发明名称 Automatic aircraft engine fuel mixture optimization
摘要 A computer-assisted method for controlling the delivery of fuel to an engine. The method includes receiving an input signal indicative of a sensed speed of the engine, validating that the engine is in a cruise power mode based on the input signal, and providing an output signal based on a sensed engine operating condition for adaptively controlling the fuel delivery to the engine when the engine is operating in the cruise power mode. Also, a fuel control module. The fuel control module includes a first portion configured for receiving an input signal indicative of a sensed speed of an engine, a second portion configured for validating that the engine is operating in a cruise power mode based on the input signal, and a third portion configured for providing an output signal based on a sensed engine operating condition for controlling fuel delivery to the engine when the engine is operating in the cruise power mode.
申请公布号 US6317680(B1) 申请公布日期 2001.11.13
申请号 US19990268181 申请日期 1999.03.15
申请人 AEROSANCE, INC. 发明人 LUTTRELL JABE R.;SMITH STEPHEN;SANTORO STEPHEN
分类号 F02D41/14;F02D41/24;(IPC1-7):F02D43/04 主分类号 F02D41/14
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