CASING OF SOLID-PROPELLANT ROCKET ENGINE, TYPE "COCOON"
rocket engines. SUBSTANCE: casing of solid-propellant rocket engine is made from composite materials and is lined with thermal protective coat. Casing is provided with load-bearing envelope with flanges and elastoflexible gaskets laid between them. Casing contains also circular band zones of attachm...
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creator | KARMANOV V.P KLJUCHNIKOV A.N KOLESNIKOV V.V MEL'NIKOV V.P KALASHNIKOV V.I GERASEV V.I JANITSKIJ A.K LOGVIN I.I MILEKHIN JU.M NEMCHAK JU.N SIDOROV V.V |
description | rocket engines. SUBSTANCE: casing of solid-propellant rocket engine is made from composite materials and is lined with thermal protective coat. Casing is provided with load-bearing envelope with flanges and elastoflexible gaskets laid between them. Casing contains also circular band zones of attachment located between thermal protective coat and inner surfaces of flanges which overlap edges of flanges. Circular band zone are made between elastoflexible gaskets and outer surfaces of flanges. Circular contact cavities are formed inside elastoflexible gaskets. Reinforcing asbestos cloth is mounted in thermal protective coat in area of bottom in such position that angles between directions of threads and meridional generatrices of casing ranges from 30 to 60 deg. EFFECT: enhanced deformability of casing in area of bottoms; enhanced resistance to burn-outs; enhanced serviceability and reliability. 3 dwg |
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SUBSTANCE: casing of solid-propellant rocket engine is made from composite materials and is lined with thermal protective coat. Casing is provided with load-bearing envelope with flanges and elastoflexible gaskets laid between them. Casing contains also circular band zones of attachment located between thermal protective coat and inner surfaces of flanges which overlap edges of flanges. Circular band zone are made between elastoflexible gaskets and outer surfaces of flanges. Circular contact cavities are formed inside elastoflexible gaskets. Reinforcing asbestos cloth is mounted in thermal protective coat in area of bottom in such position that angles between directions of threads and meridional generatrices of casing ranges from 30 to 60 deg. EFFECT: enhanced deformability of casing in area of bottoms; enhanced resistance to burn-outs; enhanced serviceability and reliability. 3 dwg</description><edition>7</edition><language>eng</language><subject>BLASTING ; COMBUSTION ENGINES ; HEATING ; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS ; JET-PROPULSION PLANTS ; LIGHTING ; MECHANICAL ENGINEERING ; WEAPONS</subject><creationdate>2001</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=20011010&DB=EPODOC&CC=RU&NR=2174619C1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25542,76290</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20011010&DB=EPODOC&CC=RU&NR=2174619C1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>KARMANOV V.P</creatorcontrib><creatorcontrib>KLJUCHNIKOV A.N</creatorcontrib><creatorcontrib>KOLESNIKOV V.V</creatorcontrib><creatorcontrib>MEL'NIKOV V.P</creatorcontrib><creatorcontrib>KALASHNIKOV V.I</creatorcontrib><creatorcontrib>GERASEV V.I</creatorcontrib><creatorcontrib>JANITSKIJ A.K</creatorcontrib><creatorcontrib>LOGVIN I.I</creatorcontrib><creatorcontrib>MILEKHIN JU.M</creatorcontrib><creatorcontrib>NEMCHAK JU.N</creatorcontrib><creatorcontrib>SIDOROV V.V</creatorcontrib><title>CASING OF SOLID-PROPELLANT ROCKET ENGINE, TYPE "COCOON"</title><description>rocket engines. SUBSTANCE: casing of solid-propellant rocket engine is made from composite materials and is lined with thermal protective coat. Casing is provided with load-bearing envelope with flanges and elastoflexible gaskets laid between them. Casing contains also circular band zones of attachment located between thermal protective coat and inner surfaces of flanges which overlap edges of flanges. Circular band zone are made between elastoflexible gaskets and outer surfaces of flanges. Circular contact cavities are formed inside elastoflexible gaskets. Reinforcing asbestos cloth is mounted in thermal protective coat in area of bottom in such position that angles between directions of threads and meridional generatrices of casing ranges from 30 to 60 deg. EFFECT: enhanced deformability of casing in area of bottoms; enhanced resistance to burn-outs; enhanced serviceability and reliability. 3 dwg</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>2001</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZDB3dgz29HNX8HdTCPb38XTRDQjyD3D18XH0C1EI8nf2dg1RcPVz9_Rz1VEIiQxwVVBy9nf29_dT4mFgTUvMKU7lhdLcDApuriHOHrqpBfnxqcUFicmpeakl8UGhRobmJmaGls6GxkQoAQDKAieO</recordid><startdate>20011010</startdate><enddate>20011010</enddate><creator>KARMANOV V.P</creator><creator>KLJUCHNIKOV A.N</creator><creator>KOLESNIKOV V.V</creator><creator>MEL'NIKOV V.P</creator><creator>KALASHNIKOV V.I</creator><creator>GERASEV V.I</creator><creator>JANITSKIJ A.K</creator><creator>LOGVIN I.I</creator><creator>MILEKHIN JU.M</creator><creator>NEMCHAK JU.N</creator><creator>SIDOROV V.V</creator><scope>EVB</scope></search><sort><creationdate>20011010</creationdate><title>CASING OF SOLID-PROPELLANT ROCKET ENGINE, TYPE "COCOON"</title><author>KARMANOV V.P ; KLJUCHNIKOV A.N ; KOLESNIKOV V.V ; MEL'NIKOV V.P ; KALASHNIKOV V.I ; GERASEV V.I ; JANITSKIJ A.K ; LOGVIN I.I ; MILEKHIN JU.M ; NEMCHAK JU.N ; SIDOROV V.V</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_RU2174619C13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng</language><creationdate>2001</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>KARMANOV V.P</creatorcontrib><creatorcontrib>KLJUCHNIKOV A.N</creatorcontrib><creatorcontrib>KOLESNIKOV V.V</creatorcontrib><creatorcontrib>MEL'NIKOV V.P</creatorcontrib><creatorcontrib>KALASHNIKOV V.I</creatorcontrib><creatorcontrib>GERASEV V.I</creatorcontrib><creatorcontrib>JANITSKIJ A.K</creatorcontrib><creatorcontrib>LOGVIN I.I</creatorcontrib><creatorcontrib>MILEKHIN JU.M</creatorcontrib><creatorcontrib>NEMCHAK JU.N</creatorcontrib><creatorcontrib>SIDOROV V.V</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>KARMANOV V.P</au><au>KLJUCHNIKOV A.N</au><au>KOLESNIKOV V.V</au><au>MEL'NIKOV V.P</au><au>KALASHNIKOV V.I</au><au>GERASEV V.I</au><au>JANITSKIJ A.K</au><au>LOGVIN I.I</au><au>MILEKHIN JU.M</au><au>NEMCHAK JU.N</au><au>SIDOROV V.V</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>CASING OF SOLID-PROPELLANT ROCKET ENGINE, TYPE "COCOON"</title><date>2001-10-10</date><risdate>2001</risdate><abstract>rocket engines. SUBSTANCE: casing of solid-propellant rocket engine is made from composite materials and is lined with thermal protective coat. Casing is provided with load-bearing envelope with flanges and elastoflexible gaskets laid between them. Casing contains also circular band zones of attachment located between thermal protective coat and inner surfaces of flanges which overlap edges of flanges. Circular band zone are made between elastoflexible gaskets and outer surfaces of flanges. Circular contact cavities are formed inside elastoflexible gaskets. Reinforcing asbestos cloth is mounted in thermal protective coat in area of bottom in such position that angles between directions of threads and meridional generatrices of casing ranges from 30 to 60 deg. EFFECT: enhanced deformability of casing in area of bottoms; enhanced resistance to burn-outs; enhanced serviceability and reliability. 3 dwg</abstract><edition>7</edition><oa>free_for_read</oa></addata></record> |
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subjects | BLASTING COMBUSTION ENGINES HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS JET-PROPULSION PLANTS LIGHTING MECHANICAL ENGINEERING WEAPONS |
title | CASING OF SOLID-PROPELLANT ROCKET ENGINE, TYPE "COCOON" |
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