Force balanced vibratory rate sensor

• US 4,267,731 A
• Filed: 02/11/1980
• Issued: 05/19/1981
• Est. Priority Date: 02/11/1980
• Status: Expired due to Term

• Current Assignee: Honeywell Incorporated (Honeywell International Inc.)
• Original Assignee: Sperry Corporation
• Inventors: Jacobson, Peter E.
• Primary Examiner(s): Gill, James J.
• Application Number:
  US06/120,179
• Time in Patent Office: 463 Days
• Field of Search: 73/505, 74/5 R
• US Class Current: 73/504.15
• CPC Class Codes: G01C 19/5642 using vibrating bars or beams
• CPC Class Codes: G01P 15/125 by capacitive pick-up
• CPC Class Codes: G01P 15/133 with piezoelectric counterbalancing means

Abstract

A vibratory inertial rate of turn sensor employs force feed back for maintaining the free end of a vibrating cantilever in a nulled lineal path when subjected to a turn about the beam axis, the electrical signal required for nulling being a measure of rate of turn of the craft. The output signal demodulation self-tracks the beam resonance frequency and the beam drive and null terms balance one another, tending to maintain the sensor scale factor constant over time and temperature. A unique pick-off and beam primary drive and restoring force drive configuration is provided.

Claims

1. A force feed back inertial rate sensor comprising:

a first support member,

a second support member,

an elongate beam cantilevered from said second support member, extending along a sensing axis about which rate of turn is to be measured, and having a free end,

first signal generating means coupled with and responsive to vibration of said free end in a first plane including said sensing axis,

first elongate drive means cantilevered from said first support member and coupled with said second support member and responsive to said first signal generating means for vibrating said elongated beam in said first plane at a frequency dependent upon the natural vibration of said elongate beam,

second signal generating means coupled with and responsive to vibration components of said free end in a second plane including said sensing axis and normal to said first plane due to rate of turn of said support member about said sensing axis, and

second elongate drive means cantilevered from said first and coupled with said second support member and responsive to said second signal generating means for vibrating said elongated beam in said second plane in a phase and amplitude such as to reduce the signal from said second signal generating means to zero whereby the signal supplied to said second driver means is proportional to said rate of turn about said sensing axis.

2. Apparatus as described in claim 1 wherein said first and second elongate drive means are each substantially as long as the length of said elongate beam and concentrically disposed thereabout.

3. Apparatus as described in claim 1 wherein said first and second elongate drive means include diametrically opposed pairs of elongate piezoelectric columns so shaped and so disposed as to provide a generally cylindrical internal opening therebetween and wherein said second support member is secured to said first and second pairs of columns with said elongate beam extending into said internal opening.

4. Apparatus as described in claim 3 wherein said elongate beam includes a mass portion at its free end, wherein said first support member comprises a support ring adapted to secure said device on a body the rate of rotation of which is to be measured, and wherein said support ring and mass portion are approximately coplanar.

5. Apparatus as described in claim 4 wherein said first and second signal generating means include capacitive pick-off means including first and second pairs of electrode means mounted on said support ring and said mass portion comprises a common electrode cooperative with said first and second pairs of electrodes.

6. Apparatus as described in claim 3 wherein said second support member includes a plurality of radially extending pads raised from said second support member and affixed to corresponding ends of said elongate piezo-electric columns so as to serve as hinged connections between said columns and said second support means.

7. Apparatus as described in claim 5 wherein said first signal generator means includes:

first opposed capacitive plate means capacity coupled to said beam free end, and

first rectifier bridge means responsive to said first opposed capacitive plate means,

said first drive means being responsive to said rectifier bridge means whereby the vibration frequency of said beam in said first plane tracks the resonant frequency of said beam.

8. Apparatus as described in claim 7 wherein said

second signal generator means includes:

second opposed capacitive plate means capacitively coupled to said beam free end, and

second rectifier bridge means responsive to said second opposed capacitive plate means,

said second drive means being responsive to said second bridge rectifier means for suppressing vibration frequency components in said second plane.

9. Apparatus as described in claim 8 further including:

demodulator means having first and second inputs,

said first and second inputs being respectively responsive to said first and second bridge rectifiers, and

utilization means responsive to said demodulator means.

10. Apparatus as described in claim 5 wherein said inertial rate sensor is enclosed within a sealed housing containing a gas medium for a long term ambient control and wherein said capacitive pick-off means includes gas pressure relief configurations whereby the amplitude of vibration of said mass portion between said first and second pairs of electrodes is not significantly attenuated.

11. Apparatus as set forth in claim 9 wherein said inertial rate sensor is enclosed within a housing including two chambers, one of said chambers containing said support members, drive means, and signal generating means and the other of said chambers including said rectifier bridge means and said demodulator means, said one chamber being hermetically sealed from said other chamber.

12. Apparatus as described in claim 1 wherein said elongate beam is characterized by a natural frequency in said second plane different from its natural resonant frequency in said second plane.

13. Apparatus as described in claim 12 wherein the natural resonant frequency of said elongate beam in said second plane is higher than its natural frequency in said first plane.

14. Apparatus as described in claim 13 wherein said

first and second signal generating means include:

first and second opposed capacitive plate means coupled with said beam free end, and

first and second rectifier bridge means responsive to said first and second respective capacitive plate means,

said first and second drive means being responsive to said first and second bridge means, respectively, whereby the vibration frequency of said elongate beam in said first plane tracks the resonant frequency of said elongate beam in said first plane and the vibration frequency of said elongate beam in said second plane tracks the resonant frequency of said elongate beam in said second plane.

15. A force feed back inertial rate sensor for providing a measure of the rate of turn thereof about a sensing axis comprising:

a substantially rigid sensor support ring generally defining the sensing axis of said sensor and adapted to secure said sensor to a craft the turn rate of which about said axis is to be measured,

an elongate cylindrical driver means of piezoelectric material having one end thereof secured to said support ring and having its axis coincident with and extending along said sensing axis, the other end of said driver means being formed in quadrants providing two pairs of diametrically opposed, orthogonal actuator elements, each pair of elements including electrodes adapted to be energized to produce opposed elongation and contraction thereto in the direction of said axis,

an elongate beam having a flanged base portion secured to the ends of said actuator elements with said beam extending interiorly along said axis and its free end terminating closely adjacent said sensor support ring,

first and second pairs of diametrically opposed pick-off means secured to said sensor ring adjacent said beam free end and axially aligned with corresponding pairs of said actuator elements for detecting motion of the beam free end in first and second orthogonal planes defined by said corresponding pick-off means and actuator elements,

first electronic means coupled between said first pair of pick-off means and corresponding actuator elements for energizing said first pair of actuator elements so as to vibrate said beam through said beam base portion in said first plane at the natural resonant frequency of said beam,

second electronic means coupled between said second pair of pick-off means and corresponding actuator elements and responsive to any components of said beam vibration in said second plane produced by a turn rate of said sensor about said sensing axis for energizing said second pair of actuator elements and vibrating said beam through said beam base portion in said second plane at said resonant frequency, the sense of said energization-producing vibration of said beam being such as to oppose said vibration component in said second plane whereby to reduce the same toward zero and thereby maintain vibration of said beam in said first plane, and

means responsive to said second electronic means for providing said rate of turn measure.