发明名称 Method of monitoring blade vibration in a turbine engine
摘要 <p>A rotor blade measurement system includes a microwave source (26) and a probe (28). A directional coupler (34) is attached to the source (26) and the probe (28). A detector (36) is attached to the directional coupler (34). The probe directs a microwave signal (30) toward a rotor (20) such that during rotation the rotor blade (22) will pass through the path of the microwave signal (30). As the rotor blade (22) passes, the microwave signal (30) is reflected back to the probe (28). The directional coupler (34) separates the original microwave signal (30) and the reflected signal (32). The detector (36) then determines the energy level of the reflected signal (32). As each rotor blade (22) passes the microwave signal (30) it generates a reflected signal that can be analyzed over time. From the length and shape of the waveform of the reflected signal (32) the amount of twisting and flutter in a rotor blade can be determined.</p>
申请公布号 EP1813778(B1) 申请公布日期 2015.09.09
申请号 EP20060256306 申请日期 2006.12.12
申请人 HAMILTON SUNDSTRAND CORPORATION 发明人 HOLMQUIST, ERIC B.;JALBERT, PAUL L.;VERSAILLES, RICHARD E.
分类号 G01H1/00;F01D17/02;F01D21/00 主分类号 G01H1/00
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