发明名称 Turbo shaft engine with acoustical compression flow amplifying ramjet
摘要 A ramjet for amplifying an air stream flow rate includes a plurality of blades positioned within a turbine housing for rotation by an intake flow received through a housing inlet port. A gas generator having a primary air duct defines intake and outlet ports, the intake port receiving the intake flow from the housing. A combustion chamber is connected to the primary air duct for igniting an admixture of fuel and a portion of the intake flow to form an energized motive flow. The motive flow is discharged from the combustion chamber back into the air intake of the primary air duct so as to amplify the flow rate of incoming intake flow by momentum transfer. A portion of the motive flow is returned directly to the housing inlet port for amplifying incoming intake flow. The remaining motive flow is again combusted and used to rotate the turbine blades.
申请公布号 US6457305(B1) 申请公布日期 2002.10.01
申请号 US20010778340 申请日期 2001.02.07
申请人 SCHIERBAUM JAMES R. 发明人 SCHIERBAUM JAMES R.
分类号 F01D1/22;F02C3/14;F02K7/12;F02K7/16;(IPC1-7):F02C3/05 主分类号 F01D1/22
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