An acoustic damper for a rotary machine includes at least one wall, at least one cooling air
inlet, at least one outlet, and at least one cap. The at least one wall extends from a back side …

A turbine engine that includes an engine core having at least a compressor section and a
combustion section. The combustion section includes a combustor. The combustor section …

A combustor liner for a gas turbine includes a liner at least partially defining a combustion
chamber. The liner includes a plurality of dilution openings therethrough, at least one …

A turbine engine that includes an engine core having at least a compressor section and a
combustion section. The combustion section includes a combustor. The combustor section …

A deflector assembly for a combustor defining an operational fluid flow. The deflector
assembly includes an upstream surface and a downstream surface opposite the upstream …

A combustor for a gas turbine engine has a combustor liner that has a cold surface side and
a hot surface side, the liner defining an upstream end and a downstream end, and a dilution …

A combustor for use in a gas turbine engine including a heat shield panel having a first
surface and a second surface opposite the first surface of the heat shield panel and a …

A rotary machine includes at least one burner including a front panel having a front side and
an opposing back side. The acoustic damper includes at least one wall, at least one cooling …

The present disclosure is directed to a bundled tube type fuel nozzle assembly. The fuel
nozzle assembly includes a fuel plenum body including a forward plate, an aft plate, an …