Abstract:Based on the safety requirements of airworthiness clauses for doors, civil aircraft doors generally use lock mechanisms and lock sensors to achieve locking and indication functions. Due to the deviation between locking/unlocking status of lock mechanisms and activation/deactivation status of lock sensors, lock sensors may give false alarms. The locking principle of over-center locking mechanisms has been analyzed. Taking the unlocking risk caused by excessive movement of locking mechanisms after passing through the center into consideration, the critical position for locking and unlocking of over-center locking mechanisms has been determined. For typical proximity sensors, the induction principle has been elucidated. Taking into account factors such as arrangement, manufacturing and assembly errors between targets and sensors, the location division of determined active zone and determined inactive zone of the sensor has been identified. Through comparative analysis, for sensor false alarm caused by mechanisms, a reliability analysis model has been established, and a reliability analysis method has been formed. Taking the sensor of the over-center locking mechanism of a certain type of civil aircraft door as an example, the failure probability of sensor false alarms caused by the mechanism has been evaluated, and optimization suggestions for the reliability of false alarms have been proposed. The results show that, optimizing the design of lock mechanism or improving the manufacturing and assembly accuracy of the mechanism, while comprehensively balancing the risk of sensor false indication of locking in place, can effectively improve the reliability of civil aircraft door indication and provide reference for the design of door indication function.