Rotation-rate sensor having a substrate having a main extension plane for detecting a rotation rate

Patent metadata

Field	Value
Publication number	US-9823073-B2
Application number	US-201414787702-A
Country	US
Kind code	B2
Filing date	May 14, 2014
Priority date	May 14, 2013
Publication date	Nov 21, 2017
Grant date	Nov 21, 2017

Abstract

A rotation-rate sensor having a substrate with main extension plane, for detecting a rotation rate, extending in a direction parallel/orthogonal to the main plane; the sensor including a primary/secondary pair of seismic masses; the primary pair having first/second primary masses; the secondary pair having first/second secondary masses; the first/second primary masses being movable relative to the substrate along a primary deflection direction extending parallel to the main plane; the first/second secondary masses being movable relative to the substrate along a secondary deflection direction extending parallel to the main plane; the first/second primary masses and the first/second primary masses being movable antiparallel or parallel to one another corresponding to the deflection direction, essentially extending orthogonally to the secondary deflection direction; and the primary pair and/or secondary pair being drivable so that, based on sensor rotation, the Coriolis force leads to deflection of the first/second primary masses and/or the first/second secondary masses.

First claim

What is claimed is:

1. A rotation-rate sensor, comprising:
a substrate having a main extension plane, for detecting a rotation rate, the rotation rate extending in a direction parallel to the main extension plane or orthogonally to the main extension plane;
a primary pair of seismic masses having a first primary mass and a second primary mass, wherein the first primary mass has a first end and a second end opposite to its first end, and the second primary mass has a first end and a second end opposite to its second end, the first end of the first primary mass being connected to the first end of the second primary mass via a first coupling element, and the second end of the first primary mass being connected to the second end of the second primary mass at a second end via a second coupling element;
a secondary pair of seismic masses having a first secondary mass and a second secondary mass, both the first secondary mass and the second secondary mass being situated between the first primary mass and the second primary mass, and also between the first coupling element and the second coupling element, so that the first primary mass, the first coupling element, the second primary mass, and the second coupling element, together, surround the first secondary mass and the second secondary mass;
wherein the first primary mass and the second primary mass are each movable relative to the substrate parallel to a primary deflection direction that extends parallel to the main extension plane of the rotation-rate sensor,
wherein the first secondary mass and the second secondary mass are each movable relative to the substrate parallel to a secondary deflection direction that extends parallel to the main extension plane of the rotation-rate sensor,
wherein the first primary mass and the second primary mass, and the first secondary mass and the second secondary mass are movable either antiparallel or parallel to one another in accordance with the particular deflection direction,
wherein the primary deflection direction essentially extends orthogonally to the secondary deflection direction,
wherein the primary pair of seismic masses and/or the secondary pair of seismic masses are drivable so that, in response to a rotation of the rotation-rate sensor, a Coriolis force leads to a deflection of the first primary mass and of the second primary mass and/or of the first secondary mass and of the second secondary mass.

2. The rotation-rate sensor of claim 1 , wherein the first primary mass is connected to the second secondary mass via the first coupling element and the second coupling element so that a primary drive motion of the first primary mass induced by the drive arrangement and of the second primary mass leads to a secondary drive motion of the first secondary mass and of the second secondary mass, and so that a primary Coriolis motion of the first primary mass induced by Coriolis forces and of the second primary mass lead to the secondary drive motion of the first secondary mass and of the second secondary mass.

3. The rotation-rate sensor of claim 1 , wherein each of the first coupling element and the second coupling element has a rocker structure.

4. The rotation-rate sensor of claim 1 , wherein the primary pair of seismic masses, and the secondary pair of seismic masses are moved by the Coriolis force in a detection direction, the detection direction extending orthogonally to the main extension plane.

5. The rotation-rate sensor of claim 4 , wherein the first secondary mass and the second secondary mass are movable in another detection direction, the other detection direction extending parallel to the main extension plane and orthogonally to the secondary deflection direction.

6. The rotation-rate sensor of claim 1 , wherein the primary pair of seismic masses and the secondary pair of seismic masses are connected to the substrate via only the first coupling element and the second coupling element.

7. The rotation-rate sensor of claim 1 , wherein the primary pair of seismic masses and/or the secondary pair of seismic masses includes a detection mass.

8. The rotation-rate sensor of claim 1 , wherein the first coupling element is connected to the first secondary mass, and the second coupling element is connected to the second secondary mass.

9. The rotation-rate sensor of claim 8 , wherein each of the first coupling element and the second coupling element has a rocker structure including a rocker base and a rocker bar, the rocker bar being mounted on the rocker base in such a way that the rocker bar executes a rotational motion about an axis of rotation orthogonal to the main extension plane.

10. The rotation-rate sensor of claim 9 , wherein the rocker bar of the first coupling element is connected to the first end of the first primary mass and the first end of the second primary mass via springs, and the rocker bar of the second coupling element is connected to the second end of the first primary mass and the second end of the second primary mass via springs.

11. The rotation-rate sensor of claim 9 , wherein the first coupling element is connected to the first secondary mass, and the second coupling element is connected to the second secondary mass.

12. The rotation-rate sensor of claim 1 , wherein the first primary mass, the first coupling element, the second primary mass, and the second coupling element, together, surround the first secondary mass and the second secondary mass, together, surround the first secondary mass and the second secondary mass in a plane extending parallel to the main extension plane.

13. The rotation-rate sensor of claim 1 , wherein the first secondary mass and the second secondary mass are coupled to the substrate via springs.

Assignees

• Bosch Gmbh Robert

Inventors

• Balslink Thorsten
• Scheben Rolf
• Schmidt Benjamin
• Ameling Ralf
• Hattass Mirko
• Kuhlmann Burkhard
• Maul Robert

Classifications

• G01C19/574

  the devices having two sensing masses in anti-phase motion · CPC title

• G01C19/5719

  using planar vibrating masses driven in a translation vibration along an axis · CPC title

• G01C19/5705 Primary

  using masses driven in reciprocating rotary motion about an axis · CPC title

• G01C19/5747 Primary

  each sensing mass being connected to a driving mass, e.g. driving frames · CPC title