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Fire extinction design for an auxiliary power unit compartment of an aircraft

机译:飞机辅助动力装置舱的灭火设计

摘要

The invention refers to an APU compartment, and a method for extinguishing a fire in an APU compartment. The APU compartment (1) comprises an APU (2), an exhaust (5), an aperture (7) providing a passage between the APU compartment (1) and the inside of the exhaust (5), and a fire detection system, wherein the APU compartment (1) of the invention is constructed as an air tight compartment, and additionally comprises a conduit (9) for providing external air to the APU compartment (1), a door (8) for closing the conduit (9) inlet, and a control unit (6) configured to close the door (8) when a fire is detected, such that when the door (8) is closed and the APU (2) is in operation, the air contained in the APU compartment (1) is sucked through the aperture (7) to be expelled out of the APU compartment (1) to extinguish the fire.
机译:本发明涉及一种APU隔室以及一种用于扑灭APU隔室中的火的方法。 APU隔室(1)包括APU(2),排气孔(5),在APU隔室(1)和排气孔(5)内部之间提供通道的孔(7)和火灾探测系统,其中本发明的APU隔室(1)构造为气密隔室,并且还包括用于向APU隔室(1)提供外部空气的导管(9),用于关闭导管(9)的门(8)。入口和控制单元(6),该单元配置为在检测到火灾时关闭门(8),以便当门(8)关闭且APU(2)运行时,APU隔室内的空气(1)通过孔(7)吸入,将其从APU隔室(1)中排出,以扑灭大火。

著录项

  • 公开/公告号EP3025965B1

    专利类型

  • 公开/公告日2017-05-31

    原文格式PDF

  • 申请/专利权人 AIRBUS OPERATIONS S.L.;

    申请/专利号EP20140382478

  • 发明设计人 PALOMARES MORA ANGEL;

    申请日2014-11-27

  • 分类号B64D41;

  • 国家 EP

  • 入库时间 2022-08-21 14:05:09

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