GAS TURBINE ROTOR ASSEMBLY AND METHOD OF ASSEMBLY

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...

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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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creator HIMES, JASON D
TRESSER, JORDAN
MECKLENBURG, DWAYNE K
WILSON, ROSS
GRIFFIN, DAVID RICHARD
VIRKLER, SCOTT D
description 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 configured to axially maintain the heat shield (106) within the slot (104).
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subjects 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
title GAS TURBINE ROTOR ASSEMBLY AND METHOD OF ASSEMBLY
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