Take-off and landing support for folding unmanned aerial vehicle
The landing support comprises an unmanned aerial vehicle body, a mounting bottom plate is fixedly mounted at the bottom of the unmanned aerial vehicle body, a folding support is fixedly mounted at the bottom of the mounting bottom plate, and a rotatable telescopic assembly is fixedly connected to th...
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creator | ZHAO ZHEWEI |
description | The landing support comprises an unmanned aerial vehicle body, a mounting bottom plate is fixedly mounted at the bottom of the unmanned aerial vehicle body, a folding support is fixedly mounted at the bottom of the mounting bottom plate, and a rotatable telescopic assembly is fixedly connected to the outer side of the folding support. The outer surface of the telescopic assembly is sleeved with a damping spring, a threaded connector is fixedly connected to the top of the telescopic assembly, a connecting screw hole is formed in the bottom of the mounting bottom plate, and the threaded connector is in threaded connection with the screw hole. According to the unmanned aerial vehicle, the folding supports, the telescopic assemblies and the damping springs are arranged in a matched mode, so that when the unmanned aerial vehicle body falls to the ground, the damping springs play a good damping and buffering role, the whole supports and the unmanned aerial vehicle body are effectively protected, the structure is si |
format | Patent |
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The outer surface of the telescopic assembly is sleeved with a damping spring, a threaded connector is fixedly connected to the top of the telescopic assembly, a connecting screw hole is formed in the bottom of the mounting bottom plate, and the threaded connector is in threaded connection with the screw hole. According to the unmanned aerial vehicle, the folding supports, the telescopic assemblies and the damping springs are arranged in a matched mode, so that when the unmanned aerial vehicle body falls to the ground, the damping springs play a good damping and buffering role, the whole supports and the unmanned aerial vehicle body are effectively protected, the structure is si</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=20220719&DB=EPODOC&CC=CN&NR=216994834U$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,309,781,886,25568,76551</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20220719&DB=EPODOC&CC=CN&NR=216994834U$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>ZHAO ZHEWEI</creatorcontrib><title>Take-off and landing support for folding unmanned aerial vehicle</title><description>The landing support comprises an unmanned aerial vehicle body, a mounting bottom plate is fixedly mounted at the bottom of the unmanned aerial vehicle body, a folding support is fixedly mounted at the bottom of the mounting bottom plate, and a rotatable telescopic assembly is fixedly connected to the outer side of the folding support. The outer surface of the telescopic assembly is sleeved with a damping spring, a threaded connector is fixedly connected to the top of the telescopic assembly, a connecting screw hole is formed in the bottom of the mounting bottom plate, and the threaded connector is in threaded connection with the screw hole. According to the unmanned aerial vehicle, the folding supports, the telescopic assemblies and the damping springs are arranged in a matched mode, so that when the unmanned aerial vehicle body falls to the ground, the damping springs play a good damping and buffering role, the whole supports and the unmanned aerial vehicle body are effectively protected, the structure is si</description><subject>AEROPLANES</subject><subject>AIRCRAFT</subject><subject>AVIATION</subject><subject>COSMONAUTICS</subject><subject>HELICOPTERS</subject><subject>PERFORMING OPERATIONS</subject><subject>TRANSPORTING</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2022</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZHAIScxO1c1PS1NIzEtRyAESmXnpCsWlBQX5RSUKaflFQJwDFivNy03My0tNUUhMLcpMzFEoS83ITM5J5WFgTUvMKU7lhdLcDEpuriHOHrqpBfnxqcUFicmpeakl8c5-RoZmlpYmFsYmoaHGRCkCABGFMf8</recordid><startdate>20220719</startdate><enddate>20220719</enddate><creator>ZHAO ZHEWEI</creator><scope>EVB</scope></search><sort><creationdate>20220719</creationdate><title>Take-off and landing support for folding unmanned aerial vehicle</title><author>ZHAO ZHEWEI</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_CN216994834UU3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>chi ; eng</language><creationdate>2022</creationdate><topic>AEROPLANES</topic><topic>AIRCRAFT</topic><topic>AVIATION</topic><topic>COSMONAUTICS</topic><topic>HELICOPTERS</topic><topic>PERFORMING OPERATIONS</topic><topic>TRANSPORTING</topic><toplevel>online_resources</toplevel><creatorcontrib>ZHAO ZHEWEI</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>ZHAO ZHEWEI</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Take-off and landing support for folding unmanned aerial vehicle</title><date>2022-07-19</date><risdate>2022</risdate><abstract>The landing support comprises an unmanned aerial vehicle body, a mounting bottom plate is fixedly mounted at the bottom of the unmanned aerial vehicle body, a folding support is fixedly mounted at the bottom of the mounting bottom plate, and a rotatable telescopic assembly is fixedly connected to the outer side of the folding support. The outer surface of the telescopic assembly is sleeved with a damping spring, a threaded connector is fixedly connected to the top of the telescopic assembly, a connecting screw hole is formed in the bottom of the mounting bottom plate, and the threaded connector is in threaded connection with the screw hole. According to the unmanned aerial vehicle, the folding supports, the telescopic assemblies and the damping springs are arranged in a matched mode, so that when the unmanned aerial vehicle body falls to the ground, the damping springs play a good damping and buffering role, the whole supports and the unmanned aerial vehicle body are effectively protected, the structure is si</abstract><oa>free_for_read</oa></addata></record> |
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language | chi ; eng |
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subjects | AEROPLANES AIRCRAFT AVIATION COSMONAUTICS HELICOPTERS PERFORMING OPERATIONS TRANSPORTING |
title | Take-off and landing support for folding unmanned aerial vehicle |
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