Dual axial gyroscope with piezoelectric ceramics

• US 6,044,706 A
• Filed: 04/27/1998
• Issued: 04/04/2000
• Est. Priority Date: 08/13/1997
• Status: Expired due to Fees

• Current Assignee: Sitraa Korea Company Limited, Yong Rae Roh
• Original Assignee: Sitraa Korea Company Limited, Yong Rae Roh
• Inventors: Roh, Yong Rae
• Primary Examiner(s): Kwok, Helen C.
• Application Number:
  US09/066,965
• Time in Patent Office: 708 Days
• Field of Search: 73/504.02, 73/504.03, 73/504.04, 73/504.08, 73/504.09, 73/504, 73/12, 73/504.14, 73/504.15, 73/514.34, 74/5.6 D, 74/5 R, 74/5.34, 310/316, 310/321, 310/367, 310/329, 310/370
• US Class Current: 73/504.12
• CPC Class Codes: G01C 19/56 Turn-sensitive devices using vibrating masses, e.g. vibratory angular rate sensors based on Coriolis forces

Abstract

A piezoelectric device is used in an dual axial gyroscope system and includes a piezoelectric exciter for generating a linear velocity on a first axis; a first piezoelectric detector element, placed on a surface of the piezoelectric exciter in a direction orthogonal to the first axis, for detecting a first Coriolis force provided in a direction orthogonal to the first detector; and as second piezoelectric detector element, placed on the surface of the piezoelectric exciter in a direction orthogonal to the first axis and the first detector, for detecting a second Coriolis force provided in a direction orthogonal to the second detector element.

Claims

1. A piezoelectric device, for use in a dual axial gyroscope system, comprising:

piezoelectric exciter means shaped in plate disposed in a first plane, for generating a linear velocity;

first piezoelectric detector means, placed on a surface of the piezoelectric exciter means and shaped in plate disposed in a second plane, for detecting a first Coriolis force provided in a direction orthogonal to the second plane, said second plane being orthogonal to the first plane; and

second piezoelectric detector means, placed on the surface of the piezoelectric exciter means and shaped in plate disposed in a third plane, for detecting a second Coriolis force provided in a direction orthogonal to the the third plane, said third plane being orthogonal to both the first plane and the second plane.

2. The piezoelectric device as recited in claim 1, wherein the first piezoelectric detector means includes two piezoelectric plates placed side by side on the second plane, and wherein each piezoelectric plate has an opposite poling direction.

3. The piezoelectric device as recited in claim 2, wherein the second piezoelectric detector means includes two piezoelectric plates placed side by side on the third plane, and wherein each piezoelectric plate has an opposite poling direction.

4. The piezoelectric device as recited in claim 3, wherein the piezoelectric exciter means includes:

a base forming a bottom portion of the piezoelectric exciter means;

a metal plate forming the surface of the piezoelectric exciter means; and

a piezoelectric exciter plate interposed between the base and the metal plate.

5. The piezoelectric device as recited in claim 4, wherein the thickness of piezoelectric exciter means plate of the piezoelectric exciter means is greater than the thickness of the piezoelectric plates for the first and the second piezoelectric detector means.

6. The piezoelectric device as recited in claim 4, wherein the piezoelectric exciter plate is made of one of PZT type ceramic, PbTiO3 type ceramic and BaTiO3 type ceramic.

7. The piezoelectric device as recited in claim 4, wherein the piezoelectric plates for the first and the second piezoelectric detector means are bonded to the metal plate by using an insulating epoxy and the piezoelectric exciter plate of the piezoelectric exciter means is made of a PZT5A type ceramic.

8. The piezoelectric device as recited in claim 4, wherein the length of the piezoelectric plate is determined in a range of 50% to 100% of a maximum height thereof and the thickness of the piezoelectric plate is selected in a range of 1/2 to 1/10 of the maximum height thereof.

9. The piezoelectric device as recited in claim 8, the thickness of the piezoelectric exciter means is 0.5 mm.

10. The piezoelectric device as recited in claim 4, wherein the base, the metal plate and the piezoelectric exciter means are glued to each other by using a conductive adhesive.

11. The piezoelectric device as recited in claim 10, wherein the base and the metal plate are made of an elastic invariable metal (permalloy).

12. The piezoelectric device as recited in claim 4, wherein the piezoelectric plates for said first and said second piezoelectric detector means are bonded on the surface of the metal plate of the piezoelectric exciter means by using an insulating adhesive.

16. The dual axis piezoelectric gyroscope system as recited in claim 12, wherein the first piezoelectric detector means includes two piezoelectric plates placed side by side on a plane formed by the first axis and a second axis orthogonal to the first Coriolis force, wherein each piezoelectric plate has an opposite poling direction.

17. The dual axis piezoelectric gyroscope system as recited in claim 16, wherein the second piezoelectric detector means includes two piezoelectric plates placed side by side on a plane formed by the first axis and a third axis orthogonal to the second Coriolis force, wherein each piezoelectric plate has an opposite poling direction.

18. The dual axis piezoelectric gyroscope system as recited in claim 17, wherein the piezoelectric exciter means includes:

a base forming a bottom portion of the piezoelectric exciter means;

a metal plate forming the surface of the piezoelectric exciter means; and

a piezoelectric exciter plate interposed between the base and the metal plate.

19. The dual axis piezoelectric gyroscope system as recited in claim 18, wherein the thickness of piezoelectric exciter plate of the piezoelectric exciter means is greater than those of the piezoelectric plates for the first and the second piezoelectric detector means.

13. A dual axis piezoelectric gyroscope system comprising:

a waveform generator for generating a sinusoidal voltage signal;

a piezoelectric device, in response to the sinusoidal voltage signal and an external rotational force, for generating two first charges representing a first Coriolis force and two second charges corresponding to a second Coriolis force;

first processing means for converting the two first charges to generate first and second detection voltage signals;

second processing means for converting the two second charges to generate third and fourth detection voltage signals;

first output means for generating a first detection signal representing a difference between the first and second detection voltage signals; and

second output means for generating a second detection signal representing a difference between the third and fourth detection voltage signals,

wherein, said piezoelectric device comprises;

piezoelectric exciter means, in response to the sinusoidal voltage, for generating a linear velocity on a first axis;

first piezoelectric detector means, placed on a surface of the piezoelectric exciter means in a direction orthogonal to the first axis, for detecting the first Coriolis force provided in a direction orthogonal to the first detector means to generate said two first charges; and

second Piezoelectric detector means, placed on the surface of the piezoelectric exciter means in a direction orthogonal to the first axis and the first piezoelectric detector means, for detecting the second Coriolis force provided in a direction orthogonal to the second detector means to generate said two second charges.

14. The dual axis piezoelectric gyroscope system as recited in claim 13, wherein each of the first and the second processing means includes two channels, each channel including:

a first charge amplifier for converting the charge to a voltage signal;

a second amplifier for amplifying the voltage signal to generate an amplified voltage signal; and

a peak detector for stabilizing the amplified voltage signal to generate a detection voltage signal.

15. The dual axis piezoelectric gyroscope system as recited in claim 14, wherein the first and the second output means are implemented by using a differential amplifier.