Vehicle attitude adjustment assembly

• US 6,885,924 B2
• Filed: 12/13/2002
• Issued: 04/26/2005
• Est. Priority Date: 10/01/1999
• Status: Expired due to Term

• Current Assignee: Innovative Design Solutions, Inc. (LCI Industries)
• Original Assignee: John P. Manfreda, Robert M. Ford, Shawn P. Haley
• Inventors: Ford, Robert M., Haley, Shawn P., Manfreda, John P.
• Primary Examiner(s): Black, Thomas G.
• Assistant Examiner(s): Tran, Dalena
• Application Number:
  US10/318,820
• Publication Number:
  US 20030135312A1
• Time in Patent Office: 865 Days
• Field of Search: 701/36, 701/110, 701/37, 701/38, 254/418, 254/423, 254/422, 180/41, 180/282, 180/89.15, 180/89.14, 180/9.52, 280/6.153, 280/6.15, 280/6.156, 280/763.1, 280/6.154, 280/6.159, 280/5.514
• US Class Current: 701/36
• CPC Class Codes: B60G 17/0161 mainly during straight-line motion B60G17/0164 takes precedence
• CPC Class Codes: B60G 2600/02 Retarders, delaying means, dead zones, threshold values, cut-off frequency, timer interruption
• CPC Class Codes: B60G 2600/20 Manual control or setting means
• CPC Class Codes: B60G 2800/012 Rolling condition
• CPC Class Codes: B60G 2800/014 Pitch; Nose dive
• CPC Class Codes: B60G 2800/16 Running
• CPC Class Codes: B60G 2800/912 Attitude Control; levelling control
• CPC Class Codes: B60S 9/02 for only lifting or supporting

Abstract

An assembly for adjusting the attitude of any selected portion a structure such as a motor vehicle. A controller connects to and controls one or more jacks operable to change the attitude of a structure. A proportional tilt sensor is connected to the controller and is supported on the structure. The tilt sensor provides signals to the controller, which represent the degree of longitudinal pitch and lateral roll of a portion of the structure the sensor is connected to. The controller moves a selected portion of the structure into a desired attitude by commanding movement of the entire structure into an attitude where the tilt sensor signals match any one of a number of preset reference values corresponding to the desired attitude of the selected portion of the structure.

Claims

1. An assembly for adjusting the attitude of any selected portion of a structure, the assembly comprising:

a controller configured to connect to and control one or more jacks operable to change the attitude of a structure; and

a proportional tilt sensor connected to the controller and configured to be supported on the structure, the tilt sensor being configured to provide signals to the controller that represent the degree of longitudinal pitch and lateral roll of a portion of the structure the sensor is connected to, the controller being additionally configured to move any selected portion of the structure into a desired attitude by commanding movement of the entire structure into an attitude where the tilt sensor signals match any one of a number of different pre-set reference values corresponding to different desired attitudes of the selected portion of the structure.

2. An assembly as defined in claim 1 in which the signals are analog signals.

3. An assembly as defined in claim 1 in which each of the reference values is defined by a set of tilt sensor signal values that the controller recognizes as indicating that the selected portion of the structure is in a desired attitude.

4. An assembly as defined in claim 1 in which the controller is configured to detect jack ground contact from a change in tilt angle.

5. An assembly for adjusting the attitude of any selected portion of a structure, the assembly comprising:

a controller configured to connect to and control one or more jacks operable to change the attitude of a structure;

a proportional tilt sensor connected to the controller and configured to be supported on the structure, the tilt sensor being configured to provide signals to the controller, which represent the degree of longitudinal pitch and lateral roll of the portion of the structure the sensor is supported on, the controller being configured to move any selected portion of the structure into a desired attitude by commanding movement of the entire structure into an attitude where the tilt sensor signals match any one of a number of different pre-set reference values corresponding to different desired attitudes of selected portions of the structure, thereby allowing any portion of the structure to be corrected to any desired attitude within a range of attitudes despite the location of the tilt sensor and allowing the tilt sensor to be located anywhere in the structure; and

a reference value selector connected to the controller and configured to transmit operator inputs to the controller, the controller being configured to select between the pre-set reference values in response to inputs received from the reference value selector.

6. An assembly as defined in claim 5 in which the controller is configured to change drive rates of the jacks based upon inputs other than tilt angle.

7. An assembly as defined in claim 5 in which the controller is configured to tailor drive rates of the jacks to respond to structural dynamics.

8. An assembly as defined in claim 5 in which the controller is configured to change drive rates of the jacks dynamically to control an attitude correction rate of the structure.

9. An assembly as defined in claim 5 in which the controller is configured to measure jack drive rates and attitude change speed of the structure using inputs from the tilt sensor.

10. An assembly as defined in claim 5 in which the controller is configured to automatically select between different jack grounding procedures, the selection being based on conditions of the structure.

11. An assembly as defined in claim 5 in which the controller is configured to infer jack ground contact based on dynamic information received from the tilt sensor and indicating jack loading.

12. An assembly as defined in claim 5 in which the controller is configured to automatically select between alternative leveling algorithms, the selection being based on conditions of the structure.

13. An assembly as defined in claim 5 in which:

the assembly includes at least two pairs of jacks supported on the structure; and

the controller is configured to correct the attitude of a structure by extending the jacks in pairs parallel to longitudinal pitch and lateral roll axes of the structure.

14. An assembly as defined in claim 5 in which the controller is configured to detect and correct whichever of the pitch and roll of the structure requires the most correction to move the structure into a desired attitude.

15. An assembly as defined in claim 5 in which the controller is configured to maximize signal stability by employing adaptive filtering based on rate of angular change and estimated signal noise.

16. An assembly as defined in claim 5 in which the controller is configured to allow an operator to choose between fully automatic or semi automatic attitude correction operations.

17. An assembly as defined in claim 5 in which the controller is configured to automatically correct long-term attitude changes that occur after attitude correction.

18. A method for calibrating an attitude correction assembly to recognize when a selected portion of a structure the assembly is installed on is in a desired attitude relative to gravity;

the method comprising the steps of;

providing a structure including jacks actuable to change the attitude of the structure;

providing an attitude correction assembly on the structure, the assembly including a controller and a tilt sensor;

actuating the jacks until the structure is in a first desired attitude;

providing an input to the controller indicating that the current set of signals being received from the tilt sensor is a first set of signal values that will represent the first desired attitude for the controller to reference when selected in future attitude correction operations;

actuating the jacks until the structure is in a second desired attitude relative to gravity; and

providing an input to the controller indicating that the current set of signals being received from the tilt sensor is a second set of signal values that will represent the second desired attitude for the controller to reference when selected in future attitude correction operations.

19. The method of claim 18 in which the step of providing an attitude correction assembly includes providing a controller programmed to include a zero mode in which the controller is ready to receive a signal that will instruct the controller to recognize signal values being received from the tilt sensor as indicating that a selected portion of the structure is in a desired attitude.

20. The method of claim 18 including the additional steps of:

providing an attitude indicator on the selected portion of the structure, the attitude indicator configured to indicate attitude relative to gravity;

actuating the jacks until the attitude indicator indicates that the selected portion of the structure is in a desired attitude relative to gravity; and

causing the controller to store signal values that the controller receives from the tilt sensor once the structure is in the desired attitude.