发明名称 LIQUID PROPELLANT ROCKET ENGINE
摘要 FIELD: engines and pumps. ^ SUBSTANCE: invention may be used in developing liquid-propellant rocket engines (LPE). Proposed LPE comprises chamber with nozzle, bottom protector with frame, combustion chamber swing system. Note here that nozzle is provided with flange whereto screen is attached representing truncated cone with smaller diameter secured to said flange and larger diameter secured to bottom protector or torus section with its one part secured to flange and another part attached to bottom protector frame. Said screen is made from metal thread, for example, from antirust steel grade "03Ñ189-Æÿ", of diameter 0.01<d<0.2 mm, while screen penetration makes 0.01<H<0.3, where d is thread diameter, H is screen penetration. Flange is made up of nozzle ring. Flange and bottom protector screen consist of at least two parts jointed together by split joint. ^ EFFECT: higher efficiency of heat protection, reduced overall dimensions and weight. ^ 4 cl, 1 dwg
申请公布号 RU2429371(C1) 申请公布日期 2011.09.20
申请号 RU20090146432 申请日期 2009.12.14
申请人 OTKRYTOE AKTSIONERNOE OBSHCHESTVO "KONSTRUKTORSKOE BJURO KHIMAVTOMATIKI" 发明人 GOROKHOV VIKTOR DMITRIEVICH;GOL'TSEV PAVEL MIKHAJLOVICH;DEM'JANOV IGOR' IVANOVICH;TURTUSHOV VALERIJ ANDREEVICH;SHVETS SERGEJ ANATOL'EVICH
分类号 B64G1/58;F02K9/64 主分类号 B64G1/58
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