In-plane translational vibrating beam accelerometer with mechanical isolation and 4-fold symmetry

Patent metadata

Field	Value
Publication number	US-10866258-B2
Application number	US-201816041187-A
Country	US
Kind code	B2
Filing date	Jul 20, 2018
Priority date	Jul 20, 2018
Publication date	Dec 15, 2020
Grant date	Dec 15, 2020

Abstract

A vibrating beam accelerometer (VBA) with an in-plane translational proof mass that may include at least two or more resonators and be built with planar geometry, discrete lever arms, four-fold symmetry and a single primary mechanical anchor between the support base and the VBA. In some examples, the VBA of this disclosure may be built according to a micro-electromechanical systems (MEMS) fabrication process. Use of a single primary mechanical anchor may minimize bias errors that can be caused by external mechanical forces applied to the circuit board, package, and/or substrate that contains the accelerometer mechanism.

First claim

The invention claimed is:

1. A device comprising:
a translational proof mass;
a support base defining a first plane;
an anchor connection structure mechanically connected to the support base with an anchor, wherein the anchor connection structure is in a second plane parallel to the first plane;
a lever arm mechanically connected to the anchor connection structure at a fulcrum of the lever arm,
wherein a first end of the lever arm is mechanically connected to the translational proof mass, and
wherein the lever arm is in the second plane;

a resonator configured to:
connect a second end of the lever arm to the anchor;
receive a force from the lever arm when the translational proof mass is accelerated; and
flex in the second plane based on the received force, wherein the resonator resonates at a driven resonant frequency and the force from the lever arm causes a change in frequency of the resonator;

wherein the translational proof mass, the lever arm and the resonator are in the second plane.

2. The device of claim 1 , wherein the resonator is a first resonator, the lever arm is a first lever arm and the resonant frequency is a first resonant frequency, the device further comprising a second resonator and a second lever arm, a third lever arm and a fourth lever arm, wherein:
the second lever arm is mechanically connected to the anchor connection structure at a fulcrum of the second lever arm,
wherein a first end of the second lever arm is mechanically connected to the translational proof mass, and a second end of the second lever arm is connected to the first resonator;

the third lever arm and the fourth lever arm:
are each mechanically connected to the anchor connection structure a respective fulcrum of each of the third lever arm and the fourth lever arm; and
are each mechanically connected to the translational proof mass at a respective first end of each of the third lever arm and the fourth lever arm;

the second resonator is configured to:
connect a respective second end of each of the third lever arm and the fourth lever arm to the anchor; and
flex in the second plane based on the translation of the translational proof mass, wherein the second resonator resonates at a second resonant frequency,

wherein the second lever arm, the third lever arm, the fourth lever arm, and the second resonator are in the second plane.

3. The device of claim 2 , further comprising a support flexure coupled to the translational proof mass, wherein the support flexure is configured to restrict out-of-plane motion of the translational proof mass with respect to the second plane.

4. The device of claim 2 , wherein the first resonator and the second resonator each comprise at least one an anchored comb and at least one released comb, wherein:
the anchored comb is in the second plane and mechanically attached to the support base in the first plane,
a released beam of the first resonator is in the second plane and mechanically attached to the anchor connection structure and mechanically attached to the second end of the first lever arm and the second end of the second lever arm, and
a released beam of the second resonator is in the second plane and mechanically attached to the anchor connection structure and mechanically attached to the second end of the third lever arm and the second end of the fourth lever arm.

5. The device of claim 2 , wherein the translational proof mass, the anchor connection structure, the first lever arm, the second lever arm, the third lever arm, the fourth lever arm form a substantially symmetrical structure.

6. The device of claim 5 , wherein the substantially symmetrical structure comprises:
the first lever arm defines a length, and wherein the second lever arm, the third lever arm, the fourth lever arm are substantially the same length as the first lever arm;
a distance between the first end of the first lever arm and the fulcrum of the first lever arm defines a first radius and a distance between the second end of the first lever arm and the fulcrum of the first lever arm defines a second radius,
wherein the second lever arm, the third lever arm, the fourth lever arm each comprise a respective first radius and a respective second radius,
wherein the respective first radius of the second lever arm, the third lever arm, the fourth lever arm are each substantially equal to the first radius of the first lever arm, and
wherein the respective second radius of the second lever arm, the third lever arm, the fourth lever arm are each substantially equal to the second radius of the first lever arm.

7. The device of claim 2 , wherein the anchor connection structure comprises a stiffness greater than an axial spring constant of each resonator of the first resonator and the second resonator.

8. The device of claim 2 , wherein the anchor is configured to allow a first thermal expansion of the support base, and a second thermal expansion of the first resonator, the second resonator and the anchor connection structure, wherein the first thermal expansion is different than the second thermal expansion.

9. The device of claim 7 , wherein the anchor connection structure is configured such that the anchor connection structure prevents bias errors from a thermal expansion mismatch between the support base and the translational proof mass, the first resonator and the second resonator.

10. The device of claim 7 , wherein a coefficient of thermal expansion for each of the translational proof mass, the anchor connection structure, the first resonator and the second resonator, lever arms and mechanical connections between the translational proof mass, the anchor connection structure, the first resonator and the second resonator, and the lever arms are substantially equal.

11. The device of claim 2 , wherein the anchor connection structure is configured to substantially prevent a force applied to the support base transferring to either the translational proof mass or to the first resonator and the second resonator.

12. The device of claim 11 , wherein force applied to the support base is a twisting force.

13. The device of claim 2 , wherein the first resonator receives a tension force while the second resonator receives a compression force.

14. The device of claim 2 , wherein the first resonator and the second resonator provide a differential frequency measurement.

15. A system comprising
a translational vibrating beam accelerometer (VBA), comprising:
a translational proof mass;
a support base defining a first plane;
an anchor connection structure mechanically connected to the support base with an anchor, wherein the anchor connection structure is in a second plane parallel to the first plane;
a lever arm mechanically connected to the anchor connection structure at a fulcrum of the lever arm,
wherein a first end of the lever arm is mechanically connected to the translational proof mass, and
wherein the lever arm is in the second plane;

two or more resonators, including a first resonator and a second resonator, wherein the first resonator is configured to:
connect a second end of the lever arm to the anchor;
receive a force from the lever arm when the translational proof mass is accelerated; and
flex in the second plane based on the received force, wherein the first resonator resonates at a driven resonant frequency and the received force from the lever arm causes a change in frequency of the first resonator;

wherein the translational proof mass, the lever arm and the first resonator are in the second plane;

a signal generation circuit operatively connected to the translational

Assignees

• Honeywell Int Inc

Inventors

• Reinke John

Classifications

• B81B2201/0235

  Accelerometers · CPC title

• G01L1/162

  using piezoelectric resonators · CPC title

• G01P15/09

  by piezoelectric pick-up · CPC title

• H03H9/2473

  Double-Ended Tuning Fork [DETF] resonators · CPC title

• G01P15/097 Primary

  by vibratory elements · CPC title