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...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Hauptverfasser: 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
Format: Patent
Sprache:eng
Schlagworte:
Online-Zugang:Volltext bestellen
Tags: Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
container_end_page
container_issue
container_start_page
container_title
container_volume
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
format Patent
fullrecord <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_RU2174619C1</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>RU2174619C1</sourcerecordid><originalsourceid>FETCH-epo_espacenet_RU2174619C13</originalsourceid><addsrcrecordid>eNrjZDB3dgz29HNX8HdTCPb38XTRDQjyD3D18XH0C1EI8nf2dg1RcPVz9_Rz1VEIiQxwVVBy9nf29_dT4mFgTUvMKU7lhdLcDApuriHOHrqpBfnxqcUFicmpeakl8UGhRobmJmaGls6GxkQoAQDKAieO</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>CASING OF SOLID-PROPELLANT ROCKET ENGINE, TYPE "COCOON"</title><source>esp@cenet</source><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</creator><creatorcontrib>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</creatorcontrib><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><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&amp;date=20011010&amp;DB=EPODOC&amp;CC=RU&amp;NR=2174619C1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25542,76290</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&amp;date=20011010&amp;DB=EPODOC&amp;CC=RU&amp;NR=2174619C1$$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>
fulltext fulltext_linktorsrc
identifier
ispartof
issn
language eng
recordid cdi_epo_espacenet_RU2174619C1
source esp@cenet
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"
url https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-29T09%3A04%3A57IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-epo_EVB&rft_val_fmt=info:ofi/fmt:kev:mtx:patent&rft.genre=patent&rft.au=KARMANOV%20V.P&rft.date=2001-10-10&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3ERU2174619C1%3C/epo_EVB%3E%3Curl%3E%3C/url%3E&disable_directlink=true&sfx.directlink=off&sfx.report_link=0&rft_id=info:oai/&rft_id=info:pmid/&rfr_iscdi=true