Loading device for suspension type unmanned aerial vehicle

Loading device for suspension type unmanned aerial vehicle

The utility model discloses a suspension type unmanned aerial vehicle loading device, which relates to the field of unmanned aerial vehicle loading devices and comprises a suspension box, four adjusting arms are arranged on the circumferential surface of the suspension box, and a U-shaped clamping p...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
1. Verfasser: BAO XIAOFANG
Format: Patent
Sprache:chi ; eng
Schlagworte:
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
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 BAO XIAOFANG
description The utility model discloses a suspension type unmanned aerial vehicle loading device, which relates to the field of unmanned aerial vehicle loading devices and comprises a suspension box, four adjusting arms are arranged on the circumferential surface of the suspension box, and a U-shaped clamping plate is lapped above each adjusting arm. Through mutual cooperation of the arranged adjusting arms, U-shaped clamping plates, sliding rods, clamping plates, cross rods and magnets, the positions of the four adjusting arms can be adjusted according to the specific orientation of the unmanned aerial vehicle supporting arms, the four adjusting arms are pulled separately, so that T-shaped sliding blocks slide in T-shaped sliding grooves and stop after moving to proper positions, and the unmanned aerial vehicle supporting arms can be conveniently adjusted. And then the position of a supporting vertical rod is adjusted according to the length of the unmanned aerial vehicle supporting arm, firstly, a nut is rotated to loo
format Patent
fullrecord <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_CN216128443UU</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>CN216128443UU</sourcerecordid><originalsourceid>FETCH-epo_espacenet_CN216128443UU3</originalsourceid><addsrcrecordid>eNrjZLDyyU9MycxLV0hJLctMTlVIyy9SKC4tLkjNK87Mz1MoqSxIVSjNy03My0tNUUhMLcpMzFEoS83ITM5J5WFgTUvMKU7lhdLcDEpuriHOHrqpBfnxqcUFicmpeakl8c5-RoZmhkYWJibGoaHGRCkCAO2fMAU</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>Loading device for suspension type unmanned aerial vehicle</title><source>esp@cenet</source><creator>BAO XIAOFANG</creator><creatorcontrib>BAO XIAOFANG</creatorcontrib><description>The utility model discloses a suspension type unmanned aerial vehicle loading device, which relates to the field of unmanned aerial vehicle loading devices and comprises a suspension box, four adjusting arms are arranged on the circumferential surface of the suspension box, and a U-shaped clamping plate is lapped above each adjusting arm. Through mutual cooperation of the arranged adjusting arms, U-shaped clamping plates, sliding rods, clamping plates, cross rods and magnets, the positions of the four adjusting arms can be adjusted according to the specific orientation of the unmanned aerial vehicle supporting arms, the four adjusting arms are pulled separately, so that T-shaped sliding blocks slide in T-shaped sliding grooves and stop after moving to proper positions, and the unmanned aerial vehicle supporting arms can be conveniently adjusted. And then the position of a supporting vertical rod is adjusted according to the length of the unmanned aerial vehicle supporting arm, firstly, a nut is rotated to loo</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&amp;date=20220325&amp;DB=EPODOC&amp;CC=CN&amp;NR=216128443U$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25544,76293</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&amp;date=20220325&amp;DB=EPODOC&amp;CC=CN&amp;NR=216128443U$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>BAO XIAOFANG</creatorcontrib><title>Loading device for suspension type unmanned aerial vehicle</title><description>The utility model discloses a suspension type unmanned aerial vehicle loading device, which relates to the field of unmanned aerial vehicle loading devices and comprises a suspension box, four adjusting arms are arranged on the circumferential surface of the suspension box, and a U-shaped clamping plate is lapped above each adjusting arm. Through mutual cooperation of the arranged adjusting arms, U-shaped clamping plates, sliding rods, clamping plates, cross rods and magnets, the positions of the four adjusting arms can be adjusted according to the specific orientation of the unmanned aerial vehicle supporting arms, the four adjusting arms are pulled separately, so that T-shaped sliding blocks slide in T-shaped sliding grooves and stop after moving to proper positions, and the unmanned aerial vehicle supporting arms can be conveniently adjusted. And then the position of a supporting vertical rod is adjusted according to the length of the unmanned aerial vehicle supporting arm, firstly, a nut is rotated to loo</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>eNrjZLDyyU9MycxLV0hJLctMTlVIyy9SKC4tLkjNK87Mz1MoqSxIVSjNy03My0tNUUhMLcpMzFEoS83ITM5J5WFgTUvMKU7lhdLcDEpuriHOHrqpBfnxqcUFicmpeakl8c5-RoZmhkYWJibGoaHGRCkCAO2fMAU</recordid><startdate>20220325</startdate><enddate>20220325</enddate><creator>BAO XIAOFANG</creator><scope>EVB</scope></search><sort><creationdate>20220325</creationdate><title>Loading device for suspension type unmanned aerial vehicle</title><author>BAO XIAOFANG</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_CN216128443UU3</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>BAO XIAOFANG</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>BAO XIAOFANG</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Loading device for suspension type unmanned aerial vehicle</title><date>2022-03-25</date><risdate>2022</risdate><abstract>The utility model discloses a suspension type unmanned aerial vehicle loading device, which relates to the field of unmanned aerial vehicle loading devices and comprises a suspension box, four adjusting arms are arranged on the circumferential surface of the suspension box, and a U-shaped clamping plate is lapped above each adjusting arm. Through mutual cooperation of the arranged adjusting arms, U-shaped clamping plates, sliding rods, clamping plates, cross rods and magnets, the positions of the four adjusting arms can be adjusted according to the specific orientation of the unmanned aerial vehicle supporting arms, the four adjusting arms are pulled separately, so that T-shaped sliding blocks slide in T-shaped sliding grooves and stop after moving to proper positions, and the unmanned aerial vehicle supporting arms can be conveniently adjusted. And then the position of a supporting vertical rod is adjusted according to the length of the unmanned aerial vehicle supporting arm, firstly, a nut is rotated to loo</abstract><oa>free_for_read</oa></addata></record>
fulltext fulltext_linktorsrc
identifier
ispartof
issn
language chi ; eng
recordid cdi_epo_espacenet_CN216128443UU
source esp@cenet
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 Loading device for suspension type 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=2025-01-27T14%3A34%3A36IST&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=BAO%20XIAOFANG&rft.date=2022-03-25&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3ECN216128443UU%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