Multi-axis inertial sensor with dual mass and integrated damping structure

• US 9,720,012 B2
• Filed: 07/21/2015
• Issued: 08/01/2017
• Est. Priority Date: 07/21/2015
• Status: Active Grant

• Current Assignee: NXP USA, Inc. (NXP Semiconductors NV)
• Original Assignee: NXP USA, Inc. (NXP Semiconductors NV)
• Inventors: Geisberger, Aaron A., Tang, Jun, Kniffin, Margaret L.
• Primary Examiner(s): KWOK, HELEN C
• Application Number:
  US14/805,105
• Publication Number:
  US 20170023608A1
• Time in Patent Office: 742 Days
• CPC Class Codes: G01P 15/125 by capacitive pick-up
• CPC Class Codes: G01P 15/18 in two or more dimensions
• CPC Class Codes: G01P 2015/0831 the mass being of the paddle type having the pivot axis between the longitudinal ends of the mass, e.g. see-saw configuration
• CPC Class Codes: G01P 2015/0882 for providing damping of vibrations

Abstract

An inertial sensor includes first and second movable elements suspended from a substrate and interconnected by a beam. The second movable element is positioned laterally adjacent to the first movable element, and each of the movable elements has a mass that is asymmetric relative to a rotational axis. A first spring system couples the first movable element to the substrate and a second spring system couples the second movable element to the substrate. The spring systems and the beam enable the movable elements to move together in response to force imposed upon the movable elements. In particular, the first and second movable elements can undergo in-plane torsion motion in response to force, such as acceleration, imposed in a sense direction. Additionally, damping structures may be integrated into the first and second movable elements to effectively increase a damping ratio of the device resulting from the in-plane torsion motion.

Claims

1. An inertial sensor comprising:

a substrate;

a first movable element suspended from said substrate;

a second movable element suspended from said substrate and positioned laterally adjacent to said first movable element, each of said first and second movable elements having a mass that is asymmetric relative to a rotational axis;

a first spring system coupling said first movable element to said substrate; and

a second spring system coupling said second movable element to said substrate, wherein said first and second spring systems enable said first and second movable elements to move together in response to force imposed upon said first and second movable elements in at least two orthogonal directions, wherein;

said first and second spring systems facilitate translatory motion of said first and second movable elements in response to a first force imposed upon said first and second movable elements in a first direction substantially parallel to a surface of said substrate; and

said first and second spring systems further facilitate in-plane torsion motion of said first and second movable elements in response to a second force imposed upon said first and second movable elements in a second direction substantially parallel to said surface of said substrate, said second direction being substantially orthogonal to said first direction.

2. The inertial sensor of claim 1 wherein said first and second spring systems further facilitate out-of-plane rotational motion of each of said first and second movable elements about said rotational axis in response to a third force imposed upon said first and second movable elements in a third direction substantially perpendicular to said surface of said substrate.

3. The inertial sensor of claim 1 further comprising a beam interconnected between said first and second movable elements.

4. The inertial sensor of claim 3 wherein:

said first movable element includes a first portion positioned on a first side of said rotational axis and a second portion positioned on a second side of said rotational axis, said first portion having greater mass than said second portion;

said second movable element includes a third portion positioned on said first side of said rotational axis and a fourth portion positioned on said second side of said rotational axis, said third portion having greater mass than said fourth portion; and

said beam has a first end coupled to a first outer edge of said first portion of said first movable element and a second end coupled to a second outer edge of said third portion of said second movable element, said first and second outer edges being distal from a midline of said inertial sensor disposed between said first and second movable elements.

5. The inertial sensor of claim 1 wherein:

said first and second movable elements are disposed on opposing sides of a midline positioned between said first and second movable elements, said midline being oriented substantially parallel to a direction of said translatory motion of said first and second movable elements; and

said rotational axis is substantially parallel to a surface of said substrate and substantially perpendicular to said midline.

6. The inertial sensor of claim 1 wherein:

said first spring system includes a first anchor element coupled to said substrate at said rotational axis and a first spring having a first end coupled to said first anchor element and a second end coupled to said first movable element; and

said second spring system includes a second anchor element coupled to said substrate at said rotational axis and a second spring having a third end coupled to said second anchor element and a fourth end coupled to said second movable element.

7. The inertial sensor of claim 1 further comprising first, second, third, and fourth electrodes coupled to a surface of said substrate, wherein:

for said first movable element, said first and second electrodes are positioned proximate a first outer edge of said first movable element and said third and fourth electrodes are positioned proximate a first inner edge of said first movable element; and

for said second movable element, said first and second electrodes are positioned proximate a second inner edge of said second movable element and said third and fourth electrodes are positioned proximate a second outer edge of said second movable element, said first and second inner edges being positioned closer to a midline of said inertial sensor than said first and second outer edges.

8. The inertial sensor of claim 1 further comprising:

a first damping structure extending from a first inner edge of said first movable element; and

a second damping structure extending from a second inner edge of said second movable element toward said first movable element, said second damping structure being operatively coupled with said first damping structure to dampen an oscillatory response of said first and second movable elements.

9. The inertial sensor of claim 8 wherein:

said first and second damping structures dampen said oscillatory response of said first and second movable elements resulting from said in-plane torsion motion.

10. The inertial sensor of claim 8 wherein:

said first movable element includes a first portion positioned on a first side of said rotational axis and a second portion positioned on a second side of said rotational axis, said first portion having greater mass than said second portion;

said second movable element includes a third portion positioned on said first side of said rotational axis and a fourth portion positioned on said second side of said rotational axis, said third portion having greater mass than said fourth portion;

said first damping structure extends from said first portion of said first movable element; and

said second damping structure extends from said third portion of said second movable element.

11. The inertial sensor of claim 8 wherein:

said first damping structure comprises a plurality of first fingers extending from said first movable element; and

said second damping structure comprises a plurality of second fingers extending from said second movable element and interleaved with said first fingers.

12. An inertial sensor comprising:

a substrate;

a first movable element suspended from said substrate;

a second movable element suspended from said substrate and positioned laterally adjacent to said first movable element, each of said first and second movable elements having a mass that is asymmetric relative to a rotational axis;

a beam interconnected between said first and second movable elements;

a first spring system coupling said first movable element to said substrate, said first spring system including a first anchor element coupled to said substrate at said rotational axis and a first spring having a first end coupled to said first anchor element and a second end coupled to said first movable element; and

a second spring system coupling said second movable element to said substrate, said second spring system including a second anchor element coupled to said substrate at said rotational axis and a second spring having a third end coupled to said second anchor element and a fourth end coupled to said second movable element wherein said beam and said first and second spring systems enable said first and second movable elements to move together in response to force imposed upon said first and second movable elements in at least two orthogonal directions, and wherein;

said first and second spring systems facilitate translatory motion of said first and second movable elements in response to a first force imposed upon said first and second movable elements in a first direction substantially parallel to a surface of said substrate; and

said first and second spring systems facilitate in-plane torsion motion of said first and second movable elements in response to a second force imposed upon said first and second movable elements in a second direction substantially parallel to said surface of said substrate, said second direction being substantially orthogonal to said first direction.

13. The inertial sensor of claim 12 wherein:

said first and second spring systems facilitate out-of-plane rotational motion of each of said first and second movable elements about said rotational axis in response to a third force imposed upon said first and second movable elements in a third direction substantially perpendicular to said surface of said substrate.

14. The inertial sensor of claim 12 wherein:

said first movable element includes a first portion positioned on a first side of said rotational axis and a second portion positioned on a second side of said rotational axis, said first portion having greater mass than said second portion;

said second movable element includes a third portion positioned on said first side of said rotational axis and a fourth portion positioned on said second side of said rotational axis, said third portion having greater mass than said fourth portion; and

said beam has a first end coupled to a first outer edge of said first portion of said first movable element and a second end coupled to a second outer edge of said third portion of said second movable element, said first and second outer edges being distal from a midline of said inertial sensor disposed between said first and second movable elements.

15. The inertial sensor of claim 12 further comprising first, second, third, and fourth electrodes coupled to a surface of said substrate, wherein:

for said first movable element, said first and second electrodes are positioned proximate a first outer edge of said first movable element and said third and fourth electrodes are positioned proximate a first inner edge of said first movable element; and

for said second movable element, said first and second electrodes are positioned proximate a second inner edge of said second movable element and said third and fourth electrodes are positioned proximate a second outer edge of said second movable element, said first and second inner edges being positioned closer to a midline of said inertial sensor than said first and second outer edges.

16. An inertial sensor comprising:

a substrate;

a first movable element suspended from said substrate;

a second movable element suspended from said substrate and positioned laterally adjacent to said first movable element, each of said first and second movable elements having a mass that is asymmetric relative to a rotational axis;

a first damping structure extending from a first inner edge of said first movable element toward said second movable element;

a second damping structure extending from a second inner edge of said second movable element toward said first movable element;

a first spring system coupling said first movable element to said substrate; and

a second spring system coupling said second movable element to said substrate, said first and second spring systems enabling said first and second movable elements to move together, wherein;

said first and second spring systems facilitate translatory motion of said first and second movable elements in response to a first force imposed upon said first and second movable elements in a first direction substantially parallel to a surface of said substrate;

said first and second spring systems further facilitate in-plane torsion motion of said first and second movable elements in response to a second force imposed upon said first and second movable elements in a second direction substantially parallel to said surface of said substrate, said second direction being substantially orthogonal to said first direction; and

said second damping structure is operatively coupled with said first damping structure to dampen an oscillatory response of said first and second movable elements resulting from said in-plane torsion motion.

17. The inertial sensor of claim 16 wherein:

said first movable element includes a first portion positioned on a first side of said rotational axis and a second portion positioned on a second side of said rotational axis, said first portion having greater mass than said second portion;

said second movable element includes a third portion positioned on said first side of said rotational axis and a fourth portion positioned on said second side of said rotational axis, said third portion having greater mass than said fourth portion; and

said inertial sensor further comprises a beam, said beam having a first end coupled to a first outer edge of said first portion of said first movable element and a second end coupled to a second outer edge of said third portion of said second movable element, said first and second outer edges being distal from a midline of said inertial sensor disposed between said first and second movable elements.

18. The inertial sensor of claim 16 wherein:

said first movable element includes a first portion positioned on a first side of said rotational axis and a second portion positioned on a second side of said rotational axis, said first portion having greater mass than said second portion;

said second movable element includes a third portion positioned on said first side of said rotational axis and a fourth portion positioned on said second side of said rotational axis, said third portion having greater mass than said fourth portion;

said first damping structure extends from said first portion of said first movable element; and

said second damping structure extends from said third portion of said second movable element.

19. The inertial sensor of claim 16 wherein:

said first damping structure comprises a plurality of first fingers extending from said first movable element; and

said second damping structure comprises a plurality of second fingers extending from said second movable element and interleaved with said first fingers.