PROPORTIONAL BRAKE CONTROLLER

• US 20130297166A1
• Filed: 11/01/2012
• Published: 11/07/2013
• Est. Priority Date: 11/01/2011
• Status: Abandoned Application

• Current Assignee: Curt Manufacturing (LCI Industries)
• Original Assignee: Curt Manufacturing (LCI Industries)
• Inventors: Limoge, Henry, Thomas, Donald, Sanchez, Joecyl
• Application Number:
  US13/666,587
• Publication Number:
  US 20130297166A1
• Time in Patent Office: Days
• US Class Current: 701/70
• CPC Class Codes: B60T 13/08 Overrun brakes
• CPC Class Codes: B60T 13/662 characterised by specified functions of the control system components
• CPC Class Codes: B60T 7/20 specially for trailers, e.g. in case of uncoupling of or overrunning by trailer inertia-actuated overrun brakes B60T13/08
• CPC Class Codes: B60T 8/1708 for lorries or tractor-trailer combinations
• CPC Class Codes: B60T 8/323 Systems specially adapted for tractor-trailer combinations
• CPC Class Codes: B60T 8/3255 Systems in which the braking action is dependent on brake pedal data

Abstract

A system, device, and method for providing braking power to a trailer proportional to the deceleration of a towing vehicle.

Claims

1. A method of applying brakes of a towed vehicle when it is association with a towing vehicle, the method comprising:

providing a brake controller having a three-axis accelerometer;

determining accelerometer offset values along three directions indicative of the towing vehicle being on level ground;

applying the determined accelerometer offset values to the three-axis accelerometer;

receiving accelerometer values along three directions from the three-axis accelerometer, the received accelerometer values being subject to the accelerometer offset values;

calculating a single acceleration magnitude based on the received accelerometer values; and

generating a braking command signal based on the calculated acceleration magnitude.

2. The method of claim 1, further comprising activating brakes of the towed vehicle in response to the braking command signal.

3. The method of claim 1, wherein generating a braking command signal includes applying a braking sensitivity factor to the acceleration magnitude.

4. A method for establishing acceleration for a vehicle, the method comprising:

using a three-axis accelerometer, determining accelerometer offset values along three directions indicative of the towing vehicle being on level ground;

applying the determined accelerometer offset values to the three-axis accelerometer;

receiving accelerometer values along three directions from the three-axis accelerometer, the received accelerometer values being subject to the accelerometer offset values; and

calculating a single acceleration magnitude based on the received accelerometer values.

5. A brake controller configured to provide braking signals to a towed vehicle, the brake controller comprising:

a three-axis accelerometer configured to provide acceleration values along three directions;

a controller operatively coupled to the three-axis accelerometer and configured to receive acceleration values along three directions from the three-axis accelerometer and to determine a single acceleration magnitude based on the received three acceleration values; and

wherein the three-axis accelerometer is configured to apply an offset to the acceleration values, the offset being indicative of a towing vehicle being on level ground.

6. A proportional brake control device comprising a brake control system, the device comprising:

an inertial measurement unit, wherein the inertial measurement unit outputs an acceleration vector and receives an offset value, wherein the acceleration vector comprises acceleration measurements along at least two axes and the offset value is subtracted from the acceleration vector before output from the inertial measurement unit;

a memory;

a relay, wherein the relay receives a brake input; and

a processor programmed to execute a program comprising the brake control system, wherein the brake control system comprises an inertial calculation function and a brake generating function;

wherein the inertial calculation function is configured to;

perform auto-calibration or new calibration;

wherein auto-calibration comprises;

accessing a gravity vector from the memory;

accessing the inertial measurement unit and storing the acceleration vector;

comparing the gravity vector to the acceleration vector;

sending the gravity vector to the inertial measurement unit as the offset value if the gravity vector is less than or equal to a generating constant multiplied by the acceleration vector; and

performing new calibration if the gravity vector is greater than the generating constant multiplied by the acceleration vector;

wherein new-calibration comprises;

determining if the proportional brake control device is on level ground;

performing auto-calibration if not on level ground; and

accessing the inertial measurement unit, setting the gravity vector equal to the acceleration vector, and sending the gravity vector to the inertial measurement unit as the offset value if on level ground;

wherein the brake generating function is configured to;

initiate when brake input is received;

access the inertial measurement unit and store the acceleration vector;

calculate a magnitude of the acceleration vector;

calculate a duty cycle, wherein the duty cycle is equal to the magnitude of the acceleration vector multiplied by a duty constant divided by a sensitivity setting factor;

compare the duty cycle to a gain setting;

output the duty cycle if the duty cycle is less than or equal to the gain setting; and

output the gain setting if the duty cycle is greater than the gain setting.

7. The brake control system of claim 6, wherein the acceleration vector comprises acceleration measurements along three axes.

8. The brake control system of claim 6, wherein the generating constant is equal to 1.

9. The brake control system of claim 6, wherein the generating constant is within the range of 1 to 1.15.

10. The brake control system of claim 6, wherein the gain setting is within the range of 0.5 to 9.9.

11. The brake control system of claim 6, wherein the inertial measurement unit comprises a three-axis digital accelerometer.

12. A proportional brake control device comprising:

an inertial measurement unit, wherein the inertial measurement unit outputs an acceleration vector and receives an offset value, wherein the acceleration vector comprises acceleration measurements along at least two axes and the offset value is subtracted from the acceleration vector before output from the inertial measurement unit;

a memory;

a relay, wherein the relay receives a brake input; and

a controller for managing the device operations such that the electronic device is configured to;

access a gravity vector from the memory;

access the inertial measurement unit and store the acceleration vector;

compare the gravity vector to the acceleration vector;

send the gravity vector to the inertial measurement unit if the gravity vector is less than or equal to a generating constant multiplied by the acceleration vector;

determine if the proportional brake control device is on level ground;

access the inertial measurement unit and store the acceleration vector as the gravity vector if on level ground;

send the gravity vector to the inertial measurement unit as the offset value if on level ground;

detect brake input is received;

calculate a magnitude of the acceleration vector;

calculate a duty cycle, wherein the duty cycle is equal to the magnitude of the acceleration vector multiplied by a duty constant divided by a sensitivity setting factor;

compare the duty cycle to a gain setting;

output the duty cycle if the duty cycle is less than or equal to the gain setting; and

output the gain setting if the duty cycle is greater than the gain setting.

13. The method of claim 12, wherein the acceleration vector comprises acceleration measurements along three axes.

14. The method of claim 12, wherein the generating constant is equal to 1.

15. The method of claim 12, wherein the generating constant is within the range of 1 to 1.15.

16. The method of claim 12, wherein the gain setting is within the range of 0.5 to 9.9.

17. The method of claim 12, wherein the inertial measurement unit comprises a three-axis digital accelerometer.

18. A method of detecting deceleration and converting it into braking power with a proportional brake control device, wherein the device comprises:

an inertial measurement unit, wherein the inertial measurement unit outputs an acceleration vector and receives an offset value, wherein the acceleration vector comprises acceleration measurements along at least two axes and the offset value is subtracted from the acceleration vector before output from the inertial measurement unit; and

a relay, wherein the relay receives a brake input;

wherein the method comprises;

accessing a gravity vector from the memory;

accessing the inertial measurement unit and store the acceleration vector;

comparing the gravity vector to the acceleration vector;

sending the gravity vector to the inertial measurement unit if gravity vector is less than or equal to a generating constant multiplied by the acceleration vector;

determining if the proportional brake control device is on level ground;

accessing the inertial measurement unit and store the acceleration vector as the gravity vector if on level ground;

sending the gravity vector to the inertial measurement unit as the offset value if on level ground;

detecting brake input is received;

calculating a magnitude of the acceleration vector;

calculating a duty cycle, wherein the duty cycle is equal to the magnitude of the acceleration vector multiplied by a duty constant divided by a sensitivity setting factor;

comparing the duty cycle to a gain setting;

outputting the duty cycle if the duty cycle is less than or equal to the gain setting; and

outputting the gain setting if the duty cycle is greater than the gain setting.

19. The method of claim 18, wherein the acceleration vector comprises acceleration measurements along three axes.

20. The method of claim 18, wherein the generating constant is equal to 1.

21. The method of claim 18, wherein the generating constant is within the range of 1 to 1.15.

22. The method of claim 18, wherein the gain setting is within the range of 0.5 to 9.9.

23. The method of claim 18, wherein the inertial measurement unit comprises a three-axis digital accelerometer.