A combustor for a gas turbine engine is provided. The combustor includes an annular inner
liner; an annular outer liner circumscribing the annular inner liner; and a combustor dome …

A rich-quench-lean combustor assembly for a gas turbine engine includes a liner extending
between a forward end and an aft end. The liner includes a plurality of quench air jets …

The present disclosure is directed to a combustor assembly for a gas turbine engine. The
combustor assembly includes a liner defining a combustion chamber therewithin and a …

(57) ABSTRACT A rich-quench-lean combustor assembly for a gas turbine engine includes
a fuel nozzle and a dome, the fuel nozzle attached to the dome. The combustor assembly …

A rich-quench-lean combustor assembly for a gas turbine engine includes a fuel nozzle and
a dome, the fuel nozzle attached to the dome. The combustor assembly additionally includes …

A gas turbine engine including a trapped vortex combustor assembly is generally provided.
The combustor assembly includes an inner liner wall extended annularly around a …

The present disclosure is directed to a combustion section for a gas turbine engine including
a combustor assembly, an outer casing, a fuel injector assembly, and an inner casing. An …

Turbo machine combustion assembly (1) comprising a com bustion chamber (10), at least
one starting injector (17), a plurality of main injectors (18) distributed at constantangular …

A combustor liner, a gas turbine engine including a combustor having the combustor liner,
and a method for regulating jet wakes in the combustor are disclosed. The combustor liner …

A combustor includes an inner liner and an outer liner defining a combustion chamber. The
inner liner includes an inner mesh structure, a plurality of hot side planks mounted to a hot …