发明名称 HIGH ENERGY PARTICLE ARRESTOR FOR AIR TURBINE STARTERS
摘要 <p>One or more particle arrestor rings are mounted in a curved radial flow portion of a gas turbine annular flow passage. The arrestor rings block line of sight paths between the turbine wheel and the annular flow passage outlet. Thus, the arrestor rings substantially inhibit relatively high energy particles from exiting the gas turbine housing, thus substantially inhibiting collateral domage to surrounding equipment and structure.</p>
申请公布号 WO2003048546(A1) 申请公布日期 2003.06.12
申请号 US2002037468 申请日期 2002.11.21
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