SEPARATION DEVICE FOR PROPULSION SYSTEM OF MISSILE AND MISSILE LAUNCHING SYSTEM HAVING THE SAME
Disclosed is a device for separating a missile from a propulsion system upon ejecting the missile out of a launcher, the device including a cover plate fixed to a rear end of the missile, a launch tube having the propulsion system for launching the missile, a fixing plate formed at a front side of t...
Gespeichert in:
Hauptverfasser: | , , |
---|---|
Format: | Patent |
Sprache: | eng ; fre |
Schlagworte: | |
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 | KIM, JAI HA HUR, YANG WOOK LEE, DONG JU |
description | Disclosed is a device for separating a missile from a propulsion system upon ejecting the missile out of a launcher, the device including a cover plate fixed to a rear end of the missile, a launch tube having the propulsion system for launching the missile, a fixing plate formed at a front side of the propulsion system, a locking unit inserted between the fixing plate and the cover plate for coupling and configured to separate the cover plate from the fixing plate by being separated from the cover plate due to a propulsive force of the propulsion system upon launching the missile, and a connection member configured to secure the locking unit to the launch tube.
L'invention porte sur un dispositif pour séparer un missile d'un système de propulsion lors de l'éjection du missile hors d'un lanceur, lequel dispositif comprend une plaque de recouvrement fixée à une extrémité arrière du missile, un tube de lancement ayant le système de propulsion pour lancer le missile, une plaque de fixation formée à un côté avant du système de propulsion, une unité de verrouillage insérée entre la plaque de fixation et la plaque de recouvrement pour le couplage, et configurée de façon à séparer la plaque de recouvrement de la plaque de fixation en étant séparée de la plaque de recouvrement du fait d'une force de propulsion du système de propulsion lors du lancement du missile, et un élément de liaison configuré de façon à fixer l'unité de verrouillage au tube de lancement. |
format | Patent |
fullrecord | <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_WO2011132821A1</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>WO2011132821A1</sourcerecordid><originalsourceid>FETCH-epo_espacenet_WO2011132821A13</originalsourceid><addsrcrecordid>eNrjZIgPdg1wDHIM8fT3U3BxDfN0dlVw8w9SCAjyDwj1CQaJBkcGh7j6Kvi7Kfh6Bgd7-rgqOPq5wNk-jqF-zh6efu4wdR6OYSBeiIerQrCjrysPA2taYk5xKi-U5mZQdnMNcfbQTS3Ij08tLkhMTs1LLYkP9zcyMDQ0NDayMDJ0NDQmThUAOCg0Iw</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>SEPARATION DEVICE FOR PROPULSION SYSTEM OF MISSILE AND MISSILE LAUNCHING SYSTEM HAVING THE SAME</title><source>esp@cenet</source><creator>KIM, JAI HA ; HUR, YANG WOOK ; LEE, DONG JU</creator><creatorcontrib>KIM, JAI HA ; HUR, YANG WOOK ; LEE, DONG JU</creatorcontrib><description>Disclosed is a device for separating a missile from a propulsion system upon ejecting the missile out of a launcher, the device including a cover plate fixed to a rear end of the missile, a launch tube having the propulsion system for launching the missile, a fixing plate formed at a front side of the propulsion system, a locking unit inserted between the fixing plate and the cover plate for coupling and configured to separate the cover plate from the fixing plate by being separated from the cover plate due to a propulsive force of the propulsion system upon launching the missile, and a connection member configured to secure the locking unit to the launch tube.
L'invention porte sur un dispositif pour séparer un missile d'un système de propulsion lors de l'éjection du missile hors d'un lanceur, lequel dispositif comprend une plaque de recouvrement fixée à une extrémité arrière du missile, un tube de lancement ayant le système de propulsion pour lancer le missile, une plaque de fixation formée à un côté avant du système de propulsion, une unité de verrouillage insérée entre la plaque de fixation et la plaque de recouvrement pour le couplage, et configurée de façon à séparer la plaque de recouvrement de la plaque de fixation en étant séparée de la plaque de recouvrement du fait d'une force de propulsion du système de propulsion lors du lancement du missile, et un élément de liaison configuré de façon à fixer l'unité de verrouillage au tube de lancement.</description><language>eng ; fre</language><subject>AMMUNITION ; APPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS,e.g. CANNONS ; BLASTING ; EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION ; HARPOON GUNS ; HEATING ; LAUNCHERS FOR ROCKETS OR TORPEDOES ; LIGHTING ; MECHANICAL ENGINEERING ; WEAPONS</subject><creationdate>2011</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=20111027&DB=EPODOC&CC=WO&NR=2011132821A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76419</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20111027&DB=EPODOC&CC=WO&NR=2011132821A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>KIM, JAI HA</creatorcontrib><creatorcontrib>HUR, YANG WOOK</creatorcontrib><creatorcontrib>LEE, DONG JU</creatorcontrib><title>SEPARATION DEVICE FOR PROPULSION SYSTEM OF MISSILE AND MISSILE LAUNCHING SYSTEM HAVING THE SAME</title><description>Disclosed is a device for separating a missile from a propulsion system upon ejecting the missile out of a launcher, the device including a cover plate fixed to a rear end of the missile, a launch tube having the propulsion system for launching the missile, a fixing plate formed at a front side of the propulsion system, a locking unit inserted between the fixing plate and the cover plate for coupling and configured to separate the cover plate from the fixing plate by being separated from the cover plate due to a propulsive force of the propulsion system upon launching the missile, and a connection member configured to secure the locking unit to the launch tube.
L'invention porte sur un dispositif pour séparer un missile d'un système de propulsion lors de l'éjection du missile hors d'un lanceur, lequel dispositif comprend une plaque de recouvrement fixée à une extrémité arrière du missile, un tube de lancement ayant le système de propulsion pour lancer le missile, une plaque de fixation formée à un côté avant du système de propulsion, une unité de verrouillage insérée entre la plaque de fixation et la plaque de recouvrement pour le couplage, et configurée de façon à séparer la plaque de recouvrement de la plaque de fixation en étant séparée de la plaque de recouvrement du fait d'une force de propulsion du système de propulsion lors du lancement du missile, et un élément de liaison configuré de façon à fixer l'unité de verrouillage au tube de lancement.</description><subject>AMMUNITION</subject><subject>APPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS,e.g. CANNONS</subject><subject>BLASTING</subject><subject>EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION</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>2011</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZIgPdg1wDHIM8fT3U3BxDfN0dlVw8w9SCAjyDwj1CQaJBkcGh7j6Kvi7Kfh6Bgd7-rgqOPq5wNk-jqF-zh6efu4wdR6OYSBeiIerQrCjrysPA2taYk5xKi-U5mZQdnMNcfbQTS3Ij08tLkhMTs1LLYkP9zcyMDQ0NDayMDJ0NDQmThUAOCg0Iw</recordid><startdate>20111027</startdate><enddate>20111027</enddate><creator>KIM, JAI HA</creator><creator>HUR, YANG WOOK</creator><creator>LEE, DONG JU</creator><scope>EVB</scope></search><sort><creationdate>20111027</creationdate><title>SEPARATION DEVICE FOR PROPULSION SYSTEM OF MISSILE AND MISSILE LAUNCHING SYSTEM HAVING THE SAME</title><author>KIM, JAI HA ; HUR, YANG WOOK ; LEE, DONG JU</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_WO2011132821A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre</language><creationdate>2011</creationdate><topic>AMMUNITION</topic><topic>APPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS,e.g. CANNONS</topic><topic>BLASTING</topic><topic>EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION</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>KIM, JAI HA</creatorcontrib><creatorcontrib>HUR, YANG WOOK</creatorcontrib><creatorcontrib>LEE, DONG JU</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>KIM, JAI HA</au><au>HUR, YANG WOOK</au><au>LEE, DONG JU</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>SEPARATION DEVICE FOR PROPULSION SYSTEM OF MISSILE AND MISSILE LAUNCHING SYSTEM HAVING THE SAME</title><date>2011-10-27</date><risdate>2011</risdate><abstract>Disclosed is a device for separating a missile from a propulsion system upon ejecting the missile out of a launcher, the device including a cover plate fixed to a rear end of the missile, a launch tube having the propulsion system for launching the missile, a fixing plate formed at a front side of the propulsion system, a locking unit inserted between the fixing plate and the cover plate for coupling and configured to separate the cover plate from the fixing plate by being separated from the cover plate due to a propulsive force of the propulsion system upon launching the missile, and a connection member configured to secure the locking unit to the launch tube.
L'invention porte sur un dispositif pour séparer un missile d'un système de propulsion lors de l'éjection du missile hors d'un lanceur, lequel dispositif comprend une plaque de recouvrement fixée à une extrémité arrière du missile, un tube de lancement ayant le système de propulsion pour lancer le missile, une plaque de fixation formée à un côté avant du système de propulsion, une unité de verrouillage insérée entre la plaque de fixation et la plaque de recouvrement pour le couplage, et configurée de façon à séparer la plaque de recouvrement de la plaque de fixation en étant séparée de la plaque de recouvrement du fait d'une force de propulsion du système de propulsion lors du lancement du missile, et un élément de liaison configuré de façon à fixer l'unité de verrouillage au tube de lancement.</abstract><oa>free_for_read</oa></addata></record> |
fulltext | fulltext_linktorsrc |
identifier | |
ispartof | |
issn | |
language | eng ; fre |
recordid | cdi_epo_espacenet_WO2011132821A1 |
source | esp@cenet |
subjects | AMMUNITION APPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS,e.g. CANNONS BLASTING EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION HARPOON GUNS HEATING LAUNCHERS FOR ROCKETS OR TORPEDOES LIGHTING MECHANICAL ENGINEERING WEAPONS |
title | SEPARATION DEVICE FOR PROPULSION SYSTEM OF MISSILE AND MISSILE LAUNCHING SYSTEM HAVING THE SAME |
url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-07T21%3A46%3A31IST&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=KIM,%20JAI%20HA&rft.date=2011-10-27&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3EWO2011132821A1%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 |