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:
Jul. 07, 2020

Filed:

Mar. 22, 2016
Applicant:

Gulfstream Aerospace Corporation, Savannah, GA (US);

Inventors:

Todd Schartner, Savannah, GA (US);

Clint Rupp, Savannah, GA (US);

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
E05C 19/16 (2006.01); B64D 11/00 (2006.01); B64C 1/14 (2006.01); E05B 63/00 (2006.01); E05C 17/56 (2006.01);
U.S. Cl.
CPC ...
E05C 19/16 (2013.01); B64C 1/1407 (2013.01); B64D 11/00 (2013.01); E05B 63/0056 (2013.01); E05C 17/56 (2013.01); Y10S 292/19 (2013.01); Y10T 292/11 (2015.04);
Abstract

A tunable stay device for an aircraft closure has a mounting base that is mountable to the closure or in an area of the aircraft in close proximity to the closure. The mounting base extends, at least in part, along a mounting axis. A holding element is mounted for movement along the mounting axis and configured to effect, at least in part, a hold force. An adjuster is mounted to at least one of the mounting base and the holding element and is configured and arranged to effect a change in position of the holding element with respect to the mounting base along the mounting axis. When the stay device is mounted to the closure or in the area of the aircraft in proximity to the closure, the hold force biases the closure in one of an open orientation and a closed orientation.


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