIONS</topic><topic>TRANSPORTING</topic><toplevel>online_resources</toplevel><creatorcontrib>LEMBKE, Torbjörn</creatorcontrib><creatorcontrib>RANDALL, Ian Morris</creatorcontrib><creatorcontrib>RANDALL, Roderick K</creatorcontrib><creatorcontrib>CONCIA, Bernardo Martin</creatorcontrib><creatorcontrib>O'REGAN, Peter</creatorcontrib><creatorcontrib>ELVANDER, Josh</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>LEMBKE, Torbjörn</au><au>RANDALL, Ian Morris</au><au>RANDALL, Roderick K</au><au>CONCIA, Bernardo Martin</au><au>O'REGAN, Peter</au><au>ELVANDER, Josh</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>SYSTEMS AND METHODS FOR VERTICAL TAKEOFF AND LANDING VEHICLE</title><date>2024-12-19</date><risdate>2024</risdate><abstract>A vertical takeoff and landing (VTOL) vehicle includes a first housing comprising a first compartment; a drive system comprising a rotor and a stator, the drive system arranged around the first housing; a second housing comprising a second compartment separated from the first compartment, the second compartment comprising one or more control systems for the controlling the drive system, the second housing spaced from the first housing and the drive system to form a gap between second housing and the drive system; and a beam extending between the first housing and the second housing across the gap.
Un véhicule à décollage et atterrissage verticaux (VTOL) comprend un premier logement comprenant un premier compartiment ; un système d'entraînement comprenant un rotor et un stator, le système d'entraînement étant agencé autour du premier logement ; un second logement comprenant un second compartiment séparé du premier compartiment, le second compartiment comprenant un ou plusieurs systèmes de commande à des fins de commande du système d'entraînement, le second logement étant espacé du premier logement et du système d'entraînement pour former un espace entre le second logement et le système d'entraînement ; et un rayon s'étendant entre le premier logement et le second logement à travers l'espace.</abstract><oa>free_for_read</oa></addata></record> |
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| subjects | AEROPLANES AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION CONVERSION OR DISTRIBUTION OF ELECTRIC POWER COSMONAUTICS DYNAMO-ELECTRIC MACHINES ELECTRICITY EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS GENERATION HELICOPTERS PARACHUTES PERFORMING OPERATIONS TRANSPORTING |
| title | SYSTEMS AND METHODS FOR VERTICAL TAKEOFF AND LANDING VEHICLE |
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