Transport safety device in rocket launcher - involves locking bolt engaging in start tube recess
The rocket fits into a start tube (1) for launching, and in an area surrounded by the start tube is at least one radially movable locking component (11). In the start tube is at least one recess (12) in which the locking component can engage. The locking arrangement (14) works with a spring (18) so...
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| creator | RUEDIGER, MANFRED., 5210 TROISDORF, DE GOERICKE, DETLEF., 5000 KOELN, DE |
| description | The rocket fits into a start tube (1) for launching, and in an area surrounded by the start tube is at least one radially movable locking component (11). In the start tube is at least one recess (12) in which the locking component can engage. The locking arrangement (14) works with a spring (18) so that the point (13) of the locking component (11) stands outwards over the periphery of the rocket. When the rocket is introduced into the start tube, the locking component together with its point is pushed backwards. The locking arrangement (14) has a pyrotechnical power component (19) which, when initiated, causes the point of the locking component to be drawn in so far that the engagement of the locking component in the recess of the start tube is nullified. The locking component (11) is a bolt, and the recess (12) in which it engages is a radial hole. USE/ADVANTAGE - To improve the fixture of a military rocket in its launching or start tube. |
| format | Patent |
| fullrecord | <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_DE4110514A1</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>DE4110514A1</sourcerecordid><originalsourceid>FETCH-epo_espacenet_DE4110514A13</originalsourceid><addsrcrecordid>eNqNjEEKwjAURLtxIeod_gUKBusBRCseoPv6G6cxGJKS_1vw9kbwAK6GmTcz6-reZY4ypawkPELf9MDiLchHysm-oBR4jvaJTHUJlxQWCIWCfHQ0pKCE6Nh9XdmIcrnSeQBlWIhsq9XIQbD76aaia9udbzWm1EMmtojQ_tI2xuyPpjmZwx-VD0W6PKY</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>Transport safety device in rocket launcher - involves locking bolt engaging in start tube recess</title><source>esp@cenet</source><creator>RUEDIGER, MANFRED., 5210 TROISDORF, DE ; GOERICKE, DETLEF., 5000 KOELN, DE</creator><creatorcontrib>RUEDIGER, MANFRED., 5210 TROISDORF, DE ; GOERICKE, DETLEF., 5000 KOELN, DE</creatorcontrib><description>The rocket fits into a start tube (1) for launching, and in an area surrounded by the start tube is at least one radially movable locking component (11). In the start tube is at least one recess (12) in which the locking component can engage. The locking arrangement (14) works with a spring (18) so that the point (13) of the locking component (11) stands outwards over the periphery of the rocket. When the rocket is introduced into the start tube, the locking component together with its point is pushed backwards. The locking arrangement (14) has a pyrotechnical power component (19) which, when initiated, causes the point of the locking component to be drawn in so far that the engagement of the locking component in the recess of the start tube is nullified. The locking component (11) is a bolt, and the recess (12) in which it engages is a radial hole. USE/ADVANTAGE - To improve the fixture of a military rocket in its launching or start tube.</description><language>eng ; ger</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>1991</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=19911024&DB=EPODOC&CC=DE&NR=4110514A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25563,76318</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=19911024&DB=EPODOC&CC=DE&NR=4110514A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>RUEDIGER, MANFRED., 5210 TROISDORF, DE</creatorcontrib><creatorcontrib>GOERICKE, DETLEF., 5000 KOELN, DE</creatorcontrib><title>Transport safety device in rocket launcher - involves locking bolt engaging in start tube recess</title><description>The rocket fits into a start tube (1) for launching, and in an area surrounded by the start tube is at least one radially movable locking component (11). In the start tube is at least one recess (12) in which the locking component can engage. The locking arrangement (14) works with a spring (18) so that the point (13) of the locking component (11) stands outwards over the periphery of the rocket. When the rocket is introduced into the start tube, the locking component together with its point is pushed backwards. The locking arrangement (14) has a pyrotechnical power component (19) which, when initiated, causes the point of the locking component to be drawn in so far that the engagement of the locking component in the recess of the start tube is nullified. The locking component (11) is a bolt, and the recess (12) in which it engages is a radial hole. USE/ADVANTAGE - To improve the fixture of a military rocket in its launching or start tube.</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>1991</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNqNjEEKwjAURLtxIeod_gUKBusBRCseoPv6G6cxGJKS_1vw9kbwAK6GmTcz6-reZY4ypawkPELf9MDiLchHysm-oBR4jvaJTHUJlxQWCIWCfHQ0pKCE6Nh9XdmIcrnSeQBlWIhsq9XIQbD76aaia9udbzWm1EMmtojQ_tI2xuyPpjmZwx-VD0W6PKY</recordid><startdate>19911024</startdate><enddate>19911024</enddate><creator>RUEDIGER, MANFRED., 5210 TROISDORF, DE</creator><creator>GOERICKE, DETLEF., 5000 KOELN, DE</creator><scope>EVB</scope></search><sort><creationdate>19911024</creationdate><title>Transport safety device in rocket launcher - involves locking bolt engaging in start tube recess</title><author>RUEDIGER, MANFRED., 5210 TROISDORF, DE ; GOERICKE, DETLEF., 5000 KOELN, DE</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_DE4110514A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; ger</language><creationdate>1991</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>RUEDIGER, MANFRED., 5210 TROISDORF, DE</creatorcontrib><creatorcontrib>GOERICKE, DETLEF., 5000 KOELN, DE</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>RUEDIGER, MANFRED., 5210 TROISDORF, DE</au><au>GOERICKE, DETLEF., 5000 KOELN, DE</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Transport safety device in rocket launcher - involves locking bolt engaging in start tube recess</title><date>1991-10-24</date><risdate>1991</risdate><abstract>The rocket fits into a start tube (1) for launching, and in an area surrounded by the start tube is at least one radially movable locking component (11). In the start tube is at least one recess (12) in which the locking component can engage. The locking arrangement (14) works with a spring (18) so that the point (13) of the locking component (11) stands outwards over the periphery of the rocket. When the rocket is introduced into the start tube, the locking component together with its point is pushed backwards. The locking arrangement (14) has a pyrotechnical power component (19) which, when initiated, causes the point of the locking component to be drawn in so far that the engagement of the locking component in the recess of the start tube is nullified. The locking component (11) is a bolt, and the recess (12) in which it engages is a radial hole. USE/ADVANTAGE - To improve the fixture of a military rocket in its launching or start tube.</abstract><oa>free_for_read</oa></addata></record> |
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| language | eng ; ger |
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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 | Transport safety device in rocket launcher - involves locking bolt engaging in start tube recess |
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