Planar Coriolis gyroscope

• US 9,303,994 B2
• Filed: 03/08/2012
• Issued: 04/05/2016
• Est. Priority Date: 03/08/2011
• Status: Active Grant

• Current Assignee: Y-Sensors, Ltd.
• Original Assignee: Y-Sensors, Ltd.
• Inventors: Netzer, Yishay, Girgel, Michael
• Primary Examiner(s): Chapman, Jr., John
• Application Number:
  US14/002,741
• Publication Number:
  US 20130333470A1
• Time in Patent Office: 1,489 Days
• Field of Search: 735/041.2
• US Class Current: 1/1
• CPC Class Codes: G01C 19/56 Turn-sensitive devices using vibrating masses, e.g. vibratory angular rate sensors based on Coriolis forces
• CPC Class Codes: G01C 19/574 the devices having two sensing masses in anti-phase motion
• CPC Class Codes: G01C 19/5747 each sensing mass being connected to a driving mass, e.g. driving frames

Abstract

A planar Coriolis gyroscope includes at least two counter oscillating masses attached to a common rigid frame by one or more elastic members defining an excitation axis. The frame is attached to a support region by one or more additional elastic members which together with the masses define a Coriolis resonator. The Coriolis resonator responds to inertial rotation of the gyroscope and in conjunction with a position pickoff provides a signal indicative on the gyroscope inertial rotation.

Claims

1. An inertial rotation rate sensor comprising:

(a) a lower substrate;

(b) a device layer substantially parallel to said lower substrate, said device layer comprising;

(i) a substantially rigid frame supported by a first plurality of compliant members that extend from a support region attached to said lower substrate, and

(ii) at least two masses each supported by a second plurality of compliant members which extend from said frame,

such that said at least two masses in conjunction with said second plurality of compliant members make up a first resonator having at least a first mode of motion relative to said frame in which said at least two masses undergo counter-oscillation,

and such that said at least two masses and said frame in conjunction with said first plurality of compliant members make up a second resonator having at least a first mode in which said frame and said at least two masses oscillate together relative to said lower substrate;

(c) an actuator deployed for exciting oscillatory motion of said first resonator, referred to as the excitation resonator; and

(d) a position pickoff deployed for sensing a current position of said second resonator, referred to as the Coriolis resonator,

such that, when said excitation resonator is driven via said actuator in an oscillatory motion, said oscillatory motion combines with an inertial rotation rate around a rotation axis to generate a Coriolis force acting on said at least two masses to excite the first mode of said Coriolis resonator, thereby allowing derivation of the inertial rotation rate about the rotation axis,

wherein said first plurality of compliant members comprises two spaced-apart parallel beams integrated at a central region of said parallel beams with said support region and integrated at extremities of said parallel beams with said frame.

2. The sensor of claim 1, wherein said first mode of said Coriolis resonator is an in-plane rotational mode.

3. The sensor of claim 2, wherein said position pickoff of said Coriolis resonator comprises at least one interdigitated comb arrangement comprising a first comb supported by said frame and a second comb supported from said substrate, wherein said comb arrangement includes comb elements aligned substantially radially with respect to said support region.

4. The sensor of claim 1, further comprising a processing system including at least one processor, said processing system being associated with said actuator and said position pickoff and being configured to:

(i) actuate said actuator so as to generate oscillatory motion of said excitation resonator, and

(ii) process a signal from said position pickoff indicative of a motion of said Coriolis oscillator, thereby determining the inertial rotation rate about the rotation axis.

5. The sensor of claim 1, wherein said position pickoff is part of a force balance arrangement deployed for opposing motion of said Coriolis oscillator, the sensor further comprising a processing system including at least one processor, said processing system being associated with said actuator and said force balance arrangement, and being configured to:

(i) actuate said actuator so as to generate oscillatory motion of said excitation resonator, and

(ii) process a signal from said force balance arrangement indicative of said Coriolis force on said at least two masses, thereby determining the inertial rotation rate about the rotation axis.

6. The sensor of claim 1, wherein positions and dimensions of said first plurality of compliant members are such that a resonant frequency of said second resonator substantially matches a resonant frequency of said first resonator.

7. The sensor of claim 1, further comprising a top substrate overlying said device layer, wherein said top substrate is attached to said support region of said device layer such that said device layer is symmetrically supported between said substrate and said top substrate.

8. The sensor of claim 7, wherein said substrate and said top substrate together form part of an at least partially evacuated sealed enclosure.