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:
Feb. 14, 2017

Filed:

May. 21, 2015
Applicant:

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

Inventors:

Alysson Kennerly Colaciti, São José dos Campos, BR;

Leandro Guilherme Crenite Simões, São José dos Campos, BR;

Alexandre Viana Ferreira, São José dos Campos, BR;

Micael Gianini Valle do Carmo, São José dos Campos, BR;

Mário Triches, Jr., São José dos Campos, BR;

Vinicius Losada Gouveia, São José dos Campos, BR;

Assignee:

EMBRAER S.A., São José dos Campos—SP, BR;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64C 7/00 (2006.01); B64C 9/18 (2006.01);
U.S. Cl.
CPC ...
B64C 7/00 (2013.01); B64C 9/18 (2013.01);
Abstract

Flap track fairing systems are split into a forward immovably fixed portion and an aft movable portion. The fixed forward portion is immovably attached to the main wing structure of an aircraft while the movable aft portion is attached either to the movable components of the flap deployment mechanism or to the lower surface of the flap. A separation line between the forward movable portion and the aft fixed portion is provided such that the movable portion does not interfere structurally with the flap fairing structure during a flap extension/retraction cycle. An airflow deflector is positioned near a forward separation edge of the aft fairing portion so as to be positioned within a gap defined between the forward edge of the aft fairing portion and a rearward edge of the forward fairing portion when the flap is in the deployed configuration thereof to thereby deflect airflow away from the interior space of the fairing.


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