In a gas turbine combustor having an inner and outer liner defining an annular combustion
chamber, at least an annular scoop ring provided on each inner and outer combustor liner …

A combustor for a turbine engine includes an inner combustion liner and an outer
combustion liner together defining at least in part an interior. The interior includes a …

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 flow device for a combustor assembly defining a longi tudinal axis around which the flow
device is positioned is provided. The flow device includes a body extended around the …

A trapped vortex combustor for use in a gas turbine engine defines a radial direction, an
axial direction, and a circumferential direction. The trapped vortex combustor includes an …

A combustor for use in a turbine engine that includes an inner combustion liner and an outer
combustion liner. An interior is defined between the inner combustion liner and the outer …

US20220333783A1 - Hydrogen-Fueled Combustor for Gas Turbines - Google Patents
US20220333783A1 - Hydrogen-Fueled Combustor for Gas Turbines - Google Patents …

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 …

A combustor includes a circumferential main combustion chamber and a plurality of air
inlets, the plurality of air inlets dispersing air into the circumferential main combustion …