Injector assembly and ducting arrangement including such injector assemblies in a combustion system for a gas turbine engine
AJ North, JEP Bilbao, WR Laster… - US Patent App. 15 …, 2017 - Google Patents
Injector assembly and ducting arrangement including such assemblies for a combustor
system in a gas turbine engine are provided. A reactant-guiding structure (42) may be
configured to define a curvilinear flow path (47) to route a flow of reactants from a first flow
direction (50) to a second flow direction (52) toward a cross-flow of combustion gases (60). A
cross-flow guiding structure (54) may further define a flow path (58) to route a portion of the
cross-flow of combustion gases toward an outlet side of the cross-flow guiding structure …
system in a gas turbine engine are provided. A reactant-guiding structure (42) may be
configured to define a curvilinear flow path (47) to route a flow of reactants from a first flow
direction (50) to a second flow direction (52) toward a cross-flow of combustion gases (60). A
cross-flow guiding structure (54) may further define a flow path (58) to route a portion of the
cross-flow of combustion gases toward an outlet side of the cross-flow guiding structure …
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