초록 ▼

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

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.

대표청구항 ▼

An adaptive aircraft cabin pressure control system for controlling cabin pressure change rates during a flight of an aircraft comprising: a. a controller that receives sensed information identifying ambient air pressure outside the aircraft (Pa), pressure inside the aircraft cabin (Pc), and informat

An adaptive aircraft cabin pressure control system for controlling cabin pressure change rates during a flight of an aircraft comprising: a. a controller that receives sensed information identifying ambient air pressure outside the aircraft (Pa), pressure inside the aircraft cabin (Pc), and information identifying pressure at a landing site (Pld), ambient pressure at cruise altitude (Pcr) and desired cabin pressure at cruise altitude (Pcc), adapted to produce output command signals; b. an outflow valve that receives output command signals from the controller adapted to modulate flow of pressurized air out of the cabin to change cabin pressure; c. schedules stored in the controller adapted to generate anticipated cabin pressure change rates for the flight as a function of Pa, Pc, Pld, Pcr and Pcc so that the controller executes the rates as output command signals; and d. adaptive control means stored in the controller for adapting cabin pressure change rates generated by the schedules closer to actual cabin pressure change rates experienced during the flight, comprising: i. means for identifying a plurality of points that define variable cabin pressure change rate curves representing the anticipated cabin pressure change rates generated by the schedules; ii. means for sensing and storing actual cabin pressure change rates at each of the plurality of points during the flight; iii. means for averaging the stored actual cabin pressure change rates; iv. means for comparing the average actual cabin pressure change rate to cabin pressure change rates anticipated by the schedules at each of the plurality of points; v. means for generating an offset for each of the plurality of points to adapt the cabin pressure change rate anticipated by the schedules at each point closer to the average actual cabin pressure change rate; and vi. means for adapting the cabin pressure change rate anticipated by the schedules for each of the plurality of points by the offset so that the anticipated cabin pressure change rates at each point are closer to the average actual cabin pressure change rate.