ROTATION RATE SENSOR AND METHOD FOR OPERATING A ROTATION RATE SENSOR WITH CIRCULAR DRIVE

• US 20160341550A1
• Filed: 05/13/2016
• Published: 11/24/2016
• Est. Priority Date: 05/19/2015
• Status: Abandoned Application

• Current Assignee: Robert Bosch GmbH
• Original Assignee: Robert Bosch GmbH
• Inventors: GECKELER, Carsten, Wellner, Patrick
• Application Number:
  US15/154,580
• Publication Number:
  US 20160341550A1
• Time in Patent Office: Days
• US Class Current: 1/1
• CPC Class Codes: G01C 19/5705 using masses driven in reciprocating rotary motion about an axis

Abstract

A rotation rate sensor, comprising a substrate having a principal extension plane and comprising a first Coriolis element movable with respect to the substrate and comprising a first suspension means movably suspending the first Coriolis element relative to the substrate, is proposed; the rotation rate sensor having a first excitation means for driving the first Coriolis element in such a way that with the first excitation means activated, the first Coriolis element continuously exhibits motion states deflected with respect to a rest position, the velocity vector of the mass center point of the first Coriolis element having, in each of the deflected motion states, an absolute value from greater than or equal to 90% of a predefined target velocity to less than or equal to 110% of the predefined target velocity.

Claims

1. A rotation rate sensor, comprising:

a substrate having a principal extension plane;

a first Coriolis element which is movable with respect to the substrate;

a first suspension element which movably suspends the first Coriolis element relative to the substrate; and

a first excitation element to drive the first Coriolis element in such a way that with the first excitation element activated, wherein the first Coriolis element continuously exhibits motion states deflected with respect to a rest position, and wherein a velocity vector of a mass center point of the first Coriolis element has, in each of the deflected motion states, has an absolute value from greater than or equal to 90% of a predefined target velocity to less than or equal to 110% of the predefined target velocity.

2. The rotation rate sensor as recited in claim 1, wherein:

the first Coriolis element is an annular first disk, the annular first disk extending substantially in a plane substantially parallel to the principal extension plane of the substrate;

the rotation rate sensor has, in a region of a center point of the annular first disk, at least one substrate-mounted first anchor point;

the annular first disk is connected to the first anchor point via a first suspension unit of the first suspension element;

the rotation rate sensor has, in a radially outwardly directed region of the annular first disk, at least one substrate-mounted second anchor point, the annular first disk being connected to the second anchor point via a second suspension unit of the first suspension element;

the excitation element is disposed in the radially outwardly directed region of the annular first disk;

the first excitation element is disposed with respect to the annular first disk in such a way that with the first excitation element activated and with no application of a physical magnitude to be detected, each motion state, deflected with respect to the rest position, of the annular first disk encompasses a position of the mass center point of the annular first disk substantially in a plane parallel to the principal extension plane of the substrate.

3. The rotation rate sensor as recited in claim 2, wherein at least one of the first suspension unit and the second suspension unit respectively include at least one spring, each of the at least one springs being at least one of a compression spring, a tension spring, a flexural spring, and a torsional spring, the number of springs being greater than 2.

4. The rotation rate sensor as recited in claim 1, wherein the first excitation element has at least one first excitation unit, the first excitation unit being embodied as a capacitive comb structure, and wherein the number of first excitation units is greater than 2.

5. The rotation rate sensor as recited in claim 1, further comprising:

a first detector including a first detection unit to detect a deflected state of the Coriolis element in the sense of a deflection of the Coriolis element out of a plane parallel to the principal extension plane and containing, in the rest state, a mass center point of the Coriolis element, and in a direction parallel to a first axis substantially perpendicular to the principal extension plane as a result of at least one of;

i) a rotation rate of the rotation rate sensor around an axis parallel to a second axis substantially parallel to the principal extension plane, and ii) a rotation rate of the rotation rate sensor around an axis parallel to a third axis substantially parallel to the principal extension plane and perpendicular to the second axis;

wherein the first detection unit includes at least one first electrode, the first electrode being embodied in substantially plate-shaped fashion and extending substantially parallel to the principal extension plane, the first electrode being disposed at least one of;

i) at least in part between the substrate and the Coriolis element, and ii) on a side of the Coriolis element facing away from the substrate.

6. The rotation rate sensor as recited in claim 1, wherein the first detector includes a second detection unit to detect a deflected state of the Coriolis element in the sense of a deflection of the Coriolis element along a plane parallel to the principal extension plane as a result of a rotation rate of the rotation rate sensor around an axis parallel to the first axis, the second detection unit encompassing at least one capacitive second electrode.

7. The rotation rate sensor as recited in claim 1, further comprising:

a second Coriolis element movable with respect to the substrate, and a second suspension element movably suspending the second Coriolis element relative to the substrate;

a second excitation element to drive the second Coriolis element in such a way that with the second excitation means activated, wherein the second Coriolis element continuously exhibits motion states deflected with respect to a rest position, wherein the velocity vector of a mass center point of the second Coriolis element has, in each of the deflected motion states, an absolute value from greater than or equal to 90% of a predefined target velocity to less than or equal to 110% of the predefined target velocity; and

a coupling structure to couple the second Coriolis element to the first Coriolis element in such a way that a motion of the first Coriolis element substantially clockwise around the first axis when looking onto the principal extension plane is possible, wherein a motion of the second Coriolis element is substantially counter-clockwise around an axis parallel to the first axis when looking onto the principal extension plane s possible.

8. The rotation rate sensor as recited in claim 7, wherein the coupling structure is connected to the substrate via a substrate-mounted third anchor point, the coupling structure being connected to the substrate via a substrate-mounted fourth anchor point, and coupling structure includes a coupling spring.

9. A method for operating a rotation rate sensor, the rotation rate sensor including a substrate having a principal extension plane, a first Coriolis element movable with respect to the substrate, a first suspension element movably suspending the first Coriolis element relative to the substrate, and a first excitation element, the method comprising:

exciting the first Coriolis element with the aid of the first excitation element into an excitation oscillation substantially along a substantially closed circular trajectory located substantially parallel to the principal extension plane and substantially clockwise around a first axis when looking onto the principal extension plane, to cause the first Coriolis element to continuously exhibit motion states deflected with respect to a rest position, the velocity vector of the mass center point of the first Coriolis element having, in each of the deflected motion states, an absolute value from greater than or equal to 90% of a predefined target velocity to less than or equal to 110% of the predefined target velocity.

10. The method as recited in claim 9, wherein the rotation rate sensor further includes a second Coriolis element movable with respect to the substrate, a second suspension element movably suspending the second Coriolis element relative to the substrate, and a second excitation element, the method further comprising:

exciting the second Coriolis element with the aid of the second excitation element into an excitation oscillation substantially along a substantially closed circular trajectory located substantially parallel to the principal extension plane and substantially counter-clockwise around an axis parallel to the first axis when looking onto the principal extension plane, to cause the second Coriolis element to continuously exhibit motion states deflected with respect to a rest position, wherein a velocity vector of a mass center point of the second Coriolis element has, in each of the deflected motion states, an absolute value from greater than or equal to 90% of a predefined target velocity to less than or equal to 110% of the predefined target velocity, wherein a coupling structure couples the second Coriolis element to the first Coriolis element.