Unmanned aerial vehicle article mounting structure

The utility model discloses an article mounting structure of an unmanned aerial vehicle. The device comprises an unmanned aerial vehicle and a connecting rod, the lower end of the unmanned aerial vehicle is fixedly connected with a hinge seat, the lower end of the hinge seat is rotatably connected w...

Ausführliche Beschreibung

Gespeichert in:

Bibliographische Detailangaben
1. Verfasser:	XU KETAO
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	XU KETAO
description	The utility model discloses an article mounting structure of an unmanned aerial vehicle. The device comprises an unmanned aerial vehicle and a connecting rod, the lower end of the unmanned aerial vehicle is fixedly connected with a hinge seat, the lower end of the hinge seat is rotatably connected with a hinge shaft, the lower end of the hinge shaft is rotatably connected with a connecting rod, the outer side of the connecting rod is fixedly connected with a fixing block, the outer side of the fixing block is fixedly connected with an elastic block, and the outer side of the elastic block is in contact connection with a limiting seat. Through hinging of the unmanned aerial vehicle and the connecting rod, the connecting rod can rotate leftwards and rightwards, when shaking occurs, the connecting rod is driven to rotate to extrude the elastic block to make contact with the limiting base, the shaking force is buffered through the elasticity of the elastic block, and therefore the shakingreducing effect is achiev
format	Patent
fullrecord	<record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_CN211996165UU</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>CN211996165UU</sourcerecordid><originalsourceid>FETCH-epo_espacenet_CN211996165UU3</originalsourceid><addsrcrecordid>eNrjZDAKzctNzMtLTVFITC3KTMxRKEvNyEzOSVVILCoB07n5pXklmXnpCsUlRaXJJaVFqTwMrGmJOcWpvFCam0HJzTXE2UM3tSA_PrW4IDE5NS-1JN7Zz8jQ0NLSzNDMNDTUmChFAFcQLWc</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>Unmanned aerial vehicle article mounting structure</title><source>esp@cenet</source><creator>XU KETAO</creator><creatorcontrib>XU KETAO</creatorcontrib><description>The utility model discloses an article mounting structure of an unmanned aerial vehicle. The device comprises an unmanned aerial vehicle and a connecting rod, the lower end of the unmanned aerial vehicle is fixedly connected with a hinge seat, the lower end of the hinge seat is rotatably connected with a hinge shaft, the lower end of the hinge shaft is rotatably connected with a connecting rod, the outer side of the connecting rod is fixedly connected with a fixing block, the outer side of the fixing block is fixedly connected with an elastic block, and the outer side of the elastic block is in contact connection with a limiting seat. Through hinging of the unmanned aerial vehicle and the connecting rod, the connecting rod can rotate leftwards and rightwards, when shaking occurs, the connecting rod is driven to rotate to extrude the elastic block to make contact with the limiting base, the shaking force is buffered through the elasticity of the elastic block, and therefore the shakingreducing effect is achiev</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>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&date=20201124&DB=EPODOC&CC=CN&NR=211996165U$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,778,883,25547,76298</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20201124&DB=EPODOC&CC=CN&NR=211996165U$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>XU KETAO</creatorcontrib><title>Unmanned aerial vehicle article mounting structure</title><description>The utility model discloses an article mounting structure of an unmanned aerial vehicle. The device comprises an unmanned aerial vehicle and a connecting rod, the lower end of the unmanned aerial vehicle is fixedly connected with a hinge seat, the lower end of the hinge seat is rotatably connected with a hinge shaft, the lower end of the hinge shaft is rotatably connected with a connecting rod, the outer side of the connecting rod is fixedly connected with a fixing block, the outer side of the fixing block is fixedly connected with an elastic block, and the outer side of the elastic block is in contact connection with a limiting seat. Through hinging of the unmanned aerial vehicle and the connecting rod, the connecting rod can rotate leftwards and rightwards, when shaking occurs, the connecting rod is driven to rotate to extrude the elastic block to make contact with the limiting base, the shaking force is buffered through the elasticity of the elastic block, and therefore the shakingreducing effect is achiev</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>2020</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZDAKzctNzMtLTVFITC3KTMxRKEvNyEzOSVVILCoB07n5pXklmXnpCsUlRaXJJaVFqTwMrGmJOcWpvFCam0HJzTXE2UM3tSA_PrW4IDE5NS-1JN7Zz8jQ0NLSzNDMNDTUmChFAFcQLWc</recordid><startdate>20201124</startdate><enddate>20201124</enddate><creator>XU KETAO</creator><scope>EVB</scope></search><sort><creationdate>20201124</creationdate><title>Unmanned aerial vehicle article mounting structure</title><author>XU KETAO</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_CN211996165UU3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>chi ; eng</language><creationdate>2020</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>XU KETAO</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>XU KETAO</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Unmanned aerial vehicle article mounting structure</title><date>2020-11-24</date><risdate>2020</risdate><abstract>The utility model discloses an article mounting structure of an unmanned aerial vehicle. The device comprises an unmanned aerial vehicle and a connecting rod, the lower end of the unmanned aerial vehicle is fixedly connected with a hinge seat, the lower end of the hinge seat is rotatably connected with a hinge shaft, the lower end of the hinge shaft is rotatably connected with a connecting rod, the outer side of the connecting rod is fixedly connected with a fixing block, the outer side of the fixing block is fixedly connected with an elastic block, and the outer side of the elastic block is in contact connection with a limiting seat. Through hinging of the unmanned aerial vehicle and the connecting rod, the connecting rod can rotate leftwards and rightwards, when shaking occurs, the connecting rod is driven to rotate to extrude the elastic block to make contact with the limiting base, the shaking force is buffered through the elasticity of the elastic block, and therefore the shakingreducing effect is achiev</abstract><oa>free_for_read</oa></addata></record>
fulltext	fulltext_linktorsrc
identifier
ispartof
issn
language	chi ; eng
recordid	cdi_epo_espacenet_CN211996165UU
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	Unmanned aerial vehicle article mounting structure
url	https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-16T07%3A52%3A44IST&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=XU%20KETAO&rft.date=2020-11-24&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3ECN211996165UU%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