MEMS tri-axial accelerometer with one or more decoupling elements

Patent metadata

Field	Value
Publication number	US-12584940-B2
Application number	US-202318308543-A
Country	US
Kind code	B2
Filing date	Apr 27, 2023
Priority date	Nov 3, 2016
Publication date	Mar 24, 2026
Grant date	Mar 24, 2026

Abstract

A MEMS tri-axial accelerometer is provided with a sensing structure having: a single inertial mass, with a main extension in a horizontal plane defined by a first horizontal axis and a second horizontal axis and internally defining a first window that traverses it throughout a thickness thereof along a vertical axis orthogonal to the horizontal plane; and a suspension structure, arranged within the window for elastically coupling the inertial mass to a single anchorage element, which is fixed with respect to a substrate and arranged within the window, so that the inertial mass is suspended above the substrate and is able to carry out, by the inertial effect, a first sensing movement, a second sensing movement, and a third sensing movement in respective sensing directions parallel to the first, second, and third horizontal axes following upon detection of a respective acceleration component. In particular, the suspension structure has at least one first decoupling element for decoupling at least one of the first, second, and third sensing movements from the remaining sensing movements.

First claim

The invention claimed is:

1 . A device, comprising:
a substrate; a tri-axial accelerometer that includes:
an anchorage element fixed to the substrate;
an inertial mass on the substrate, having a main extension in a horizontal plane defined by a first horizontal axis and a second horizontal axis, the mass including:
a first window through the mass, a thickness of the mass extending along a vertical axis orthogonal to the horizontal plane, the anchorage element being within the first window;

a suspension structure in the first window and elastically coupled between the inertial mass and the anchorage element, the inertial mass spaced from the substrate, the inertial mass configured to, in operation, perform:
a first sensing movement in a first sensing direction parallel to the first horizontal axis in response to a first acceleration component;
a second sensing movement along a second sensing direction parallel to the second horizontal axis in response to a second acceleration component; and
a third sensing movement along a third sensing direction parallel to the vertical axis in response to a third acceleration component, and

wherein the suspension structure includes a first decoupling element configured to, in operation, decouple at least one of the first, second, and third sensing movements from the remaining sensing movements of the inertial mass.

2 . The device according to claim 1 , wherein the suspension structure comprises first elastic elements elastically coupled between the first decoupling element and the anchorage element, and second elastic elements elastically coupled between the first decoupling element and the inertial mass, the second elastic elements are configured to, in operation, enable and control, independently and exclusively, the at least one of the first, second, and third sensing movements.

3 . The device according to claim 2 , wherein the at least one of the first, the second, and the third sensing movements is a resonant vibration movement, and the second elastic elements are configured to, in operation, determine a vibrational mode of the at least one of the first, the second, and the third sensing movements.

4 . The device according to claim 2 , wherein the first elastic elements are rigid with respect to the at least one of the first, second, and third sensing movements.

5 . The device according to claim 2 , wherein the first decoupling element is a frame and includes a second window, the first elastic elements and the anchorage element being within the frame.

6 . The device according to claim 5 , wherein the first elastic elements extend, within the second window, from the first decoupling element to the anchorage element, and the second elastic elements extend, outside the second window, from the first decoupling element to the inertial mass.

7 . The device according to claim 2 , wherein the first elastic elements are a linear type and extend parallel to the first horizontal axis, aligned on opposite sides with respect to the anchorage element along the first horizontal axis and the second elastic elements are of a folded type and extend, aligned on opposite sides of the anchorage element along the second horizontal axis, between the inertial mass and the first decoupling element.

8 . The device according to claim 2 , wherein the suspension structure further comprises a second decoupling element configured to, in operation, decouple at least one further of the first, second, and third sensing movements, different from the at least one of the first, second, and third sensing movements, from the remaining sensing movements.

9 . The device according to claim 8 , wherein the first, second, and third sensing movements are resonant vibration movements, and wherein the suspension structure is configured to, in operation, decouple each of the first, second, and third sensing movements from the remaining sensing movements, and to determine a vibrational mode independently and exclusively.

10 . The device according to claim 8 , wherein the first elastic elements are elastically coupled between the first decoupling element and the second decoupling element and the suspension structure further comprises third elastic elements, elastically coupling the second decoupling element to the anchorage element.

11 . A device, comprising:
a substrate; a tri-axial accelerometer that includes:
an anchorage element fixed to the substrate;
an inertial mass on the substrate, having a main extension in a horizontal plane defined by a first horizontal axis and a second horizontal axis, the first horizontal axis is transverse to the second horizontal axis, the mass including:
a first window through the mass, a thickness of the mass extending along a vertical axis orthogonal to the horizontal plane, the anchorage element being within the first window;

a suspension structure in the first window and elastically coupled between the inertial mass and the anchorage element, the inertial mass spaced from the substrate, the inertial mass configured to, in operation, perform:
a first sensing movement in a first sensing direction parallel to the first horizontal axis in response to a first acceleration component, and the first sensing movement is a first rotational movement;
a second sensing movement along a second sensing direction parallel to the second horizontal axis in response to a second acceleration component; and
a third sensing movement along a third sensing direction parallel to the vertical axis in response to a third acceleration component, and the third sensing movement is a second rotational movement, and

wherein the suspension structure includes a first decoupling element configured to, in operation, decouple at least one of the first, second, and third sensing movements from the remaining sensing movements of the inertial mass, and
wherein the suspension structure comprises first elastic elements elastically coupled between the first decoupling element and the anchorage element, and second elastic elements elastically coupled between the first decoupling element and the inertial mass, the second elastic elements are configured to, in operation, enable and control, independently and exclusively, the at least one of the first, second, and third sensing movements.

12 . The device of claim 11 , wherein the first horizontal axis is perpendicular to the second horizontal axis.

13 . The device of claim 12 , wherein the vertical axis is perpendicular to the first horizontal axis and the second horizontal axis.

14 . The device of claim 11 , wherein the second sensing movement is a linear movement.

15 . The device of claim 11 , wherein:
the first rotational movement is about the vertical axis; and the second rotational movement is about the first horizontal axis.

16 . The device of claim 11 , wherein the first horizontal axis is perpendicular to the second horizontal axis.

17 . The device of claim 11 , wherein the vertical axis is perpendicular to the first horizontal axis and the second horizontal axis.

18 . The device of claim 11 , wherein:
the first rotational movement is about the vertical axis; and the second rotational movement is about the first horizontal axis.

19 . The device of claim 11 , further comprising one or more fixed electrodes on the substrate.

20 . A device, comprising:
a substrate; a tri-axial accelerometer that includes:
an anchorage element fixed to the substrate;
an inertial mass on the substrate, having a main extens

Assignees

• St Microelectronics Srl

Inventors

• Tocchio Alessandro
• Rizzini Francesco

Classifications

• G01P2015/0848

  using a plurality of mechanically coupled spring-mass systems, the sensitive direction of each system being different · CPC title

• G01P15/125 Primary

  by capacitive pick-up · CPC title

• G01P15/097

  by vibratory elements · CPC title

• G01P2015/0845

  using a plurality of spring-mass systems being arranged on one common planar substrate, the systems not being mechanically coupled and the sensitive direction of each system being different · CPC title

• G01P15/18 Primary

  in two or more dimensions · CPC title