INTERCOOLER FOR MULTISTAGE COMPRESSOR TURBOCHARGER

PROBLEM TO BE SOLVED: To provide effective air cooling between stages of a multistage turbocharger. SOLUTION: Diffuser vanes, direction changing vanes and/or swirl removing vanes are used as heat exchangers in an intermediate duct. A coolant is fed to the heat exchangers, between which is flows in s...

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Bibliographic Details
Main Authors GLADDEN JOHN R, HOUTZ PHILLIP J
Format Patent
LanguageEnglish
Published 17.05.2002
Edition7
Subjects
AIR INTAKES FOR JET-PROPULSION PLANTS
BLASTING
COMBUSTION ENGINES
COMBUSTION ENGINES IN GENERAL
CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
GAS-TURBINE PLANTS
HEATING
HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
INTERNAL-COMBUSTION PISTON ENGINES
LIGHTING
MECHANICAL ENGINEERING
WEAPONS
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Summary:PROBLEM TO BE SOLVED: To provide effective air cooling between stages of a multistage turbocharger. SOLUTION: Diffuser vanes, direction changing vanes and/or swirl removing vanes are used as heat exchangers in an intermediate duct. A coolant is fed to the heat exchangers, between which is flows in series through an internal coolant link or through an internal cavity formed by a turbocharger housing.
Bibliography:Application Number: JP20010285271