Patent · US Active

Combustor for a gas turbine engine

US12152777B2 · kind B2 · utility

0Cited by

37References

14Claims

0Family size

Assignee

General Electric Company · US

Inventors

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

Key dates

Filing date	Jun 7, 2021
Grant date	Nov 26, 2024
Priority date	—
Expiry date	Jun 7, 2041

Classification

Technology area (CPC F)Mechanical Engineering; Lighting; Heating
CPC primaryF23R2900/03043
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 liner at least partially defining a combustion chamber, the liner including a dilution slot in fluid communication with the combustion chamber; and one or more guides configured to redirect cooling medium into the dilution slot.

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