SERVICE TUBE FOR A TURBINE ENGINE

An apparatus and method of reducing operating temperatures of a gas turbine engine 10, exposed to a service tube assembly 84 by utilizing a skirt 98 and radially outer mount 90. The reduction in temperature exposure minimizes temperatures of the service tube assembly 84 during engine 10 operation to...

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Bibliographic Details
Main Authors JAKOMIN, John Martin, AGARA, Karthik Gopal Rao, RAJAGOPALAN, Vinodh, FEMIA, Steven
Format Patent
LanguageEnglish
French
German
Published 23.08.2017
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
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Summary:An apparatus and method of reducing operating temperatures of a gas turbine engine 10, exposed to a service tube assembly 84 by utilizing a skirt 98 and radially outer mount 90. The reduction in temperature exposure minimizes temperatures of the service tube assembly 84 during engine 10 operation to reduce the incidence of oil coking or varnish.
Bibliography:Application Number: EP20170156325