Hall sensor

• US 10,527,455 B2
• Filed: 04/15/2016
• Issued: 01/07/2020
• Est. Priority Date: 04/16/2015
• Status: Active Grant

• Current Assignee: Max Baermann GmbH
• Original Assignee: Max Baermann GmbH
• Inventors: Schliesch, Thomas
• Primary Examiner(s): Koval, Melissa J
• Assistant Examiner(s): Nguyen, Trung
• Application Number:
  US15/565,975
• Publication Number:
  US 20180106642A1
• Time in Patent Office: 1,362 Days
• Field of Search: 32420711-20725, 324200, 324233, 324600, 324617, 324622, 324631, 324500, 324521, 324683, 324709, 324 66, 324 7611, 324 7652- 7677, 324 86, 324107
• CPC Class Codes: G01D 5/145 influenced by the relative movement between the Hall device and magnetic fields see G01R33/06
• CPC Class Codes: H02K 11/215 Magnetic effect devices, e.g. Hall-effect or magneto-resistive elements

Abstract

A sensor assembly is provided for determining an angular position of a rotor in relation to a stator, including two components, a magnet and a sensor, where the components are arranged in such a way that the components can be rotated in relation to each other about an axis of rotation, and the sensor includes a first and a second sensor pair, each having a first and a second sensor element. A straight line is associated with each sensor pair, along which straight line the two sensor elements lie and which straight line intersects with the axis of rotation, where the first sensor element has a smaller distance from the axis of rotation than the second sensor element, and the straight line associated with the first sensor pair is spaced apart from the straight line associated with the second sensor pair by a rotational angle about the axis of rotation.

Claims

1. A sensor assembly (1) for determining an angular position of a rotor (4) relative to a stator (5), comprising two components, namely a magnet (2) and a sensor (3),

wherein said components (2, 3) are arranged for rotation relative to each other about an axis of rotation (A),

wherein the sensor (3) comprises a first and a second sensor pair (31, 32), each one having a first sensor element and a second sensor element (311, 312, 321, 322), each one of the sensor elements (311, 312, 321, 322) being configured for determining a magnetic field strength to which it is exposed;

wherein each sensor pair (31, 32) has a straight line (313, 323) associated therewith, along which the two sensor elements (311, 312, 321, 322) lie and which intersects with the axis of rotation (A),

wherein the first sensor element (311, 321) has a smaller radial distance from the axis of rotation (A) than the second sensor element (312, 322),

wherein both sensor elements (311, 312, 321, 322) lie on the same radial side of the axis of rotation (A), and

wherein the straight line (313) associated with the first sensor pair (31) is spaced apart from the straight line (323) associated with the second sensor pair (32) by a rotational angle (β

) about the axis of rotation (A),

the sensor assembly (1) further comprising a computing unit for determining the angular position of the rotor (4) relative to the stator (5), wherein the computing unit is configured to determine measured values from the sensor elements (311, 312, 321, 322), which measured values are proportional to a magnetic field prevailing at the respective sensor element (311, 312, 321, 322),

wherein, for eliminating an interfering influence of an external interfering magnetic field, the computing unit is configured to determine a first differential value by subtracting a measured value determined from the first sensor element (311) of the first sensor pair (31) from a measured value determined from the second sensor element (312) of the first sensor pair (31), and to determine a second differential value by subtracting a measured value determined from the first sensor element (321) of the second sensor pair (32) from a measured value determined from the second sensor element (322) of the second sensor pair (32), and to determine the angular position of the rotor (4) relative to the stator (5) from the ratio of said differential values.

2. The sensor assembly (1) as claimed in claim 1, wherein the radial distance between the two sensor elements (321, 322) of the first sensor pair (31) corresponds to the radial distance between the two sensor elements (311, 312) of the second sensor pair (32).

3. The sensor assembly (1) as claimed in claim 1, wherein the first sensor element (311) of the first sensor pair (31) has the same radial distance from the axis of rotation (A) as the first sensor element (321) of the second sensor pair (32);

and/or wherein the second sensor element (312) of the first sensor pair (31) has the same radial distance from the axis of rotation (A) as the second sensor element (322) of the second sensor pair (32).

4. The sensor assembly (1) as claimed in claim 1, wherein the magnet (2) is configured as a multi-pole magnet (2) with at least two, in particular at least four poles, for providing a magnetic field with a magnetic field strength that is distributed periodically about the axis of rotation (A) as a function of a rotational angle, with a period length τ

.

5. The sensor assembly (1) as claimed in claim 4, wherein the rotational angle (β

) about which the straight lines (313, 323) of the two sensor pairs (31, 32) are spaced apart from each other is

6. The sensor assembly (1) as claimed in claim 1, wherein the magnet (2) is configured so that a magnetic field component of a specific direction of a magnetic field generated by the magnet (2) changes monotonically, in particular linearly, within a radius section, wherein the sensor elements (311, 312, 321, 322) of the sensor (3) are arranged within said radius section.

7. The sensor assembly (1) as claimed in claim 1, wherein at least one of the sensor pairs (31, 32) comprises at least three of the sensor elements (311, 312, 321, 322), each one lying along the straight line (313, 323) associated with the sensor pair (31, 32);

and/or wherein the sensor (3) comprises at least three sensor pairs (31, 32) each one having a respective straight line (313, 323) associated therewith along which the sensor elements (311, 312, 321, 322) of the respective sensor pair (31, 32) are arranged, wherein all the straight lines (313, 323) are spaced apart from each other by a rotational angle about the axis of rotation (A) and intersect in the axis of rotation (A).

8. The sensor assembly (1) as claimed in claim 1, wherein the sensor elements (311, 312, 321, 322) are configured as Hall sensor elements outputting a Hall voltage as a measured value.

9. The sensor assembly (1) as claimed in claim 1, wherein the measured values are proportional to a field component of the magnetic field perpendicular to the axis of rotation (A), in particular proportional to a radial field component of the magnetic field.

10. The sensor assembly (1) as claimed in claim 1, wherein the computing unit is configured to determine the angular position based on an angle α

, and to determine the angle α

using the equation

11. The sensor assembly (1) as claimed in claim 1, further comprising the stator (5) and the rotor (4),

wherein one of the two components (2, 3) is arranged on the rotor (4) and the other one is arranged on the stator (5).

12. Use of a sensor assembly (1) as claimed in claim 1 for determining the angular position of the rotor (4) relative to the stator (5), wherein measured values are derived from the sensor elements (311, 312, 321, 322) of the sensor pairs (31, 32), wherein for eliminating an interfering influence of an external interfering magnetic field, a first differential value is determined by subtracting a measured value determined from the first sensor element (311) of the first sensor pair (31) from a measured value determined from the second sensor element (312) of the first sensor pair (31), and a second differential value is determined by subtracting a measured value determined from the first sensor element (321) of the second sensor pair (32) from a measured value determined from the second sensor element (322) of the second sensor pair (32), and the angular position is determined from the ratio of the two differential values.

13. A method for determining an angular position of a rotor (4) relative to a stator (5) using a sensor assembly (1) that comprises two components, namely a magnet (2) and a sensor (3), one of the two components (2, 3) being arranged on the rotor (4) and the other one on the stator (5),

wherein the sensor (3) comprises a first and a second sensor pair (31, 32), each one comprising two sensor elements (311, 312, 321, 322),

wherein each sensor pair (31, 32) has a straight line (313, 323) associated therewith, along which the two sensor elements (311, 312, 321, 322) lie and which intersects with the axis of rotation (A),

wherein the first sensor element (311, 321) has a smaller radial distance from the axis of rotation (A) than the second sensor element (312, 322),

wherein both sensor elements (311, 312, 321, 322) lie on the same radial side of the axis of rotation (A), and

wherein the straight line (313) associated with the first sensor pair (31) is spaced apart from the straight line (323) associated with the second sensor pair (32) by a rotational angle (β

) about the axis of rotation (A), such that the sensor pairs (31, 32) are spaced apart from each other by a rotational angle (β

) about an axis of rotation (A) about which the rotor (4) is rotatable relative to the stator (5),

wherein measured values are determined from the sensor elements (311, 312, 321, 322), each measured value being proportional to a magnetic field prevailing at the respective sensor element (311, 312, 321, 322),

wherein, for eliminating an interfering influence of an external interfering magnetic field, a first differential value is determined by subtracting a measured value determined from the first sensor element (311) of the first sensor pair (31) from a measured value determined from the second sensor element (312) of the first sensor pair (31), and a second differential value is determined by subtracting a measured value determined from the first sensor element (321) of the second sensor pair (32) from a measured value determined from the second sensor element (322) of the second sensor pair (32), and

wherein the angular position is determined from the ratio of the two differential values.