Invention Application
- Patent Title: CAVITY STAGING IN A COMBUSTOR
- Patent Title (中): 在一个COMBUSTOR的CAVITY STAGING
-
Application No.: US14791684Application Date: 2015-07-06
-
Publication No.: US20170009993A1Publication Date: 2017-01-12
- Inventor: Sarah Marie Monahan , Narendra Digamber Joshi , Venkat Eswarlu Tangirala , Matthieu Marc Masquelet
- Applicant: General Electric Company
- Main IPC: F23R3/28
- IPC: F23R3/28 ; F23R3/34

Abstract:
A combustor assembly including a combustor liner defining therein a combustion chamber for the downstream flow of a main fluid. At least two annular trapped vortex cavities are located on the combustor liner and staged axially spaced apart. A cavity opening is located at a radially inner end of each of the at least two annular trapped vortex cavities spaced apart from a radially outer wall and extending between an aft wall and a forward wall of each cavity. A plurality of injectors are configured tangentially relative to the circular radially outer wall to provide for an injection of air and fuel to form an annular rotating trapped vortex of a fuel and air mixture within a respective annular trapped vortex cavity. The annular rotating trapped vortex of the fuel and air mixture at the cavity openings is substantially perpendicular to the downstream flow of the main fluid. A gas turbine engine including the combustor assembly is disclosed.
Public/Granted literature
- US10072846B2 Trapped vortex cavity staging in a combustor Public/Granted day:2018-09-11
Information query