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...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
1. Verfasser: ZHAO ZHEWEI
Format: Patent
Sprache:chi ; eng
Schlagworte:
Online-Zugang:Volltext bestellen
Tags: Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
container_end_page
container_issue
container_start_page
container_title
container_volume
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
fullrecord <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_CN216994834UU</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>CN216994834UU</sourcerecordid><originalsourceid>FETCH-epo_espacenet_CN216994834UU3</originalsourceid><addsrcrecordid>eNrjZHAIScxO1c1PS1NIzEtRyAESmXnpCsWlBQX5RSUKaflFQJwDFivNy03My0tNUUhMLcpMzFEoS83ITM5J5WFgTUvMKU7lhdLcDEpuriHOHrqpBfnxqcUFicmpeakl8c5-RoZmlpYmFsYmoaHGRCkCABGFMf8</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>Take-off and landing support for folding unmanned aerial vehicle</title><source>esp@cenet</source><creator>ZHAO ZHEWEI</creator><creatorcontrib>ZHAO ZHEWEI</creatorcontrib><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><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&amp;date=20220719&amp;DB=EPODOC&amp;CC=CN&amp;NR=216994834U$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,309,781,886,25568,76551</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&amp;date=20220719&amp;DB=EPODOC&amp;CC=CN&amp;NR=216994834U$$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>
fulltext fulltext_linktorsrc
identifier
ispartof
issn
language chi ; eng
recordid cdi_epo_espacenet_CN216994834UU
source esp@cenet
subjects AEROPLANES
AIRCRAFT
AVIATION
COSMONAUTICS
HELICOPTERS
PERFORMING OPERATIONS
TRANSPORTING
title Take-off and landing support for folding unmanned aerial vehicle
url https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2024-12-17T06%3A37%3A45IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-epo_EVB&rft_val_fmt=info:ofi/fmt:kev:mtx:patent&rft.genre=patent&rft.au=ZHAO%20ZHEWEI&rft.date=2022-07-19&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3ECN216994834UU%3C/epo_EVB%3E%3Curl%3E%3C/url%3E&disable_directlink=true&sfx.directlink=off&sfx.report_link=0&rft_id=info:oai/&rft_id=info:pmid/&rfr_iscdi=true