Gas turbine combustor liner with asymmetric dilution holes machined from a single piece form

1. Field of the Invention An annular gas turbine engine combustor liner has a single piece annular shell circumscribed about a first axis of revolution. The shell has a hot side and a cold side, an annular dilution hole section, and a plurality of asymmetrical cylindrical dilution holes extending th...

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Bibliographische Detailangaben

Hauptverfasser:	Farmer, Gilbert, Brown, Daniel D, Rutherford, Myron E, Vise, Steven C, Martini, Jeffrey M
Format:	Patent
Sprache:	eng
Online-Zugang:	Volltext bestellen
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