Multisensor assembly with angular rate piezoelectric crystal beam

• US 4,715,227 A
• Filed: 09/02/1986
• Issued: 12/29/1987
• Est. Priority Date: 09/02/1986
• Status: Expired due to Term

• Current Assignee: Singer Company The Little Falls NJ
• Original Assignee: Singer Company (SVP Holdings Ltd.)
• Inventors: Pittman, Roland
• Primary Examiner(s): CHAPMAN JR, JOHN E
• Application Number:
  US06/902,695
• Time in Patent Office: 483 Days
• Field of Search: 73/504, 73/510, 73/DIG. 4, 74/5 F, 74/5.6 D, 310/329, 310/330, 310/353
• US Class Current: 73/504.03
• CPC Class Codes: G01C 19/005 Measuring angular rate using gyroscopic effects
• CPC Class Codes: G01C 19/28 Pick-offs, i.e. devices for taking-off an indication of the displacement of the rotor axis
• CPC Class Codes: G01P 15/09 by piezoelectric pick-up
• CPC Class Codes: Y10S 73/04 Piezoelectric

Abstract

In a multisensor assembly for detecting angular rates and linear accelerations, a diamond-shaped piezoelectric crystal beam is used to restrain a gyroscopic element to a base of the multisensor assembly. The diamond-shaped piezoelectric crystal is fixed to both the gyroscopic element and the base of the assembly by means of wires in an orientation orthogonal to the hinge axis and the spin axis of the assembly. This allows the piezoelectric crystal to experience only one degree of freedom. To improve the accuracy of the output electrical signal, oblong electrodes are placed on opposite surfaces of the piezoelectric crystal beam.

Claims

1. In a navigation sensor having a gyroscopic element rotatable about an axis and at least one flexure hinge for resiliently mounting the gyroscopic element to a base, the gyroscopic element including an aperture concentric to the axis, the navigation sensor further having a torque sensing assembly comprising:

a piezoelectric beam aligned in coaxial relationship with the axis;

first restraining means for fixing orthogonal to the axis one edge portion of the beam to the gyroscopic element;

second restraining means for fixing orthogonal to the axis an opposite edge portion of the beam to the base;

third restraining means intermediate to the first and second restraining means for fixing to the gyroscopic element opposite midsection portions of the beam orthogonal to the axis;

whereby the restrained beam converts an angular rate of the gyroscopic element to a corresponding electrical signal.

2. The torque sensing assembly according to claim 1, wherein the first restraining means fixes the one edge portion of the piezoelectric beam to the inner circumferential edge of the aperture of the gyroscopic element and the third restraining means fixes the opposite midsection portions of the piezoelectric beam to the bottom inner circumferential edge of the gyroscopic element, the first and third restraining means fixing the piezoelectric beam within the aperture of the gyroscopic element.

3. The torque sensing assembly according to claim 1, wherein the piezoelectric beam is diamond-shaped.

4. The torque sensing assembly according to claim 1, wherein all the restraining means comprise wires having coefficients of expansion similar to that of the piezoelectric beam.

5. The torque sensing assembly according to claim 3, wherein the piezoelectric beam has on opposite surfaces thereof oblong electrode areas.

6. The torque sensing assembly according to claim 4, wherein the wires for fixing the piezoelectric beam to the gyroscopic element and the base are coaxially aligned in a direction orthogonal to the longitudinal axis of the flexure hinges.

7. The torque sensing assembly according to claim 4, wherein all of the wires are straight.

8. The torque sensing assembly according to claim 4, wherein the wire for fixing the one edge portion of the beam to the base has at least one kink and wherein the remaining wires are straight.

9. A navigation sensor comprising:

a gyroscopic element rotatable about an axis, the gyroscopic element having an aperture concentric to the axis;

a base;

at least one flexure hinge for resiliently mounting the gyroscopic element to the base;

a torque sensing assembly engaged to the gyroscopic element and the base, the torque sensing assembly including;

(a) a first piezoelectric beam aligned in coaxial relationship with the axis;

(b) first restraining means for fixing orthogonal to the axis one edge portion of the beam to the gyroscopic element;

(c) second restraining means for fixing orthogonal to the axis an opposite edge portion of the beam to the base; and

(d) third restraining means intermediate to the first and second restraining means for fixing to the gyroscopic element opposite midsection portions of the beam orthogonal to the axis;

whereby the first restrained beam converts an angular rate of the gyroscopic element to a first corresponding electrical signal; and

second piezoelectric beams mounted in uniform spaced relation to the axis for generating a second electric signal proportional to a linear acceleration of the sensor in a direction perpendicular to the axis.

10. The sensor according to claim 9, wherein the first piezoelectric beam is diamond-shaped.

11. The sensor according to claim 10, wherein the first piezoelectric beam has on opposite surfaces thereof oblong electrodes.

12. The sensor according to claim 9, wherein all the restraining means comprise wires having coefficients of expansion similar to that of the first piezoelectric beam.

13. The sensor according the claim 10, wherein the second restraining means comprises a wire having at least one kink.