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:
Sep. 10, 2024

Filed:

Jun. 07, 2021
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Ravindra Shankar Ganiger, Bangalore, IN;

Hiranya Kumar Nath, Bangalore, IN;

Daniel J. Kirtley, Blue Ash, OH (US);

Shai Birmaher, Cincinnati, OH (US);

Veeraraju Vanapalli, Bangalore, IN;

Karthikeyan Sampath, Bangalore, IN;

Deepak Ghiya, Bangalore, IN;

Perumallu Vukanti, Bangalore, IN;

Rajendra Mahadeorao Wankhade, Bangalore, IN;

Pradeep Naik, Bangalore, IN;

Rimple Rakeshkumar Rangrej, Bangalore, IN;

Saket Singh, Bangalore, IN;

Assignee:

GENERAL ELECTRIC COMPANY, Cincinnati, OH (US);

Attorneys:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F23R 3/42 (2006.01); F02C 3/02 (2006.01); F02C 3/14 (2006.01);
U.S. Cl.
CPC ...
F23R 3/42 (2013.01); F02C 3/02 (2013.01); F02C 3/14 (2013.01); F05D 2220/32 (2013.01); F05D 2240/35 (2013.01);
Abstract

A combustor for a gas turbine engine, the gas turbine engine defining a longitudinal centerline extending in a longitudinal direction, a radial direction extending orthogonally outward from the longitudinal centerline, and a circumferential direction extending concentrically around the longitudinal centerline, the combustor including: a forward liner segment; and an aft liner segment disposed downstream from the forward liner segment relative to a direction of flow through the combustor, the forward and aft liner segments at least partially defining a combustion chamber, wherein the forward and aft liner segments are coupled together at a moveable interface.


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