Unmanned aerial vehicle with flight anti-collision structure
The invention relates to the technical field of unmanned aerial vehicles, and discloses an unmanned aerial vehicle with a flight anti-collision structure, the unmanned aerial vehicle comprises an unmanned aerial vehicle body, an anti-collision mechanism, a hovering mechanism and a damping mechanism...
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creator | WU XIEHUI DAI JIAQIAO CAI XIAOGANG |
description | The invention relates to the technical field of unmanned aerial vehicles, and discloses an unmanned aerial vehicle with a flight anti-collision structure, the unmanned aerial vehicle comprises an unmanned aerial vehicle body, an anti-collision mechanism, a hovering mechanism and a damping mechanism are sequentially arranged on the unmanned aerial vehicle body, the anti-collision mechanism comprises eight screw holes, and every two screw holes are formed in the front face, the back face, the left side and the right side of the unmanned aerial vehicle body respectively; the number of the mounting plates is eight, each mounting plate is in threaded connection with the corresponding screw hole through a bolt, the number of the bolts is eight, each mounting plate corresponds to the corresponding screw hole in a one-to-one mode, the number of the connecting arms is four, one ends of the connecting arms are fixedly connected between every two mounting plates, and the other ends of the connecting arms are fixedly con |
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the number of the mounting plates is eight, each mounting plate is in threaded connection with the corresponding screw hole through a bolt, the number of the bolts is eight, each mounting plate corresponds to the corresponding screw hole in a one-to-one mode, the number of the connecting arms is four, one ends of the connecting arms are fixedly connected between every two mounting plates, and the other ends of the connecting arms are fixedly con</description><language>chi ; eng</language><subject>AEROPLANES ; AIRCRAFT ; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT ; AVIATION ; COSMONAUTICS ; EQUIPMENT FOR FITTING IN OR TO AIRCRAFT ; FLYING SUITS ; HELICOPTERS ; PARACHUTES ; PERFORMING OPERATIONS ; 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=20230530&DB=EPODOC&CC=CN&NR=116176889A$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20230530&DB=EPODOC&CC=CN&NR=116176889A$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>WU XIEHUI</creatorcontrib><creatorcontrib>DAI JIAQIAO</creatorcontrib><creatorcontrib>CAI XIAOGANG</creatorcontrib><title>Unmanned aerial vehicle with flight anti-collision structure</title><description>The invention relates to the technical field of unmanned aerial vehicles, and discloses an unmanned aerial vehicle with a flight anti-collision structure, the unmanned aerial vehicle comprises an unmanned aerial vehicle body, an anti-collision mechanism, a hovering mechanism and a damping mechanism are sequentially arranged on the unmanned aerial vehicle body, the anti-collision mechanism comprises eight screw holes, and every two screw holes are formed in the front face, the back face, the left side and the right side of the unmanned aerial vehicle body respectively; the number of the mounting plates is eight, each mounting plate is in threaded connection with the corresponding screw hole through a bolt, the number of the bolts is eight, each mounting plate corresponds to the corresponding screw hole in a one-to-one mode, the number of the connecting arms is four, one ends of the connecting arms are fixedly connected between every two mounting plates, and the other ends of the connecting arms are fixedly con</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>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</subject><subject>FLYING SUITS</subject><subject>HELICOPTERS</subject><subject>PARACHUTES</subject><subject>PERFORMING OPERATIONS</subject><subject>TRANSPORTING</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2023</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZLAJzctNzMtLTVFITC3KTMxRKEvNyEzOSVUozyzJUEjLyUzPKFFIzCvJ1E3Oz8nJLM7Mz1MoLikqTS4pLUrlYWBNS8wpTuWF0twMim6uIc4euqkF-fGpxQWJyal5qSXxzn6GhmaG5mYWFpaOxsSoAQAQyjBV</recordid><startdate>20230530</startdate><enddate>20230530</enddate><creator>WU XIEHUI</creator><creator>DAI JIAQIAO</creator><creator>CAI XIAOGANG</creator><scope>EVB</scope></search><sort><creationdate>20230530</creationdate><title>Unmanned aerial vehicle with flight anti-collision structure</title><author>WU XIEHUI ; DAI JIAQIAO ; CAI XIAOGANG</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_CN116176889A3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>chi ; eng</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>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</topic><topic>FLYING SUITS</topic><topic>HELICOPTERS</topic><topic>PARACHUTES</topic><topic>PERFORMING OPERATIONS</topic><topic>TRANSPORTING</topic><toplevel>online_resources</toplevel><creatorcontrib>WU XIEHUI</creatorcontrib><creatorcontrib>DAI JIAQIAO</creatorcontrib><creatorcontrib>CAI XIAOGANG</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>WU XIEHUI</au><au>DAI JIAQIAO</au><au>CAI XIAOGANG</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Unmanned aerial vehicle with flight anti-collision structure</title><date>2023-05-30</date><risdate>2023</risdate><abstract>The invention relates to the technical field of unmanned aerial vehicles, and discloses an unmanned aerial vehicle with a flight anti-collision structure, the unmanned aerial vehicle comprises an unmanned aerial vehicle body, an anti-collision mechanism, a hovering mechanism and a damping mechanism are sequentially arranged on the unmanned aerial vehicle body, the anti-collision mechanism comprises eight screw holes, and every two screw holes are formed in the front face, the back face, the left side and the right side of the unmanned aerial vehicle body respectively; the number of the mounting plates is eight, each mounting plate is in threaded connection with the corresponding screw hole through a bolt, the number of the bolts is eight, each mounting plate corresponds to the corresponding screw hole in a one-to-one mode, the number of the connecting arms is four, one ends of the connecting arms are fixedly connected between every two mounting plates, and the other ends of the connecting arms are fixedly con</abstract><oa>free_for_read</oa></addata></record> |
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language | chi ; eng |
recordid | cdi_epo_espacenet_CN116176889A |
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subjects | AEROPLANES AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS HELICOPTERS PARACHUTES PERFORMING OPERATIONS TRANSPORTING |
title | Unmanned aerial vehicle with flight anti-collision structure |
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