CREWLESS AIRCRAFT, SYSTEM, AND CONTROL METHOD
An unmanned aerial vehicle (10m) includes: a vehicle main body (1912) having a first length (N1) in a first direction longer than a second length (N2) in a second direction orthogonal to the first direction; propellers (22) that rotate in a virtual plane parallel to the first and second directions;...
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| creator | KATO, Tatsuya TAKAHAMA, Takuya AOYAMA, Hideki AMAGAI, Ryosuke SASAKI, Gaku OSHIMA, Mitsuaki HAYASHI, Nobuaki TANIUCHI, Naoyuki MURAMATSU, Fumio KITAZAWA, Kazuma |
| description | An unmanned aerial vehicle (10m) includes: a vehicle main body (1912) having a first length (N1) in a first direction longer than a second length (N2) in a second direction orthogonal to the first direction; propellers (22) that rotate in a virtual plane parallel to the first and second directions; first propeller actuation motors (23) that are provided on the vehicle main body (1912) and respectively rotate the propellers (22); at least one connector (1720) that is hangable from at least one rail (7) spaced apart from the ground surface; at least one side propeller (22a1) that provides propulsion force for propelling the vehicle main body (1912) in the first direction; at least one third propeller actuation motor (22a3) that is provided on the vehicle main body (1912) and rotates the at least one side propeller (22a1); and a control processor (11) that controls the first propeller actuation motors (23) and the at least one third propeller actuation motor (22a3). |
| format | Patent |
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fre ; ger</language><subject>AEROPLANES ; AIRCRAFT ; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT ; AVIATION ; COSMONAUTICS ; CRANES ; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING ORREPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR ; EQUIPMENT FOR FITTING IN OR TO AIRCRAFT ; EQUIPMENT THEREFOR NOT OTHERWISE PROVIDED FOR ; FLYING SUITS ; GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLYADAPTED FOR USE IN CONNECTION WITH AIRCRAFT ; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFTCOMPONENTS, NOT OTHERWISE PROVIDED FOR ; HAULING ; HELICOPTERS ; HOISTING ; HOISTING, LIFTING, HAULING OR PUSHING, NOT OTHERWISE PROVIDEDFOR, e.g. DEVICES WHICH APPLY A LIFTING OR PUSHING FORCEDIRECTLY TO THE SURFACE OF A LOAD ; LIFTING ; LOAD-ENGAGING ELEMENTS OR DEVICES FOR CRANES, CAPSTANS,WINCHES, OR TACKLES ; PARACHUTES ; PERFORMING OPERATIONS ; RAILWAY SYSTEMS ; RAILWAYS ; TRANSPORTING</subject><creationdate>2023</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=20230719&DB=EPODOC&CC=EP&NR=4101756A4$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25542,76290</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20230719&DB=EPODOC&CC=EP&NR=4101756A4$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>KATO, Tatsuya</creatorcontrib><creatorcontrib>TAKAHAMA, Takuya</creatorcontrib><creatorcontrib>AOYAMA, Hideki</creatorcontrib><creatorcontrib>AMAGAI, Ryosuke</creatorcontrib><creatorcontrib>SASAKI, Gaku</creatorcontrib><creatorcontrib>OSHIMA, Mitsuaki</creatorcontrib><creatorcontrib>HAYASHI, Nobuaki</creatorcontrib><creatorcontrib>TANIUCHI, Naoyuki</creatorcontrib><creatorcontrib>MURAMATSU, Fumio</creatorcontrib><creatorcontrib>KITAZAWA, Kazuma</creatorcontrib><title>CREWLESS AIRCRAFT, SYSTEM, AND CONTROL METHOD</title><description>An unmanned aerial vehicle (10m) includes: a vehicle main body (1912) having a first length (N1) in a first direction longer than a second length (N2) in a second direction orthogonal to the first direction; propellers (22) that rotate in a virtual plane parallel to the first and second directions; first propeller actuation motors (23) that are provided on the vehicle main body (1912) and respectively rotate the propellers (22); at least one connector (1720) that is hangable from at least one rail (7) spaced apart from the ground surface; at least one side propeller (22a1) that provides propulsion force for propelling the vehicle main body (1912) in the first direction; at least one third propeller actuation motor (22a3) that is provided on the vehicle main body (1912) and rotates the at least one side propeller (22a1); and a control processor (11) that controls the first propeller actuation motors (23) and the at least one third propeller actuation motor (22a3).</description><subject>AEROPLANES</subject><subject>AIRCRAFT</subject><subject>ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT</subject><subject>AVIATION</subject><subject>COSMONAUTICS</subject><subject>CRANES</subject><subject>DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING ORREPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR</subject><subject>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</subject><subject>EQUIPMENT THEREFOR NOT OTHERWISE PROVIDED FOR</subject><subject>FLYING SUITS</subject><subject>GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLYADAPTED FOR USE IN CONNECTION WITH AIRCRAFT</subject><subject>HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFTCOMPONENTS, NOT OTHERWISE PROVIDED FOR</subject><subject>HAULING</subject><subject>HELICOPTERS</subject><subject>HOISTING</subject><subject>HOISTING, LIFTING, HAULING OR PUSHING, NOT OTHERWISE PROVIDEDFOR, e.g. DEVICES WHICH APPLY A LIFTING OR PUSHING FORCEDIRECTLY TO THE SURFACE OF A LOAD</subject><subject>LIFTING</subject><subject>LOAD-ENGAGING ELEMENTS OR DEVICES FOR CRANES, CAPSTANS,WINCHES, OR TACKLES</subject><subject>PARACHUTES</subject><subject>PERFORMING OPERATIONS</subject><subject>RAILWAY SYSTEMS</subject><subject>RAILWAYS</subject><subject>TRANSPORTING</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2023</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZNB1DnIN93ENDlZw9AxyDnJ0C9FRCI4MDnH11VFw9HNRcPb3Cwny91HwdQ3x8HfhYWBNS8wpTuWF0twMCm6uIc4euqkF-fGpxQWJyal5qSXxrgEmhgaG5qZmjibGRCgBAG0jJPg</recordid><startdate>20230719</startdate><enddate>20230719</enddate><creator>KATO, Tatsuya</creator><creator>TAKAHAMA, Takuya</creator><creator>AOYAMA, Hideki</creator><creator>AMAGAI, Ryosuke</creator><creator>SASAKI, Gaku</creator><creator>OSHIMA, Mitsuaki</creator><creator>HAYASHI, Nobuaki</creator><creator>TANIUCHI, Naoyuki</creator><creator>MURAMATSU, Fumio</creator><creator>KITAZAWA, Kazuma</creator><scope>EVB</scope></search><sort><creationdate>20230719</creationdate><title>CREWLESS AIRCRAFT, SYSTEM, AND CONTROL METHOD</title><author>KATO, Tatsuya ; TAKAHAMA, Takuya ; AOYAMA, Hideki ; AMAGAI, Ryosuke ; SASAKI, Gaku ; OSHIMA, Mitsuaki ; HAYASHI, Nobuaki ; TANIUCHI, Naoyuki ; MURAMATSU, Fumio ; KITAZAWA, Kazuma</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_EP4101756A43</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre ; ger</language><creationdate>2023</creationdate><topic>AEROPLANES</topic><topic>AIRCRAFT</topic><topic>ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT</topic><topic>AVIATION</topic><topic>COSMONAUTICS</topic><topic>CRANES</topic><topic>DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING ORREPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR</topic><topic>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</topic><topic>EQUIPMENT THEREFOR NOT OTHERWISE PROVIDED FOR</topic><topic>FLYING SUITS</topic><topic>GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLYADAPTED FOR USE IN CONNECTION WITH AIRCRAFT</topic><topic>HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFTCOMPONENTS, NOT OTHERWISE PROVIDED FOR</topic><topic>HAULING</topic><topic>HELICOPTERS</topic><topic>HOISTING</topic><topic>HOISTING, LIFTING, HAULING OR PUSHING, NOT OTHERWISE PROVIDEDFOR, e.g. DEVICES WHICH APPLY A LIFTING OR PUSHING FORCEDIRECTLY TO THE SURFACE OF A LOAD</topic><topic>LIFTING</topic><topic>LOAD-ENGAGING ELEMENTS OR DEVICES FOR CRANES, CAPSTANS,WINCHES, OR TACKLES</topic><topic>PARACHUTES</topic><topic>PERFORMING OPERATIONS</topic><topic>RAILWAY SYSTEMS</topic><topic>RAILWAYS</topic><topic>TRANSPORTING</topic><toplevel>online_resources</toplevel><creatorcontrib>KATO, Tatsuya</creatorcontrib><creatorcontrib>TAKAHAMA, Takuya</creatorcontrib><creatorcontrib>AOYAMA, Hideki</creatorcontrib><creatorcontrib>AMAGAI, Ryosuke</creatorcontrib><creatorcontrib>SASAKI, Gaku</creatorcontrib><creatorcontrib>OSHIMA, Mitsuaki</creatorcontrib><creatorcontrib>HAYASHI, Nobuaki</creatorcontrib><creatorcontrib>TANIUCHI, Naoyuki</creatorcontrib><creatorcontrib>MURAMATSU, Fumio</creatorcontrib><creatorcontrib>KITAZAWA, Kazuma</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>KATO, Tatsuya</au><au>TAKAHAMA, Takuya</au><au>AOYAMA, Hideki</au><au>AMAGAI, Ryosuke</au><au>SASAKI, Gaku</au><au>OSHIMA, Mitsuaki</au><au>HAYASHI, Nobuaki</au><au>TANIUCHI, Naoyuki</au><au>MURAMATSU, Fumio</au><au>KITAZAWA, Kazuma</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>CREWLESS AIRCRAFT, SYSTEM, AND CONTROL METHOD</title><date>2023-07-19</date><risdate>2023</risdate><abstract>An unmanned aerial vehicle (10m) includes: a vehicle main body (1912) having a first length (N1) in a first direction longer than a second length (N2) in a second direction orthogonal to the first direction; propellers (22) that rotate in a virtual plane parallel to the first and second directions; first propeller actuation motors (23) that are provided on the vehicle main body (1912) and respectively rotate the propellers (22); at least one connector (1720) that is hangable from at least one rail (7) spaced apart from the ground surface; at least one side propeller (22a1) that provides propulsion force for propelling the vehicle main body (1912) in the first direction; at least one third propeller actuation motor (22a3) that is provided on the vehicle main body (1912) and rotates the at least one side propeller (22a1); and a control processor (11) that controls the first propeller actuation motors (23) and the at least one third propeller actuation motor (22a3).</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 COSMONAUTICS CRANES DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING ORREPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR EQUIPMENT FOR FITTING IN OR TO AIRCRAFT EQUIPMENT THEREFOR NOT OTHERWISE PROVIDED FOR FLYING SUITS GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLYADAPTED FOR USE IN CONNECTION WITH AIRCRAFT HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFTCOMPONENTS, NOT OTHERWISE PROVIDED FOR HAULING HELICOPTERS HOISTING HOISTING, LIFTING, HAULING OR PUSHING, NOT OTHERWISE PROVIDEDFOR, e.g. DEVICES WHICH APPLY A LIFTING OR PUSHING FORCEDIRECTLY TO THE SURFACE OF A LOAD LIFTING LOAD-ENGAGING ELEMENTS OR DEVICES FOR CRANES, CAPSTANS,WINCHES, OR TACKLES PARACHUTES PERFORMING OPERATIONS RAILWAY SYSTEMS RAILWAYS TRANSPORTING |
| title | CREWLESS AIRCRAFT, SYSTEM, AND CONTROL METHOD |
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