GAS TURBINE AND SPACER DISK FOR GAS TURBINE

To suppress generation of stress created in a rim of a spacer disk for a gas turbine.SOLUTION: A gas turbine spacer disk 310 includes a disk portion 320, a rim portion 322, a first fillet, and a second fillet. An outer face of the rim portion defines a plurality of grooves 334 extending in a circumf...

Ausführliche Beschreibung

Bibliographische Detailangaben

1. Verfasser:	FRED THOMAS WILLETT JR
Format:	Patent
Sprache:	eng ; jpn
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!