Combustor turbine interface for a gas turbine engine

A turbine vane (42) downstream of a combustor section (16) includes an arcuate outer vane platform (38) defined about an axis. The arcuate outer vane platform (38) includes a segment (38S) of the arcuate outer vane platform (38) along the axis which follows an outer combustor liner panel structure (...

Ausführliche Beschreibung

Gespeichert in:

Bibliographische Detailangaben
Hauptverfasser:	HOKE, JAMES B, KIRSOPP, PHILIP J
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	BLASTING ENGINE PLANTS IN GENERAL HEATING LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES STEAM ENGINES WEAPONS
Online-Zugang:	Volltext bestellen
Tags:	Tag hinzufügen Keine Tags, Fügen Sie den ersten Tag hinzu!

Beschreibung
Zusammenfassung:	A turbine vane (42) downstream of a combustor section (16) includes an arcuate outer vane platform (38) defined about an axis. The arcuate outer vane platform (38) includes a segment (38S) of the arcuate outer vane platform (38) along the axis which follows an outer combustor liner panel structure (46). An arcuate inner vane platform (40) is defined about the axis. The arcuate inner vane platform (40) includes a segment (40S) of the arcuate inner vane platform (40) along the axis which follows an inner combustor liner panel structure (48). This affords a smooth flow path from the combustor section (16) into a turbine section (18).