Novel-layout vertical take-off and landing fixed-wing unmanned aerial vehicle
The invention discloses a novel layout vertical take-off and landing fixed-wing unmanned aerial vehicle. The unmanned aerial vehicle comprises a fuselage main body, wings, wingtip winglets, aileron systems, tilting power systems, an electronic cabin, a cabin door opening and closing structure, a duc...
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creator | WANG MINGYUAN ZHANG LONG SHAN ZEZHONG GUO QIANG TANG ZHENGUO LIU CHENGWEI LU XIANG WANG CAIJU WU HONGXIA XIAO HAIJIAN HAO QINGYU |
description | The invention discloses a novel layout vertical take-off and landing fixed-wing unmanned aerial vehicle. The unmanned aerial vehicle comprises a fuselage main body, wings, wingtip winglets, aileron systems, tilting power systems, an electronic cabin, a cabin door opening and closing structure, a duct power system, a cargo cabin loading structure and an undercarriage structure. Compared with a traditional vertical take-off and landing unmanned aerial vehicle, the vertical take-off and landing unmanned aerial vehicle has the advantages that the pneumatic effect is better, the hovering effect is better, the flight attitude is more stable, the application range is wider, the endurance time is greatly prolonged, the loading level is improved, and the flight performance and the operation safety are greatly improved; the layout has more advantages when applied to a heavy-load and long-endurance vertical take-off and landing fixed-wing unmanned aerial vehicle, the performance of an electric unmanned aerial vehicle ca |
format | Patent |
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The unmanned aerial vehicle comprises a fuselage main body, wings, wingtip winglets, aileron systems, tilting power systems, an electronic cabin, a cabin door opening and closing structure, a duct power system, a cargo cabin loading structure and an undercarriage structure. Compared with a traditional vertical take-off and landing unmanned aerial vehicle, the vertical take-off and landing unmanned aerial vehicle has the advantages that the pneumatic effect is better, the hovering effect is better, the flight attitude is more stable, the application range is wider, the endurance time is greatly prolonged, the loading level is improved, and the flight performance and the operation safety are greatly improved; the layout has more advantages when applied to a heavy-load and long-endurance vertical take-off and landing fixed-wing unmanned aerial vehicle, the performance of an electric unmanned aerial vehicle ca</description><language>chi ; eng</language><subject>AEROPLANES ; AIRCRAFT ; AVIATION ; COSMONAUTICS ; HELICOPTERS ; PERFORMING OPERATIONS ; TRANSPORTING</subject><creationdate>2022</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=20221014&DB=EPODOC&CC=CN&NR=115180138A$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25543,76293</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20221014&DB=EPODOC&CC=CN&NR=115180138A$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>WANG MINGYUAN</creatorcontrib><creatorcontrib>ZHANG LONG</creatorcontrib><creatorcontrib>SHAN ZEZHONG</creatorcontrib><creatorcontrib>GUO QIANG</creatorcontrib><creatorcontrib>TANG ZHENGUO</creatorcontrib><creatorcontrib>LIU CHENGWEI</creatorcontrib><creatorcontrib>LU XIANG</creatorcontrib><creatorcontrib>WANG CAIJU</creatorcontrib><creatorcontrib>WU HONGXIA</creatorcontrib><creatorcontrib>XIAO HAIJIAN</creatorcontrib><creatorcontrib>HAO QINGYU</creatorcontrib><title>Novel-layout vertical take-off and landing fixed-wing unmanned aerial vehicle</title><description>The invention discloses a novel layout vertical take-off and landing fixed-wing unmanned aerial vehicle. 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The unmanned aerial vehicle comprises a fuselage main body, wings, wingtip winglets, aileron systems, tilting power systems, an electronic cabin, a cabin door opening and closing structure, a duct power system, a cargo cabin loading structure and an undercarriage structure. Compared with a traditional vertical take-off and landing unmanned aerial vehicle, the vertical take-off and landing unmanned aerial vehicle has the advantages that the pneumatic effect is better, the hovering effect is better, the flight attitude is more stable, the application range is wider, the endurance time is greatly prolonged, the loading level is improved, and the flight performance and the operation safety are greatly improved; the layout has more advantages when applied to a heavy-load and long-endurance vertical take-off and landing fixed-wing unmanned aerial vehicle, the performance of an electric unmanned aerial vehicle ca</abstract><oa>free_for_read</oa></addata></record> |
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subjects | AEROPLANES AIRCRAFT AVIATION COSMONAUTICS HELICOPTERS PERFORMING OPERATIONS TRANSPORTING |
title | Novel-layout vertical take-off and landing fixed-wing unmanned aerial vehicle |
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