The invention provides an aircraft fuel tank venting and inerting device, an aircraft, a fluid flow conduit, and a method of venting and inerting an aircraft fuel tank. The device comprises a fuel tank (2, 3, 4), a discharge fluid flow path (60, 61) between the fuel tank (2, 3, 4) and a discharge outlet (14, 15, 16, 18, 22, 24), an inerting fluid flow path (50) for delivering an inerting fluid to the fuel tank, at least a portion of the discharge fluid flow path being provided by a fluid flow conduit (5, 6, 7) and at least a portion of the inerting fluid flow path being provided by the fluid flow conduit (5, 6, 7).
本发明提供了一种飞行器燃料箱排放和惰化装置、飞行器、流体流动导管以及使飞行器燃料箱排放和惰化的方法。该装置包括燃料箱(2、3、4)、位于燃料箱(2、3、4)与排放出口(14、15、16、18、22、24)之间的排放流体流动路径(60、61)、用于将惰化流体输送至燃料箱的惰化流体流动路径(50),排放流体流动路径的至少一部分由流体流动导管(5、6、7)提供,并且惰化流体流动路径的至少一部分由流体流动导管(5、6、7)提供。
Aircraft fuel tank venting and inerting device, aircraft, fluid flow conduit, and method of venting and inerting aircraft fuel tank
飞行器燃料箱排放和惰化装置、飞行器、流体流动导管以及使飞行器燃料箱排放和惰化的方法
2024-10-29
Patent
Electronic Resource
Chinese
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |