发明名称 AIRCRAFT POWER PLANT
摘要 FIELD: transport. ^ SUBSTANCE: hybrid power plant comprises high-temperature solid-oxide fuel cells with the outlet of their cathode chambers communicated via tight ducts with heat exchanger gas chambers, afterburner and micro turbine. The latter has output shaft coupled with radial-flow compressor. Inlet of said cathode chambers is communicated with air chambers of heat exchanger and compressor. Power plant comprises jet nozzle communicated with micro turbine outlet and propeller coupled with synchronous motor. The latter comprises superconducting elements cooled in rotor by liquid nitrogen. Said motor is connected via inverter to fuel cells. Tank with liquid nitrogen, motor rotor, inverter and evaporator communicated with fuel cell anode chamber inlet are concatenated via tight channels. Outlets of fuel elements are communicated with afterburner. ^ EFFECT: decreased specific weight, higher efficiency. ^ 1 dwg
申请公布号 RU2462398(C2) 申请公布日期 2012.09.27
申请号 RU20100149030 申请日期 2010.11.30
申请人 GOSUDARSTVENNOE OBRAZOVATEL'NOE UCHREZHDENIE VYSSHEGO PROFESSIONAL'NOGO OBRAZOVANIJA "OMSKIJ GOSUDARSTVENNYJ TEKHNICHESKIJ UNIVERSITET" 发明人 KUZNETSOV VIKTOR IVANOVICH;SHPAKOVSKIJ DENIS DANILOVICH
分类号 B60K6/32;B64D33/00;F01K23/10;H01M8/10 主分类号 B60K6/32
代理机构 代理人
主权项
地址