首页> 外国专利> Temperature threshold overshoot detecting device for e.g. aircraft's turbojet engine, has helical spring to contact with or separated from bottom based on temperature greater or lesser than transition temperature of shape memory material

Temperature threshold overshoot detecting device for e.g. aircraft's turbojet engine, has helical spring to contact with or separated from bottom based on temperature greater or lesser than transition temperature of shape memory material

机译:温度阈值过冲检测装置,例如飞机的涡轮喷气发动机,具有螺旋弹簧,可根据大于或小于形状记忆材料转变温度的温度与底部接触或与底部分离

摘要

The device has an electroconductive element i.e. helical spring (32) subjected to a temperature to be controlled, where the element is made of shape memory material. The spring contacts with or separated from an electroconductive bottom (20) of a tube (12) serving as an electric current passage terminal, according to a temperature greater or lesser than a transition temperature of the material. The bottom is connected to an electric wire (18) of a current source and the element is connected to a connecting rod (26) of the source. The element forms a micro-switch (10) of signaling circuit.
机译:该装置具有导电元件,即螺旋弹簧(32),其经受要控制的温度,其中该元件由形状记忆材料制成。弹簧根据大于或小于材料的转变温度的温度与用作电流通过端子的管(12)的导电底部(20)接触或分离。底部连接到电流源的电线(18),并且该元件连接到电流源的连杆(26)。该元件形成信令电路的微动开关(10)。

著录项

  • 公开/公告号FR2927994A1

    专利类型

  • 公开/公告日2009-08-28

    原文格式PDF

  • 申请/专利权人 SNECMA SOCIETE ANONYME;

    申请/专利号FR20080001065

  • 发明设计人 MONS CLAUDE MARCEL;

    申请日2008-02-27

  • 分类号G01K5/48;G01K7;

  • 国家 FR

  • 入库时间 2022-08-21 19:07:12

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