Redundant rate sensor and method

• US 6,462,530 B1
• Filed: 01/25/2001
• Issued: 10/08/2002
• Est. Priority Date: 01/25/2001
• Status: Expired due to Fees

• Current Assignee: BEI Technologies, Incorporated
• Original Assignee: BEI Technologies, Incorporated
• Inventors: Layton, Michael R.
• Primary Examiner(s): Le, N.
• Assistant Examiner(s): Kerveros, James
• Application Number:
  US09/770,792
• Publication Number:
  US 20020097037A1
• Time in Patent Office: 621 Days
• Field of Search: 324/76.49, 318/564, 735/041.6, 331/116.M, 310/25
• US Class Current: 324/76.49
• CPC Class Codes: G01C 19/5607 using vibrating tuning forks double-ended tuning forks using planar vibrating masses suspended at opposite ends G01C19/5719
• CPC Class Codes: G01C 19/5783 Mountings or housings not specific to any of the devices covered by groups G01C19/5607 - G01C19/5719

Abstract

Redundant rate sensor and method in which inertial rate is monitored with a plurality of vibratory sensing elements mounted in a single enclosure, signals from the sensing elements are processed to provide an independent rate output signal for each of the sensing elements, and the independent rate output signals are delivered to a connector which is accessible externally of the enclosure.

Claims

1. A redundant rate sensor, comprising an enclosure, a plurality of independent and separate vibratory rate sensing elements within the enclosure, an output connector accessible externally of the enclosure, and circuit means within the enclosure for processing signals from each of the sensing elements and delivering to the output connector an independent rate output signal for each of the sensing elements.

2. The redundant rate sensor of claim 1 wherein each of the vibratory rate sensing elements includes a tuning fork.

3. The redundant rate sensor of claim 2 wherein each of the tuning forks is fabricated of quartz.

4. The redundant rate sensor of claim 1 wherein each of the sensing elements is mounted on a common circuit board within the enclosure.

5. The redundant rate sensor of claim 4 wherein the circuit means is also mounted on the circuit board.

6. The redundant rate sensor of claim 1 including means within the enclosure for exciting each of the sensing elements at a different drive frequency.

7. The redundant rate sensor of claim 1 wherein each of the sensing elements has a drive frequency and a pickup frequency which are separated from each other by a predetermined amount, with the drive and pickup frequencies for different ones of the sensing elements being separated by different amounts.

8. The redundant rate sensor of claim 1 wherein the circuit means includes a separate processing circuit for each of the sensing elements.

9. In a method of sensing inertial rate, the steps of:

monitoring inertial rate with a plurality of vibratory sensing elements mounted in a single enclosure, processing signals from the sensing elements to provide an independent rate output signal for each of the sensing elements, and delivering the independent rate output signals to a connector which is accessible externally of the enclosure.

10. The method of claim 9 wherein each of the sensing elements is excited at a different drive frequency.

11. The method of claim 10 wherein each of the sensing elements is operated at a drive frequency and a pickup frequency which are separated from each other by a predetermined amount, with the drive and pickup frequencies for different ones of the sensing elements being separated by different amounts.

12. A redundant rate sensor, comprising an enclosure, first and second vibratory rate sensing elements mounted in the enclosure with the input axes of the two sensing elements perpendicular to each other for sensing rotation about perpendicular axes, and a third vibratory rate sensing element mounted in the enclosure with the input axis of the third sensing element parallel to the input axis of the first sensing element to provide redundancy for the first sensing element.

13. The redundant rate sensor of claim 12 wherein each of the vibratory rate sensing elements includes a tuning fork.

14. The redundant rate sensor of claim 13 wherein each of the tuning forks is fabricated of quartz.

15. A redundant rate sensor, comprising an enclosure, first and second vibratory rate sensing elements mounted in the enclosure with the input axes of the two sensing elements perpendicular to each other, and a third vibratory rate sensing element mounted in the enclosure with the input axis of the third sensing element at a non-orthogonal angle relative to the input axes of the first and second sensing elements to provide redundancy for the first and second sensing elements.

16. The redundant rate sensor of claim 15 wherein each of the vibratory rate sensing elements includes a tuning fork.

17. The redundant rate sensor of claim 16 wherein each of the tuning forks is fabricated of quartz.

18. The redundant rate sensor of claim 15 wherein the axis of the third sensing element is at an angle of 45°

relative to the input axes of the first and second sensing elements.

19. A redundant rate sensor, comprising an enclosure, three vibratory rate sensing elements mounted in the enclosure with the input axes of the three sensing elements perpendicular to each other for sensing rotation about perpendicular axes, and a fourth vibratory rate sensing element mounted in the enclosure to provide redundancy for at least one of the three sensing elements.

20. The redundant rate sensor of claim 19 wherein the input axis of the fourth sensing element is parallel to the input axis of one of the three sensing elements.

21. The redundant rate sensor of claim 19 wherein the input axis of the fourth sensing element is oriented at a non-orthogonal angle relative to the input axes of at least two of the three sensing elements.