Three-Axis Nano-Resonator Accelerometer Device and Method

• US 20140090471A1
• Filed: 10/18/2013
• Published: 04/03/2014
• Est. Priority Date: 12/13/2011
• Status: Abandoned Application

• Current Assignee: Ying Wen Hsu
• Original Assignee: Ying Wen Hsu
• Inventors: Hsu, Ying Wen
• Application Number:
  US14/057,013
• Publication Number:
  US 20140090471A1
• Time in Patent Office: Days
• US Class Current: 73/514.29
• CPC Class Codes: G01C 19/5712 the devices involving a micromechanical structure
• CPC Class Codes: G01C 19/5776 Signal processing not specific to any of the devices covered by groups G01C19/5607 - G01C19/5719
• CPC Class Codes: G01P 15/097 by vibratory elements
• CPC Class Codes: G01P 15/0975 by acoustic surface wave resonators or delay lines

Abstract

An inertial measurement device and method for measuring acceleration in three axes. Three orthogonally disposed accelerometers are defined on a common planar substrate. At least one of the accelerometers is provided with a proof mass coupled to a nano-resonator element. The nano-resonator element is oscillated at a first predetermined frequency, which may be a first resonant frequency, and is altered to oscillate at a second frequency, which may be a second resonant frequency, in response to a resultant force produced by the acceleration of the proof mass. The degree of change in nano-resonator element output frequency is sensed and processed using suitable processing circuitry as a change in acceleration on the active axis.

Claims

1. A method for measuring acceleration on three orthogonal axes comprising the steps of:

providing a first, a second and a third inertial sensor on a planar substrate,

orienting the first inertial sensor to measure a first acceleration on a first axis parallel to the substrate,

orienting the second inertial sensor to measure a second acceleration on a second axis perpendicular to the first axis and parallel to the substrate,

orienting the third inertial sensor to measure a third acceleration on a third axis perpendicular to the substrate,

wherein at least one of the inertial sensors comprises a proof mass coupled to a plurality of nano-resonators that are longitudinally disposed parallel to a direction of deflection of the proof mass resulting from the first, second or third accelerations,

the nano-resonators comprising a sense means and a drive means disposed on a first thickness of the nano-resonators,

the nano-resonators configured to be capable of being oscillated at a first predetermined frequency and configured to oscillate at a second frequency in response to a resultant force produced by the first, second or third accelerations of the proof mass.

2. The method of claim 1 wherein the at least one inertial sensor further comprises a proof mass drive means configured for oscillating the proof mass at a proof mass frequency, wherein the proof mass and the nano-resonator element of the at least one inertial sensor are coupled whereby the proof mass frequency modulates a nano-resonator output frequency.

3. A three-axis accelerometer structure comprising:

a planar substrate,

a first accelerometer device supported by the planar substrate and configured to measure a first acceleration on a first axis extending in a plane of the substrate,

a second accelerometer device supported by the planar substrate and configured to measure a second acceleration on a second axis extending in the plane of the substrate and perpendicular to the first axis,

a third accelerometer device supported by the planar substrate and configured to measure a third acceleration on a third axis that is perpendicular to the plane of the substrate,

wherein at least one of the accelerometer devices comprises a proof mass coupled to a plurality of nano-resonators that are longitudinally disposed parallel to a direction of deflection of the proof mass resulting from the first, second or third accelerations,

the nano-resonators comprising a sense means and a drive means disposed on a first thickness of the nano-resonators, and,

the nano-resonators configured to be oscillated at a first predetermined frequency and configured to be altered to oscillate at a second frequency in response to a resultant force produced by the first, second or third accelerations of the proof mass.

4. The structure of claim 3 wherein at least one of the accelerometer devices further comprises proof mass drive means for oscillating the proof mass at a proof mass frequency wherein the proof mass and the nano-resonator are coupled whereby the proof mass frequency modulates a nano-resonator output frequency.

5. A method for measuring acceleration on three orthogonal axes comprising the steps of:

providing a first, a second and a third inertial sensor on a planar substrate,

orienting the first inertial sensor to measure a first acceleration on a first axis parallel to the substrate,

orienting the second inertial sensor to measure a second acceleration on a second axis perpendicular to the first axis and parallel to the substrate,

orienting the third inertial sensor to measure a third acceleration on a third axis perpendicular to the substrate,

wherein at least one of the inertial sensors comprises a proof mass coupled to a plurality of nano-resonators that are longitudinally disposed parallel to a direction of deflection of the proof mass resulting from an acceleration,

the nano-resonators comprising a sense means and a drive means disposed on a first thickness of the nano-resonators,

the nano-resonators configured to be capable of being oscillated at a first predetermined frequency and configured to oscillate at a second frequency in response to a resultant force produced by the acceleration of the proof mass.