The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
May. 26, 2020

Filed:

Oct. 26, 2017
Applicant:

Cnh Industrial America, Llc, New Holland, PA (US);

Inventors:

Jason T. Czapka, Munster, IN (US);

Kevin D. McKee, Naperville, IL (US);

Kevin M. Smith, Narvon, PA (US);

Robert J. Longua, Palatine, IL (US);

Keith W. Wendte, Willowbrook, IL (US);

Marvin A. Prickel, Homer Glen, IL (US);

Assignee:

CNH Industrial America LLC, New Holland, PA (US);

Attorneys:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
A01B 73/06 (2006.01); A01B 76/00 (2006.01);
U.S. Cl.
CPC ...
A01B 73/067 (2013.01); A01B 73/065 (2013.01); A01B 76/00 (2013.01);
Abstract

In one aspect, a method for automatically actuating wing assemblies an agricultural implement associated with a work vehicle may include monitoring, with one or more computing devices, a first wing movement parameter associated with folding or unfolding a wing assembly of the agricultural implement during the performance of a wing movement operation. The method may also include determining, with the one or more computing devices, whether the first wing movement parameter satisfies a first condition associated with a first predetermined threshold value defined for the wing movement operation. The method may include, automatically initiating, with the one or more computing devices, movement of the work vehicle relative to a surface on which the work vehicle is supported to assist the folding or unfolding of the wing assembly during the performance of the wing movement operation when it is determined that the first wing movement parameter satisfies the first condition.


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