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:
Mar. 23, 2021

Filed:

Apr. 23, 2018
Applicant:

Parker-hannifin Corporation, Cleveland, OH (US);

Inventors:

Luther Wirtz, Mentor, OH (US);

Jeffrey Lehtinen, Concord Township, OH (US);

Adel Mansour, Mentor, OH (US);

David Tibbs, Summerville, SC (US);

Robert Pelletier, Chardon, OH (US);

Jon Stockill, Rugeley, GB;

Assignee:

Parker-Hannifin Corporation, Cleveland, OH (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F23R 3/28 (2006.01); F23R 3/12 (2006.01); F23R 3/14 (2006.01);
U.S. Cl.
CPC ...
F23R 3/12 (2013.01); F23R 3/14 (2013.01); F23R 3/28 (2013.01); F23R 2900/00005 (2013.01);
Abstract

A fuel injector for a gas turbine engine of an aircraft having a fuel nozzle including a fuel swirler and/or an outer air swirler. The fuel swirler may include a manifold for receiving fuel from a fuel conduit, and a plurality of fuel passages to direct fuel from the manifold to discharge orifices that direct fuel with swirling flow. The fuel swirler may be configured to provide uniform spray while minimizing recirculation zones; reduce residence time as fuel enters the manifold; minimize flow disruptions, boundary layer growth, and/or pressure drop as fuel flows through the fuel passages; reduces coking internally of the nozzle; reduces thermal stresses; and is simple and low-cost to manufacture.


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