Patent · US Active

Combustor for a gas turbine engine

US12085283B2 · kind B2 · utility

0Cited by

40References

17Claims

0Family size

Assignee

General Electric Company · US

Inventors

Ravindra Shankar Ganiger · Kanchinakote, IN
Hiranya Nath · Bengaluru, IN
Daniel J. Kirtley · Blue Ash, US
Shai Birmaher · Cincinnati, US
Veeraraju Vanapalli · Bengaluru, IN
Karthikeyan Sampath · Bengaluru, IN
Deepak Ghiya · Kanchinakote, IN
Perumallu Vukanti · Bengaluru, IN
Rajendra Mahadeorao Wankhade · Bengaluru, IN
Pradeep Naik · Kanchinakote, IN
Rimple Rangrej · Bengaluru, IN
Saket Singh · Bengaluru, IN

Key dates

Filing date	Jun 7, 2021
Grant date	Sep 10, 2024
Priority date	—
Expiry date	Oct 18, 2041

Classification

Technology area (CPC F)Mechanical Engineering; Lighting; Heating
CPC primaryF23R2900/00005
WIPO fieldEngines, pumps, turbines
WIPO sectorMechanical engineering

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.

Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.