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 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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