AIR COOLED ELECTRONIC TURBO ACTUATOR

A number of variations may include a product comprising an engine having an intake manifold and an exhaust manifold; a turbocharger having a compressor operatively attached to a turbine, wherein the compressor is in fluid communication with the intake manifold through a first conduit and the turbine...

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Bibliographic Details
Main Authors GARRARD, Tyler R, HANDLON, Brian E, ZAGONE, John R
Format Patent
LanguageEnglish
French
German
Published 17.07.2019
Subjects
BLASTING
COMBUSTION ENGINES
COMBUSTION ENGINES IN GENERAL
COOLING OF INTERNAL-COMBUSTION ENGINES
COOLING OF MACHINES OR ENGINES IN GENERAL
ENGINE PLANTS IN GENERAL
HEATING
HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
INTERNAL-COMBUSTION PISTON ENGINES
LIGHTING
MACHINES OR ENGINES IN GENERAL
MECHANICAL ENGINEERING
STEAM ENGINES
WEAPONS
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Summary:A number of variations may include a product comprising an engine having an intake manifold and an exhaust manifold; a turbocharger having a compressor operatively attached to a turbine, wherein the compressor is in fluid communication with the intake manifold through a first conduit and the turbine is in fluid communication with the exhaust manifold through a second conduit; an actuator in operative communication with one of a vane pack or a wastegate; a charge air cooler disposed within the first conduit; a first air filter in fluid communication with the compressor through a third conduit; a mass air flow sensor disposed within the third conduit; and an actuator cooling system operatively attached to an interior of the actuator to deliver an air flow to the interior of the actuator to cool the actuator.
Bibliography:Application Number: EP20190151290