Vibrating beam accelerometer

• US 4,628,735 A
• Filed: 12/14/1984
• Issued: 12/16/1986
• Est. Priority Date: 12/14/1984
• Status: Expired due to Fees

• Current Assignee: Sundstrand Corporation (Raytheon Technologies Corporation d/b/a RTX)
• Original Assignee: Sundstrand Data Control, Inc.
• Inventors: Kirkpatrick, Gordon S.
• Primary Examiner(s): Levy, Stewart J.
• Assistant Examiner(s): Chapman, Jr., John E.
• Application Number:
  US06/681,564
• Time in Patent Office: 732 Days
• Field of Search: 73/517 AV, 73/1 D, 73/DIG. 1, 310/329
• 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

The elimination of activity dips in the output of vibrating beam accelerometers has often required an adjustment of parameters in conflict with other design criteria. This problem is overcome by the present accelerometer that comprises a pendulum (48) and a force transducer. The pendulum has first (49) and second (52) ends and a first axis (P) extending between the first and second ends. The pendulum is hingedly connected at its first end to a support (50) along a second axis (F) perpendicular to the first axis. The force transducer comprises an oscillator and a dual beam force sensing element (53) connected between the second end of the pendulum and the support. The point of connection of the force sensing element to the pendulum lies along the first axis. The force transducer is adapted for vibration over a predetermined operating range (44) of beam vibration frequencies. The second end of the pendulum is formed so as to cause the frequencies of pendulum vibration modes to lie outside the operating range, preferably by controlling the mass of the pendulum at the outer edges of the second end so as to cause the normal mode frequency of twisting vibration of the pendulum about the first axis to lie outside the operating range. In another aspect, the pendulum has a width dimension parallel to the second axis, and the width of the pendulum decreases from a point intermediate the ends of the pendulum to the second end.

Claims

1. An accelerometer, comprising:

a pendulum having first and second ends, the pendulum having a first axis extending between the first and second ends and being hingedly connected at the first end to a support along a second axis perpendicular to the first axis, the pendulum having a width dimension parallel to the second axis;

a force transducer comprising an oscillator and a dual beam force sensing element connected between the second end of the pendulum and the support, the point of connection of the force sensing element to the pendulum lying along the first axis, the force transducer being adapted for vibration over a predetermined operating range of beam vibration frequencies; and

the second end of the pendulum being formed with a width that is smaller than the width of the pendulum adjacent the first end so as to cause the frequencies of pendulum vibration modes to lie outside the operating range.

2. The accelerometer of claim 1, wherein the pendulum is symmetric with respect to the first axis.

3. The accelerometer of claim 2, wherein the second end of the pendulum is formed so as to cause the normal mode frequency of twisting vibration of the pendulum about the first axis to lie outside the operating range.

4. The accelerometer of claim 3, wherein the normal mode frequency is caused to lie above the operating range by forming the second end with a width that is smaller than the width of the pendulum adjacent the first end.

5. The accelerometer of claim 4, wherein the width of the pendulum decreases from a point intermediate the ends of the pendulum to the second end.

6. The accelerometer of claim 5, wherein the decrease of width from said point to the second end is linear.

7. The accelerometer of claim 6, wherein the decreasing width portion of the pendulum between said point and the second end forms an angle of approximately 45°

with respect to the first axis.

8. The accelerometer of claim 7, wherein the width of the second end is approximately half of the width of the first end.

9. The accelerometer of claim 4, wherein the width of the second end is approximately equal to the width of the portion of the force sensing element attached to the second end.

10. An accelerometer, comprising:

a pendulum having first and second ends, the pendulum being symmetric with respect to a first axis extending between the first and second ends and being hingedly connected at the first end to a support along a second axis perpendicular to the first axis, the pendulum having a width dimension parallel to the second axis, the width of the pendulum decreasing from a point intermediate the ends of the pendulum to the second end, and

a force transducer comprising an oscillator and a dual beam force sensing element connected between the second end of the pendulum and the support, the point of connection of the force sensing element to the pendulum lying along the first axis.

11. The accelerometer of claim 10, wherein the decrease of width from said point to the second end is linear.

12. The accelerometer of claim 11, wherein the decreasing width portion of the pendulum between said point and the second end forms an angle of approximately 45°

with respect to the first axis.

13. The accelerometer of claim 12, wherein the width of the second end is approximately half of the width of the first end.

14. The accelerometer of claim 10, wherein the width of the second end is approximately equal to the width of the portion of the force sensing element attached to the second end.