An aircraft fuel tank venting and inerting arrangement is provided. It comprises a fuel tank (2, 3, 4, figure 1) , a venting fluid flow path between the fuel tank and a venting outlet, an inerting fluid flow path or delivering inerting fluid to the fuel tank, at least part of the venting fluid flow path being provided by a fluid flow conduit and at least part of the inerting fluid flow path being provided by the fluid flow conduit 5, 6, 7. In some embodiments, the conduit may comprise a first venting region for the passage of venting fluid 102, and a second inerting region 103, for the passage of inerting fluid.
Aircraft fuel tank venting and inerting
2024-10-30
Patent
Electronic Resource
English
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
European Patent Office | 2024
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