SEPARATION SYSTEM FOR SEPARABLE ELEMENTS OF A SPACECRAFT OR LAUNCHER

Separation system (1) for separable elements of spacecrafts and launchers that comprises an upper ring (5), a lower ring (6) and a band (2) with an inner channel (3) which houses a plurality of slidable clamps (4), which are applied against the upper ring (5) and the lower ring (6) that form the con...

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1. Verfasser:	RIVAS SÁNCHEZ, Francisco Javier
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AIRCRAFT AMMUNITION AVIATION BLASTING COSMONAUTICS EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION HEATING LIGHTING MECHANICAL ENGINEERING PERFORMING OPERATIONS TRANSPORTING VEHICLES OR EQUIPMENT THEREFOR WEAPONS
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creator	RIVAS SÁNCHEZ, Francisco Javier
description	Separation system (1) for separable elements of spacecrafts and launchers that comprises an upper ring (5), a lower ring (6) and a band (2) with an inner channel (3) which houses a plurality of slidable clamps (4), which are applied against the upper ring (5) and the lower ring (6) that form the connection interface between the two separable elements, and a device (19) for joining/separating the ends of the band (2), both the upper ring (5) and the lower ring (6) comprising an outer protruding element (7, 8) with a wedged section to be lodged in the clamps (4), wherein the upper ring (5) additionally comprises an inner protruding element (9) with a wedged section that matches a channel shaped section (10) in the lower ring (6), the lower ring (6) also comprising an outer portion (11) including the outer protruding element (8) with a wedged section and the channel shaped section (10), the outer portion (11) protruding from a main part (12) of the lower ring (6) and being spaced from it creating a groove (13).
format	Patent
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fre ; ger</language><subject>AIRCRAFT ; AMMUNITION ; AVIATION ; BLASTING ; COSMONAUTICS ; EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION ; HEATING ; LIGHTING ; MECHANICAL ENGINEERING ; PERFORMING OPERATIONS ; TRANSPORTING ; VEHICLES OR EQUIPMENT THEREFOR ; WEAPONS</subject><creationdate>2019</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=20190102&DB=EPODOC&CC=EP&NR=3225558B1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25542,76289</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20190102&DB=EPODOC&CC=EP&NR=3225558B1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>RIVAS SÁNCHEZ, Francisco Javier</creatorcontrib><title>SEPARATION SYSTEM FOR SEPARABLE ELEMENTS OF A SPACECRAFT OR LAUNCHER</title><description>Separation system (1) for separable elements of spacecrafts and launchers that comprises an upper ring (5), a lower ring (6) and a band (2) with an inner channel (3) which houses a plurality of slidable clamps (4), which are applied against the upper ring (5) and the lower ring (6) that form the connection interface between the two separable elements, and a device (19) for joining/separating the ends of the band (2), both the upper ring (5) and the lower ring (6) comprising an outer protruding element (7, 8) with a wedged section to be lodged in the clamps (4), wherein the upper ring (5) additionally comprises an inner protruding element (9) with a wedged section that matches a channel shaped section (10) in the lower ring (6), the lower ring (6) also comprising an outer portion (11) including the outer protruding element (8) with a wedged section and the channel shaped section (10), the outer portion (11) protruding from a main part (12) of the lower ring (6) and being spaced from it creating a groove (13).</description><subject>AIRCRAFT</subject><subject>AMMUNITION</subject><subject>AVIATION</subject><subject>BLASTING</subject><subject>COSMONAUTICS</subject><subject>EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION</subject><subject>HEATING</subject><subject>LIGHTING</subject><subject>MECHANICAL ENGINEERING</subject><subject>PERFORMING OPERATIONS</subject><subject>TRANSPORTING</subject><subject>VEHICLES OR EQUIPMENT THEREFOR</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2019</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZHAJdg1wDHIM8fT3UwiODA5x9VVw8w9SgIg6-bgquPq4-rr6hQQr-LspOCoEBzg6uzoHObqFKABV-TiG-jl7uAbxMLCmJeYUp_JCaW4GBTfXEGcP3dSC_PjU4oLE5NS81JJ41wBjIyNTU1MLJ0NjIpQAAP0QK0Q</recordid><startdate>20190102</startdate><enddate>20190102</enddate><creator>RIVAS SÁNCHEZ, Francisco Javier</creator><scope>EVB</scope></search><sort><creationdate>20190102</creationdate><title>SEPARATION SYSTEM FOR SEPARABLE ELEMENTS OF A SPACECRAFT OR LAUNCHER</title><author>RIVAS SÁNCHEZ, Francisco Javier</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_EP3225558B13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre ; ger</language><creationdate>2019</creationdate><topic>AIRCRAFT</topic><topic>AMMUNITION</topic><topic>AVIATION</topic><topic>BLASTING</topic><topic>COSMONAUTICS</topic><topic>EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION</topic><topic>HEATING</topic><topic>LIGHTING</topic><topic>MECHANICAL ENGINEERING</topic><topic>PERFORMING OPERATIONS</topic><topic>TRANSPORTING</topic><topic>VEHICLES OR EQUIPMENT THEREFOR</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>RIVAS SÁNCHEZ, Francisco Javier</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>RIVAS SÁNCHEZ, Francisco Javier</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>SEPARATION SYSTEM FOR SEPARABLE ELEMENTS OF A SPACECRAFT OR LAUNCHER</title><date>2019-01-02</date><risdate>2019</risdate><abstract>Separation system (1) for separable elements of spacecrafts and launchers that comprises an upper ring (5), a lower ring (6) and a band (2) with an inner channel (3) which houses a plurality of slidable clamps (4), which are applied against the upper ring (5) and the lower ring (6) that form the connection interface between the two separable elements, and a device (19) for joining/separating the ends of the band (2), both the upper ring (5) and the lower ring (6) comprising an outer protruding element (7, 8) with a wedged section to be lodged in the clamps (4), wherein the upper ring (5) additionally comprises an inner protruding element (9) with a wedged section that matches a channel shaped section (10) in the lower ring (6), the lower ring (6) also comprising an outer portion (11) including the outer protruding element (8) with a wedged section and the channel shaped section (10), the outer portion (11) protruding from a main part (12) of the lower ring (6) and being spaced from it creating a groove (13).</abstract><oa>free_for_read</oa></addata></record>
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language	eng ; fre ; ger
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subjects	AIRCRAFT AMMUNITION AVIATION BLASTING COSMONAUTICS EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION HEATING LIGHTING MECHANICAL ENGINEERING PERFORMING OPERATIONS TRANSPORTING VEHICLES OR EQUIPMENT THEREFOR WEAPONS
title	SEPARATION SYSTEM FOR SEPARABLE ELEMENTS OF A SPACECRAFT OR LAUNCHER
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