发明名称 Particle bed reactor-powered turbine engine
摘要 The combustion chamber and associated fuel injection and ignition equipment of a turbine engine is removed and replaced with a particle bed reactor. The reactor has central fuel elements removed to receive a shaft therein. The shaft is connected between a turbo compressor and drive turbine. Air compressed by the compressor turbine is heated by the reactor and the heated gas passes across rotor vanes of the drive turbine, the latter powering the interconnecting shaft. Exhaust gases from the drive turbine furnish resultant thrust.
申请公布号 US5255509(A) 申请公布日期 1993.10.26
申请号 US19910777928 申请日期 1991.10.17
申请人 GRUMMAN AEROSPACE CORPORATION 发明人 POWELL, JAMES R.;BELISLE, JOSEPH A.
分类号 F02C1/05;G21D5/02;(IPC1-7):F02K11/00 主分类号 F02C1/05
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