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发明授权
CN101365625B 用来控制飞行器机舱内的压力的方法和系统 有权

用来控制飞行器机舱内的压力的方法和系统
摘要：
在用来控制飞行器机舱内的压力的方法和系统(10)中，由至少一个检测装置(12a-c、14a-c、16a-c、18a-c)来检测至少一个飞行器舱门的状态。表示飞行器舱门状态的信号被传送至用来控制航空电子设备通风系统的单元(36)。根据表示飞行器舱门状态的信号来控制航空电子设备通风系统，使得当表示飞行器舱门状态的信号指示飞行器舱门未完全闭合并固定时阻止飞行器机舱内的增压。
摘要（英）：

In a process and a system (10) for controlling the pressure in an aircraft cabin the status of at least one aircraft door is detected by at least one detection device (12a-c, 14a-c, 16a-c, 18a-c). A signal indicative of the status of the aircraft door is transmitted to a unit (36) for controlling an avionics ventilation system. The avionics ventilation system is controlled in dependence upon the signal indicative of the status of the aircraft door in such a way that a build-up of pressure in the aircraft cabin is prevented when the signal indicative of the status of the aircraft door indicates that the aircraft door is not fully closed and secured.

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