发明名称 Air turbine starter assembly
摘要 An aircraft engine starter assembly provides for liquid cooling of the clutch assembly and overrunning engine by integrating a pitot pump in the system. The system includes a starter motor, a torque transfer connection, a clutch assembly and the pitot pump. The torque transfer connection is adapted to be coupled to the aircraft engine. The clutch assembly is coupled to one of the starter motor or the torque transfer connection. The pitot pump is coupled to one or both of the torque transfer or the clutch assembly via a first oil line and a second oil line. The pitot pump comprises a pitot tube in fluidic communication with an oil reservoir for the delivery of oil under pressure to lubricate one or both of the torque transfer or the clutch assembly.
申请公布号 US2007199785(A1) 申请公布日期 2007.08.30
申请号 US20060364140 申请日期 2006.02.27
申请人 HONEYWELL INTERNATIONAL, INC. 发明人 LANE GLENN H.;LANGSTON TODD A.;BURNS MICHAEL J.
分类号 F16D41/12 主分类号 F16D41/12
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