Rotation speed sensor

• US 6,752,017 B2
• Filed: 03/19/2003
• Issued: 06/22/2004
• Est. Priority Date: 02/21/2001
• Status: Active Grant

• Current Assignee: Robert Bosch GmbH
• Original Assignee: Robert Bosch GmbH
• Inventors: Gomez, Udo Martin, Hauer, Joerg, Funk, Karsten, Lutz, Markus, Bauer, Wolfram, Willig, Rainer, Kuhlmann, Burkhard, Neul, Reinhard, Doering, Christian, Wucher, Gerhard, Bischof, Udo, Franz, Jochen, Goetz, Siegbert, Fehrenbach, Michael, Thomae, Andreas
• Primary Examiner(s): Williams, Hezron
• Assistant Examiner(s): MILLER, ROSE MARY
• Application Number:
  US10/258,339
• Publication Number:
  US 20030164040A1
• Time in Patent Office: 461 Days
• Field of Search: 735/040.2, 735/040.3, 735/040.4, 735/040.8, 735/041.2, 735/041.5, 735/041.6
• US Class Current: 73/504.04
• CPC Class Codes: G01C 19/5747 each sensing mass being connected to a driving mass, e.g. driving frames

Abstract

A yaw-rate sensor is proposed having a first and a second Coriolis element (100, 200) which are arranged side-by-side above a surface (1) of a substrate. The Coriolis elements (100, 200) are induced to oscillate parallel to a first axis. Due to a Coriolis force, the Coriolis elements (100, 200) are deflected in a second axis which is perpendicular to the first axis. The first and second Coriolis elements (100, 200) are coupled by a spring (52) which is designed to be yielding in the first and in the second axis. Thus, the frequencies of the oscillations in the two axes are developed differently for the in-phase and antiphase oscillation.

Claims

1. A yaw-rate sensor, comprising:

a substrate;

a first coriolis element;

a second coriolis element;

an excitation arrangement to induce the first coriolis element and the second coriolis element to oscillate parallel to a first axis;

a detection arrangement to verify a deflection of the first coriolis element and the second coriolis element based on a coriolis force in a second axis that is perpendicular to the first axis, the first axis and the second axis being parallel to the surface of the substrate; and

a coupling spring to connect the first coriolis element and the second coriolis element to each other, and that is yielding in the first axis and in the second axis;

wherein the first coriolis element and the second coriolis are arranged side-by-side and above a surface of the substrate.

2. The yaw-rate sensor of claim 1, wherein the first coriolis element includes a first gravitational center and the second coriolis element includes a second gravitational center, and in response to oscillation, the first gravitational center and the second gravitational, without the effect of the coriolis force, execute a movement on straight lines parallel to the surface of the substrate which are perpendicular to a straight line running through the first gravitational center and the second gravitational center.

3. The yaw-rate sensor of claim 1, wherein the first coriolis element includes a gravitational center and the second coriolis element includes a gravitational center, and in response to oscillation, the first gravitational center and the second gravitational center without the effect of the coriolis force, execute a movement on a straight line that runs through the first gravitational center and the second gravitational center.

4. The yaw-rate sensor of claim 1, wherein the first coriolis element includes a first drive element and the second coriolis element includes a second drive element, and the first drive element and the second drive element are connected to the first coriolis element and the second coriolis element by a plurality of springs that are stiff in the first axis and yielding in the second axis.

5. The yaw-rate sensor of claim 4, wherein the first drive element and the second drive element are connected to the substrate by a plurality of springs that are yielding in the first axis and stiff in the second axis, and the excitation arrangement is connected to the first drive element and the second drive element.

6. The yaw-rate sensor of claim 5, wherein the excitation arrangement includes a plurality of electrostatic comb drives.

7. The yaw-rate sensor of claim 1, wherein the detection arrangement includes a plurality of movable electrodes connected to the first coriolis element and the second coriolis element, and that are arranged opposite a plurality of stationary electrodes that are connected to the substrate.

8. The yaw-rate sensor of claim 1, wherein the detection arrangement includes a first verification element and a second verification element that are connected to the first coriolis element and the second coriolis element by a plurality of springs that are yielding in the first axis and stiff in the second axis.

9. The yaw-rate sensor of claim 8, wherein the first verification element and the second verification element include a plurality of movable electrodes that are arranged opposite to a plurality of stationary electrodes that are connected to the substrate.

10. The yaw-rate sensor of claim 8, wherein the first verification element and the second verification element are connected to the substrate by a plurality of springs that are stiff in the first axis and yielding in the second axis.