Unmanned aerial vehicle with buffer structure
The utility model discloses an unmanned aerial vehicle with buffer structure, do you including cabin and wing, still include mini the SAR module, mini the SAR module include radar host and with radarhost signal connection's antenna, radar host sets up and is connected with unmanned aerial vehic...
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creator | YUAN LI ZHOU YUNBO LIAO XIAOLU PAN XING ZHAO ZHEN LI XIAOJUN CHENG DUOXIANG |
description | The utility model discloses an unmanned aerial vehicle with buffer structure, do you including cabin and wing, still include mini the SAR module, mini the SAR module include radar host and with radarhost signal connection's antenna, radar host sets up and is connected with unmanned aerial vehicle's data link host computer in the cabin and through the data line, the antenna includes a receiving antenna and an emit antenna, and all installs in the wing below, undercarriage 3 includes nose -gear and back undercarriage, and the nose -gear includes two stabilizer blades that lie in the fuselage both sides, and the wheel is installed to the stabilizer blade bottom, every stabilizer blade all corresponds and sets up a gas spring connecting rod, and gas spring connecting rod's one end is connected on stabilizer blade 3, and the other end is connected on the fuselage, and formation acute triangle region between gas spring connecting rod that stabilizer blade, stabilizer blade corresponded andthe fuselage. Wherein the |
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Wherein the</description><subject>AEROPLANES</subject><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>HELICOPTERS</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>eNrjZNANzctNzMtLTVFITC3KTMxRKEvNyEzOSVUozyzJUEgqTUtLLVIoLikqTS4pLUrlYWBNS8wpTuWF0twMSm6uIc4euqkF-fGpxQWJyal5qSXxzn5GBuamRsaWpsahocZEKQIANW0rOw</recordid><startdate>20180622</startdate><enddate>20180622</enddate><creator>YUAN LI</creator><creator>ZHOU YUNBO</creator><creator>LIAO XIAOLU</creator><creator>PAN XING</creator><creator>ZHAO ZHEN</creator><creator>LI XIAOJUN</creator><creator>CHENG DUOXIANG</creator><scope>EVB</scope></search><sort><creationdate>20180622</creationdate><title>Unmanned aerial vehicle with buffer structure</title><author>YUAN LI ; ZHOU YUNBO ; LIAO XIAOLU ; PAN XING ; ZHAO ZHEN ; LI XIAOJUN ; CHENG DUOXIANG</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_CN207523953UU3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>chi ; eng</language><creationdate>2018</creationdate><topic>AEROPLANES</topic><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>HELICOPTERS</topic><topic>PARACHUTES</topic><topic>PERFORMING OPERATIONS</topic><topic>TRANSPORTING</topic><toplevel>online_resources</toplevel><creatorcontrib>YUAN LI</creatorcontrib><creatorcontrib>ZHOU YUNBO</creatorcontrib><creatorcontrib>LIAO XIAOLU</creatorcontrib><creatorcontrib>PAN XING</creatorcontrib><creatorcontrib>ZHAO ZHEN</creatorcontrib><creatorcontrib>LI XIAOJUN</creatorcontrib><creatorcontrib>CHENG DUOXIANG</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>YUAN LI</au><au>ZHOU YUNBO</au><au>LIAO XIAOLU</au><au>PAN XING</au><au>ZHAO ZHEN</au><au>LI XIAOJUN</au><au>CHENG DUOXIANG</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Unmanned aerial vehicle with buffer structure</title><date>2018-06-22</date><risdate>2018</risdate><abstract>The utility model discloses an unmanned aerial vehicle with buffer structure, do you including cabin and wing, still include mini the SAR module, mini the SAR module include radar host and with radarhost signal connection's antenna, radar host sets up and is connected with unmanned aerial vehicle's data link host computer in the cabin and through the data line, the antenna includes a receiving antenna and an emit antenna, and all installs in the wing below, undercarriage 3 includes nose -gear and back undercarriage, and the nose -gear includes two stabilizer blades that lie in the fuselage both sides, and the wheel is installed to the stabilizer blade bottom, every stabilizer blade all corresponds and sets up a gas spring connecting rod, and gas spring connecting rod's one end is connected on stabilizer blade 3, and the other end is connected on the fuselage, and formation acute triangle region between gas spring connecting rod that stabilizer blade, stabilizer blade corresponded andthe fuselage. Wherein the</abstract><oa>free_for_read</oa></addata></record> |
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language | chi ; eng |
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subjects | AEROPLANES AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS HELICOPTERS PARACHUTES PERFORMING OPERATIONS TRANSPORTING |
title | Unmanned aerial vehicle with buffer structure |
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