RADIAL COMPRESSOR FOR AN EXHAUST GAS TURBO CHARGER

The compressor (1) has a sleeve-like adapter element (10) sectionally including a surface contour (13) at an axial front side (12), which faces towards a compressor wheel (6) in an axial fixing position. The surface contour is formed complementary to an axial wheel-surface contour (9) so that a widt...

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Bibliographische Detailangaben
Hauptverfasser:	Haslinger, Fabian, Fiedler, Max, Hanig, Urs
Format:	Patent
Sprache:	eng ; fre ; ger
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 NON-POSITIVE DISPLACEMENT PUMPS POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PUMPS FOR LIQUIDS OR ELASTIC FLUIDS WEAPONS
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Beschreibung
Zusammenfassung:	The compressor (1) has a sleeve-like adapter element (10) sectionally including a surface contour (13) at an axial front side (12), which faces towards a compressor wheel (6) in an axial fixing position. The surface contour is formed complementary to an axial wheel-surface contour (9) so that a width (w) of a passage gap (14) is adjusted by axially moving an adapter element in a fastening section (11) in a non-fixed condition of the adapter element. The gap is axially formed between the adapter element and the compressor wheel along the surface contours facing towards each other. The adapter element is made of a plastic material. Independent claims are also included for the following: (1) a turbocharger (2) a method for manufacturing a radial compressor.