DUESENTRIEBWERK, INSBESONDERE RAKETENTRIEBWERK MIT EINER DUESE, DIE MIT DEM MANTEL DER BRENNKAMMER MECHANISCH UND WAERMEISOLIERT VERBUNDEN IST

The connection consists of a single connecting ring 14 fixed to the nozzle 1 and resiliently connected to the wound casing 6. The ring 14 is made from a low density insulating material, resistant to mechanical forces as well as to mechanical shocks and thermal stresses, preferably a composite materi...

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1. Verfasser:	DONGUY,PAUL
Format:	Patent
Sprache:	ger
Schlagworte:	BLASTING COMBUSTION ENGINES HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS JET-PROPULSION PLANTS LIGHTING MECHANICAL ENGINEERING WEAPONS
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creator	DONGUY,PAUL
description	The connection consists of a single connecting ring 14 fixed to the nozzle 1 and resiliently connected to the wound casing 6. The ring 14 is made from a low density insulating material, resistant to mechanical forces as well as to mechanical shocks and thermal stresses, preferably a composite material with multidirectional reinforcements and a ceramic matrix. In particular the invention relates to a solid propelled rocket motor having a hot nozzle made from a heat-conducting refractory material.
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The ring 14 is made from a low density insulating material, resistant to mechanical forces as well as to mechanical shocks and thermal stresses, preferably a composite material with multidirectional reinforcements and a ceramic matrix. In particular the invention relates to a solid propelled rocket motor having a hot nozzle made from a heat-conducting refractory material.</description><language>ger</language><subject>BLASTING ; COMBUSTION ENGINES ; HEATING ; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS ; JET-PROPULSION PLANTS ; LIGHTING ; MECHANICAL ENGINEERING ; WEAPONS</subject><creationdate>1982</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=19820304&DB=EPODOC&CC=DE&NR=3119712A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=19820304&DB=EPODOC&CC=DE&NR=3119712A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>DONGUY,PAUL</creatorcontrib><title>DUESENTRIEBWERK, INSBESONDERE RAKETENTRIEBWERK MIT EINER DUESE, DIE MIT DEM MANTEL DER BRENNKAMMER MECHANISCH UND WAERMEISOLIERT VERBUNDEN IST</title><description>The connection consists of a single connecting ring 14 fixed to the nozzle 1 and resiliently connected to the wound casing 6. The ring 14 is made from a low density insulating material, resistant to mechanical forces as well as to mechanical shocks and thermal stresses, preferably a composite material with multidirectional reinforcements and a ceramic matrix. In particular the invention relates to a solid propelled rocket motor having a hot nozzle made from a heat-conducting refractory material.</description><subject>BLASTING</subject><subject>COMBUSTION ENGINES</subject><subject>HEATING</subject><subject>HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS</subject><subject>JET-PROPULSION PLANTS</subject><subject>LIGHTING</subject><subject>MECHANICAL ENGINEERING</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>1982</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNqNizEKwkAURNNYiHqHf4BYxBRiuZsdySfZH_i7MWUQWStRQc_hmQ1iYWk1jzcz8-zlegRIVIYdoE1OLMEidOKgIDUN4k9NniOBBUqfY06O8ZEOnryRiHZCJasQaYz3E3tUtREOVU29OBoM1IND1zI00gFqJw0hDnGZzc7HyyOtvrnIaI9Y1et0v43pcT-e0jU9R4eyKHbbYmOK8o_JG3RiP6w</recordid><startdate>19820304</startdate><enddate>19820304</enddate><creator>DONGUY,PAUL</creator><scope>EVB</scope></search><sort><creationdate>19820304</creationdate><title>DUESENTRIEBWERK, INSBESONDERE RAKETENTRIEBWERK MIT EINER DUESE, DIE MIT DEM MANTEL DER BRENNKAMMER MECHANISCH UND WAERMEISOLIERT VERBUNDEN IST</title><author>DONGUY,PAUL</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_DE3119712A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>ger</language><creationdate>1982</creationdate><topic>BLASTING</topic><topic>COMBUSTION ENGINES</topic><topic>HEATING</topic><topic>HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS</topic><topic>JET-PROPULSION PLANTS</topic><topic>LIGHTING</topic><topic>MECHANICAL ENGINEERING</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>DONGUY,PAUL</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>DONGUY,PAUL</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>DUESENTRIEBWERK, INSBESONDERE RAKETENTRIEBWERK MIT EINER DUESE, DIE MIT DEM MANTEL DER BRENNKAMMER MECHANISCH UND WAERMEISOLIERT VERBUNDEN IST</title><date>1982-03-04</date><risdate>1982</risdate><abstract>The connection consists of a single connecting ring 14 fixed to the nozzle 1 and resiliently connected to the wound casing 6. The ring 14 is made from a low density insulating material, resistant to mechanical forces as well as to mechanical shocks and thermal stresses, preferably a composite material with multidirectional reinforcements and a ceramic matrix. In particular the invention relates to a solid propelled rocket motor having a hot nozzle made from a heat-conducting refractory material.</abstract><oa>free_for_read</oa></addata></record>
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language	ger
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subjects	BLASTING COMBUSTION ENGINES HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS JET-PROPULSION PLANTS LIGHTING MECHANICAL ENGINEERING WEAPONS
title	DUESENTRIEBWERK, INSBESONDERE RAKETENTRIEBWERK MIT EINER DUESE, DIE MIT DEM MANTEL DER BRENNKAMMER MECHANISCH UND WAERMEISOLIERT VERBUNDEN IST
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