Accelerometer with coplanar push-pull force transducers

• US 5,005,413 A
• Filed: 02/27/1989
• Issued: 04/09/1991
• Est. Priority Date: 02/27/1989
• Status: Expired due to Term

• Current Assignee: Alliedsignal Inc.
• Original Assignee: Sundstrand Data Control, Inc.
• Inventors: Novack, Mitchell J., Woodruff, James R., Norling, Brian L.
• Primary Examiner(s): CHAPMAN JR, JOHN E
• Application Number:
  US07/316,399
• Time in Patent Office: 771 Days
• Field of Search: 73/517 AV, 73/517 R, 73/DIG. 1, 310/329, 338/5, 338/46
• US Class Current: 73/514.29
• CPC Class Codes: G01P 15/097 by vibratory elements
• CPC Class Codes: G01P 2015/0828 the mass being of the paddle type being suspended at one of its longitudinal ends

Abstract

A push-pull accelerometer in which both force transducers lie in a common plane. Thus, when implemented in silicon micromachined device, both transducers can be fabricated from a single crystal layer, thereby producing transducers with closely matched common mode responses.

Claims

1. In an accelerometer of the type comprising a support, a proof mass, flexure means connected between the support and the proof mass such that the flexure means mounts the proof mass for rotational movement with respect to the support about a hinge axis (HA) in response to acceleration along a sensitive axis, and first and second force transducers physically separate from the flexure means, each force transducer having opposite first and second ends and a longitudinal axis extending therebetween, each force transducer having its first end connected to the proof mass and its second end connected to the support, the force transducers being connected in a push-pull arrangement wherein for a given acceleration along the sensitive axis, one force transducer is subjected to a compression force along its respective longitudinal axis, and the other force transducer is subjected to a tension force along its respective longitudinal axis, the improvement wherein the transducers are positioned such that their longitudinal axes are located in a common plane that is approximately perpendicular to the sensitive axis, and wherein the hinge axis is normal to the sensitive axis and parallel to but spaced from the common plane.

2. The improvement of claim 1, wherein the proof mass includes a surface lying in said common plane.

3. The improvement of claim 1, wherein the longitudinal axes are parallel to one another, and approximately parallel to a pendulous axis that is normal to the hinge axis and to the sensitive axis and that passes through the hinge axis and a center of mass of the proof mass.

4. The improvement of claim 3, wherein the force transducers are spaced from one another along the hinge axis.

5. The improvement of claim 3, wherein the force transducers are positioned on opposite sides of the proof mass from one another.

6. The improvement of claim 4, wherein the flexure means comprises at least two flexures, and wherein the force transducers are positioned between the flexures.

7. The improvement of claim 6, wherein the proof mass includes a proof mass arm extending from the proof mass towards the support in a first direction along the pendulous axis, wherein the support includes a support arm extending from the support towards the proof mass in a second direction along the pendulous axis, the second direction being opposite to the first direction, and wherein one of the force transducers extends between the proof mass arm and the support arm.

8. The improvement of claim 7, wherein the proof mass arm is positioned between the force transducers.

9. The improvement of claim 4, wherein the longitudinal axis are positioned along a common line.

10. The improvement of claim 4, wherein the force transducers are spaced from one another along the pendulous axis.

11. The improvement of claim 1, wherein each force transducer comprises a vibrating beam force transducer.

12. The improvement of claim 11, wherein each force transducer is a double-ended tuning fork vibrating beam force transducer.