Turbo Systems Switzerland Ltd.

Accelleron Switzerland Ltd.

Moritz Mosdzien

Wolfgang Joos

Andreas Schmid

Marcel Joho

Stefan Gantert

Peter Limacher

Davide Marra

According to embodiments described herein, an oil-cooled exhaust turbine apparatus is provided. The exhaust turbine apparatus comprises a rotatable shaft with a turbine wheel, a bearing member comprising a bearing, a bearing housing comprising a sealing bush portion for providing a first sealing device axially between the turbine wheel and the bearing member; an oil cooling chamber for cooling an inner face of the bearing housing, an oil channel for providing oil into the oil cooling chamber, an oil drainage chamber arranged axially between the bearing member and the sealing bush portion and an oil barrier wall surrounding, in at least a vertically top circumferential segment, a radially outer side of the oil drainage chamber for covering the oil drainage chamber from the oil cooling chamber.

Oil-cooled exhaust turbine apparatus

A shaft bearing assembly having a shaft supported in a bearing housing is described. The shaft bearing assembly includes a pressure reduction device for generating an underpressure inside the bearing housing. The pressure reduction device is operated by employing an incompressible fluid. Further, a method of reducing a pressure inside a bearing housing supporting a shaft is described. The method includes using an incompressible fluid for operating a pressure reduction device for generating an underpressure inside the bearing housing.

Shaft bearing assembly having a pressure reduction device and method of reducing a pressure inside a bearing housing supporting a shaft

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Baden, Switzerland

Moritz Mosdzien