Patent ID: 8997485
Filing Date: 2015-04-07
Classification: F01D,F05D

Abstract:
1. A turbine of an exhaust gas turbocharger ( 22 ) of an internal combustion engine ( 10 ), comprising at least a first inner housing part ( 56 ), which has at least two spiral inlet channels ( 58 ) with trumpet-shaped inlet areas ( 80 ) which are arranged circumferentially spaced around the first housing part ( 56 ), the first housing part ( 56 ) with the at least two spiral inlet channels ( 58 ) being disposed in a second, outer housing part ( 72 ) extending annularly all around the first housing part ( 56 ) in spaced relationship therefrom and forming a sealed accommodating chamber ( 74 ) in communication with the internal combustion engine to receive and direct an exhaust gas flow of the internal combustion engine ( 10 ) through the at least two spiral inlet channels ( 58 ) to a turbine wheel ( 60 ) disposed within the first housing part ( 56 ).