Gas turbine engine combustor

F - Mech Eng,Light,Heat,Weapons – 23 – N

Patent

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F23N 5/08 (2006.01)

Patent

CA 2708944

A combustor for a gas turbine engine, and including an integrated dome and deflector having a conical shape optimized for each individual combustor cup in an array of combustor cups, as determined by CFD analysis for eliminating combustor air recirculation zones and swirling. A related method is also disclosed.

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