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. 28, 2023

Filed:

Sep. 27, 2019
Applicant:

The Boeing Company, Chicago, IL (US);

Inventors:

Abhishek Sahay, Everett, WA (US);

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

Assignee:

The Boeing Company, Arlington, VA (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64D 33/04 (2006.01); B64D 27/18 (2006.01); B64D 29/06 (2006.01); F02C 7/20 (2006.01); F02C 7/24 (2006.01); F02K 1/52 (2006.01); F02K 1/44 (2006.01);
U.S. Cl.
CPC ...
B64D 33/04 (2013.01); B64D 27/18 (2013.01); B64D 29/06 (2013.01); F02C 7/20 (2013.01); F02C 7/24 (2013.01); F02K 1/44 (2013.01); F02K 1/52 (2013.01); F05D 2220/323 (2013.01); F05D 2240/90 (2013.01);
Abstract

Aircraft engine exhaust systems enabling short aft fairings are described. An example turbofan engine exhaust system of an aircraft includes a primary nozzle having a leading edge and a trailing edge, and a heat shield coupled to an aft strut fairing. The heat shield has an upstream end and a downstream end. The downstream end of the heat shield is substantially coterminous with the trailing edge of the primary nozzle.


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