发明名称 LIQUID PROPELLANT ROCKET ENGINE ANNULAR CHAMBER
摘要 FIELD: engines and pumps. ^ SUBSTANCE: proposed chamber comprises nozzle, cooled combustion chamber with mixing head arranged axially symmetric inside the nozzle and fuel and oxidiser feed branch pipes. Said combustion chamber features profiled inner wall and is arranged along its lengthwise axis. It houses cooled cylinder with one face jointed with mixing head and another face connected with the nozzle central part, to form, together with the chamber profiled inner wall, an annular critical section. Cooled cylinder outer surface and combustion chamber inner surface are furnished with lengthwise ribs. ^ EFFECT: improved heat exchange between combustion products and coolant. ^ 1 dwg
申请公布号 RU2403425(C2) 申请公布日期 2010.11.10
申请号 RU20080149584 申请日期 2008.12.17
申请人 GOSUDARSTVENNOE OBRAZOVATEL'NOE UCHREZHDENIE VYSSHEGO PROFESSIONAL'NOGO OBRAZOVANIJA "VORONEZHSKIJ GOSUDARSTVENNYJ TEKHNICHESKIJ UNIVERSITET" 发明人 GOROKHOV VIKTOR DMITRIEVICH;CHERNICHENKO VLADIMIR VIKTOROVICH;STOGNEJ VLADIMIR GRIGOR'EVICH
分类号 F02K9/64 主分类号 F02K9/64
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