AIRCRAFT CABIN PRESSURE CONTROL SYSTEM AND METHOD FOR AIRCRAFT HAVING MULTIPLE DIFFERENTIAL PRESSURE LIMITS

摘要

A cabin pressure control system and method controls aircraft cabin pressure in aircraft having multiple cabin-to-atmosphere differential pressure limits. The control system and method ensures that the cabin pressure is automatically controlled during typical in-flight operations, as well as during pressurized landing operations and/or pressurized take-off operations, without exceeding the different cabin-to-atmosphere differential pressure limits that may be associated with these different operations.