MECHANISM FOR BYPASS CORRECTION OF INTERNAL COMBUSTION ENGINE'S SUPERCHARGING TURBO-BLOWER

The device for by-pass correction of turbocharger of combustion engine consists of fluidic jet-driven distributing element (40) equipped with feeding nozzle (41) and two collectors (46, 47). In the fluidic jet-driven distributing element (40) between the feeding nozzle (41) and the first collector (...

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Bibliographische Detailangaben
Hauptverfasser:	TESAR VACLAV CSC.,CS, TAKATS MICHAL CSC.,CS
Format:	Patent
Sprache:	eng
Schlagworte:	ARRANGEMENT OR MOUNTING OF PLURAL DIVERSE PRIME-MOVERS INVEHICLES ARRANGEMENT OR MOUNTING OF PROPULSION UNITS OR OFTRANSMISSIONS IN VEHICLES ARRANGEMENTS IN CONNECTION WITH COOLING, AIR INTAKE, GASEXHAUST OR FUEL SUPPLY OF PROPULSION UNITS, IN VEHICLES AUXILIARY DRIVES FOR VEHICLES BLASTING CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TOTRANSPORTATION COMBUSTION ENGINES COMBUSTION ENGINES IN GENERAL CONTROLLING COMBUSTION ENGINES GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS INSTRUMENTATION OR DASHBOARDS FOR VEHICLES INTERNAL-COMBUSTION PISTON ENGINES LIGHTING MECHANICAL ENGINEERING PERFORMING OPERATIONS TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINSTCLIMATE CHANGE TRANSPORTING VEHICLES IN GENERAL WEAPONS
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Beschreibung
Zusammenfassung:	The device for by-pass correction of turbocharger of combustion engine consists of fluidic jet-driven distributing element (40) equipped with feeding nozzle (41) and two collectors (46, 47). In the fluidic jet-driven distributing element (40) between the feeding nozzle (41) and the first collector (46) and the second collector (47) there are two holding walls (44, 45). The fluidic jet-driven distributing element (40) is equipped with the first controlling nozzle (42) and the second controlling nozzle, oriented opposite each other. The first controlling nozzle (42) is connected by means of feed-back channel (51) with vortex chamber (52) of the fluidic vortex amplifier. The second controlling nozzle (43) is connected with the vortex chamber (52) by means of a radial nozzle (521). The air pipeline (1) is connected with the vortex chamber (52) by means of tangential nozzle (513) and interconnecting pipeline (15). The air pipeline is connected also with compressor output (10). The device for by-pass correction of turbocharger of combustion engine can be applied in facilities producing combustion engines, mainly of vehicle-type, or in facilities producing turbochargers.