DUCTED COWL SUPPORT FOR A GAS TURBINE ENGINE

A ducted cowl support (54) includes an annular structure configured to be mounted to an annular turbine engine frame (46) and including one or more bypass ducts (62) integrally formed therein.

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Bibliographic Details
Main Authors HASTING, WILLIAM HOWARD, DALE, DAVID EDWARD, WOLFE, JARED MATTHEW
Format Patent
LanguageEnglish
French
German
Published 06.07.2016
Subjects
AIR INTAKES FOR JET-PROPULSION PLANTS
BLASTING
COMBUSTION ENGINES
CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
GAS-TURBINE PLANTS
HEATING
HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
JET-PROPULSION PLANTS
LIGHTING
MECHANICAL ENGINEERING
WEAPONS
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Summary:A ducted cowl support (54) includes an annular structure configured to be mounted to an annular turbine engine frame (46) and including one or more bypass ducts (62) integrally formed therein.
Bibliography:Application Number: EP20150200690