发明名称 LIQUID-PROPELLANT JET ENGINE THRUST UNIT
摘要 FIELD: engines and pumps.SUBSTANCE: proposed unit comprises bearing frame, rotary combustion chamber with nozzle, bottom protection with moving and fixed shields and clearance there between. Bottom protection is arranged nearby nozzle critical diameter and with clearance between shields at diameter smaller than nozzle OD. Fixed shield surface bulges outward while shield thickness increases toward nozzle. Bottom protection on nozzle side has surface with higher reflection of heat radiation.EFFECT: higher reliability.4 cl, 4 dwg
申请公布号 RU2469925(C1) 申请公布日期 2012.12.20
申请号 RU20110116755 申请日期 2011.04.27
申请人 OTKRYTOE AKTSIONERNOE OBSHCHESTVO "URAL'SKIJ NAUCHNO-ISSLEDOVATEL'SKIJ INSTITUT KOMPOZITSIONNYKH MATERIALOV" 发明人 SHIRJAEV MIKHAIL IVANOVICH;VEDERNIKOV VALERIJ GENNAD'EVICH;SUDJUKOV PAVEL ALEKSANDROVICH;CHUNAEV VLADIMIR JUR'EVICH;FEDOTOV JURIJ DMITRIEVICH
分类号 B64G1/00 主分类号 B64G1/00
代理机构 代理人
主权项
地址