End rail mate-face low pressure vortex minimization
Abstract:
A combustor assembly for a turbine engine includes a liner panel defining a portion of an inner surface of a combustor chamber. The liner panel includes an end face transverse the inner surface and at least one diffuser through the end face. A method of assembling a combustor for a turbine engine is also disclosed.
Public/Granted literature
Information query
Patent Agency Ranking
0/0