发明名称 PRETRENCHED ROTOR FOR GAS TURBINE ENGINE
摘要 <p>A gas turbine engine according to an exemplary aspect of the present disclosure includes, among other things, a rotor having a pretrench that receives at least a portion of a tip of a stator, the portion of the tip extending radially into the pretrench.</p>
申请公布号 WO2014189564(A3) 申请公布日期 2015.02.19
申请号 WO2014US16240 申请日期 2014.02.13
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 ALVANOS, IOANNIS
分类号 F01D5/02;F04D29/26 主分类号 F01D5/02
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