Aircraft wing external hanging structure
The invention belongs to the aviation geophysical prospecting cable hanging technology, and relates to an aircraft wing external hanging structure. The structure comprises a connecting rod assembly, ahanging cabin body, a wing fixing connector and a hanging fixing connector, the connecting rod assem...
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| creator | GAO WANCHUN GUO YUCHUN JIANG XIAOLONG ZHAO SIHUI LIU RUI HAO WANGJUN MA YANPENG LIU ZHIFANG ZHANG KEXIAO YIN HONGSHAN WANG DONGBING HAO GANGYONG LIU BAIQI LI YANG WANG FANGFANG YU LIN ZHANG YU WANG GUOKU |
| description | The invention belongs to the aviation geophysical prospecting cable hanging technology, and relates to an aircraft wing external hanging structure. The structure comprises a connecting rod assembly, ahanging cabin body, a wing fixing connector and a hanging fixing connector, the connecting rod assembly comprises a plurality of connecting rods, one end of each connecting rod is fixedly connected with a wing through the wing fixing connector, the other end of each connecting rod is fixedly connected with the hanging cabin body through the hanging fixing connector, and the angles of the connecting rods can be adjusted.structure According to the invention, connection modes such as rod system and cable clamping plate fixing are adopted, so that the single-side weight of the external suspensionof the wing is effectively controlled, and the bare-handed carrying operation requirement of personnel is met. And in addition, through rod system connection, aerodynamic loads generated by externalhanging of the wings are ef |
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The structure comprises a connecting rod assembly, ahanging cabin body, a wing fixing connector and a hanging fixing connector, the connecting rod assembly comprises a plurality of connecting rods, one end of each connecting rod is fixedly connected with a wing through the wing fixing connector, the other end of each connecting rod is fixedly connected with the hanging cabin body through the hanging fixing connector, and the angles of the connecting rods can be adjusted.structure According to the invention, connection modes such as rod system and cable clamping plate fixing are adopted, so that the single-side weight of the external suspensionof the wing is effectively controlled, and the bare-handed carrying operation requirement of personnel is met. And in addition, through rod system connection, aerodynamic loads generated by externalhanging of the wings are ef</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>2021</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=20210226&DB=EPODOC&CC=CN&NR=112407309A$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20210226&DB=EPODOC&CC=CN&NR=112407309A$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>GAO WANCHUN</creatorcontrib><creatorcontrib>GUO YUCHUN</creatorcontrib><creatorcontrib>JIANG XIAOLONG</creatorcontrib><creatorcontrib>ZHAO SIHUI</creatorcontrib><creatorcontrib>LIU RUI</creatorcontrib><creatorcontrib>HAO WANGJUN</creatorcontrib><creatorcontrib>MA YANPENG</creatorcontrib><creatorcontrib>LIU ZHIFANG</creatorcontrib><creatorcontrib>ZHANG KEXIAO</creatorcontrib><creatorcontrib>YIN HONGSHAN</creatorcontrib><creatorcontrib>WANG DONGBING</creatorcontrib><creatorcontrib>HAO GANGYONG</creatorcontrib><creatorcontrib>LIU BAIQI</creatorcontrib><creatorcontrib>LI YANG</creatorcontrib><creatorcontrib>WANG FANGFANG</creatorcontrib><creatorcontrib>YU LIN</creatorcontrib><creatorcontrib>ZHANG YU</creatorcontrib><creatorcontrib>WANG GUOKU</creatorcontrib><title>Aircraft wing external hanging structure</title><description>The invention belongs to the aviation geophysical prospecting cable hanging technology, and relates to an aircraft wing external hanging structure. The structure comprises a connecting rod assembly, ahanging cabin body, a wing fixing connector and a hanging fixing connector, the connecting rod assembly comprises a plurality of connecting rods, one end of each connecting rod is fixedly connected with a wing through the wing fixing connector, the other end of each connecting rod is fixedly connected with the hanging cabin body through the hanging fixing connector, and the angles of the connecting rods can be adjusted.structure According to the invention, connection modes such as rod system and cable clamping plate fixing are adopted, so that the single-side weight of the external suspensionof the wing is effectively controlled, and the bare-handed carrying operation requirement of personnel is met. And in addition, through rod system connection, aerodynamic loads generated by externalhanging of the wings are ef</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>2021</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZNBwzCxKLkpMK1Eoz8xLV0itKEktykvMUchIzEsHCRSXFJUml5QWpfIwsKYl5hSn8kJpbgZFN9cQZw_d1IL8-NTigsTk1LzUknhnP0NDIxMDc2MDS0djYtQAAO4lKJY</recordid><startdate>20210226</startdate><enddate>20210226</enddate><creator>GAO WANCHUN</creator><creator>GUO YUCHUN</creator><creator>JIANG XIAOLONG</creator><creator>ZHAO SIHUI</creator><creator>LIU RUI</creator><creator>HAO WANGJUN</creator><creator>MA YANPENG</creator><creator>LIU ZHIFANG</creator><creator>ZHANG KEXIAO</creator><creator>YIN HONGSHAN</creator><creator>WANG DONGBING</creator><creator>HAO GANGYONG</creator><creator>LIU BAIQI</creator><creator>LI YANG</creator><creator>WANG FANGFANG</creator><creator>YU LIN</creator><creator>ZHANG YU</creator><creator>WANG GUOKU</creator><scope>EVB</scope></search><sort><creationdate>20210226</creationdate><title>Aircraft wing external hanging structure</title><author>GAO WANCHUN ; GUO YUCHUN ; JIANG XIAOLONG ; ZHAO SIHUI ; LIU RUI ; HAO WANGJUN ; MA YANPENG ; LIU ZHIFANG ; ZHANG KEXIAO ; YIN HONGSHAN ; WANG DONGBING ; HAO GANGYONG ; LIU BAIQI ; LI YANG ; WANG FANGFANG ; YU LIN ; ZHANG YU ; WANG GUOKU</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_CN112407309A3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>chi ; eng</language><creationdate>2021</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>GAO WANCHUN</creatorcontrib><creatorcontrib>GUO YUCHUN</creatorcontrib><creatorcontrib>JIANG XIAOLONG</creatorcontrib><creatorcontrib>ZHAO SIHUI</creatorcontrib><creatorcontrib>LIU RUI</creatorcontrib><creatorcontrib>HAO WANGJUN</creatorcontrib><creatorcontrib>MA YANPENG</creatorcontrib><creatorcontrib>LIU ZHIFANG</creatorcontrib><creatorcontrib>ZHANG KEXIAO</creatorcontrib><creatorcontrib>YIN HONGSHAN</creatorcontrib><creatorcontrib>WANG DONGBING</creatorcontrib><creatorcontrib>HAO GANGYONG</creatorcontrib><creatorcontrib>LIU BAIQI</creatorcontrib><creatorcontrib>LI YANG</creatorcontrib><creatorcontrib>WANG FANGFANG</creatorcontrib><creatorcontrib>YU LIN</creatorcontrib><creatorcontrib>ZHANG YU</creatorcontrib><creatorcontrib>WANG GUOKU</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>GAO WANCHUN</au><au>GUO YUCHUN</au><au>JIANG XIAOLONG</au><au>ZHAO SIHUI</au><au>LIU RUI</au><au>HAO WANGJUN</au><au>MA YANPENG</au><au>LIU ZHIFANG</au><au>ZHANG KEXIAO</au><au>YIN HONGSHAN</au><au>WANG DONGBING</au><au>HAO GANGYONG</au><au>LIU BAIQI</au><au>LI YANG</au><au>WANG FANGFANG</au><au>YU LIN</au><au>ZHANG YU</au><au>WANG GUOKU</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Aircraft wing external hanging structure</title><date>2021-02-26</date><risdate>2021</risdate><abstract>The invention belongs to the aviation geophysical prospecting cable hanging technology, and relates to an aircraft wing external hanging structure. The structure comprises a connecting rod assembly, ahanging cabin body, a wing fixing connector and a hanging fixing connector, the connecting rod assembly comprises a plurality of connecting rods, one end of each connecting rod is fixedly connected with a wing through the wing fixing connector, the other end of each connecting rod is fixedly connected with the hanging cabin body through the hanging fixing connector, and the angles of the connecting rods can be adjusted.structure According to the invention, connection modes such as rod system and cable clamping plate fixing are adopted, so that the single-side weight of the external suspensionof the wing is effectively controlled, and the bare-handed carrying operation requirement of personnel is met. And in addition, through rod system connection, aerodynamic loads generated by externalhanging of the wings are ef</abstract><oa>free_for_read</oa></addata></record> |
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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 | Aircraft wing external hanging structure |
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