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:
Dec. 03, 2019

Filed:

Sep. 12, 2016
Applicant:

Lord Corporation, Cary, NC (US);

Inventors:

Benjamin Bozon, Metz-Tessy, FR;

Alexandre Kursner, Prangins, CH;

Baptiste Narbon, Annecy le Vieux, FR;

Daniel Zameroski, McKean, PA (US);

Assignee:

LORD Corporation, Cary, NC (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64D 27/26 (2006.01); B64C 27/00 (2006.01); B64D 13/00 (2006.01); B64D 41/00 (2006.01); F16F 15/08 (2006.01);
U.S. Cl.
CPC ...
B64D 27/26 (2013.01); B64C 27/001 (2013.01); B64D 13/00 (2013.01); B64D 41/00 (2013.01); F16F 15/08 (2013.01); B64C 2027/002 (2013.01); B64D 2027/262 (2013.01); B64D 2041/002 (2013.01); F16F 2230/0041 (2013.01); F16F 2230/16 (2013.01); Y02T 50/44 (2013.01);
Abstract

Aircraft support structures, systems, and methods are disclosed. In one embodiment, an aircraft system includes a rotating component and a support (e.g. strut) that supports the rotating component. The support includes a locking assembly (P) that is configured to lock, automatically, an inner member () of the support with respect to an outer member () of the support for stiffening the support in response to reaching or exceeding a predetermined threshold amount of displacement, load, stress, or rotation. The aircraft support structures, systems, and methods herein utilize self-locking and self-unlocking supports (e.g. struts) for increasing or decreasing a stiffness of the support.


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