Aircraft launching device
The invention relates to the technical field of aerospace equipment pushing and shooting, in particular to an aircraft launching device which comprises a pushing and shooting device provided with a sliding rail and a supporting table, and the pushing and shooting device is used for moving along a pu...
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creator | GUAN JINKAI HUANG LEI GUO XINYAN DUAN SHUJING ZHU JIANGSHAN ZHAI HAITAO HUANG QIANG |
description | The invention relates to the technical field of aerospace equipment pushing and shooting, in particular to an aircraft launching device which comprises a pushing and shooting device provided with a sliding rail and a supporting table, and the pushing and shooting device is used for moving along a pushing and shooting rail; one end of the switching section is used for being detachably connected to the tail of the aircraft, and the other end of the switching section is connected to the supporting table; one end of the adapter is used for being detachably connected to the peripheral side of the aircraft, and the other end of the adapter is slidably connected to the sliding rail; in the driving stage, the aircraft is connected to the ejector through the switching section, the assembly of the ejector and the aircraft moves in an accelerated mode, and then the assembly of the ejector and the aircraft slides in an unpowered mode and enters the constant-speed movement stage. And after the aircraft reaches a specified |
format | Patent |
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And after the aircraft reaches a specified</description><language>chi ; eng</language><subject>APPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS,e.g. CANNONS ; BLASTING ; HARPOON GUNS ; HEATING ; LAUNCHERS FOR ROCKETS OR TORPEDOES ; LIGHTING ; MECHANICAL ENGINEERING ; WEAPONS</subject><creationdate>2024</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=20240308&DB=EPODOC&CC=CN&NR=117663900A$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20240308&DB=EPODOC&CC=CN&NR=117663900A$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>GUAN JINKAI</creatorcontrib><creatorcontrib>HUANG LEI</creatorcontrib><creatorcontrib>GUO XINYAN</creatorcontrib><creatorcontrib>DUAN SHUJING</creatorcontrib><creatorcontrib>ZHU JIANGSHAN</creatorcontrib><creatorcontrib>ZHAI HAITAO</creatorcontrib><creatorcontrib>HUANG QIANG</creatorcontrib><title>Aircraft launching device</title><description>The invention relates to the technical field of aerospace equipment pushing and shooting, in particular to an aircraft launching device which comprises a pushing and shooting device provided with a sliding rail and a supporting table, and the pushing and shooting device is used for moving along a pushing and shooting rail; one end of the switching section is used for being detachably connected to the tail of the aircraft, and the other end of the switching section is connected to the supporting table; one end of the adapter is used for being detachably connected to the peripheral side of the aircraft, and the other end of the adapter is slidably connected to the sliding rail; in the driving stage, the aircraft is connected to the ejector through the switching section, the assembly of the ejector and the aircraft moves in an accelerated mode, and then the assembly of the ejector and the aircraft slides in an unpowered mode and enters the constant-speed movement stage. And after the aircraft reaches a specified</description><subject>APPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS,e.g. CANNONS</subject><subject>BLASTING</subject><subject>HARPOON GUNS</subject><subject>HEATING</subject><subject>LAUNCHERS FOR ROCKETS OR TORPEDOES</subject><subject>LIGHTING</subject><subject>MECHANICAL ENGINEERING</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2024</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZJB0zCxKLkpMK1HISSzNS87IzEtXSEkty0xO5WFgTUvMKU7lhdLcDIpuriHOHrqpBfnxqcUFicmpeakl8c5-hobmZmbGlgYGjsbEqAEAGm0ilw</recordid><startdate>20240308</startdate><enddate>20240308</enddate><creator>GUAN JINKAI</creator><creator>HUANG LEI</creator><creator>GUO XINYAN</creator><creator>DUAN SHUJING</creator><creator>ZHU JIANGSHAN</creator><creator>ZHAI HAITAO</creator><creator>HUANG QIANG</creator><scope>EVB</scope></search><sort><creationdate>20240308</creationdate><title>Aircraft launching device</title><author>GUAN JINKAI ; HUANG LEI ; GUO XINYAN ; DUAN SHUJING ; ZHU JIANGSHAN ; ZHAI HAITAO ; HUANG QIANG</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_CN117663900A3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>chi ; eng</language><creationdate>2024</creationdate><topic>APPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS,e.g. CANNONS</topic><topic>BLASTING</topic><topic>HARPOON GUNS</topic><topic>HEATING</topic><topic>LAUNCHERS FOR ROCKETS OR TORPEDOES</topic><topic>LIGHTING</topic><topic>MECHANICAL ENGINEERING</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>GUAN JINKAI</creatorcontrib><creatorcontrib>HUANG LEI</creatorcontrib><creatorcontrib>GUO XINYAN</creatorcontrib><creatorcontrib>DUAN SHUJING</creatorcontrib><creatorcontrib>ZHU JIANGSHAN</creatorcontrib><creatorcontrib>ZHAI HAITAO</creatorcontrib><creatorcontrib>HUANG QIANG</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>GUAN JINKAI</au><au>HUANG LEI</au><au>GUO XINYAN</au><au>DUAN SHUJING</au><au>ZHU JIANGSHAN</au><au>ZHAI HAITAO</au><au>HUANG QIANG</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Aircraft launching device</title><date>2024-03-08</date><risdate>2024</risdate><abstract>The invention relates to the technical field of aerospace equipment pushing and shooting, in particular to an aircraft launching device which comprises a pushing and shooting device provided with a sliding rail and a supporting table, and the pushing and shooting device is used for moving along a pushing and shooting rail; one end of the switching section is used for being detachably connected to the tail of the aircraft, and the other end of the switching section is connected to the supporting table; one end of the adapter is used for being detachably connected to the peripheral side of the aircraft, and the other end of the adapter is slidably connected to the sliding rail; in the driving stage, the aircraft is connected to the ejector through the switching section, the assembly of the ejector and the aircraft moves in an accelerated mode, and then the assembly of the ejector and the aircraft slides in an unpowered mode and enters the constant-speed movement stage. And after the aircraft reaches a specified</abstract><oa>free_for_read</oa></addata></record> |
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language | chi ; eng |
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subjects | APPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS,e.g. CANNONS BLASTING HARPOON GUNS HEATING LAUNCHERS FOR ROCKETS OR TORPEDOES LIGHTING MECHANICAL ENGINEERING WEAPONS |
title | Aircraft launching device |
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