WALL ELEMENTS FOR GAS TURBINE ENGINE COMBUSTORS

PROBLEM TO BE SOLVED: To provide an improved cooling film as a wall element for gas turbine engine combustors. SOLUTION: A combustor wall element arrangement for a gas turbine engine comprises an upstream wall element 50A overlapping a downstream wall element 50B and defining a gap 37 and an outlet...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: MILLS STEPHEN JOHN, WOOLFORD JAMES RICHARD, WHITE KEVIN ANDREW
Format: Patent
Sprache:eng
Schlagworte:
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