CH606969
An improved device for breaking the connection between an electric control system and a missile by separating a control cable or umbilical cord joining the missile to its launcher housing during launch. A plurality of continuous, flexible conductors are passed through openings in a non-conductive in...
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creator | GUNNAR JACOBSON LARS EVERT FREDRIKSSON VRETA KLOSTER OLOF BERTIL OLSSON |
description | An improved device for breaking the connection between an electric control system and a missile by separating a control cable or umbilical cord joining the missile to its launcher housing during launch. A plurality of continuous, flexible conductors are passed through openings in a non-conductive insert in the surface of the missile. Because the conductors are secured to both the missile and the housing on opposite sides of the insert, they are tensioned against and bent over the outer edge of the opening during launch and broken due to the concentration of tensile and bending stress at the point of contact. |
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A plurality of continuous, flexible conductors are passed through openings in a non-conductive insert in the surface of the missile. Because the conductors are secured to both the missile and the housing on opposite sides of the insert, they are tensioned against and bent over the outer edge of the opening during launch and broken due to the concentration of tensile and bending stress at the point of contact.</description><language>eng</language><subject>AIRCRAFT ; APPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS,e.g. CANNONS ; AVIATION ; BASIC ELECTRIC ELEMENTS ; BLASTING ; CABLES ; CONDUCTORS ; COSMONAUTICS ; ELECTRICITY ; HARPOON GUNS ; HEATING ; INSULATORS ; LAUNCHERS FOR ROCKETS OR TORPEDOES ; LIGHTING ; MECHANICAL ENGINEERING ; PERFORMING OPERATIONS ; SELECTION OF MATERIALS FOR THEIR CONDUCTIVE, INSULATING ORDIELECTRIC PROPERTIES ; TRANSPORTING ; VEHICLES OR EQUIPMENT THEREFOR ; WEAPONS</subject><creationdate>1978</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=19781130&DB=EPODOC&CC=CH&NR=606969A5$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25542,76290</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=19781130&DB=EPODOC&CC=CH&NR=606969A5$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>GUNNAR JACOBSON</creatorcontrib><creatorcontrib>LARS EVERT FREDRIKSSON</creatorcontrib><creatorcontrib>VRETA KLOSTER</creatorcontrib><creatorcontrib>OLOF BERTIL OLSSON</creatorcontrib><title>CH606969</title><description>An improved device for breaking the connection between an electric control system and a missile by separating a control cable or umbilical cord joining the missile to its launcher housing during launch. A plurality of continuous, flexible conductors are passed through openings in a non-conductive insert in the surface of the missile. Because the conductors are secured to both the missile and the housing on opposite sides of the insert, they are tensioned against and bent over the outer edge of the opening during launch and broken due to the concentration of tensile and bending stress at the point of contact.</description><subject>AIRCRAFT</subject><subject>APPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS,e.g. CANNONS</subject><subject>AVIATION</subject><subject>BASIC ELECTRIC ELEMENTS</subject><subject>BLASTING</subject><subject>CABLES</subject><subject>CONDUCTORS</subject><subject>COSMONAUTICS</subject><subject>ELECTRICITY</subject><subject>HARPOON GUNS</subject><subject>HEATING</subject><subject>INSULATORS</subject><subject>LAUNCHERS FOR ROCKETS OR TORPEDOES</subject><subject>LIGHTING</subject><subject>MECHANICAL ENGINEERING</subject><subject>PERFORMING OPERATIONS</subject><subject>SELECTION OF MATERIALS FOR THEIR CONDUCTIVE, INSULATING ORDIELECTRIC PROPERTIES</subject><subject>TRANSPORTING</subject><subject>VEHICLES OR EQUIPMENT THEREFOR</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>1978</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZOBw9jAzMLM0s-RhYE1LzClO5YXS3Azybq4hzh66qQX58anFBYnJqXmpJfEw5Y6mxoRVAACPGBoA</recordid><startdate>19781130</startdate><enddate>19781130</enddate><creator>GUNNAR JACOBSON</creator><creator>LARS EVERT FREDRIKSSON</creator><creator>VRETA KLOSTER</creator><creator>OLOF BERTIL OLSSON</creator><scope>EVB</scope></search><sort><creationdate>19781130</creationdate><title>CH606969</title><author>GUNNAR JACOBSON ; LARS EVERT FREDRIKSSON ; VRETA KLOSTER ; OLOF BERTIL OLSSON</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_CH606969A53</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng</language><creationdate>1978</creationdate><topic>AIRCRAFT</topic><topic>APPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS,e.g. CANNONS</topic><topic>AVIATION</topic><topic>BASIC ELECTRIC ELEMENTS</topic><topic>BLASTING</topic><topic>CABLES</topic><topic>CONDUCTORS</topic><topic>COSMONAUTICS</topic><topic>ELECTRICITY</topic><topic>HARPOON GUNS</topic><topic>HEATING</topic><topic>INSULATORS</topic><topic>LAUNCHERS FOR ROCKETS OR TORPEDOES</topic><topic>LIGHTING</topic><topic>MECHANICAL ENGINEERING</topic><topic>PERFORMING OPERATIONS</topic><topic>SELECTION OF MATERIALS FOR THEIR CONDUCTIVE, INSULATING ORDIELECTRIC PROPERTIES</topic><topic>TRANSPORTING</topic><topic>VEHICLES OR EQUIPMENT THEREFOR</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>GUNNAR JACOBSON</creatorcontrib><creatorcontrib>LARS EVERT FREDRIKSSON</creatorcontrib><creatorcontrib>VRETA KLOSTER</creatorcontrib><creatorcontrib>OLOF BERTIL OLSSON</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>GUNNAR JACOBSON</au><au>LARS EVERT FREDRIKSSON</au><au>VRETA KLOSTER</au><au>OLOF BERTIL OLSSON</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>CH606969</title><date>1978-11-30</date><risdate>1978</risdate><abstract>An improved device for breaking the connection between an electric control system and a missile by separating a control cable or umbilical cord joining the missile to its launcher housing during launch. A plurality of continuous, flexible conductors are passed through openings in a non-conductive insert in the surface of the missile. Because the conductors are secured to both the missile and the housing on opposite sides of the insert, they are tensioned against and bent over the outer edge of the opening during launch and broken due to the concentration of tensile and bending stress at the point of contact.</abstract><oa>free_for_read</oa></addata></record> |
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subjects | AIRCRAFT APPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS,e.g. CANNONS AVIATION BASIC ELECTRIC ELEMENTS BLASTING CABLES CONDUCTORS COSMONAUTICS ELECTRICITY HARPOON GUNS HEATING INSULATORS LAUNCHERS FOR ROCKETS OR TORPEDOES LIGHTING MECHANICAL ENGINEERING PERFORMING OPERATIONS SELECTION OF MATERIALS FOR THEIR CONDUCTIVE, INSULATING ORDIELECTRIC PROPERTIES TRANSPORTING VEHICLES OR EQUIPMENT THEREFOR WEAPONS |
title | CH606969 |
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