Man Energy Solutions Se

Harald Denkel

Steffen Braun

Bernd Haas

Johannes Niebuhr

Stefan Weihard

Urban Spatz

Daniel Albrecht

Sven Brandt

Claudius Wurm

Tobias Weisbrod

Matthias Glathe

A turbocharger, with a turbine for expanding a first medium, a compressor for compressing a second medium utilising energy extracted in the turbine during expansion of the first medium. A turbine housing and a compressor housing are connected to a bearing housing. A casing radially and axially surrounds the turbine housing, the compressor housing, and/or the bearing housing at least in sections, which is connected to the respective housing via multiple fastening devices. At least some of the fastening devices extend through a wall of the casing into the housing include metallic damping elements made of wire on opposite sides of the wall of the casing through which the same extend.

Turbocharger

A casing of a turbocharger, which surrounds a housing to be encased such as a turbine housing and/or a compressor housing and/or a bearing housing of the turbocharger at least in sections, with axial casing segments, which axially adjoin the housing to be encased, with at least one radial casing segment, which radially adjoins the housing to be encased radially outside, and at least one stiffening element is formed or acts on at least one casing segment.

Casing of a turbocharger and turbocharger

A burst protection device for a gas radial turbo engine configured annularly around a central axis in the circumferential direction and like a box in a cross sectional direction, to grip a turbine housing in the area of the turbine wheel. The burst protection device includes at least one axial wall section extending in an axial direction and at least one radial wall section extending in the radial direction are indirectly interconnected via an intermediate wall section lying in between. A partial area of the intermediate wall section in the axial direction runs inclined and/or curved relative to the orientation of the axial wall section and radial wall section.

Burst protection device for a gas turbo engine

A turbocharger, with a turbine a turbine housing and a turbine rotor, with a compressor with a compressor housing and a compressor rotor that is coupled to the turbine rotor via a shaft, with a bearing housing arranged between the turbine housing and the compressor housing, wherein both the turbine housing and also the compressor housing are connected to the bearing housing, with at least one bearing, via which the shaft is mounted in the bearing housing, wherein the respective bearing comprises a bearing bush arranged in the bearing housing, wherein between the bearing bush and the bearing housing a radially outer lubricating gap and between the bearing bush and the shaft a radially inner lubricating gap are formed, wherein the radially outer lubricating gap and the radially inner lubricating gap are suppliable with lubricating oil emanating from an oil supply main line independently of one another.

A radial compressor (), with a compressor rotor having moving blades and with a compressor housing () accommodating an insert piece () and a diffuser (), in which the insert piece () delimits a flow duct leading to the moving blades of the rotor and the diffuser () a flow duct leading away from the moving blades of the rotor at least in sections, and in which the diffuser () is designed as bladeless diffuser and as an integral part of the insert piece ().

Radial compressor and turbocharger

A turbocharger having a turbine with a turbine rotor, a compressor with a compressor rotor that is coupled to the turbine rotor via a shaft. A bearing housing arranged between the turbine housing and the compressor housing, wherein both the turbine housing and also the compressor housing are connected to the bearing housing, with at least one bearing, via which the shaft is mounted in the bearing housing, wherein the respective bearing includes a bearing bush that is mounted on the bearing housing in a rotationally fixed manner, wherein between the bearing bush and the bearing housing a radially outer lubricating cap and between the bearing bush and the shaft a radially inner lubricating gap is formed, and wherein axial ends of the respective bearing bush, at a radially outer section of the same have a greater axial extent than on a radially inner section of the same.

Growing community of inventors

Baar, Germany

Harald Denkel