Method for detecting disturbances when determining the rotational speed of a rotor and evaluation circuit

• US 7,295,000 B2
• Filed: 05/27/2005
• Issued: 11/13/2007
• Est. Priority Date: 05/26/2004
• Status: Active Grant

• Current Assignee: Infineon Technologies AG
• Original Assignee: Infineon Technologies AG
• Inventors: Werth, Tobias
• Primary Examiner(s): LEDYNH, BOT L
• Application Number:
  US11/140,590
• Publication Number:
  US 20050278136A1
• Time in Patent Office: 900 Days
• Field of Search: 324/207.25, 324/160, 324/166, 735/143.1, 735/143.9, 702/142, 702/145
• US Class Current: 324/166
• CPC Class Codes: G01P 13/045 with speed indication
• CPC Class Codes: G01P 3/489 Digital circuits therefor

Abstract

The invention relates to a rotary encoder and to a method for detecting disturbances in such a rotary encoder. In this case, vibrations or other disturbances are detected by means of the phase difference between a rotational speed signal, which represents a rotational speed of a rotor, and a direction of rotation signal, which represents a direction of rotation of the rotor.

Claims

1. A method for detecting disturbances when determining a rotational speed of a rotor, the method comprising:

providing a first rotational speed signal representative of a rotational speed of the rotor;

providing a first direction of rotation signal representative of a direction of rotation of the rotor; and

determining a phase difference between the first rotational speed signal and the first direction of rotation signal.

2. The method of claim 1, further comprising:

detecting a disturbance when the phase difference falls below a lower limit value or exceeds an upper limit value.

3. The method of claim 2, wherein:

the lower limit value is at most approximately 70 degrees less than a desired phase difference; and

the upper limit value is at most approximately 70 degrees greater than the desired phase difference.

4. The method of claim 2, wherein the lower and upper limit values are based on the first rotational speed signal.

5. The method of claim 4, wherein the lower and upper limit values are based on an amplitude of the first rotational speed signal.

6. The method of claim 1, wherein the step of determining the phase difference further comprises:

ascertaining a first signal value for the first direction of rotation signal at a first instant, the first instant being ascertained at a zero crossing of the first rotational speed signal in a rising signal profile;

ascertaining a second signal value for the first direction of rotation signal at a second instant, the second instant being ascertained at a zero crossing of the first rotational speed signal in a falling signal profile; and

determining the difference between the first signal value and the second signal value.

7. The method according to claim 6, wherein the first and second instants are ascertained in successive zero crossings of the first rotational speed signal.

8. The method of claim 1, wherein the rotational speed signal is a sinusoidal signal.

9. The method of claim 1, further comprising:

providing a first signal source for generating a first phase signal corresponding to at least one rotation of a rotor;

providing a second signal source for generating a second phase signal corresponding to the at least one rotation of the rotor;

providing a third signal source for generating a third phase signal corresponding to the at least one rotation of the rotor;

generating the first rotational speed signal based on a difference between the first phase signal and the third phase signal;

generating the first direction of rotation signal based on a difference between the second phase signal and half of a sum of the first phase signal and the third phase signal.

10. A method for generating a signal containing information about a rotational speed or direction of a rotor, the method comprising:

providing a first rotational speed signal representing the rotational speed of a rotor;

providing a first direction of rotation signal representing the direction of rotation of the rotor;

detecting disturbances by analyzing a phase difference between the first rotational speed signal and the first direction rotation signal; and

in cases where no disturbance is detected, generating an output signal based on the first rotational speed signal or the first direction of rotation signal.

11. The method of claim 10, wherein the output signal comprises at least one of the group consisting of:

a second rotational speed signal based on the first rotational speed signal; and

a second direction of rotation signal based on the first direction of rotation signal.