发明名称 GEARED TURBOFAN GAS TURBINE ENGINE WITH RELIABILITY CHECK ON GEAR CONNECTION
摘要 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.
申请公布号 US2013219913(A1) 申请公布日期 2013.08.29
申请号 US201213440085 申请日期 2012.04.05
申请人 MCCUNE MICHAEL E.;SCHWARZ FREDERICK M. 发明人 MCCUNE MICHAEL E.;SCHWARZ FREDERICK M.
分类号 F02C7/00;F02C3/06 主分类号 F02C7/00
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