Method to detect marginally large air gaps on heavy vehicle wheel speed sensor installations

• US 8,818,673 B1
• Filed: 03/28/2013
• Issued: 08/26/2014
• Est. Priority Date: 03/28/2013
• Status: Active Grant

• Current Assignee: Bendix Commercial Vehicle Systems LLC (Estate of Heinz Hermann Thiele)
• Original Assignee: Bendix Commercial Vehicle Systems LLC (Estate of Heinz Hermann Thiele)
• Inventors: Frashure, Timothy J., Haehn, Craig S., Thakkar, Kirit A., Zula, Daniel P., Weed, Thomas J., Miller, Julie A.
• Primary Examiner(s): Tarcza, Thomas
• Assistant Examiner(s): ALHARBI, ADAM MOHAMED
• Application Number:
  US13/852,637
• Time in Patent Office: 516 Days
• Field of Search: None
• US Class Current: 701/70
• CPC Class Codes: B60W 2422/80 on wheel hub bearing
• CPC Class Codes: B60W 2520/28 Wheel speed
• CPC Class Codes: G01P 21/02 of speedometers

Abstract

When detecting unacceptably large airgaps between wheel speed sensors and their exciter rings on wheel ends of a vehicle, wheel speed sensor output is filtered and monitored to detect signal amplitudes that correspond to the airgaps. When signal peak amplitude below a predetermined threshold is detected, the airgap is too large. Wheel ends having unacceptably large air gaps are indicated to the driver or technician via blink sequences (e.g., on an electronic stability program (ESP) indicator light or other suitable indicator), wherein each wheel end is associated with a unique blink sequence.

Claims

1. A method for performing an all-wheel marginally large airgap test (AWMLAT), comprising:

upon test initiation, receiving a signal from each of a plurality of wheel speed sensors on a vehicle, the signal being indicative of a exciter ring sensed by the sensor;

for each wheel speed sensor;

monitoring exciter ring frequency to determine whether exciter ring frequency is within a predetermined frequency range;

when exciter ring frequency is within the predetermined frequency range, measuring wheel speed sensor signal peak amplitude;

comparing the measured wheel speed sensor signal peak amplitude to a predetermined minimum amplitude that represents the maximum allowable airgap between the wheel speed sensor and the exciter ring; and

identifying wheel ends for which the wheel speed sensor signal peak amplitude is less than the predetermined minimum amplitude as having an airgap that is larger than a predetermined acceptable airgap size.

2. The method according to claim 1, wherein the predetermined acceptable airgap size is less than about 0.03 inches.

3. The method of claim 1, wherein test initiation occurs upon receiving at least one of:

an indication that an antilock brake system diagnostic switch has been toggled a predetermined number of times; and

a test initiation command received over a diagnostic communication link.

4. The method according to claim 1, further comprising:

when the exciter ring frequency is below a lower frequency limit of the predetermined frequency range, flashing an antilock brake system indicator light at a first frequency to instruct a driver to accelerate the vehicle; and

when the tone wheel frequency is above an upper frequency limit of the predetermined frequency range, determining whether the speed of the wheel coupled to the tone wheel is greater than a predetermined threshold speed.

5. The method according to claim 4, further comprising:

when the wheel speed is not greater than the predetermined threshold speed, flashing an antilock brake system indicator light at a second frequency, which is higher than the first frequency, to instruct a driver to decelerate the vehicle; and

when the wheel speed is greater than the predetermined threshold speed, terminating the test.

6. The method according to claim 4, wherein the predetermined threshold speed is at least 10 mph.

7. The method according to claim 1, further comprising:

causing an antilock brake system indicator light to remain steadily illuminated when the exciter ring frequency within the predetermined frequency range to instruct a driver to maintain a constant speed.

8. The method according to claim 1, further comprising:

indicating the identified wheel ends to the user by flashing an electronic stability program (ESP) indicator light, wherein each wheel end is associated with a unique blink code sequence that is output when the wheel end is determined to have a marginally large airgap, and wherein the ESP indicator light remains unlit if no wheel end is identified as having a marginally large airgap.

9. A processor that executes an all-wheel marginally large airgap test (AWMLAT), wherein the processor is configured to:

upon test initiation, receive a signal from each of a plurality of wheel speed sensors on a vehicle, the signal being indicative of a exciter ring sensed by the sensor; and

for each wheel speed sensor;

monitor exciter ring frequency to determine whether exciter ring frequency is within a predetermined frequency range;

when exciter ring frequency is within the predetermined frequency range, measure wheel speed sensor signal peak amplitude;

compare the measured wheel speed sensor signal peak amplitude to a predetermined minimum amplitude that represents the maximum allowable airgap between the wheel speed sensor and the exciter ring; and

identify wheel ends for which the wheel speed sensor signal amplitude is less than the predetermined minimum amplitude as having an airgap that is larger than a predetermined acceptable airgap size.

10. The processor according to claim 9, wherein the predetermined acceptable airgap size is less than about 0.03 inches.

11. The processor of claim 9, wherein the processor is further configured to initiate the test upon receiving:

at least one of;

an indication that an antilock brake system diagnostic switch has been toggled a predetermined number of times; and

an initiation command received over a diagnostic communication link.

12. The processor according to claim 9, wherein the processor is further configured to:

when the exciter ring frequency is below a lower frequency limit of the predetermined frequency range, flash an antilock brake system indicator light at a first frequency to instruct a driver to accelerate the vehicle; and

when the tone wheel frequency is above an upper frequency limit of the predetermined frequency range, determine whether the speed of the wheel coupled to the tone wheel is greater than a predetermined threshold speed.

13. The processor according to claim 12, wherein the processor is further configured to:

when the wheel speed is not greater than the predetermined threshold speed, flash an antilock brake system indicator light at a second frequency, which is higher than the first frequency, to instruct a driver to decelerate the vehicle; and

when the wheel speed is greater than the predetermined threshold speed, terminate the test.

14. The processor according to claim 12, wherein the predetermined threshold speed is at least 10 mph.

15. The processor according to claim 9, wherein the processor is further configured to:

steadily illuminate an antilock brake system indicator light when the exciter ring frequency within the predetermined frequency range in order to instruct a driver to maintain a constant speed.

16. The processor according to claim 9, further comprising preconditioning the wheel speed sensor signal by passing the signal through a low pass filter.

17. The system according to claim 9, wherein the processor is further configured to:

indicate the identified wheel ends to the user by flashing an electronic stability program (ESP) indicator light, wherein each wheel end is associated with a unique blink code sequence that is output when the wheel end is determined to have a marginally large airgap; and

wherein the ESP indicator light remains unlit if no wheel end is identified as having a marginally large airgap.

18. A system that facilitates performing an all-wheel marginally large airgap test (AWMLAT), comprising:

an antilock brake system comprising

a plurality of wheel speed sensors that respectively monitor a plurality of exciter rings; and

an indicator light; and

a processor configured to, upon test initiation, receive a signal from each of a plurality of wheel speed sensors on a vehicle, the signal being indicative of a exciter ring sensed by the sensor;

wherein the processor is further configured to, for each wheel speed sensor;

monitor exciter ring frequency to determine whether exciter ring frequency is within a predetermined frequency range;

when exciter ring frequency is within the predetermined frequency range, measure wheel speed sensor signal peak amplitude;

compare the measured wheel speed sensor signal peak amplitude to a predetermined minimum amplitude that represents the maximum allowable airgap between the wheel speed sensor and the exciter ring; and

identify wheel ends for which the wheel speed sensor signal peak amplitude is less than the predetermined minimum amplitude as having an airgap that is larger than a predetermined acceptable airgap size.

19. The system according to claim 18, wherein the processor is further configured to:

when the exciter ring frequency is below a lower frequency limit of the predetermined frequency range, flash the antilock brake system indicator light at a first frequency; and

when the tone wheel frequency is above an upper frequency limit of the predetermined frequency range, determine whether the speed of the wheel coupled to the tone wheel is greater than a predetermined threshold speed.

20. The system according to claim 19, wherein the processor is further configured to:

when the wheel speed is not greater than the predetermined threshold speed, flash the antilock brake system indicator light at a second frequency, which is higher than the first frequency; and

when the wheel speed is greater than the predetermined threshold speed, terminate the test.

21. The system according to claim 20, wherein the processor is further configured to:

steadily illuminate the antilock brake system indicator light when the exciter ring frequency within the predetermined frequency range.

22. The system according to claim 18, further including a plurality of low pass filters, each filter being positioned in-line a respective wheel speed sensor and the processor.

23. The system according to claim 18, wherein the processor is further configured to:

indicate the identified wheel ends to the user by flashing an electronic stability program (ESP) indicator light, wherein each wheel end is associated with a unique blink code sequence that is output when the wheel end is determined to have a marginally large airgap, and wherein an absence of EPS indicator illumination indicates that no wheel end is identified as having a marginally large airgap.

24. An apparatus that facilitates performing an all-wheel marginally large airgap test (AWMLAT), comprising:

receiving means for receiving a signal from each of a plurality of wheel speed sensors on a vehicle, the signal being indicative of a exciter ring sensed by the sensor; and

for each wheel speed sensor;

monitoring means for monitoring exciter ring frequency to determine whether exciter ring frequency is within a predetermined frequency range;

measuring means for, when exciter ring frequency is within the predetermined frequency range, measuring wheel speed sensor signal peak amplitude;

comparing means for comparing the measured wheel speed sensor signal amplitude to a predetermined minimum peak amplitude that represents the maximum allowable airgap between the wheel speed sensor and the exciter ring; and

identifying means for identifying wheel ends for which the wheel speed sensor signal amplitude is less than the predetermined minimum peak amplitude as having an airgap that is larger than a predetermined acceptable airgap size.

25. A method for performing wheel-end marginally large airgap test (WEMLAT), comprising for each wheel on a vehicle:

spinning a roller under the wheel for a predetermined number of revolutions within a preset speed range;

measuring wheel speed sensor output during spinning;

requesting status and results for all wheels;

receiving status and result data;

checking a predetermined status byte in the received data to determine the status of an airgap between the wheel speed sensor and an exciter ring coupled to the first wheel; and

outputting to a user an indication of any wheels having an airgap that is larger than a predetermined allowable airgap threshold size.

26. The method according to claim 25, wherein the predetermined number of revolutions is at least 2.

27. The method according to claim 25, wherein the preset speed range is between 2.5 mph and 10 mph.

28. The method according to claim 25, wherein the output indication is provided to the user by blinking an electronic stability program (ESP) indicator light, wherein each wheel is assigned a unique blink sequence and wherein each wheel having an airgap larger than the predetermined allowable airgap threshold size is indicated by blinking the indicator light in the unique blink sequence for that wheel, and wherein the ESP indicator light remains unlit if no wheel is determined to have an airgap larger than the predetermined allowable airgap threshold size.