Quick release structure for mounting unmanned aerial vehicle and unmanned aerial vehicle
The utility model belongs to the technical field of unmanned aerial vehicles, and relates to a quick release structure for mounting an unmanned aerial vehicle, which comprises a quick release module and a quick release base which are matched with each other, the left outer side surface and the right...
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creator | NIE JUN HU HUAZHI LIU YONG HU HAISHENG JIA ZONGLIN |
description | The utility model belongs to the technical field of unmanned aerial vehicles, and relates to a quick release structure for mounting an unmanned aerial vehicle, which comprises a quick release module and a quick release base which are matched with each other, the left outer side surface and the right outer side surface of the quick release module are respectively provided with a slide rail (1), and the top of the quick release module is provided with a spring bolt (2) capable of stretching up and down; the left inner side face and the right inner side face of the quick-release base are each provided with a sliding groove (7), the inner side face of the top of the quick-release base is provided with a groove (6), the sliding rails (1) can be inserted into the sliding grooves (7) and can slide front and back in the sliding grooves (7), and the spring bolts (2) can be buckled in the grooves (6) so that the quick-release module and the quick-release base can be connected together. The mounting part of the unmanned |
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The mounting part of the unmanned</description><language>chi ; eng</language><subject>AIRCRAFT ; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT ; AVIATION ; COSMONAUTICS ; EQUIPMENT FOR FITTING IN OR TO AIRCRAFT ; FLYING SUITS ; PARACHUTES ; 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=20220624&DB=EPODOC&CC=CN&NR=216805850U$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25542,76289</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20220624&DB=EPODOC&CC=CN&NR=216805850U$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>NIE JUN</creatorcontrib><creatorcontrib>HU HUAZHI</creatorcontrib><creatorcontrib>LIU YONG</creatorcontrib><creatorcontrib>HU HAISHENG</creatorcontrib><creatorcontrib>JIA ZONGLIN</creatorcontrib><title>Quick release structure for mounting unmanned aerial vehicle and unmanned aerial vehicle</title><description>The utility model belongs to the technical field of unmanned aerial vehicles, and relates to a quick release structure for mounting an unmanned aerial vehicle, which comprises a quick release module and a quick release base which are matched with each other, the left outer side surface and the right outer side surface of the quick release module are respectively provided with a slide rail (1), and the top of the quick release module is provided with a spring bolt (2) capable of stretching up and down; the left inner side face and the right inner side face of the quick-release base are each provided with a sliding groove (7), the inner side face of the top of the quick-release base is provided with a groove (6), the sliding rails (1) can be inserted into the sliding grooves (7) and can slide front and back in the sliding grooves (7), and the spring bolts (2) can be buckled in the grooves (6) so that the quick-release module and the quick-release base can be connected together. The mounting part of the unmanned</description><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>PARACHUTES</subject><subject>PERFORMING OPERATIONS</subject><subject>TRANSPORTING</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2022</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZIgILM1MzlYoSs1JTSxOVSguKSpNLiktSlVIyy9SyM0vzSvJzEtXKM3LTczLS01RSEwtykzMUShLzchMzklVSMxLwSXHw8CalphTnMoLpbkZlNxcQ5w9dFML8uNTiwsSk1PzUkvinf2MDM0sDEwtTA1CQ42JUgQAU-o7ew</recordid><startdate>20220624</startdate><enddate>20220624</enddate><creator>NIE JUN</creator><creator>HU HUAZHI</creator><creator>LIU YONG</creator><creator>HU HAISHENG</creator><creator>JIA ZONGLIN</creator><scope>EVB</scope></search><sort><creationdate>20220624</creationdate><title>Quick release structure for mounting unmanned aerial vehicle and unmanned aerial vehicle</title><author>NIE JUN ; HU HUAZHI ; LIU YONG ; HU HAISHENG ; JIA ZONGLIN</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_CN216805850UU3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>chi ; eng</language><creationdate>2022</creationdate><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>PARACHUTES</topic><topic>PERFORMING OPERATIONS</topic><topic>TRANSPORTING</topic><toplevel>online_resources</toplevel><creatorcontrib>NIE JUN</creatorcontrib><creatorcontrib>HU HUAZHI</creatorcontrib><creatorcontrib>LIU YONG</creatorcontrib><creatorcontrib>HU HAISHENG</creatorcontrib><creatorcontrib>JIA ZONGLIN</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>NIE JUN</au><au>HU HUAZHI</au><au>LIU YONG</au><au>HU HAISHENG</au><au>JIA ZONGLIN</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Quick release structure for mounting unmanned aerial vehicle and unmanned aerial vehicle</title><date>2022-06-24</date><risdate>2022</risdate><abstract>The utility model belongs to the technical field of unmanned aerial vehicles, and relates to a quick release structure for mounting an unmanned aerial vehicle, which comprises a quick release module and a quick release base which are matched with each other, the left outer side surface and the right outer side surface of the quick release module are respectively provided with a slide rail (1), and the top of the quick release module is provided with a spring bolt (2) capable of stretching up and down; the left inner side face and the right inner side face of the quick-release base are each provided with a sliding groove (7), the inner side face of the top of the quick-release base is provided with a groove (6), the sliding rails (1) can be inserted into the sliding grooves (7) and can slide front and back in the sliding grooves (7), and the spring bolts (2) can be buckled in the grooves (6) so that the quick-release module and the quick-release base can be connected together. The mounting part of the unmanned</abstract><oa>free_for_read</oa></addata></record> |
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language | chi ; eng |
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subjects | AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS PARACHUTES PERFORMING OPERATIONS TRANSPORTING |
title | Quick release structure for mounting unmanned aerial vehicle and unmanned aerial vehicle |
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