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    • 7. 发明公开
    • DISPOSITIF D'INERTAGE, RÉSERVOIR ET AÉRONEF MUNIS D'UN TEL DISPOSITIF ET PROCÉDÉ CORRESPONDANT
    • INERTISIERUNGSVORRICHTUNG,TANK UND FLUGZEUG MIT EINER DERARTIGEN VORRICHTUNG SOWIE ENTSPRECHENDES VERFAHREN
    • EP2825463A1
    • 2015-01-21
    • EP13704199.2
    • 2013-01-25
    • L'Air Liquide Société Anonyme pour l'Etude et l'Exploitation des Procédés Georges Claude
    • TIGER, Xavier
    • B64D37/32
    • B64D37/32B64D37/10G05D16/204Y10T137/86485
    • The invention relates to an inerting device for a pressurized aircraft fuel tank, i.e. for a tank provided with a main vessel (2) and a separate overflow space (3), the device including a generator (1) of nitrogen-enriched gas, a circuit (4, 5) for transferring the nitrogen-enriched gas produced by the generator (1), the transfer circuit (4, 5) including an upstream end connected to the generator (1), a first downstream end (4) which can be coupled to the main vessel (2) and a second downstream end (5) which can be coupled to the overflow space (3), the device including a sensor array (6, 7) for measuring information representative of the pressure differential (P3-Pa) between the interior of the overflow space (3) and the exterior of the tank, the device further including an electronic logic (8) receiving the measurements from the sensor array (6, 7), the electronic logic (8) being connected to the generator (1) and/or to the transfer circuit (4, 5), and being designed to control the supply of a nitrogen-enriched gas flow to the second downstream end (5) when the pressure differential (P3-Pa) between the interior of the overflow space and the exterior drops below a predetermined threshold S.
    • 本发明涉及一种用于加压飞机燃料箱的惰化装置,即用于设置有主容器和独立溢流空间的罐,该装置包括富氮气体的发生器,用于输送产生的富氮气体的回路 通过发电机,传输电路包括连接到发电机的上游端,可连接到主容器的第一下游端和可连接到溢流空间的第二下游端,该装置包括用于测量的传感器阵列 信息表示溢流空间的内部与罐的外部之间的压力差,该装置还包括接收来自传感器阵列的测量值的电子逻辑单元,电子逻辑单元连接到发电机和/或 传输电路,并且被设计成当压力di时控制向第二下游端供应富氮气流 微分下降到预定阈值S以下