GAS TURBINE FAN FAIRING PLATFORM AND METHOD OF FAIRING A ROOT LEADING EDGE OF A FAN BLADE OF A GAS TURBINE ENGINE

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United States of America Patent

APP PUB NO 20170058916A1
SERIAL NO

14841852

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Abstract

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A gas turbine fan fairing platform includes at least one body defining a surface and having an opening receptive to a blade, a protrusion extending outwardly from the surface in a direction that will position the protrusion along a leading edge near a root of the blade.

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Patent Owner(s)

Patent OwnerAddress
RAYTHEON TECHNOLOGIES CORPORATION10 FARM SPRINGS ROAD FARMINGTON CT 06032-2568

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Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Franklin, Jordan J Hartford, US 5 5
McComb, Patrick James Cromwell, US 11 30
Weisse, Michael A Tolland, US 55 792
Whitehurst, Sean A South Windsor, US 12 29

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