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 US2010079136(A1) 申请公布日期 2010.04.01
申请号 US20080286262 申请日期 2008.09.29
申请人 ROSEMOUNT AEROSPACE INC. 发明人 PHILLIPS RICHARD W.;STAY CHAD P.
分类号 G01B7/00 主分类号 G01B7/00
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