Unmanned aerial vehicle take-off and landing buffer protection frame

Unmanned aerial vehicle take-off and landing buffer protection frame

The invention discloses an unmanned aerial vehicle take-off and landing buffer protection frame, which comprises a connecting base, a transverse rod, a linear buffer assembly and a rotary buffer assembly, wherein the connecting base is fixed to the bottom of an unmanned aerial vehicle, and the conne...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Hauptverfasser: ZHAO ZHONGBIAO, LI NA, YIN XUEYONG
Format: Patent
Sprache:chi ; eng
Schlagworte:
AEROPLANES
AIRCRAFT
AVIATION
COSMONAUTICS
HELICOPTERS
PERFORMING OPERATIONS
TRANSPORTING
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 ZHONGBIAO
LI NA
YIN XUEYONG
description The invention discloses an unmanned aerial vehicle take-off and landing buffer protection frame, which comprises a connecting base, a transverse rod, a linear buffer assembly and a rotary buffer assembly, wherein the connecting base is fixed to the bottom of an unmanned aerial vehicle, and the connecting base is connected with the transverse rod in an angle fine adjustment mode; an accommodating groove distributed in the length direction of the transverse rod is formed in the transverse rod, and an adjusting rod capable of rotating by 90 degrees is arranged in the accommodating groove; a linear buffer assembly is fixed to the bottom of the adjusting rod, and two sets of rotating buffer assemblies are symmetrically arranged at the bottom of the linear buffer assembly. When the unmanned aerial vehicle takes off and lands, the adjusting rod rotates to the vertical direction, so that the linear buffer assembly and the rotary buffer assembly can buffer force from the vertical direction, andwhen the unmanned aerial
format Patent
fullrecord <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_CN111619794A</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>CN111619794A</sourcerecordid><originalsourceid>FETCH-epo_espacenet_CN111619794A3</originalsourceid><addsrcrecordid>eNrjZHAJzctNzMtLTVFITC3KTMxRKEvNyEzOSVUoScxO1c1PS1NIzEtRyAESmXnpCkmlaWmpRQoFRfklqcklmfl5CmlFibmpPAysaYk5xam8UJqbQdHNNcTZQze1ID8-tbggMTk1L7Uk3tnP0NDQzNDS3NLE0ZgYNQCYeDKm</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>Unmanned aerial vehicle take-off and landing buffer protection frame</title><source>esp@cenet</source><creator>ZHAO ZHONGBIAO ; LI NA ; YIN XUEYONG</creator><creatorcontrib>ZHAO ZHONGBIAO ; LI NA ; YIN XUEYONG</creatorcontrib><description>The invention discloses an unmanned aerial vehicle take-off and landing buffer protection frame, which comprises a connecting base, a transverse rod, a linear buffer assembly and a rotary buffer assembly, wherein the connecting base is fixed to the bottom of an unmanned aerial vehicle, and the connecting base is connected with the transverse rod in an angle fine adjustment mode; an accommodating groove distributed in the length direction of the transverse rod is formed in the transverse rod, and an adjusting rod capable of rotating by 90 degrees is arranged in the accommodating groove; a linear buffer assembly is fixed to the bottom of the adjusting rod, and two sets of rotating buffer assemblies are symmetrically arranged at the bottom of the linear buffer assembly. When the unmanned aerial vehicle takes off and lands, the adjusting rod rotates to the vertical direction, so that the linear buffer assembly and the rotary buffer assembly can buffer force from the vertical direction, andwhen the unmanned aerial</description><language>chi ; eng</language><subject>AEROPLANES ; AIRCRAFT ; AVIATION ; COSMONAUTICS ; HELICOPTERS ; PERFORMING OPERATIONS ; TRANSPORTING</subject><creationdate>2020</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=20200904&amp;DB=EPODOC&amp;CC=CN&amp;NR=111619794A$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25543,76294</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&amp;date=20200904&amp;DB=EPODOC&amp;CC=CN&amp;NR=111619794A$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>ZHAO ZHONGBIAO</creatorcontrib><creatorcontrib>LI NA</creatorcontrib><creatorcontrib>YIN XUEYONG</creatorcontrib><title>Unmanned aerial vehicle take-off and landing buffer protection frame</title><description>The invention discloses an unmanned aerial vehicle take-off and landing buffer protection frame, which comprises a connecting base, a transverse rod, a linear buffer assembly and a rotary buffer assembly, wherein the connecting base is fixed to the bottom of an unmanned aerial vehicle, and the connecting base is connected with the transverse rod in an angle fine adjustment mode; an accommodating groove distributed in the length direction of the transverse rod is formed in the transverse rod, and an adjusting rod capable of rotating by 90 degrees is arranged in the accommodating groove; a linear buffer assembly is fixed to the bottom of the adjusting rod, and two sets of rotating buffer assemblies are symmetrically arranged at the bottom of the linear buffer assembly. When the unmanned aerial vehicle takes off and lands, the adjusting rod rotates to the vertical direction, so that the linear buffer assembly and the rotary buffer assembly can buffer force from the vertical direction, andwhen the unmanned aerial</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>2020</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZHAJzctNzMtLTVFITC3KTMxRKEvNyEzOSVUoScxO1c1PS1NIzEtRyAESmXnpCkmlaWmpRQoFRfklqcklmfl5CmlFibmpPAysaYk5xam8UJqbQdHNNcTZQze1ID8-tbggMTk1L7Uk3tnP0NDQzNDS3NLE0ZgYNQCYeDKm</recordid><startdate>20200904</startdate><enddate>20200904</enddate><creator>ZHAO ZHONGBIAO</creator><creator>LI NA</creator><creator>YIN XUEYONG</creator><scope>EVB</scope></search><sort><creationdate>20200904</creationdate><title>Unmanned aerial vehicle take-off and landing buffer protection frame</title><author>ZHAO ZHONGBIAO ; LI NA ; YIN XUEYONG</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_CN111619794A3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>chi ; eng</language><creationdate>2020</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 ZHONGBIAO</creatorcontrib><creatorcontrib>LI NA</creatorcontrib><creatorcontrib>YIN XUEYONG</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>ZHAO ZHONGBIAO</au><au>LI NA</au><au>YIN XUEYONG</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Unmanned aerial vehicle take-off and landing buffer protection frame</title><date>2020-09-04</date><risdate>2020</risdate><abstract>The invention discloses an unmanned aerial vehicle take-off and landing buffer protection frame, which comprises a connecting base, a transverse rod, a linear buffer assembly and a rotary buffer assembly, wherein the connecting base is fixed to the bottom of an unmanned aerial vehicle, and the connecting base is connected with the transverse rod in an angle fine adjustment mode; an accommodating groove distributed in the length direction of the transverse rod is formed in the transverse rod, and an adjusting rod capable of rotating by 90 degrees is arranged in the accommodating groove; a linear buffer assembly is fixed to the bottom of the adjusting rod, and two sets of rotating buffer assemblies are symmetrically arranged at the bottom of the linear buffer assembly. When the unmanned aerial vehicle takes off and lands, the adjusting rod rotates to the vertical direction, so that the linear buffer assembly and the rotary buffer assembly can buffer force from the vertical direction, andwhen the unmanned aerial</abstract><oa>free_for_read</oa></addata></record>
fulltext fulltext_linktorsrc
identifier
ispartof
issn
language chi ; eng
recordid cdi_epo_espacenet_CN111619794A
source esp@cenet
subjects AEROPLANES
AIRCRAFT
AVIATION
COSMONAUTICS
HELICOPTERS
PERFORMING OPERATIONS
TRANSPORTING
title Unmanned aerial vehicle take-off and landing buffer protection frame
url https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-23T10%3A28%3A25IST&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%20ZHONGBIAO&rft.date=2020-09-04&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3ECN111619794A%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