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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Bibliographische Detailangaben
Hauptverfasser:	GLADDEN JOHN R, HOUTZ PHILLIP J
Format:	Patent
Sprache:	eng
Schlagworte:	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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Beschreibung
Zusammenfassung:	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.