Unmanned aerial vehicle parachute system
The utility model relates to an unmanned aerial vehicle parachute system, including unmanned aerial vehicle, still including the control mainboard, gas generator, the parachute, the rope, the guide cylinder, the anticreep circle, the link, support and bracing piece, unmanned aerial vehicle's mi...
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creator | NIU BAOGUO ZHAO LEI |
description | The utility model relates to an unmanned aerial vehicle parachute system, including unmanned aerial vehicle, still including the control mainboard, gas generator, the parachute, the rope, the guide cylinder, the anticreep circle, the link, support and bracing piece, unmanned aerial vehicle's middle part device control mainboard, the central upper portion installation gas generator of control mainboard, gas generator's upper portion is equipped with the parachute, be equipped with the rope on the parachute, gas generator's the circumference outside is equipped with the guide cylinder, the circumference outside of guide cylinder sets up the anticreep circle, set up the link on the control mainboard between guide cylinder and the anticreep circle, stationary rope's end on the link. The utility model has the advantages of the utility model has the advantages of simple structure, the gas generator modularization can be changed, and gas generator has triggered mainboard autotrigger or remote control equipment button and has triggered, and convenient operation avoids unmanned aerial vehicle by the high altitude damage of falling under the out -of -control condition. |
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The utility model has the advantages of the utility model has the advantages of simple structure, the gas generator modularization can be changed, and gas generator has triggered mainboard autotrigger or remote control equipment button and has triggered, and convenient operation avoids unmanned aerial vehicle by the high altitude damage of falling under the out -of -control condition.</description><language>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>2015</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=20151007&DB=EPODOC&CC=CN&NR=204688423U$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25542,76516</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20151007&DB=EPODOC&CC=CN&NR=204688423U$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>NIU BAOGUO</creatorcontrib><creatorcontrib>ZHAO LEI</creatorcontrib><title>Unmanned aerial vehicle parachute system</title><description>The utility model relates to an unmanned aerial vehicle parachute system, including unmanned aerial vehicle, still including the control mainboard, gas generator, the parachute, the rope, the guide cylinder, the anticreep circle, the link, support and bracing piece, unmanned aerial vehicle's middle part device control mainboard, the central upper portion installation gas generator of control mainboard, gas generator's upper portion is equipped with the parachute, be equipped with the rope on the parachute, gas generator's the circumference outside is equipped with the guide cylinder, the circumference outside of guide cylinder sets up the anticreep circle, set up the link on the control mainboard between guide cylinder and the anticreep circle, stationary rope's end on the link. The utility model has the advantages of the utility model has the advantages of simple structure, the gas generator modularization can be changed, and gas generator has triggered mainboard autotrigger or remote control equipment button and has triggered, and convenient operation avoids unmanned aerial vehicle by the high altitude damage of falling under the out -of -control condition.</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>2015</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZNAIzctNzMtLTVFITC3KTMxRKEvNyEzOSVUoSCxKTM4oLUlVKK4sLknN5WFgTUvMKU7lhdLcDEpuriHOHrqpBfnxqcUFicmpeakl8c5-RgYmZhYWJkbGoaHGRCkCADeNKVM</recordid><startdate>20151007</startdate><enddate>20151007</enddate><creator>NIU BAOGUO</creator><creator>ZHAO LEI</creator><scope>EVB</scope></search><sort><creationdate>20151007</creationdate><title>Unmanned aerial vehicle parachute system</title><author>NIU BAOGUO ; ZHAO LEI</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_CN204688423UU3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng</language><creationdate>2015</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>NIU BAOGUO</creatorcontrib><creatorcontrib>ZHAO LEI</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>NIU BAOGUO</au><au>ZHAO LEI</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Unmanned aerial vehicle parachute system</title><date>2015-10-07</date><risdate>2015</risdate><abstract>The utility model relates to an unmanned aerial vehicle parachute system, including unmanned aerial vehicle, still including the control mainboard, gas generator, the parachute, the rope, the guide cylinder, the anticreep circle, the link, support and bracing piece, unmanned aerial vehicle's middle part device control mainboard, the central upper portion installation gas generator of control mainboard, gas generator's upper portion is equipped with the parachute, be equipped with the rope on the parachute, gas generator's the circumference outside is equipped with the guide cylinder, the circumference outside of guide cylinder sets up the anticreep circle, set up the link on the control mainboard between guide cylinder and the anticreep circle, stationary rope's end on the link. The utility model has the advantages of the utility model has the advantages of simple structure, the gas generator modularization can be changed, and gas generator has triggered mainboard autotrigger or remote control equipment button and has triggered, and convenient operation avoids unmanned aerial vehicle by the high altitude damage of falling under the out -of -control condition.</abstract><oa>free_for_read</oa></addata></record> |
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language | eng |
recordid | cdi_epo_espacenet_CN204688423UU |
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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 |
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