发明名称 BLADE TIP CLEARANCE MEASUREMENT SENSOR AND METHOD FOR GAS TURBINE ENGINES
摘要 An electromagnetic field sensor assembly for blade tip clearance measurement in a gas turbine engine is disclosed that includes a ceramic sensor body, a multi-layered wire coil wound about a distal end portion of the sensor body for producing an electromagnetic field, a ceramic well enclosing the sensor body and the coil, and a metallic housing surrounding the well and having an open distal end.
申请公布号 US2012019237(A1) 申请公布日期 2012.01.26
申请号 US201113196260 申请日期 2011.08.02
申请人 PHILLIPS RICHARD W.;STAY CHAD P.;HARRISON MARTIN;WHERRITT PETER 发明人 PHILLIPS RICHARD W.;STAY CHAD P.;HARRISON MARTIN;WHERRITT PETER
分类号 G01R33/12 主分类号 G01R33/12
代理机构 代理人
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