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:
Jul. 14, 2026

Filed:

Apr. 01, 2025
Applicant:

General Electric Company, Evendale, OH (US);

Inventors:

Paul Hadley Vitt, Liberty Township, OH (US);

Michal Osusky, Rexford, NY (US);

Jonathan A. Filipa, Liberty Township, OH (US);

Assignee:

General Electric Company, Evendale, OH (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F01D 9/04 (2006.01);
U.S. Cl.
CPC ...
F01D 9/041 (2013.01); F05D 2200/11 (2013.01); F05D 2200/12 (2013.01); F05D 2200/13 (2013.01); F05D 2200/14 (2013.01); F05D 2200/221 (2013.01); F05D 2200/261 (2013.01); F05D 2200/262 (2013.01); F05D 2220/3212 (2013.01); F05D 2240/121 (2013.01); F05D 2240/122 (2013.01); F05D 2240/123 (2013.01); F05D 2240/124 (2013.01); F05D 2240/125 (2013.01); F05D 2240/35 (2013.01); F05D 2260/941 (2013.01); F23R 2900/00005 (2013.01);
Abstract

A gas turbine engine includes a compressor section, a combustion section defining a combustion chamber, and a turbine section disposed in serial flow order along a central axis of the gas turbine engine. The combustion section includes a plurality of fuel nozzles in fluid communication with the combustion chamber. The plurality of fuel nozzles define a fuel nozzle pitch extending between a fuel nozzle centerline of adjacent ones of the plurality of fuel nozzles. The turbine section includes a plurality of vanes and a plurality of rotor blades. The turbine section defines a clocking pitch fraction in degrees about the central axis and the clocking pitch fraction is defined between a peak temperature region and a midpoint of a vane pitch. The vane pitch is defined between the leading edge of adjacent ones of the plurality of vanes.


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