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. 19, 2018

Filed:

Aug. 19, 2014
Applicant:

The Boeing Company, Chicago, IL (US);

Inventors:

David F. Cerra, Woodinville, WA (US);

Robert H. Willie, Bothell, WA (US);

Assignee:

The Boeing Company, Chicago, IL (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F02K 1/72 (2006.01); F02K 1/12 (2006.01); F02K 3/02 (2006.01); F02K 1/76 (2006.01); F02K 1/70 (2006.01); F02K 1/11 (2006.01);
U.S. Cl.
CPC ...
F02K 1/72 (2013.01); F02K 1/11 (2013.01); F02K 1/12 (2013.01); F02K 1/1207 (2013.01); F02K 1/70 (2013.01); F02K 1/763 (2013.01); F02K 3/025 (2013.01); F05D 2260/50 (2013.01);
Abstract

A thrust reverse variable area nozzle system for a nacelle of an aircraft engine system may include a reverse thrust opening disposed in the nacelle, and a thrust reverser door pivotally movable relative to the nacelle for selectively covering the reverse thrust opening, wherein the thrust reverser door is pivotally movable between a first position for completely covering the reverse thrust opening, a second position for partially uncovering a forward portion of the reverse thrust opening and discharging a bypass airflow through the forward portion of the reverse thrust opening in a forward direction, and a third position for partially uncovering an aft portion of the reverse thrust opening and discharging the bypass airflow through the aft portion of the reverse thrust opening in an aft direction.


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