AIRCRAFT SKIN PANEL WITH ULTRASONIC GAUGE
    7.
    发明公开
    AIRCRAFT SKIN PANEL WITH ULTRASONIC GAUGE 审中-公开
    与超声测量装置飞机盖板

    公开(公告)号:EP2335034A1

    公开(公告)日:2011-06-22

    申请号:EP09785677.7

    申请日:2009-09-22

    摘要: An aircraft panel which is a wall of a fluid tank when in use, the panel comprising a skin layer with an outer surface which is an aerodynamic surface of an aircraft when in use; a hole in the skin layer; an ultrasonic gauge which is mounted to an inner surface of the skin layer adjacent to the hole in the skin layer; and an access panel which covers the hole and can be removed to gain access to the gauge.

    MAGNETISCHER PASSIVER POSITIONSSENSOR
    9.
    发明公开
    MAGNETISCHER PASSIVER POSITIONSSENSOR 有权
    磁性位置传感器的被动

    公开(公告)号:EP2250468A1

    公开(公告)日:2010-11-17

    申请号:EP09715582.4

    申请日:2009-01-20

    IPC分类号: G01D5/251 B60K15/06 G01F23/36

    摘要: The invention relates to a magnetic passive position sensor (1) comprising a base plate (2) and a cover (9) which form a housing, a magnet (13) that can be moved outside the housing, a resistance network (3) that has several individual electric contacts (4), and a plurality of contact spring elements (5) that are arranged within the range of motion of the magnet, are interconnected by means of a common base (8), and consist of a bending zone (6) and a contact zone (7). The contact spring elements (5) face the contacts (4) of the resistance network (3) in such a way that the contact zones (7) can be moved from the magnets against the contacts (4) of the resistance network (3), the contact zones (7) of at least two contact spring elements (5) being assigned to each individual contact (4) of the resistance network (3). Two adjoining contact spring elements (5a; 5b; 5c; 5d) are mechanically interconnected.