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. 08, 2019

Filed:

Nov. 18, 2013
Applicant:

United Technologies Corporation, Hartford, CT (US);

Inventors:

Jeffery A. Lovett, Tolland, CT (US);

Darin A. Knaus, Lyme, NH (US);

Scott D. Phillips, Enfield, NH (US);

Daniel J. Micka, Enfield, NH (US);

Patrick Magari, Plainfield, NH (US);

Assignee:

United Technologies Corporation, Farmington, CT (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 7/22 (2006.01); F23R 3/20 (2006.01); F23R 3/30 (2006.01); F23R 3/28 (2006.01); F02K 3/10 (2006.01);
U.S. Cl.
CPC ...
F02C 7/22 (2013.01); F02K 3/10 (2013.01); F23R 3/20 (2013.01); F23R 3/286 (2013.01); F23R 3/30 (2013.01); Y10T 29/494 (2015.01);
Abstract

A fuel injection system for a gas turbine engine includes a vane in an airflow path within the gas turbine engine, the vane includes an air channel with an outlet in communication with the airflow path; and a fuel nozzle within the vane operable to inject fuel into the air channel to at least partially premix and prevaporize the fuel with a secondary airflow from within the vane in the air channel prior to entry into the airflow path through the outlet. A method of injecting fuel within a gas turbine engine includes at least partially premixing and prevaporizing fuel with a secondary airflow from within a vane in an air channel within the vane, the vane within an airflow path of the gas turbine engine.


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