Inertial sensor with flexure arrangement and method
An inertial sensor comprising; a central anchor; a proof mass, wherein the proof mass surrounds the central anchor; a flexure; and a plurality of electrodes is disclosed. The flexure has a shape comprising a first plurality of spiral arms, each winding about the central anchor in a first sense, and a second plurality of spiral arms, each winding about the central anchor in a second sense, the second sense being opposite to the first sense Each of the arms are connected between the central anchor and the proof mass. Advantageously, energy lost through anchor losses and thermoelastic dissipation are reduced in this arrangement, resulting in a higher quality factor for the modes of vibration.
1 . An inertial sensor comprising:
a central anchor;
a proof mass, wherein the proof mass surrounds the central anchor;
a flexure, the flexure having a shape comprising a first set of spiral arms, the first set of spiral arms comprising a first plurality of N spiral arms and a second plurality of N spiral arms, where N is an integer greater than 1, each of the arms connected between the central anchor and the proof mass and lying in a first plane, each of the arms of the first plurality of N spiral arms winding about the central anchor in a first sense and each of the arms of the second plurality of N spiral arms winding about the central anchor in a second sense, the second sense being opposite to the first sense; and
a plurality of electrodes comprising,
at least one drive electrode for driving the proof mass in a first mode of vibration, and
at least one sense electrode for sensing a response of the proof mass in a second mode of vibration.
2 . An inertial sensor according to claim 1 , wherein the arms of the first plurality of N spiral arms are equally spaced at 360/N degree intervals about the central anchor.
3 . An inertial sensor according to claim 1 , wherein the arms of the second plurality of N spiral arms are equally spaced at 360/N degree intervals about the central anchor.
4 . An inertial sensor according to claim 1 , wherein each of the arms in the first plurality of N spiral arms meets or crosses all of the arms from the second plurality of N spiral arms at least once.
5 . An inertial sensor according to claim 1 , wherein the flexure exhibits N-fold rotational symmetry about an axis perpendicular to the first plane.
6 . An inertial sensor according to claim 1 , wherein the central anchor, flexure and proof mass each exhibit N-fold rotational symmetry about an axis perpendicular to the first plane.
7 . An inertial sensor according to claim 1 , wherein the flexure has a shape comprising a plurality of nested quatrefoils, with each quatrefoil rotated by 45 degrees relative to adjacent quatrefoils.
8 . An inertial sensor according to claim 1 , wherein the flexure has a shape comprising a second set of spiral arms nested concentrically around the first set of spiral arms, the second set of spiral arms comprising a first plurality of N spiral arms and a second plurality of N spiral arms, each of the arms of the first plurality of N spiral arms winding about the central anchor in a first sense and each of the arms of the second plurality of N spiral arms winding about the central anchor in a second sense, the second sense being opposite to the first sense, wherein the arms of the second set of spiral arms may have a different curvature or shape to the arms of the first set of spiral arms.
9 . An inertial sensor according to claim 8 , wherein the flexure has a shape comprising further sets of spiral arms, wherein the sets of spiral arms are concentrically nested.
10 . An inertial sensor according to claim 1 , wherein each arm has a first end connected to the central anchor and a second end connected to the proof mass, wherein the first end connects to the central anchor at a point on the central anchor that is furthest from the second end of the arm.
11 . An inertial sensor according to claim 1 , wherein the proof mass is ring shaped.
12 . An inertial sensor according to claim 1 , wherein the thickness of the proof mass is greater than the thickness of the flexure.
13 . An inertial sensor according to claim 1 , wherein the flexure has a shape further comprising a plurality of N radial spokes, wherein each of the radial spokes are connected to the proof mass.
14 . An inertial sensor according to claim 1 , wherein each of the radial spokes are connected to at least one arm from the first plurality of N spiral arms or the second plurality of N spiral arms.
15 . An inertial sensor according to claim 1 , wherein Nis an integer multiple of 4.
16 . An inertial sensor according to claim 1 , wherein the plurality of electrodes comprises at least one electrode positioned outside of the proof mass.
17 . An inertial sensor according to claim 1 , wherein the inertial sensor is a micro-electro-mechanical system or MEMS device.
18 . A navigation system comprising an inertial sensor according to claim 1 .
19 . A method of inertial sensing using an inertial sensor according to claim 1 , comprising the steps of;
driving the proof mass in the first mode using at least one drive electrode;
sensing the response of the proof mass in a second mode using at least one sense electrode;
tuning the frequency of the first mode with respect to the second mode or tuning the frequency of the second mode with respect to the first mode to match the frequencies of the first mode and the second mode; and
calculating the value of an input measurand based on the response of the proof mass in the second mode.
20 . A method of inertial sensing according to claim 1 , wherein the value of the input measurand is calculated based on the difference between the resonant frequency of the first mode and the resonant frequency of the second mode.