Auxiliary Tillage Implement Control for Foldable Wings

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Solution Overview

Problem

Auxiliary tillage implements often interfere with the folding process of main tillage implements during transportation, as they are not easily compatible with the folding mechanism.

Innovation Solution

A control system that allows independent positioning of auxiliary implements on foldable sections of the tillage implement, using actuators and pivotal arms to move them out of the way during the folding process, ensuring they do not interfere with each other or the main implement.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Productivity

If auxiliary implements are coupled to foldable wing sections, then multiple functions can be performed simultaneously, but the auxiliary implements interfere with the folding process during transportation

Engineering Contradiction:
Improvemultiple functions in single passVSAvoidfolding process compatibility
Core Design Contradiction:
ProductivityVSEase of operation

Solution Approach 1:

The auxiliary implement is made dynamically adjustable through a control system that independently positions the implement during folding operations. The control system actuates the auxiliary implement to assume different positions based on whether the implement is in field mode or transport mode, resolving the conflict between maintaining functionality during operation and compatibility during folding.

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The control system performs preliminary positioning of the auxiliary implement before the folding process begins. By detecting when the wing section is being folded and pre-positioning the auxiliary implement out of the folding path, the system prevents interference before it occurs, enabling smooth folding operations.

Inventive Principle:
Principle #10Preliminary action

2Adaptability or versatility

If auxiliary implements are positioned to avoid interference during folding, then transport compatibility is improved, but additional control mechanisms are required

Engineering Contradiction:
Improvetransport compatibilityVSAvoidcontrol system requirements
Core Design Contradiction:
Adaptability or versatilityVSDevice complexity

Solution Approach 1:

The control system serves multiple functions: it positions the auxiliary implement during folding operations, maintains proper positioning during field operations, and coordinates with the foldable wing section mechanisms. This multi-functional approach consolidates control capabilities rather than adding separate dedicated mechanisms for each function.

Inventive Principle:
Principle #6Universality (Multi-functionality)

Solution Approach 2:

The control system incorporates feedback mechanisms that detect the position and folding state of the wing section, then automatically adjust the auxiliary implement positioning accordingly. This feedback loop eliminates the need for complex manual control mechanisms by using automated sensing and response.

Inventive Principle:
Principle #23Feedback

Applied Scientific Principles

This section explains which scientific principles are used to turn an abstract innovation direction into a practical engineering solution.

Function Achieved in This Case

Enables the auxiliary implements to be moved to a non-interfering position during transport, maintaining compatibility with the folding mechanism and adhering to regulatory dimensions for oversized vehicles, thus facilitating safe and efficient transportation.

Implementation Method 1

at least one actuator coupled to both the support member and the pivotal arm

Methodology Applied
Scientific EffectMechanical force: Mechanical Force

Data Source

PatentUS9974224B2Agricultural auxiliary tillage implement control
Publication Date: 2018.05.22 BLUE LEAF I P INC
  • US9974224B2 patent drawing
  • US9974224B2 patent drawing
  • US9974224B2 patent drawing

AI summary

An agricultural tillage implement includes a main section including a hitch extending in a travel direction, a plurality of foldable wing sections coupled with the main section, at least one auxiliary implement assembly coupled to each of the wing sections and a control system. Each auxiliary implement assembly includes at least one support member, at least one pivotal arm pivotally coupled to the support member, at least one actuator coupled to both the support member and the pivotal arm and a ground contacting implement coupled to the pivotal arm. The control system is configured to actuate the actuators to control a position of each ground contacting implement in each of the sections when the agricultural implement is transitioning to a transport mode.