TURBOMACHINE NOZZLE WITH AN AIRFOIL HAVING A CIRCULAR TRAILING EDGE

TURBOMACHINE NOZZLE WITH AN AIRFOIL HAVING A CIRCULAR TRAILING EDGE

A gas turbine engine (10) defines an axial direction (A), a radial direction (R) perpendicular to the axial direction (A), and a circumferential direction (C) extending concentrically around the axial direction (A). The gas turbine engine (10) includes a nozzle (202) having an inner platform (208),...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Hauptverfasser: KARAKASIS, Marios, IVANOV, Konstantin Valerievich
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 gas turbine engine (10) defines an axial direction (A), a radial direction (R) perpendicular to the axial direction (A), and a circumferential direction (C) extending concentrically around the axial direction (A). The gas turbine engine (10) includes a nozzle (202) having an inner platform (208), an outer platform (210), and an airfoil (212). The airfoil (212) includes a leading edge (218), a trailing edge (220) downstream of the leading edge (218), a pressure side surface (224), and a suction side surface (226) opposite the pressure side surface (224). The trailing edge (220) defines a circular arc between the inner platform (208) and the outer platform (210).