Patent application number | Description | Published |
20090022581 | TURBOCHARGER COMPRISING ADJUSTABLE GUIDE BLADES, BLADE LEVER AND ADJUSTING RING THEREFOR - The invention relates to a turbocharger ( | 01-22-2009 |
20090067996 | BLADE BEARING RING ASSEMBLY OF A TURBOCHARGER WITH A VARIABLE TURBINE GEOMETRY - The invention relates to a turbocharger with a variable turbine geometry. Said turbocharger comprises a blade bearing ring assembly ( | 03-12-2009 |
20100104425 | CHARGING EQUIPMENT - The invention relates to a piece of charging equipment having a variable turbine geometry ( | 04-29-2010 |
20100166541 | CHARGING DEVICE - The invention relates to a charging device ( | 07-01-2010 |
20100196146 | TURBOCHARGER WITH VARIABLE TURBINE GEOMETRY - The guide blades provided for the variable turbine geometry are adjustably arranged within a radial gap through which gases can flow on a moveable carrier ring, which is axially clamped against stops on or in the radial gap with a thrust spring device. According to the invention, the thrust spring device loads the carrier ring on the positions closely adjacent to the stops. The thrust spring device is designed open without sealing function and if applicable combined with a separate seal without thrust function. | 08-05-2010 |
20100232937 | CHARGING DEVICE, MORE PREFERABLY FOR A MOTOR VEHICLE, WITH A VARIABLE TURBINE GEOMETRY - The invention relates to a charging device, more preferably a turbocharger, with a spring for clamping the guide blade carrier ( | 09-16-2010 |
20110038742 | TURBINE, IN PARTICULAR FOR AN EXHAUST GAS TURBOCHARGER, AND EXHAUST GAS TURBOCHARGER - An exhaust gas turbocharger, comprising: a turbine rotor rotatably mounted in a housing, which is associated with at least one guide apparatus forming a radial inlet channel, wherein the guide apparatus includes at least one of a guide vane bearing ring, a plurality of guide vanes radially surrounding the turbine rotor and located in the inlet channel and a guide vane cover ring. The inlet channel is axially delimited by the guide vane bearing ring and the guide vane cover ring wherein the guide vane bearing ring and the guide vane cover ring are moveably mounted at least one of axially and radially relative to each other and to the housing. The guide apparatus is subjected to at least one of an axial and radial preload, wherein a line of axial preload flux runs through the guide apparatus substantially parallel to the rotational axis of the turbine rotor. | 02-17-2011 |
20140212306 | TURBINE, PARTICULARLY FOR AN EXHAUST GAS TUROBCHARGER, AND EXHAUST GAS TURBOCHARGER - The invention relates to a turbine ( | 07-31-2014 |