MEMS gyroscope for determining rotational movements about an x, y, and/or z axis

• US 9,909,873 B2
• Filed: 07/28/2014
• Issued: 03/06/2018
• Est. Priority Date: 02/27/2009
• Status: Active Grant

• Current Assignee: Hanking Electronics Hongkong Company Limited
• Original Assignee: Hanking Electronics, Ltd.
• Inventors: Rocchi, Alessandro
• Primary Examiner(s): KWOK, HELEN C
• Application Number:
  US14/444,800
• Publication Number:
  US 20160025492A1
• Time in Patent Office: 1,317 Days
• Field of Search: 7350408, 7350402, 7350404, 7350412, 73510, 73511, 7350414
• CPC Class Codes: G01C 19/5712 the devices involving a micromechanical structure
• CPC Class Codes: G01C 19/574 the devices having two sensing masses in anti-phase motion

Abstract

The invention relates to a MEMS gyroscope for detecting rotational motions about an x-, y-, and/or z-axis, in particular a 3-D sensor, containing a substrate, several, at least two, preferably four, drive masses (2) that are movable radially with respect to a center and drive elements (7) for the oscillating vibration of the drive masses (2) in order to generate Coriolis forces on the drive masses (2) in the event of rotation of the substrate about the x-, y-, and/or z-axis. The oscillating drive masses (2) are connected to at least one further non-oscillating sensor mass (3) that however can be rotated about the x-, y-, and/or z-axis together with the oscillating drive masses (2) on the substrate. Sensor elements (9, 10) are used to detect deflections of the sensor mass (3) and/or drive masses (2) in relation to the substrate due to the generated Coriolis forces. At least two, preferably four anchors (5) are used to rotatably fasten the sensor mass (3) to the substrate by means of springs (4).

Claims

1. A gyroscope comprising:

a substrate;

at least two driving masses that are arranged on the substrate and radially oscillate relative to a central point;

a first drive element coupled to a first driving mass of the at least two driving masses, the first drive element causes radial oscillating vibration of the first driving mass in order to generate Coriolis forces on the first driving mass in a first event of rotation of the substrate about a first axis of the gyroscope;

a second drive element coupled to a second driving mass of the at least two driving masses, the second drive element causes radial oscillating vibration of the second driving mass in order to generate Coriolis forces on the second driving mass in a second event of rotation of the substrate about a second axis of the gyroscope;

synchronization springs that link the first and second driving masses and cause the radial oscillating vibrations of the first and second driving masses to occur in synchrony with each other;

a first sensor element that detects displacement of the first driving mass in response to the Coriolis forces on the first driving mass in the first event of rotation of the substrate about the first axis; and

a second sensor element that detects displacement of the second driving mass in response to the Coriolis forces on the first driving mass in the first event of rotation of the substrate about the second axis.

2. The gyroscope of claim 1 wherein the displacement of the first driving mass causes a first change in capacitance relating to a first rate of rotation about the first axis.

3. The gyroscope of claim 2 wherein the displacement of the second driving mass causes a second change in capacitance relating to a second rate of rotation about the second axis.

4. The gyroscope of claim 1 wherein the radial oscillating vibration of the first driving mass is along a first path and the radial oscillating vibration of the second driving mass is along a second path, the first and second paths being separated by ninety degrees.

5. The gyroscope of claim 4 wherein the first path is along an x-axis of the gyroscope and the second path is along a y-axis of the gyroscope.

6. The gyroscope of claim 1 further comprising a first suspension spring coupled to the first driving mass and the substrate, the first suspension spring facilitating the radial oscillating vibration of the first driving mass.

7. The gyroscope of claim 6 further comprising a second suspension spring coupled to the second driving mass and the substrate, the second suspension spring facilitating the radial oscillating vibration of the second driving mass.

8. The gyroscope of claim 1 further comprising:

a first interface on which a signal is transmitted relating to a first rate of rotation about the first axis; and

a second interface on which a signal is transmitted relating to a second rate of rotation about the second axis.

9. A gyroscope comprising:

a substrate;

a first pair of driving masses that are arranged on the substrate and radially oscillate in synchronized opposition to each other relative to a central point along a first axis of the gyroscope;

a first drive element coupled to a first driving mass of the first pair of driving masses, the first drive element causes radial oscillating vibration of the first driving mass in order to generate Coriolis forces on the first driving mass in an event of rotation of the substrate about the first axis;

a second drive element coupled to a second driving mass of the first pair of driving masses, the second drive element causes radial oscillating vibration of the second driving mass in order to generate Coriolis forces on the second driving mass in the event of rotation of the substrate about the first axis, the first and second drive elements being adapted to vibrate the first and second driving masses in synchronized opposition to each other;

synchronization springs that link the first and second driving masses so that the radial oscillating vibrations of the first and second driving masses occur in synchrony with each other;

a first sensor element that detects displacement of the first driving mass in response to the Coriolis forces on the first driving mass in the first event of rotation of the substrate about the first axis; and

a second sensor element that detects displacement of the second driving mass in response to the Coriolis forces on the first driving mass in the first event of rotation of the substrate about the first axis.

10. The gyroscope of claim 9 further comprising:

a first interface on which a first signal is transmitted relating to a first sensed rate of rotation about the first axis from the first sensor element; and

a second interface on which a second signal is transmitted relating to a second sensed rate of rotation about the first axis from the second sensor element.

11. The gyroscope of claim 10 wherein a differential value related to a rate of rotation about the first axis is derived from the first and second signals.

12. The gyroscope of claim 11 further comprising a central anchor coupled to the substrate, the central anchor having at least one first spring coupled to the first driving mass and at least one second spring coupled to the second driving mass.

13. The gyroscope of claim 11 wherein the first axis is an x-axis of the gyroscope.

14. The gyroscope of claim 12 further comprising:

a first flexural spring coupled to the first driving mass and the substrate, the first flexural spring facilitates the radial oscillating vibration of the first driving mass relative to the central anchor; and

a second flexural spring coupled to the second driving mass and the substrate, the second flexural spring facilitates the radial oscillating vibration of the second driving mass relative to the central anchor.

15. The gyroscope of claim 10 wherein the first signal is generated by a capacitance change caused by the displacement of the first driving mass detected by the first sensor element.

16. The gyroscope of 10 further comprising a third sensor element located above the first driving mass, the third sensor element comprising a plurality of capacitive plates that detect rotation of the substrate about a second axis of the gyroscope.

17. The gyroscope of claim 16 wherein the second axis is a z-axis of the gyroscope.

18. A gyroscope comprising:

a substrate;

a first driving mass that is arranged on the substrate and radially oscillates relative to a central anchor along a first axis of the gyroscope;

a second driving mass that is arranged on the substrate and radially oscillates relative to the central anchor along a second axis of the gyroscope that is ninety degrees from the first axis;

a third driving mass that is arranged on the substrate and radially oscillates relative to the central anchor along the first axis;

a fourth driving mass that is arranged on the substrate and radially oscillates relative to the central anchor along the second axis;

a first drive element coupled to the first driving mass, the first drive element causes radial oscillating vibration of the first driving mass in order to generate Coriolis forces on the first driving mass in a first event of rotation of the substrate about the first axis;

a second drive element coupled to the second driving mass, the second drive element causes radial oscillating vibration of the second driving mass in order to generate Coriolis forces on the second driving mass in a second event of rotation of the substrate about the second axis;

synchronization springs that link the first, second, third and fourth driving masses so that radial oscillating vibrations of the third and fourth driving masses occur in synchrony with the radial oscillating vibrations of the first and second driving masses, the radial oscillating vibrations of the first and third driving masses occur in synchronized opposition to each other, and the radial oscillating vibrations of the second and fourth driving masses occur in synchronized opposition to each other;

a first sensor element that detects displacement of the first driving mass in response to the Coriolis forces on the first driving mass in the first event of rotation of the substrate about the first axis;

a second sensor element that detects displacement of the second driving mass in response to the Coriolis forces on the second driving mass in the second event of rotation of the substrate about the second axis;

a third sensor element that detects displacement of the third driving mass in response to the Coriolis forces on the third driving mass in the first event of rotation of the substrate about the first axis; and

a fourth sensor element that detects displacement of the fourth driving mass in response to the Coriolis forces on the fourth driving mass in the second event of rotation of the substrate about the second axis.