GAS TURBINE ENGINE BLADE SLOT HEAT SHIELD

GAS TURBINE ENGINE BLADE SLOT HEAT SHIELD

A gas turbine engine rotor assembly includes a rotor disk with a slot. A rotor blade has a root supported within the slot. A heat shield is arranged in a cavity in the slot between the root and the rotor disk. An axial retention feature is configured to axially maintain the heat shield within the sl...

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Hauptverfasser: HIMES JASON D, TRESSER JORDAN, WILSON ROSS, VIRKLER SCOTT D, GRIFFIN DAVID RICHARD, MECKLENBURG DWAYNE K
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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creator HIMES JASON D
TRESSER JORDAN
WILSON ROSS
VIRKLER SCOTT D
GRIFFIN DAVID RICHARD
MECKLENBURG DWAYNE K
description A gas turbine engine rotor assembly includes a rotor disk with a slot. A rotor blade has a root supported within the slot. A heat shield is arranged in a cavity in the slot between the root and the rotor disk. An axial retention feature is configured to axially maintain the heat shield within the slot.
format Patent
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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 ENGINE BLADE SLOT HEAT SHIELD
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