发明名称 LIQUID-PROPELLANT ENGINE
摘要 FIELD: engines and pumps. ^ SUBSTANCE: invention can be used during development of alternator-free liquid propellant engines operating on cryogenic components, e.g. oxygen and hydrogen. Liquid propellant engine includes annular chamber with mixing head and plate nozzle of external expansion, shaped central body and annular critical section. Control units and power supply units, which include turbine-pump unit with turbine, are located in cavity of shaped central body. Shaped central body consists of several parts; at that, at least one part of shaped central body is provided with possibility of radial axisymmetrical rotation about longitudinal axis of shaped central body and is kinematically connected to power supply units; on its external surface there installed are blades for putting it into rotary movement, and between movable and fixed parts of shaped central body there is shaped annular slot the cavity of which is connected to outlet cavity of turbine of turbine-pump unit. ^ EFFECT: increasing specific burst of power and pressure in chamber at minimum overall dimensions, simplifying pneumatic-hydraulic circuit. ^ 1 dwg
申请公布号 RU2391538(C1) 申请公布日期 2010.06.10
申请号 RU20080149560 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 CHERNICHENKO VLADIMIR VIKTOROVICH;GOROKHOV VIKTOR DMITRIEVICH;DUBANIN VLADIMIR JUR'EVICH
分类号 F02K9/64 主分类号 F02K9/64
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