The aircraft comprises:-at least one engine (4); -at least one fuel tank (6); -a chamber (22) located in the tank and comprising at least one sensor (24, 26, 28) for measuring a characteristic of the fuel; a system (8) for injecting fuel into the engine; and-a conduit (32) for introducing fuel from the injection system into the chamber. The conduit includes a valve (36) that can prevent fuel from the injection system from being introduced into the chamber via the conduit.

    飞行器包括:‑至少一个发动机(4);‑至少一个燃料箱(6);‑腔室(22),该腔室位于箱中,并且该腔室包括用于测量燃料的特性的至少一个传感器(24,26,28);‑系统(8),该系统用于将燃料喷射到发动机中;以及‑管道(32),该管道用于将燃料从喷射系统引入到腔室中。管道包括阀(36),该阀可以防止来自喷射系统的燃料经由管道引入到腔室中。


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    Title :

    Aircraft comprising chamber provided with sensor in fuel tank of aircraft


    Additional title:

    在飞行器的燃料箱中包括设置有传感器的腔室的飞行器


    Contributors:

    Publication date :

    2023-02-14


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    F02C Gasturbinenanlagen , GAS-TURBINE PLANTS / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / G01F Messen des Volumens, des Durchflussvolumens, des Massendurchflusses oder des Füllstandes , MEASURING VOLUME, VOLUME FLOW, MASS FLOW, OR LIQUID LEVEL



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