Patent · US Active

Turbo machine combustor assembly having separable portions coupled at a fitted interface

US12173897B2 · kind B2 · utility

0Cited by

19References

12Claims

0Family size

Assignee

General Electric Company · US

Inventors

Ryan Christopher Jones · West Chester, US
Paul Christopher Schilling · Neckargemünd, DE
Andrew Scott Bilse · Cincinnati, US
Daniel Endecott Osgood · St. Bernard, US
Donald Lee Gardner · Sharonville, US

Key dates

Filing date	Feb 18, 2022
Grant date	Dec 24, 2024
Priority date	—
Expiry date	Apr 23, 2042

Classification

Technology area (CPC F)Mechanical Engineering; Lighting; Heating
CPC primaryF23R2900/00018
WIPO fieldEngines, pumps, turbines
WIPO sectorMechanical engineering

Abstract

Embodiments of a combustor assembly for a turbine engine are generally provided. The combustor assembly includes a first separable portion defining a dome assembly, and a second separable portion defining a deflector assembly. The first separable portion and the second separable portion are coupled together at a fitted interface.

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