发明名称 Adaptive aircraft cabin pressure control system
摘要 An adaptive aircraft cabin pressure control system is disclosed that customizes basic ascent and descent schedules to accommodate variable requirements of specific airlines, the airlines' route structures, and regional air traffic control standards. The system includes an adaptive control logic that identifies a plurality of points generated by the schedules that define ascent and descent curves corresponding to anticipated cabin pressure change rates during ascent and descent. During aircraft flight, the logic samples and stores actual cabin pressure change rates at each of the plurality of points. After the flight, the actual cabin pressure change rates are averaged and the average rate is compared to the anticipated cabin pressure change rate at each point. An offset is then calculated representing the difference between the average actual rate and an anticipated rate, and the ascent and/or descent schedules are adapted by the offset to bring the anticipated cabin pressure change rates closer to the average actual rate. After several flights, the ascent and descent schedules are customized by the adaptive control logic to a particular airline's requirements.
申请公布号 US5273486(A) 申请公布日期 1993.12.28
申请号 US19920982555 申请日期 1992.11.27
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 EMMONS, F. RICHARD;DONAHUE, THOMAS W.
分类号 B64D13/02;B64D13/04;(IPC1-7):B64D13/00 主分类号 B64D13/02
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