FAN BLADE OF A GAS TURBINE ENGINE

A fan of a gas turbine engine includes a plurality of fan blades (70) secured to a rotor, each of the plurality of fan blades having an airfoil (72) secured to the rotor at one end, wherein the airfoil comprises pockets (90) filled with an elastomeric composite.

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Hauptverfasser: WEISSE, Michael A, BALES, Daniel A, HANSEN, James O, HERTEL, Christopher J, GRAVES, William R
Format: Patent
Sprache:eng ; fre ; ger
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creator WEISSE, Michael A
BALES, Daniel A
HANSEN, James O
HERTEL, Christopher J
GRAVES, William R
description A fan of a gas turbine engine includes a plurality of fan blades (70) secured to a rotor, each of the plurality of fan blades having an airfoil (72) secured to the rotor at one end, wherein the airfoil comprises pockets (90) filled with an elastomeric composite.
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language eng ; fre ; ger
recordid cdi_epo_espacenet_EP3513903B1
source esp@cenet
subjects BLASTING
COMBINED OPERATIONS
ENGINE PLANTS IN GENERAL
HEATING
LIGHTING
MACHINE TOOLS
MACHINES OR ENGINES IN GENERAL
MECHANICAL ENGINEERING
METAL-WORKING NOT OTHERWISE PROVIDED FOR
NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES
OTHER WORKING OF METAL
PERFORMING OPERATIONS
STEAM ENGINES
TRANSPORTING
UNIVERSAL MACHINE TOOLS
WEAPONS
title FAN BLADE OF A GAS TURBINE ENGINE
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