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:
Jun. 05, 2018

Filed:

Jul. 09, 2014
Applicant:

Zodiac Seats Us Llc, Gainesville, TX (US);

Inventors:

Ty W. Parker, Sanger, TX (US);

Jeffrey Johnston, Huntington Beach, CA (US);

Matthew K. Zemler, Corinth, TX (US);

Sebastian S. Delgadillo, Denton, TX (US);

Matt Jones, Rosston, TX (US);

Assignee:

Zodiac Seats US LLC, Gainesville, TX (US);

Attorneys:
Primary Examiner:
Int. Cl.
CPC ...
F16M 13/02 (2006.01); B60R 11/02 (2006.01); B64D 11/06 (2006.01); B64D 11/00 (2006.01); F16M 11/12 (2006.01); F16M 11/18 (2006.01); F16M 11/20 (2006.01); B60N 2/24 (2006.01); B60N 3/00 (2006.01); B61D 33/00 (2006.01); B61D 37/00 (2006.01); B60R 11/00 (2006.01);
U.S. Cl.
CPC ...
F16M 13/02 (2013.01); B60N 2/242 (2013.01); B60N 3/002 (2013.01); B60R 11/0235 (2013.01); B61D 33/0007 (2013.01); B61D 37/00 (2013.01); B64D 11/0015 (2013.01); B64D 11/00151 (2014.12); B64D 11/0638 (2014.12); F16M 11/126 (2013.01); F16M 11/18 (2013.01); F16M 11/2021 (2013.01); B60R 2011/0082 (2013.01); B60R 2011/0085 (2013.01); F16M 2200/022 (2013.01); F16M 2200/024 (2013.01); F16M 2200/06 (2013.01);
Abstract

Deployment apparatus () including a deployment object (), a deployment arm () with a first end () coupled to the deployment object and a second end () having a pivot (), and a hinge assembly () rotatably attached to the pivot of the deployment arm. The hinge assembly () includes an enclosure () and a friction stop device () disposed within the enclosure such that the friction stop device includes a friction portion () configured to be pressed against a lateral surface of the pivot () of the deployment arm such that the friction portion provides a predetermined torque. The predetermined torque may be calculated based on maintaining a deployed angle of the deployment arm () such that the deployment object () is held in a raised deployed position.


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