VARIABLE TURBINE GEOMETRY COMPONENT WEAR MITIGATION IN RADIAL TURBOMACHINES WITH DIVIDED VOLUTES BY AERODYNAMIC FORCE OPTIMIZATION AT ALL VANES OR ONLY VANE(S) ADJACENT TO VOLUTE TONGUE(S)

An entryway system includes a divided volute turbocharger having variable turbine geometry (VTG). The turbocharger includes a turbine housing, first and second volutes separated by a wall having a first and second tongue, and a turbine housing outlet. The system also includes a turbine wheel dispose...

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Bibliographische Detailangaben

Hauptverfasser:	Troxler, Paul, Biswas, Abhishek, Zagone, John Robert, Colont, Craig Andrew
Format:	Patent
Sprache:	eng
Schlagworte:	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 LIGHTING MECHANICAL ENGINEERING WEAPONS
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