发明名称 Turbocharger with downstream pressure-gain combustor
摘要 A pressure-gain combustor is placed in the exhaust path of the turbine in a turbocharger or turbine engine, thus increasing the pressure drop in the engine. The increased pressure drop in the engine leads to increased turbine power output when the turbocharger or turbine engine is operating under no-load or partial load conditions, thus reducing the problem of turbo lag.
申请公布号 US5014516(A) 申请公布日期 1991.05.14
申请号 US19890322284 申请日期 1989.03.13
申请人 TIERNAY TURBINES 发明人 SHERIKAR, SANJAY V.
分类号 F02B37/00;F02B37/12;F02C6/00 主分类号 F02B37/00
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