Unmanned aerial vehicle parachute system

The invention discloses an unmanned aerial vehicle parachute system. The unmanned aerial vehicle parachute system comprises a parachute device; the parachute device comprises a parachute catapulting cabin, a parachute and a catapulting plate; a cabin cover is arranged at a cabin opening of the parac...

Ausführliche Beschreibung

Gespeichert in:

Bibliographische Detailangaben
Hauptverfasser:	ZHANG SHAORONG, SUN SHANLIN, TAN ZHICHENG, YAO XING, XIN YILI, XIE LEI, HAN YIFAN, LI YUN, SUN PENG
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	ZHANG SHAORONG SUN SHANLIN TAN ZHICHENG YAO XING XIN YILI XIE LEI HAN YIFAN LI YUN SUN PENG
description	The invention discloses an unmanned aerial vehicle parachute system. The unmanned aerial vehicle parachute system comprises a parachute device; the parachute device comprises a parachute catapulting cabin, a parachute and a catapulting plate; a cabin cover is arranged at a cabin opening of the parachute catapulting cabin, one end of the cabin cover is hinged to the cabin opening, and the other endof the cabin cover is locked and closed at the cabin opening through a parachute opening mechanism; the catapulting plate is mounted to catapulting springs through the locked and closed cabin cover in a pressed mode, wherein the catapulting springs are evenly distributed on the circumference in the parachute catapulting cabin; the folded parachute is arranged between the cabin cover and the catapulting plate; and a parachute rope of the parachute penetrates through a center hole of the catapulting plate to be fixedly connected to the cabin bottom of the parachute catapulting cabin. Accordingto the unmanned aerial veh
format	Patent
fullrecord	<record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_CN108688821A</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>CN108688821A</sourcerecordid><originalsourceid>FETCH-epo_espacenet_CN108688821A3</originalsourceid><addsrcrecordid>eNrjZNAIzctNzMtLTVFITC3KTMxRKEvNyEzOSVUoSCxKTM4oLUlVKK4sLknN5WFgTUvMKU7lhdLcDIpuriHOHrqpBfnxqcUFicmpeakl8c5-hgYWZhYWFkaGjsbEqAEA4NsoiQ</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>Unmanned aerial vehicle parachute system</title><source>esp@cenet</source><creator>ZHANG SHAORONG ; SUN SHANLIN ; TAN ZHICHENG ; YAO XING ; XIN YILI ; XIE LEI ; HAN YIFAN ; LI YUN ; SUN PENG</creator><creatorcontrib>ZHANG SHAORONG ; SUN SHANLIN ; TAN ZHICHENG ; YAO XING ; XIN YILI ; XIE LEI ; HAN YIFAN ; LI YUN ; SUN PENG</creatorcontrib><description>The invention discloses an unmanned aerial vehicle parachute system. The unmanned aerial vehicle parachute system comprises a parachute device; the parachute device comprises a parachute catapulting cabin, a parachute and a catapulting plate; a cabin cover is arranged at a cabin opening of the parachute catapulting cabin, one end of the cabin cover is hinged to the cabin opening, and the other endof the cabin cover is locked and closed at the cabin opening through a parachute opening mechanism; the catapulting plate is mounted to catapulting springs through the locked and closed cabin cover in a pressed mode, wherein the catapulting springs are evenly distributed on the circumference in the parachute catapulting cabin; the folded parachute is arranged between the cabin cover and the catapulting plate; and a parachute rope of the parachute penetrates through a center hole of the catapulting plate to be fixedly connected to the cabin bottom of the parachute catapulting cabin. Accordingto the unmanned aerial veh</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>2018</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=20181023&DB=EPODOC&CC=CN&NR=108688821A$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25563,76418</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20181023&DB=EPODOC&CC=CN&NR=108688821A$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>ZHANG SHAORONG</creatorcontrib><creatorcontrib>SUN SHANLIN</creatorcontrib><creatorcontrib>TAN ZHICHENG</creatorcontrib><creatorcontrib>YAO XING</creatorcontrib><creatorcontrib>XIN YILI</creatorcontrib><creatorcontrib>XIE LEI</creatorcontrib><creatorcontrib>HAN YIFAN</creatorcontrib><creatorcontrib>LI YUN</creatorcontrib><creatorcontrib>SUN PENG</creatorcontrib><title>Unmanned aerial vehicle parachute system</title><description>The invention discloses an unmanned aerial vehicle parachute system. The unmanned aerial vehicle parachute system comprises a parachute device; the parachute device comprises a parachute catapulting cabin, a parachute and a catapulting plate; a cabin cover is arranged at a cabin opening of the parachute catapulting cabin, one end of the cabin cover is hinged to the cabin opening, and the other endof the cabin cover is locked and closed at the cabin opening through a parachute opening mechanism; the catapulting plate is mounted to catapulting springs through the locked and closed cabin cover in a pressed mode, wherein the catapulting springs are evenly distributed on the circumference in the parachute catapulting cabin; the folded parachute is arranged between the cabin cover and the catapulting plate; and a parachute rope of the parachute penetrates through a center hole of the catapulting plate to be fixedly connected to the cabin bottom of the parachute catapulting cabin. Accordingto the unmanned aerial veh</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>2018</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZNAIzctNzMtLTVFITC3KTMxRKEvNyEzOSVUoSCxKTM4oLUlVKK4sLknN5WFgTUvMKU7lhdLcDIpuriHOHrqpBfnxqcUFicmpeakl8c5-hgYWZhYWFkaGjsbEqAEA4NsoiQ</recordid><startdate>20181023</startdate><enddate>20181023</enddate><creator>ZHANG SHAORONG</creator><creator>SUN SHANLIN</creator><creator>TAN ZHICHENG</creator><creator>YAO XING</creator><creator>XIN YILI</creator><creator>XIE LEI</creator><creator>HAN YIFAN</creator><creator>LI YUN</creator><creator>SUN PENG</creator><scope>EVB</scope></search><sort><creationdate>20181023</creationdate><title>Unmanned aerial vehicle parachute system</title><author>ZHANG SHAORONG ; SUN SHANLIN ; TAN ZHICHENG ; YAO XING ; XIN YILI ; XIE LEI ; HAN YIFAN ; LI YUN ; SUN PENG</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_CN108688821A3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>chi ; eng</language><creationdate>2018</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>ZHANG SHAORONG</creatorcontrib><creatorcontrib>SUN SHANLIN</creatorcontrib><creatorcontrib>TAN ZHICHENG</creatorcontrib><creatorcontrib>YAO XING</creatorcontrib><creatorcontrib>XIN YILI</creatorcontrib><creatorcontrib>XIE LEI</creatorcontrib><creatorcontrib>HAN YIFAN</creatorcontrib><creatorcontrib>LI YUN</creatorcontrib><creatorcontrib>SUN PENG</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>ZHANG SHAORONG</au><au>SUN SHANLIN</au><au>TAN ZHICHENG</au><au>YAO XING</au><au>XIN YILI</au><au>XIE LEI</au><au>HAN YIFAN</au><au>LI YUN</au><au>SUN PENG</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Unmanned aerial vehicle parachute system</title><date>2018-10-23</date><risdate>2018</risdate><abstract>The invention discloses an unmanned aerial vehicle parachute system. The unmanned aerial vehicle parachute system comprises a parachute device; the parachute device comprises a parachute catapulting cabin, a parachute and a catapulting plate; a cabin cover is arranged at a cabin opening of the parachute catapulting cabin, one end of the cabin cover is hinged to the cabin opening, and the other endof the cabin cover is locked and closed at the cabin opening through a parachute opening mechanism; the catapulting plate is mounted to catapulting springs through the locked and closed cabin cover in a pressed mode, wherein the catapulting springs are evenly distributed on the circumference in the parachute catapulting cabin; the folded parachute is arranged between the cabin cover and the catapulting plate; and a parachute rope of the parachute penetrates through a center hole of the catapulting plate to be fixedly connected to the cabin bottom of the parachute catapulting cabin. Accordingto the unmanned aerial veh</abstract><oa>free_for_read</oa></addata></record>
fulltext	fulltext_linktorsrc
identifier
ispartof
issn
language	chi ; eng
recordid	cdi_epo_espacenet_CN108688821A
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 parachute system
url	https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-08T12%3A19%3A40IST&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=ZHANG%20SHAORONG&rft.date=2018-10-23&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3ECN108688821A%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