Abstract: An exhaust gas turbocharger includes: a compressor wheel; a turbine; and a shaft configured to rotatably interconnect the compressor wheel and the turbine. The shaft is mounted in the turbocharger by a bearing configured to absorb axial forces acting on the shaft. The turbocharger further includes a one-piece thrust ring arranged on the shaft, the one-piece thrust ring indirectly connecting the shaft with the bearing and being configured to transmit the axial forces acting on the shaft both in a thrust direction and in a counter-thrust direction opposite to the thrust direction.

Abstract: 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.

Abstract: 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.

Abstract: A casing which surrounds a housing of the turbocharger has a first casing body, which emanating from a first side of the housing can be pushed onto the housing in an axial direction. The first casing body has an axial casing segment adjoining the housing adjoining the first side axially outside, and multiple casing segments adjoining the housing radially outside. A second casing body can be pushed onto the housing in the axial direction has an axial casing segment adjoining the housing adjoining a second side axially outside, and a radial casing segment, which adjoins the housing radially outside, covers the first casing body radially outside in sections and is connected to the first casing body. Multiple supports each has first sections, via which the respective support can be mounted to the housing. Each support has second sections), via which the first casing body is mounted to the respective support.

Abstract: 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.

Abstract: A turbocharger includes a turbine for expanding a first medium and a compressor for compressing a second medium utilizing energy extracted in the turbine during the expansion of the first medium. A turbine housing of the turbine and a compressor housing of the compressor each are connected to a bearing housing arranged therebetween. A casing: surrounds the turbine housing radially outside and axially outside at least in certain sections, and/or surrounds the compressor housing radially outside and axially outside at least in certain sections. The respective casing is positioned loosely around the turbine housing without direct connection to the turbine housing or loosely around the compressor housing without direct connection to the compressor housing. The respective casing is connected to an assembly which, during the operation of the turbocharger, has a temperature level corresponding to the respective casing.

Abstract: A turbocharger, having a turbine with a turbine housing and a turbine rotor, (a compressor with a compressor housing and 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, in which the shaft is mounted via a bearing. An end disc adjoins the bearing ring or the bearing bush. On an axial surface facing the bearing ring or the bearing bush of the bearing facing the turbine, a swirl chamber that is open in the direction of the bearing ring or the bearing bush is introduced into the end disc, which collects and discharges oil leaking from a lubrication gap of the bearing.

Abstract: A compensation device for two interconnected components arranged for the axial and radial compensation of thermally induced expansions of the two components between the two components and includes a central connecting portion for mechanically connecting to the first component and a plurality of connecting portions for connecting to the second component, which are connected to the central connecting portion in one piece. The connecting portions are at least partly formed offset relative to the connecting portion in an axial direction.

Abstract: 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.

Abstract: A radial compressor (10), with a compressor rotor having moving blades and with a compressor housing (11) accommodating an insert piece (12) and a diffuser (13), in which the insert piece (12) delimits a flow duct leading to the moving blades of the rotor and the diffuser (13) a flow duct leading away from the moving blades of the rotor at least in sections, and in which the diffuser (13) is designed as bladeless diffuser and as an integral part of the insert piece (12).

Abstract: 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.

Abstract: A burst protection device for a gas turbomachine formed of at least one pipe section of a pipe in the form of a bend segment of the pipe section for assembly about a turbine wheel housing and/or compressor housing of the gas turbomachine. The bend segment of the pipe section seen in the circumferential direction of the pipe has an interruption for the gas or air outlet of the turbine wheel housing or compressor housing.

Abstract: A burst protection device for a turbo machine having a rotor housing, which includes an axle and a rotor that is rotatably mounted about the axle in the rotor housing. The burst protection device surrounds the rotor housing at least in the region of the rotor in a circumferential direction of the rotor and is formed in one part of at least one burst protection element. The at least one burst protection element is a material having an elongation at break of at least 30%.

Abstract: A turbocharger, with a turbine and a compressor. A turbine housing of the turbine and a compressor housing of the compressor are connected to a bearing housing arranged between the same. A casing surrounds the turbine housing and/or the compressor housing and/or the bearing housing radially outside and axially outside at least in sections, which are connected to the respective housing to be encased via multiple fastening devices. At least one fastening device forms a fixed bearing-like connection and at least one fastening device a loose bearing-like connection of the casing on the respective housing to be encased.

Abstract: 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.

Abstract: A casing of a turbocharger, surrounding a turbine, compressor, and/or a bearing housing of the turbocharger at least in sections, with axial casing segments that adjoin the housing axially outside, and with radial casing segments that adjoin the housing to be encased radially outside. An additional casing segment encloses or completes the axial casing segments and/or the radial casing segments in the region of an inlet flange or outlet flange of the housing.

Abstract: 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.

Abstract: A turbocharger, with a turbine for expanding a first medium, a compressor for compressing a second medium utilising energy extracted in the turbine during the expansion of the first medium, a turbine housing of the turbine and a compressor housing of the compressor connected to a bearing housing arranged between the same, with a casing that radially and axially surrounds one or more of the turbine housing, the compressor housing, and the bearing housing at least in sections. At least one loose fibre of a defined length is introduced into a hollow space between the casing and a respective housing.

Abstract: 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.

Abstract: A turbine guide apparatus for a radial turbocharger that is assembled in multiple parts from a first annular disc element, a second annular disc element, and a multiplicity of guide blades, which are arranged between the first and second annular disc element. The guide blades are connected to each annular disc element in a firmly bonded, and/or non-positive, and/or positive manner.