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:
Nov. 10, 2015

Filed:

Apr. 25, 2014
Applicant:

Embraer S.a., São José Dos Campos, BR;

Inventors:

Bruno Kimura Castanha, São José Dos Campos, BR;

Fernando Henrique Da Silva, São José Dos Campos, BR;

Jay Beever, Melbourne, FL (US);

Oliver Turci De Camargo, São José Dos Campos, BR;

Joshua Rea, Melbourne, FL (US);

Rainer Zierer, Melbourne, FL (US);

Assignee:

EMBRAER S.A., São José Dos Campos-SP, BR;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
E04C 2/38 (2006.01); B60R 13/02 (2006.01); B64D 11/00 (2006.01); B64C 1/06 (2006.01);
U.S. Cl.
CPC ...
B60R 13/0206 (2013.01); B60R 13/02 (2013.01); B64C 1/066 (2013.01); B64D 11/00 (2013.01);
Abstract

Adaptive, self-adjusting decorative trim assemblies are especially adapted for use in aircraft cabin interiors where the fuselage undergoes deformation and/or distortion due to pressurization during flight. The self-adjusting features of the decorative trim assemblies according to the embodiments described herein thus allow for relative movement between mutually intersecting interior cabin panels without jeopardizing the cabin interior aesthetics (e.g., since the relative positioning of the panels is not disrupted by virtue of such fuselage deformations).


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