An aircraft includes a fuselage defining a cabin and baggage bay, engine compartments for receiving engines, an auxiliary power unit compartment for receiving an auxiliary power unit, and a fire suppression system including first and second reservoirs containing a fire suppressant. The reservoirs are each connected to all of the engine compartments for distribution of the fire suppressant thereto.The first reservoir is connected to only one of the auxiliary power unit compartment and baggage bay, and the second reservoir is connected to only the other of the auxiliary power unit compartment and baggage bay. A fire suppression system for an aircraft and a method of connecting a fire suppression system of an aircraft are also discussed.

    一种飞机,包括限定客舱和行李架的机身、用于接收发动机的发动机舱、用于接收辅助动力单元的辅助动力单元舱、以及灭火系统,所述灭火系统包括容纳灭火剂的第一储存器和第二储存器。储存器均连接到所有的发动机舱,以用于向其分配灭火剂。第一储存器连接到辅助动力单元舱和行李架中的仅一个,第二储存器连接到辅助动力单元舱和行李架中的仅另一个。还讨论了一种用于飞机的灭火系统以及连接飞机的灭火系统的方法。


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    Title :

    Aircraft fire suppression system


    Additional title:

    飞机的灭火系统



    Publication date :

    2020-06-16


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    A62C FIRE-FIGHTING , Feuerbekämpfung / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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