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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Main Authors | , , |
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Format | Patent |
Language | English French German |
Published |
06.07.2016
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Subjects | |
Online Access | Get full text |
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Abstract | 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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AbstractList | 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. |
Author | HASTING, WILLIAM HOWARD WOLFE, JARED MATTHEW DALE, DAVID EDWARD |
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Discipline | Medicine Chemistry Sciences |
DocumentTitleAlternate | KANALGEFÜHRTER HAUBENTRÄGER FÜR EINEN GASTURBINENMOTOR SUPPORT DE CAPOT CARÉNÉ POUR UN MOTEUR À TURBINE À GAZ |
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RelatedCompanies | GENERAL ELECTRIC COMPANY |
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Snippet | 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... |
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SubjectTerms | 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 |
Title | DUCTED COWL SUPPORT FOR A GAS TURBINE ENGINE |
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