Neutron gamma integrated detection system

The invention discloses a neutron gamma integrated detection system. The neutron gamma integrated detection system at least comprises a detection module, a control module, a display module and a transmission module, an unmanned aerial vehicle detection device at least comprises an unmanned aerial ve...

Ausführliche Beschreibung

Gespeichert in:

Bibliographische Detailangaben
Hauptverfasser:	YAN YUCHENG, ZHANG ZEQING, ZUO ZHUO, SUN AIKOU
Format:	Patent
Sprache:	chi ; eng
Schlagworte:	AEROPLANES AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS HELICOPTERS MEASUREMENT OF NUCLEAR OR X-RADIATION MEASURING PARACHUTES PERFORMING OPERATIONS PHYSICS TESTING 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	YAN YUCHENG ZHANG ZEQING ZUO ZHUO SUN AIKOU
description	The invention discloses a neutron gamma integrated detection system. The neutron gamma integrated detection system at least comprises a detection module, a control module, a display module and a transmission module, an unmanned aerial vehicle detection device at least comprises an unmanned aerial vehicle detection device body, an undercarriage is arranged below the unmanned aerial vehicle detection device body, and supporting legs are fixed to the two sides of the undercarriage; and a detection box is arranged between the two supporting legs, a lifting block is arranged in the detection box, and a plurality of probes are fixed to the lifting block. The unmanned aerial vehicle detection device carries the probes to detect a target site, so that potential safety hazards are reduced, the detection efficiency is improved, and meanwhile, under the action of the lifting block, the probes are located in the detection box when not used, so that the probability that the probes are damaged whennot used is reduced, the
format	Patent
fullrecord	<record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_CN112078783A</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>CN112078783A</sourcerecordid><originalsourceid>FETCH-epo_espacenet_CN112078783A3</originalsourceid><addsrcrecordid>eNrjZND0Sy0tKcrPU0hPzM1NVMjMK0lNL0osSU1RSEktSU0uyQRKFVcWl6Tm8jCwpiXmFKfyQmluBkU31xBnD93Ugvz41OKCxOTUvNSSeGc_Q0MjA3MLcwtjR2Ni1AAAJx4pEw</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>Neutron gamma integrated detection system</title><source>esp@cenet</source><creator>YAN YUCHENG ; ZHANG ZEQING ; ZUO ZHUO ; SUN AIKOU</creator><creatorcontrib>YAN YUCHENG ; ZHANG ZEQING ; ZUO ZHUO ; SUN AIKOU</creatorcontrib><description>The invention discloses a neutron gamma integrated detection system. The neutron gamma integrated detection system at least comprises a detection module, a control module, a display module and a transmission module, an unmanned aerial vehicle detection device at least comprises an unmanned aerial vehicle detection device body, an undercarriage is arranged below the unmanned aerial vehicle detection device body, and supporting legs are fixed to the two sides of the undercarriage; and a detection box is arranged between the two supporting legs, a lifting block is arranged in the detection box, and a plurality of probes are fixed to the lifting block. The unmanned aerial vehicle detection device carries the probes to detect a target site, so that potential safety hazards are reduced, the detection efficiency is improved, and meanwhile, under the action of the lifting block, the probes are located in the detection box when not used, so that the probability that the probes are damaged whennot used is reduced, the</description><language>chi ; eng</language><subject>AEROPLANES ; AIRCRAFT ; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT ; AVIATION ; COSMONAUTICS ; EQUIPMENT FOR FITTING IN OR TO AIRCRAFT ; FLYING SUITS ; HELICOPTERS ; MEASUREMENT OF NUCLEAR OR X-RADIATION ; MEASURING ; PARACHUTES ; PERFORMING OPERATIONS ; PHYSICS ; TESTING ; 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=20201215&DB=EPODOC&CC=CN&NR=112078783A$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,309,781,886,25568,76551</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20201215&DB=EPODOC&CC=CN&NR=112078783A$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>YAN YUCHENG</creatorcontrib><creatorcontrib>ZHANG ZEQING</creatorcontrib><creatorcontrib>ZUO ZHUO</creatorcontrib><creatorcontrib>SUN AIKOU</creatorcontrib><title>Neutron gamma integrated detection system</title><description>The invention discloses a neutron gamma integrated detection system. The neutron gamma integrated detection system at least comprises a detection module, a control module, a display module and a transmission module, an unmanned aerial vehicle detection device at least comprises an unmanned aerial vehicle detection device body, an undercarriage is arranged below the unmanned aerial vehicle detection device body, and supporting legs are fixed to the two sides of the undercarriage; and a detection box is arranged between the two supporting legs, a lifting block is arranged in the detection box, and a plurality of probes are fixed to the lifting block. The unmanned aerial vehicle detection device carries the probes to detect a target site, so that potential safety hazards are reduced, the detection efficiency is improved, and meanwhile, under the action of the lifting block, the probes are located in the detection box when not used, so that the probability that the probes are damaged whennot used is reduced, 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>MEASUREMENT OF NUCLEAR OR X-RADIATION</subject><subject>MEASURING</subject><subject>PARACHUTES</subject><subject>PERFORMING OPERATIONS</subject><subject>PHYSICS</subject><subject>TESTING</subject><subject>TRANSPORTING</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2020</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZND0Sy0tKcrPU0hPzM1NVMjMK0lNL0osSU1RSEktSU0uyQRKFVcWl6Tm8jCwpiXmFKfyQmluBkU31xBnD93Ugvz41OKCxOTUvNSSeGc_Q0MjA3MLcwtjR2Ni1AAAJx4pEw</recordid><startdate>20201215</startdate><enddate>20201215</enddate><creator>YAN YUCHENG</creator><creator>ZHANG ZEQING</creator><creator>ZUO ZHUO</creator><creator>SUN AIKOU</creator><scope>EVB</scope></search><sort><creationdate>20201215</creationdate><title>Neutron gamma integrated detection system</title><author>YAN YUCHENG ; ZHANG ZEQING ; ZUO ZHUO ; SUN AIKOU</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_CN112078783A3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>chi ; eng</language><creationdate>2020</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>MEASUREMENT OF NUCLEAR OR X-RADIATION</topic><topic>MEASURING</topic><topic>PARACHUTES</topic><topic>PERFORMING OPERATIONS</topic><topic>PHYSICS</topic><topic>TESTING</topic><topic>TRANSPORTING</topic><toplevel>online_resources</toplevel><creatorcontrib>YAN YUCHENG</creatorcontrib><creatorcontrib>ZHANG ZEQING</creatorcontrib><creatorcontrib>ZUO ZHUO</creatorcontrib><creatorcontrib>SUN AIKOU</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>YAN YUCHENG</au><au>ZHANG ZEQING</au><au>ZUO ZHUO</au><au>SUN AIKOU</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Neutron gamma integrated detection system</title><date>2020-12-15</date><risdate>2020</risdate><abstract>The invention discloses a neutron gamma integrated detection system. The neutron gamma integrated detection system at least comprises a detection module, a control module, a display module and a transmission module, an unmanned aerial vehicle detection device at least comprises an unmanned aerial vehicle detection device body, an undercarriage is arranged below the unmanned aerial vehicle detection device body, and supporting legs are fixed to the two sides of the undercarriage; and a detection box is arranged between the two supporting legs, a lifting block is arranged in the detection box, and a plurality of probes are fixed to the lifting block. The unmanned aerial vehicle detection device carries the probes to detect a target site, so that potential safety hazards are reduced, the detection efficiency is improved, and meanwhile, under the action of the lifting block, the probes are located in the detection box when not used, so that the probability that the probes are damaged whennot used is reduced, the</abstract><oa>free_for_read</oa></addata></record>
fulltext	fulltext_linktorsrc
identifier
ispartof
issn
language	chi ; eng
recordid	cdi_epo_espacenet_CN112078783A
source	esp@cenet
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 MEASUREMENT OF NUCLEAR OR X-RADIATION MEASURING PARACHUTES PERFORMING OPERATIONS PHYSICS TESTING TRANSPORTING
title	Neutron gamma integrated detection system
url	https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2024-12-17T03%3A14%3A24IST&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=YAN%20YUCHENG&rft.date=2020-12-15&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3ECN112078783A%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