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:
Oct. 09, 2018

Filed:

Feb. 04, 2014
Applicant:

The Boeing Company, Chicago, IL (US);

Inventors:

Matthew D. Moore, Everett, WA (US);

Edward C. Marques, Issaquah, WA (US);

Assignee:

THE BOEING COMPANY, Chicago, IL (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F02K 1/48 (2006.01); F02K 3/02 (2006.01); F02K 1/38 (2006.01); F02K 1/72 (2006.01); F02K 1/76 (2006.01); F02K 1/82 (2006.01); F02K 3/077 (2006.01); B64D 33/02 (2006.01);
U.S. Cl.
CPC ...
F02K 3/02 (2013.01); F02K 1/386 (2013.01); F02K 1/48 (2013.01); F02K 1/72 (2013.01); F02K 1/766 (2013.01); F02K 1/827 (2013.01); F02K 3/077 (2013.01); B64D 2033/024 (2013.01); Y02T 50/672 (2013.01);
Abstract

A method of controlling plume exhaust heat and/or noise radiation from a turbofan engine assembly having a short nacelle. A mixer duct shell is supported such that a downstream edge of the short nacelle overlays an upstream portion of the mixer duct shell. A first portion of fan exhaust may be routed through the mixer duct shell between its inner surface and an outer surface of a core engine shroud. A second portion of fan exhaust may be routed over an outer surface of the mixer duct shell. At least one of the inner surface and an outer surface of the mixer duct shell may have an acoustic lining including a honeycomb core structure.


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