发明名称 Method and system for inductive sensing of blades in a turbine engine
摘要 A method is provided for determining timing points indicative of the passage of a blade in a turbine engine. The method comprises the steps of: providing a first sensing coil proximate to a path of the blade, providing a second sensing coil proximate to the path of the blade, the second sensing coil spaced from the first sensing coil in a direction parallel to the path of the blade, and comparing a signal generated in the first sensing coil with a signal generated in the second sensing coil to derive a timing point indicative of the passage of the blade.
申请公布号 GB2482468(B) 申请公布日期 2013.12.18
申请号 GB20100008282 申请日期 2010.05.18
申请人 WESTON AEROSPACE LIMITED 发明人 ANTHONY PALMER;MATTHEW CLIFTON-WELKER;LESLIE WILLIAM ALLEN
分类号 G01D5/20;F01D21/00;G01D3/028;G01D5/22;G01P3/488;G01P3/489;G01P3/49;G01P13/00 主分类号 G01D5/20
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