发明名称 AIRCRAFT CABIN PRESSURE CONTROLS WITH AN OPEN-LOOP MOTOR CONTROL SYSTEM: NON-LINEAR CONTROL LAW LOGIC TO COMPENSATE FOR EXCESSIVE MOTOR LOADS OR MOTOR DEGRADATION
摘要 A cabin pressure control system (CPCS) software control logic modification may boost the voltage applied to a motor when conditions are sensed indicating a combination of larger than normal cabin pressure and cabin rate error conditions. The motor may be part of an open-loop system for operating a butterfly valve that may regulate outflow from the aircraft cabin. The larger than normal cabin pressure and cabin rate error conditions may be an indication that the outflow valve is not responding in a normal manner, potentially caused by excessive loading to the motor or motor degradation. By boosting the motor voltage during excessive load conditions or with a degraded motor, CPCS performance and robustness may be improved.
申请公布号 US2008194191(A1) 申请公布日期 2008.08.14
申请号 US20070673100 申请日期 2007.02.09
申请人 HONEYWELL INTERNATIONAL INC. 发明人 MCCOY GERARD L.
分类号 B64D13/04 主分类号 B64D13/04
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