Patent · US Active

Combustor for a gas turbine engine

US11774098B2 · kind B2 · utility

1Cited by

36References

20Claims

0Family size

Assignee

General Electric Company · US

Inventors

Pradeep Naik · Kanchinakote, IN
Rimple Rangrej · Bengaluru, IN
Saket Singh · Bengaluru, IN
Narasimha Chiranthan R · Kanchinakote, IN
Shai Birmaher · Cincinnati, US
Hiranya Nath · Bengaluru, IN
Ravindra Shankar Ganiger · Kanchinakote, IN

Key dates

Filing date	Jun 7, 2021
Grant date	Oct 3, 2023
Priority date	—
Expiry date	Jun 17, 2041

Classification

Technology area (CPC F)Mechanical Engineering; Lighting; Heating
CPC primaryF23R2900/03042
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; 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; and a fence disposed between the forward and aft liner segments, wherein the fence extends in the circumferential direction, and wherein the fence extends into the combustion chamber along the radial direction.

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