General Electric Company
Combustor Assembly for a Turbo Machine
Last updated:
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.
Status:
Application
Type:
Utility
Filling date:
23 Aug 2018
Issue date:
27 Feb 2020