发明名称 System for controlling fuel delivery at altitude
摘要 A control system for an engine having a combustion chamber is disclosed. The control system has a first sensor, a second sensor, and a third sensor. The first sensor generates a signal indicative of ambient air pressure. The second sensor generates a signal indicative of the pressure of air entering the combustion chamber. The third sensor generates a signal indicative of a speed of the engine. The control system also has a controller configured to reference a first map to determine a first fuel limit value based on the pressure of air entering the combustion chamber and the speed of the engine, reference a second map to determine a second fuel limit value based on the pressure of air entering the combustion chamber and the speed of the engine, and determine a third fuel limit value based on the first and second fuel limit values and the ambient air pressure.
申请公布号 US7263426(B2) 申请公布日期 2007.08.28
申请号 US20050261572 申请日期 2005.10.31
申请人 CATERPILLAR INC 发明人 WITHROW MICHAEL P.;BOND MICHAEL S.;WALENTA CLAYTON D.
分类号 F02D41/40;F02D43/04 主分类号 F02D41/40
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