POWER PLANT OF CONTROLLED LIQUID-PROPELLANT ROCKET VEHICLE
flying vehicles. SUBSTANCE: proposed power plant of controlled liquid-propellant rocket vehicle has several reaction chambers arranged around vehicle centerline, one0axis hinge hangers for mounting chambers on vehicle for turning to control thrust vector, and actuators with end joints for fastening...
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creator | PRISHCHEPA V.I BAKHMUTOV A.A BUKANOV V.T KLEPIKOV I.A |
description | flying vehicles. SUBSTANCE: proposed power plant of controlled liquid-propellant rocket vehicle has several reaction chambers arranged around vehicle centerline, one0axis hinge hangers for mounting chambers on vehicle for turning to control thrust vector, and actuators with end joints for fastening to chambers and vehicle body to provide turning of vehicle. Each chamber is connected with two neighbor chambers by tie-rods with end joints. Both joints can be made ball-type, or one of joints is ball-type, and the other is one-axis joint. Lengths between centers of joint tie-rods are equal to each other are parallel to lengths between centers of hangers of connected chambers. Number of actuators is equal to number of chamber. So one actuator with ball joint and/or one-axis joint belongs to each actuator. EFFECT: reduced size of power plant in diameter. 6 dwg |
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SUBSTANCE: proposed power plant of controlled liquid-propellant rocket vehicle has several reaction chambers arranged around vehicle centerline, one0axis hinge hangers for mounting chambers on vehicle for turning to control thrust vector, and actuators with end joints for fastening to chambers and vehicle body to provide turning of vehicle. Each chamber is connected with two neighbor chambers by tie-rods with end joints. Both joints can be made ball-type, or one of joints is ball-type, and the other is one-axis joint. Lengths between centers of joint tie-rods are equal to each other are parallel to lengths between centers of hangers of connected chambers. Number of actuators is equal to number of chamber. So one actuator with ball joint and/or one-axis joint belongs to each actuator. EFFECT: reduced size of power plant in diameter. 6 dwg</description><edition>7</edition><language>eng ; rus</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=20010220&DB=EPODOC&CC=RU&NR=2163304C1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20010220&DB=EPODOC&CC=RU&NR=2163304C1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>PRISHCHEPA V.I</creatorcontrib><creatorcontrib>BAKHMUTOV A.A</creatorcontrib><creatorcontrib>BUKANOV V.T</creatorcontrib><creatorcontrib>KLEPIKOV I.A</creatorcontrib><title>POWER PLANT OF CONTROLLED LIQUID-PROPELLANT ROCKET VEHICLE</title><description>flying vehicles. SUBSTANCE: proposed power plant of controlled liquid-propellant rocket vehicle has several reaction chambers arranged around vehicle centerline, one0axis hinge hangers for mounting chambers on vehicle for turning to control thrust vector, and actuators with end joints for fastening to chambers and vehicle body to provide turning of vehicle. Each chamber is connected with two neighbor chambers by tie-rods with end joints. Both joints can be made ball-type, or one of joints is ball-type, and the other is one-axis joint. Lengths between centers of joint tie-rods are equal to each other are parallel to lengths between centers of hangers of connected chambers. Number of actuators is equal to number of chamber. So one actuator with ball joint and/or one-axis joint belongs to each actuator. EFFECT: reduced size of power plant in diameter. 6 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>eNrjZLAK8A93DVII8HH0C1Hwd1Nw9vcLCfL38XF1UfDxDAz1dNENCPIPcPUBywf5O3u7hiiEuXp4Ovu48jCwpiXmFKfyQmluBgU31xBnD93Ugvz41OKCxOTUvNSS-KBQI0MzY2MDE2dDYyKUAACBUCjs</recordid><startdate>20010220</startdate><enddate>20010220</enddate><creator>PRISHCHEPA V.I</creator><creator>BAKHMUTOV A.A</creator><creator>BUKANOV V.T</creator><creator>KLEPIKOV I.A</creator><scope>EVB</scope></search><sort><creationdate>20010220</creationdate><title>POWER PLANT OF CONTROLLED LIQUID-PROPELLANT ROCKET VEHICLE</title><author>PRISHCHEPA V.I ; BAKHMUTOV A.A ; BUKANOV V.T ; KLEPIKOV I.A</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_RU2163304C13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; rus</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>PRISHCHEPA V.I</creatorcontrib><creatorcontrib>BAKHMUTOV A.A</creatorcontrib><creatorcontrib>BUKANOV V.T</creatorcontrib><creatorcontrib>KLEPIKOV I.A</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>PRISHCHEPA V.I</au><au>BAKHMUTOV A.A</au><au>BUKANOV V.T</au><au>KLEPIKOV I.A</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>POWER PLANT OF CONTROLLED LIQUID-PROPELLANT ROCKET VEHICLE</title><date>2001-02-20</date><risdate>2001</risdate><abstract>flying vehicles. SUBSTANCE: proposed power plant of controlled liquid-propellant rocket vehicle has several reaction chambers arranged around vehicle centerline, one0axis hinge hangers for mounting chambers on vehicle for turning to control thrust vector, and actuators with end joints for fastening to chambers and vehicle body to provide turning of vehicle. Each chamber is connected with two neighbor chambers by tie-rods with end joints. Both joints can be made ball-type, or one of joints is ball-type, and the other is one-axis joint. Lengths between centers of joint tie-rods are equal to each other are parallel to lengths between centers of hangers of connected chambers. Number of actuators is equal to number of chamber. So one actuator with ball joint and/or one-axis joint belongs to each actuator. EFFECT: reduced size of power plant in diameter. 6 dwg</abstract><edition>7</edition><oa>free_for_read</oa></addata></record> |
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language | eng ; rus |
recordid | cdi_epo_espacenet_RU2163304C1 |
source | esp@cenet |
subjects | BLASTING COMBUSTION ENGINES HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS JET-PROPULSION PLANTS LIGHTING MECHANICAL ENGINEERING WEAPONS |
title | POWER PLANT OF CONTROLLED LIQUID-PROPELLANT ROCKET VEHICLE |
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