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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.

Patent No.:

US 10040560 B1

PDFFull Text
Date of Patent:
Aug. 07, 2018

Filed:

Sep. 30, 2015

Trailing edge core compartment vent for an aircraft engine

Applicant:

The Boeing Company, Chicago, IL (US);

Inventors:

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

Paul R. Tretow, Mukilteo, WA (US);

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

Assignee:

THE BOEING COMPANY, Chicago, IL (US);

Attorney:

MH2 Technology Law Group LLP

Primary Examiner:

Tien Dinh

Assistant Examiner:

Michael A Fabula

Int. Cl.
CPC ...
B64D 33/04 (2006.01); B64D 27/12 (2006.01); B64D 29/00 (2006.01); F02K 1/82 (2006.01); F02K 3/04 (2006.01); F01D 25/26 (2006.01); F02K 1/38 (2006.01); F02C 7/18 (2006.01);
U.S. Cl.
CPC ...
B64D 27/12 (2013.01); B64D 29/00 (2013.01); F01D 25/26 (2013.01); F02C 7/18 (2013.01); F02K 1/38 (2013.01); F02K 1/82 (2013.01); F02K 1/822 (2013.01); F02K 3/04 (2013.01); F05D 2220/36 (2013.01); F05D 2240/128 (2013.01); F05D 2260/605 (2013.01); F05D 2260/608 (2013.01); Y02T 50/671 (2013.01); Y02T 50/675 (2013.01);
Abstract

A turbine engine nozzle can include a primary outer wall extending from an engine core area to an annular wall terminus that surrounds an engine tail cone, to form a core nozzle. The turbine engine nozzle also includes a single engine core cowl extending from the engine core area to an annular cowl terminus to form a core compartment vent nozzle. The core compartment vent nozzle exhausts air from a core compartment in a trailing edge between the single engine core cowl and the primary outer wall.

Find Patent Forward Citations

Willie, Robert. (2018). Trailing edge core compartment vent for an aircraft engine (U.S. Patent No. 10040560). U.S. Patent and Trademark Office. https://idiyas.com/patent/badge/10040560

Data source: USPTO (United States Patent and Trademark Office) public patent records. Weekly synchronization. How IDiyas builds this profile

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