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Tank level sensor, system and process

机译:罐电平传感器,系统和过程

摘要

A liquid level sensor (1) for vertically installing in a liquid storage tank of an aircraft includes at least one first measurement path (V1), which includes a plurality of first detection components (C1-C3, C5-C6),Each sensor (1) is configured to vary between a first state and a second state to infer a first level measurement (N1), and the sensor (1) has at least one second measurement path (V2),Independent of the first measurement path (V1),Having at least one second detection element (C4),The second level (N2) measurement is obtained, The longitudinal position of the second sensing part (C4) is strictly between the longitudinal position of the first foot sensing part (C1) of the first measurement path (V1) and the longitudinal position of the first head sensing part (C6).Abstract figure: Figure 2
机译:用于垂直安装在飞机的液体储罐中的液位传感器(1)包括至少一个第一测量路径(V1),其包括多个第一检测组件(C1-C3,C5-C6),每个传感器( 1)被配置为在第一状态和第二状态之间变化以推断第一电平测量(N1),并且传感器(1)具有至少一个第二测量路径(V2),而独立于第一测量路径(V1)具有至少一个第二检测元件(C4),获得第二级(N2)测量,第二感测部分(C4)的纵向位置严格在第一英尺传感部分(C1)的纵向位置之间第一测量路径(V1)和第一磁头传感部分(C6)的纵向位置。抽象图:图2

著录项

  • 公开/公告号FR3104253A1

    专利类型

  • 公开/公告日2021-06-11

    原文格式PDF

  • 申请/专利权人 SAFRAN AIRCRAFT ENGINES;

    申请/专利号FR20190013916

  • 发明设计人 AUDREY DUPONT;

    申请日2019-12-09

  • 分类号G01F23/74;

  • 国家 FR

  • 入库时间 2022-08-24 19:09:45

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