Guiding device for waste gas turbocharger axial air intaking turbine

A guiding device for axial air intaking turbine of waste gas turbocharger of internal combustion engine with heavy oil as fuel comprises a plurality of guide vanes asway located on the housing washer (3) of the guide vanes, the guide vanes can rotate corresponding to the housing washer (3) of the gu...

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Bibliographische Detailangaben
Hauptverfasser:	SWEET T, WAGAS A, WUTZ D
Format:	Patent
Sprache:	chi ; eng
Schlagworte:	AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING COMBUSTION ENGINES COMBUSTION ENGINES IN GENERAL CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS ENGINE PLANTS IN GENERAL GAS-TURBINE PLANTS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS INDEXING SCHEME FOR ASPECTS RELATING TONON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES ORJET-PROPULSION PLANTS INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUSSUBCLASSES OF CLASSES F01-F04 INTERNAL-COMBUSTION PISTON ENGINES LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES STEAM ENGINES WEAPONS
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Beschreibung
Zusammenfassung:	A guiding device for axial air intaking turbine of waste gas turbocharger of internal combustion engine with heavy oil as fuel comprises a plurality of guide vanes asway located on the housing washer (3) of the guide vanes, the guide vanes can rotate corresponding to the housing washer (3) of the guide vanes with the help of an adjusting rod (5) and an adjusting ring which is combined acted by the corresponding adjusting rod as well as the adjusting device on the adjusting ring. For the angle position of the guide vanes, the guiding device can abandon the accurate position and prescription because the symmetrical force leading-in on the circle of the adjusting ring, the adjusting device acting on the adjusting ring comprises a plurality of articulated connecting elements (7, 8, 9) which are symmetrically distributed on the circle of the adjusting ring, the connecting elements are severally drove by the servomotor supported on the opposite part of the adjusting ring, wherein the servomotor is synchronous to ea