GAS TURBINE ROTOR ASSEMBLY AND METHOD OF ASSEMBLY

A gas turbine engine rotor assembly includes a rotor disk (68) with a slot (104). A rotor blade (64) has a root (74) supported within the slot (104). A heat shield (106) is arranged in a cavity in the slot (104) between the root (74) and the rotor disk (68). An axial retention feature (116,118) is c...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	HIMES, JASON D, TRESSER, JORDAN, MECKLENBURG, DWAYNE K, WILSON, ROSS, GRIFFIN, DAVID RICHARD, VIRKLER, SCOTT D
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
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