CONVECTION COOLING AT LOW EFFUSION DENSITY REGION OF COMBUSTOR PANEL

A combustor for a gas turbine engine includes a combustion chamber defined between an inner shell and an outer shell. The combustor further includes a bulkhead extending between the inner shell and the outer shell. The combustor further includes a liner panel mounted to one of the inner shell and th...

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Bibliographische Detailangaben
Hauptverfasser: Ichihashi, Fumitaka, Lienau, Jeffrey J
Format: Patent
Sprache:eng
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