<p>A sensor assembly for a gas turbine engine (100) includes a telemetry module (130) mounted at a rotor bearing compartment (118) for sensing engine operational parameters and a cooling system for cooling the telemetry module separate from a rotor bearing lubricant flow.
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申请公布号
EP1843011(A3)
申请公布日期
2011.08.03
申请号
EP20070251468
申请日期
2007.04.02
申请人
UNITED TECHNOLOGIES CORPORATION
发明人
BABU, MICHAEL;WALKER, MICHAEL IAN;SHERIDAN, WILLIAM G.;DOMONKOS, RICHARD E.;CHELTE, MICHAEL T.
