发明名称 GEARED TURBOFAN GAS TURBINE ENGINE WITH RELIABILITY CHECK ON GEAR CONNECTION
摘要 <p>A gas turbine engine includes a fan and a compressor. A combustor drives a turbine, including a first turbine with a shaft to drive the compressor. A fan drive turbine drives the fan through a speed reduction. A sensor senses a speed of rotation of the fan and communicates sensed speed information to a control. The control develops an expected speed for the fan. A problem is identified should the sensed speed be less than the expected speed by more than a predetermined amount. A method is also described.</p>
申请公布号 SG11201405922S(A) 申请公布日期 2014.10.30
申请号 SG11201405922S 申请日期 2013.04.02
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 MCCUNE, MICHAEL E.;SCHWARZ, FREDERICK M.
分类号 F02C7/36;F01D21/00 主分类号 F02C7/36
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