COMBINED TURBINE NOZZLE AND SHROUD DEFLECTION LIMITER

A gas turbine engine annular turbine nozzle assembly includes airfoils extending between inner and outer band segments coaxial and circumscribed about a centerline axis. Shroud segment extends downstream from outer band segment. A middle outer flange may be between the segments and they may be integ...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	LENIHAN, MEGHAN MARY, TAGLIERI, MICHAEL EDMUND, MANTEIGA, JOHN ALAN, HOOPER, TYLER FREDERICK
Format:	Patent
Sprache:	eng
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
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