MICROELECTROMECHANICAL DEVICE WITH OUT-OF-PLANE STOPPER STRUCTURE AND PROCESS FOR MANUFACTURING A MICROELECTROMECHANICAL DEVICE

    公开(公告)号:EP4095484A1

    公开(公告)日:2022-11-30

    申请号:EP22174359.4

    申请日:2022-05-19

    Abstract: A microelectromechanical device includes a substrate (21), a first structural layer (23), and a second structural layer (25) of semiconductor material. A sensing mass (32; 132) extends in the first structural layer (23) and is coupled to the substrate (21) by first elastic connections (35) that oscillate in a sensing direction (Z) perpendicular to the substrate (21), with a maximum elongation with respect to a resting position. An out-of-plane stopper structure (38) includes an anchorage (39) fixed to the substrate (21) and a mechanical end-of-travel structure (40), which extends in the second structural layer (25), faces the sensing mass (32), and is separated therefrom by a gap (41) having a width (W) smaller than the maximum elongation. The mechanical end-of-travel structure (40) is coupled to the anchorage (39) by second elastic connections (42) that enable shifts of the mechanical end-of-travel structure (40) with respect to the sensing direction (Z) in response to an impact of the sensing mass (32).

    MICROELECTROMECHANICAL GYROSCOPE FOR SENSING ANGULAR RATE AND METHOD OF SENSING ANGULAR RATE
    12.
    发明公开
    MICROELECTROMECHANICAL GYROSCOPE FOR SENSING ANGULAR RATE AND METHOD OF SENSING ANGULAR RATE 审中-公开
    微机电陀螺仪FOR速度确定和方法的角度确定角速度

    公开(公告)号:EP3086089A1

    公开(公告)日:2016-10-26

    申请号:EP15200480.0

    申请日:2015-12-16

    CPC classification number: G01C19/5733 G01C19/5747 G01C19/5762

    Abstract: A microelectromechanical gyroscope includes: a substrate (2); a stator sensing structure (16b) fixed to the substrate (2); a first mass (7) elastically constrained to the substrate (2) and movable with respect to the substrate (2) in a first direction (D1); a second mass (8) elastically constrained to the first mass (7) and movable with respect to the first mass (7) in a second direction (D2); and a third mass (10) elastically constrained to the second mass (8) and to the substrate (2) and capacitively coupled to the stator sensing structure (16b), the third mass (10) being movable with respect to the substrate (2) in the second direction (D2) and with respect to the second mass (8) in the first direction (D1).

    Abstract translation: 一种微机电陀螺仪,包括:衬底(2); 定子感测结构(16B)固定在基板(2); 第一质量(7)弹性地约束于基板(2)和可相对于第一方向(D1)的基板(2); 第二质量(8)在第二方向(D2)弹性地约束到所述第一质量块(7)和可相对于所述第一质量块(7); 和第三质量块(10)弹性地约束到所述第二质量块(8)和所述基材(2)和电容耦合到可相对于基板的定子感测结构(16B),所述第三质量块(10)(2 )(在第二方向(D2),并且相对于在所述第一方向(D1),第二质量块8)。

    COMPACT MICROELECTROMECHANICAL ANGULAR RATE SENSOR

    公开(公告)号:EP4253909A2

    公开(公告)日:2023-10-04

    申请号:EP23163094.8

    申请日:2023-03-21

    Abstract: A MEMS angular rate sensor is presented with two pairs of suspended masses that are micromachined on a semiconductor layer. A first pair includes two masses opposite to and in mirror image of each other. The first pair of masses has driving structures to generate a mechanical oscillation in a linear direction. A second pair of masses includes two masses opposite to and in mirror image of each other. The second pair of masses is coupled to the first pair of driving masses with coupling elements. The two pairs of masses are coupled to a central bridge. The central bridge has a differential configuration to reject any external disturbances. Each of the masses of the two pairs of masses includes different portions to detect different linear and angular movements.

    MEMS GYROSCOPE HAVING AN IMPROVED REJECTION OF THE QUADRATURE ERROR

    公开(公告)号:EP4124827A1

    公开(公告)日:2023-02-01

    申请号:EP22184619.9

    申请日:2022-07-13

    Abstract: The MEMS gyroscope (1) is formed by a substrate (5), a first mass (7) and a second mass (10), wherein the first and the second masses are suspended over the substrate and extend, at rest, in a plane of extension (XY) defining a first direction (X) and a second direction (Y) transversal to the first direction. The MEMS gyroscope further has a drive structure (48) coupled to the first mass and configured, in use, to cause a movement of the first mass in the first direction, and an elastic coupling structure (25), which extends between the first mass and the second mass and is configured to couple the movement of the first mass in the first direction (X) with a movement of the second mass in the second direction (Y). The elastic coupling structure has a first portion (27, 28, 30, 31, 36, 37) having a first stiffness and a second portion (26, 33, 34) having a second stiffness greater than the first stiffness. The first portion of the elastic coupling structure extends, at rest, in the first and the second directions, and the second portion extends, at rest, in a third direction (C), in the plane of extension, transversal to the first and the second directions.

    INERTIAL MEASUREMENT CIRCUIT, CORRESPONDING DEVICE AND METHOD

    公开(公告)号:EP4098973A1

    公开(公告)日:2022-12-07

    申请号:EP22174570.6

    申请日:2022-05-20

    Abstract: A circuit (10) comprises an inertial measurement unit such as a MEMS gyroscope (12) configured to be oscillated via a driving signal ( D + , D - , Dsq ) produced by driving circuitry (14A, 14B, 16, 18, 20A, 20B, 22, 24, 26, 28, 30, 32) and a lock-in amplifier, LIA (38) receiving a sensing signal ( S + , S - , Ssq ) from the inertial measurement unit (12) as well as a reference demodulation signal which is a function of the driving signal ( D + , D - , Dsq ). The LIA amplifier (38) is configured to produce an inertial measurement signal ( Vout ) based on the sensing signal ( S + , S - , Ssq ) from the inertial measurement unit (12) and the reference demodulation signal, wherein the reference demodulation signal is affected by a variable phase error. Phase meter circuitry (40) configured to receive the driving signal ( D + , D - , Dsq ) and the sensing signal ( S + , S - , Ssq ) produces, as a function of the phase difference ( ΔΦds ) between the driving signal ( D + , D - , Dsq ) and the sensing signal ( S + , S - , Ssq ), a phase correction signal. The phase correction signal is applied (56) to the reference demodulation signal of the lock-in amplifier (38). In response to the phase correction signal being applied (56) to the reference demodulation signal of the lock-in amplifier (38) the phase error is maintained in the in the vicinity of a reference value ( Φer0 ), thus minimizing the effects of the variation of the phase error.

    FREQUENCY MODULATION MEMS TRIAXIAL GYROSCOPE
    17.
    发明公开
    FREQUENCY MODULATION MEMS TRIAXIAL GYROSCOPE 审中-公开
    频率调制MEMS三轴陀螺仪

    公开(公告)号:EP3312559A1

    公开(公告)日:2018-04-25

    申请号:EP17177405.2

    申请日:2017-06-22

    CPC classification number: G01C19/5747 G01C19/574 G01C19/5769

    Abstract: A frequency modulation MEMS triaxial gyroscope (10), having two mobile masses (11A, 11B); a first and a second driving body (31A, 31B) coupled to the mobile masses (11A, 11B) through elastic elements (41A, 41B) rigid in a first direction (X) and compliant in a second direction transverse to the first direction (Y); and a third and a fourth driving body (32A, 32B) coupled to the mobile masses through elastic elements (42A, 42B) rigid in the second direction and compliant in the first direction (X). A first and a second driving element (59A) are coupled to the first and second driving bodies (31A, 31B) for causing the mobile masses to translate in the first direction in phase opposition. A third and a fourth driving element (63A) are coupled to the third and fourth driving bodies (32A, 32B) for causing the mobile masses to translate in the second direction and in phase opposition. An out-of-plane driving element (68A) is coupled to the first and second mobile masses for causing a translation in a third direction (Z), in phase opposition. Movement-sensing electrodes (60A, 64A, 69A) generate frequency signals as a function of external angular velocities.

    Abstract translation: 一种频率调制MEMS三轴陀螺仪(10),具有两个移动质量块(11A,11B); 第一和第二驱动体(31A,31B),其通过在第一方向(X)上刚性且在横向于第一方向(X)的第二方向上柔性的弹性元件(41A,41B) Y); 以及通过在第二方向上刚性且在第一方向(X)上柔性的弹性元件(42A,42B)联接到移动质量块的第三和第四驱动体(32A,32B)。 第一和第二驱动元件(59A)联接到第一和第二驱动体(31A,31B),用于使可动质量块在第一方向上反相平移。 第三和第四驱动元件(63A)联接到第三和第四驱动体(32A,32B),用于使可动质量块在第二方向上平移并且反相。 平面外驱动元件(68A)联接到第一和第二可动质量块上,用于在第三方向(Z)上进行反相的平移。 运动感测电极(60A,64A,69A)产生作为外部角速度的函数的频率信号。

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