• 专利附录
  • 专利说明
  • 权利要求
  • 类似技术
  • 同族专利
  • 引用文献
  • 法律状态
  • 优先权
    • 专利摘要:
    Cladding (1) of a turbocharger, which surrounds a housing to be verschalendes as a turbine housing and / or a compressor housing and / or a bearing housing of the turbocharger, at least in sections, with axial Verschalungssegmenten (3), which connect axially outside to the housing to be boarded, and with radial Verschalungssegmenten (4, 5), which connect radially outside to the housing to be boarded. Slot-like material recesses (6) are introduced into the radial shuttering segments (4, 5), with two adjacent slot-like material recesses (6) delimiting in each case one lug (7) of the respective radial shuttering segment (4, 5). The radial Verschalungssegmente (4, 5) are connected in the region of the respective tab (7) exclusively with the housing to be boarded. The radial Verschalungssegmente (4, 5) are outside the respective tab (7) exclusively connected to the axial Verschalungssegmenten (3).
    公开号:CH714607A2
    申请号:CH00009/19
    申请日:2019-01-07
    公开日:2019-07-31
    发明作者:Weisbrod Tobias；Uhlenbrock Santiago；Braun Steffen；Spatz Urban；Schmidt Heiko
    申请人:Man Energy Solutions Se；
    IPC主号:
    专利说明:

    Description: The invention relates to a casing of a turbocharger, a connecting element and a turbocharger.
    The basic structure of a turbocharger is known to those skilled in the art. A turbocharger has a turbine in which a first medium is expanded. Furthermore, a turbocharger has a compressor in which a second medium is compressed, using the energy obtained in the turbine when the first medium is expanded. The turbine of the turbocharger has a turbine housing and a turbine rotor. The turbocharger's compressor has a compressor housing and a compressor rotor. A bearing housing is positioned between the turbine housing of the turbine and the compressor housing of the compressor, the bearing housing being connected on the one hand to the turbine housing and on the other hand to the compressor housing. A shaft is mounted in the bearing housing, via which the turbine rotor is coupled to the compressor rotor.
    In the operation of a turbocharger, there is a risk that a rotor, for example the turbine rotor or the compressor rotor, of the turbocharger breaks and fragments of the rotor break through the corresponding housing, that is to say the turbine housing or the compressor housing. There is then a risk that the fragments of the turbocharger get into the environment. In order to take account of this problem of the bursting of a rotor of the turbocharger, the respective housing in turbochargers known from practice is designed such that a damage to the respective housing is not to be expected and even if the respective rotor breaks, fragments thereof do not penetrate the respective housing can. However, this increases the weight of the turbocharger.
    In order not to unnecessarily increase the weight of the turbocharger and also to protect turbochargers already used in the field from breakdown of fragments of a rotor into the environment, it is already known in practice to equip a turbocharger with a casing which surrounds a turbine housing and / or a compressor housing and / or a bearing housing of the turbocharger radially on the outside and axially on the outside at least in sections.
    Such formwork is not only used to provide burst protection. Such formwork can also be used for the thermal insulation of assemblies of the turbocharger.
    Known from practice formwork for turbochargers have axial formwork elements and radial formwork elements. Axial formwork elements connect axially on the outside to the side of the turbocharger housing to be formworked. Radial shuttering elements adjoin the housing to be shuttered radially on the outside and essentially extend between the axial shuttering segments.
    The casing of a turbocharger is connected to a casing of the turbocharger to be clad by screw connections. During operation, the turbocharger and thus also the casing of the turbocharger to be clad is exposed to high temperature loads, namely cyclical thermal loads. This can lead to screwed connections failing between the casing and the turbocharger housing to be casing. This affects the function of the formwork.
    Proceeding from this, the invention has for its object to provide a novel formwork of a turbocharger, a connecting element and a turbocharger with such a formwork.
    This object is achieved by a casing of a turbocharger according to claim 1.
    According to the invention, slot-like material recesses are introduced into the radial shuttering segments of the shuttering, two adjacent slot-like material recesses each delimiting a tab of the respective radial shuttering segment. The radial shuttering segments of the shuttering are exclusively connected to the housing to be shuttered in the area of the respective tab. The radial formwork segments of the formwork are connected exclusively to the axial formwork segments of the formwork outside of the respective tab adjacent to the same.
    Cyclic thermal loads which act on the casing via the casing of the turbine to be casing can be reduced via the tabs which are introduced into the radial casing elements of the casing. This makes it possible to drastically reduce the forces acting on the formwork. This reduces the risk that connections of the casing with the casing of the turbocharger to be casing fail. The function of the formwork can be maintained longer.
    Preferably, the radial formwork segments of the formwork have a first section extending between the axial formwork segments of the formwork and a second section extending adjacent to an axial formwork segment, the slot-like material recesses extending from the second section into the first section , This allows a particularly advantageous reduction in the cyclic thermal load which acts on the casing starting from the casing to be casing.
    Preferably, first fastening means, via which the radial shuttering segments of the shuttering in the area of the respective tab are connected to the housing to be shuttered, extend through the second section of the respective radial shuttering segment. In the projection of the first fastening means, the respective axial formwork segment of the formwork has a material recess that is open radially on the outside. Second
    CH 714 607 A2
    Fastening means, by means of which the radial formwork segments of the formwork are connected to the respective axial formwork segments of the formwork outside the respective tab, likewise extend through the second section of the respective radial formwork segment. In this way, the cyclic thermal load acting on the formwork can be reduced particularly advantageously.
    [0014] The slot-like material cutouts, which delimit the tabs, preferably have an expansion in the region of the first section of the respective radial shuttering segment. The widening of such slot-like material cutouts, which each delimit a tab, face away from one another. Notch stresses in the area of the tabs can be reduced via the widening. This can further reduce the cyclic thermal load on the formwork acting on the formwork and further increase the lifespan of the formwork.
    The connecting element according to the invention is defined in claim 9.
    [0016] The turbocharger according to the invention is defined in claim 10.
    Preferred further developments of the invention result from the dependent claims and the following description. Exemplary embodiments of the invention are explained in more detail with reference to the drawing, without being restricted to this. It shows:
    1 shows a perspective section of a casing according to the invention for a turbocharger,
    FIG. 2 shows a cross section through the detail from FIG. 1;
    Fig. 3 shows a detail of the detail of Fig. 1 in a perspective view.
    The invention relates to a casing of a turbocharger and a turbocharger with a casing.
    The basic structure of a turbocharger is familiar to the expert addressed here. A turbocharger thus comprises a turbine for expanding a first medium, in particular for expanding exhaust gas, and a compressor for compressing a second medium, in particular for compressing charge air, using the energy obtained in the turbine when expanding the first medium.
    [0020] The turbine has a turbine rotor and a turbine housing. The compressor has a compressor rotor and a compressor housing. The turbine rotor and the compressor rotor are coupled via a shaft which is mounted in a bearing housing of the turbocharger, the bearing housing being connected to both the turbine housing and the compressor housing.
    If, for example, the turbine rotor or the compressor rotor breaks during operation, fragments of the same can break through the respective housing, that is to say the turbine housing or the compressor housing, and get into the environment. This must be avoided, for which it is known to equip a turbocharger with a casing which surrounds the turbine housing and / or the compressor housing and / or the bearing housing of the turbocharger.
    Preferably, in the area of the turbine housing and the compressor housing, a separate casing is used, which surrounds the respective casing of the turbocharger to be clad radially on the outside and axially on the outside at least in sections.
    Such formwork not only serves to provide a burst protection to increase containment security, but such a formwork can also be used for thermal insulation of the housing to be shuttered.
    1, 2 and 3 each show views of different sections of a casing 1 of a turbocharger. The casing 1 shown in FIGS. 1, 2 and 3 is in particular the casing of a turbine inflow housing, not shown, of the turbocharger. The casing 1 can also be the casing of a compressor housing of the turbocharger.
    The formwork 1 has axial formwork segments 2, 3. An axial formwork segment 2, 3 is preferably positioned on each axial side of the housing to be formulated, which connects axially on the outside to the respective housing to be formulated and the respective housing to be formulated covers at least partially on the corresponding axial side.
    The formwork 1 also has radial formwork segments 4, 5. The radial formwork segments 4, 5 connect radially outside to the respective casing of the turbocharger to be formwork and, viewed in the axial direction, essentially extend between the axial formwork segments 2, third
    In the preferred exemplary embodiment shown, the radial formwork segments 4, 5 each have a first section 4a, 5a extending between the axial formwork segments 2, 3 and an angled relative to this first section 4a, 5a, adjacent to one of the axial formwork segments 2 , 3 extending, second section 4b, 5b.
    CH 714 607 A2 The second section 4b of the radial formwork segment 4 extends essentially parallel to the axial formwork segment 2. The second section 5b of the radial formwork segment 5 extends essentially parallel to the axial formwork segment 3.
    The first sections 4a, 5a of the two radial shuttering segments 4, 5 extend at a radial distance substantially parallel to one another, in the exemplary embodiment shown the first section 4a of the radial shuttering segment 4 running radially outside from the first section 5a of the radial shuttering segment 5. Spacers are preferably arranged between the first sections 4a, 5a of the two radial shuttering segments 4, 5.
    Slot-like material cutouts 6 are introduced into the radial shuttering segments 4, 5. In the exemplary embodiment shown, the slot-like material recesses 6 extend from the respective second section 4b, 5b of the respective radial shuttering segment 4, 5 into the first section 4a, 5a of the respective radial shuttering element 4, 5, with two adjacent slot-like material recesses 6 each one Limit tab 7 of the respective radial shuttering segment 4, 5.
    The radial shuttering segments 4, 5 are connected in the area of the respective tab 7 exclusively to the housing to be shuttered, namely via first fastening means 8, which extend through the second section 4b, 5b of the respective radial shuttering segment 4, 5 in the area of the respective Extend tab 7 through.
    The radial formwork segments 4, 5 are connected outside the respective tab 7 adjacent to the same exclusively with the respective adjacent axial formwork segment 2, 3, namely via second fastening elements (not shown).
    The second fastening elements (not shown) likewise extend through the second sections 4b, 5b of the respective radial formwork segment 4, 5, namely into the respective axial formwork segment 2, 3 and outside of the respective tab 7.
    1 and 3, recesses 9 for these second fastening means are shown, by means of which the radial formwork segments 4, 5 are connected outside the area of the tabs 7 to a respective axial formwork segment 2, 3.
    As can be seen in FIG. 3, the respective axial formwork segment 2, 3 in the axial projection of the first fastening means 8 has a material recess 10 which is open radially on the outside. As a result, the respective tab 7 of the respective radial formwork segment 3, 4 can move independently of the adjacent, respective axial formwork segment 2, 3.
    1 and 3, the slot-like material cutouts 6, which delimit the tabs 7, have in the area of the first section 4a, 5a of the respective radial shuttering segment 4, 5, namely at the end of the respective slot-like material cutout 6, a curved or round expansion 6a of the material recess 6, so that the slot-like material recesses 6 have a golf club-like contour. The widenings 6a of such slot-like material cutouts 6, which together each delimit a tab 7, are preferably facing away from one another.
    Via the tabs 7 of the radial shuttering segments 4, 5, which can also be referred to as thermal tabs, it is possible to reduce forces which are introduced into the shuttering 1 due to a cyclically thermal load on the housing to be shuttered.
    As a result, screw connections of the casing 1 are exposed to a lower load, as a result of which the risk that the casing 1 fails can be reduced.
    The notch tension in the tabs 7 can be reduced via the widenings 6a of the material cutouts 6, as a result of which the service life can be increased still further.
    The first sections 4a, 5a of the radial shuttering segments 4, 5 can be connected outside the tabs 7 via further fastening elements 12 which extend through recesses 11 in the first sections 4a, 5a of the radial shuttering segments 4, 5.
    [0041] The invention is preferably used for formwork which serves to provide burst protection or containment protection. However, the invention is not limited to this application. It can also be used for formwork that serves as thermal insulation.
    Reference symbol list [0042]
    Formwork axial formwork segment axial formwork segment
    CH 714 607 A2 radial formwork segment
    4a first section
    4b second section of radial shuttering segment
    5a first section
    5b second section
    material cut
    6a expansion
    flap
    fastener
    recess
    material cut
    recess
    fastener
    权利要求:
    Claims (10)
    [1]
    claims
    1. Formwork (1) of a turbocharger, which at least in sections surrounds a housing to be formwork-like a turbine housing and / or a compressor housing and / or a bearing housing of the turbocharger, with axial formwork segments (2, 3), which are axially outward to the formwork to be formulated Connect the housing with radial shuttering segments (4, 5), which adjoin the outside of the housing to be shuttered, characterized in that slot-like material recesses (6) are made in the radial shuttering segments (4, 5), two adjacent slot-like material recesses each (6) each delimit a tab (7) of the respective radial shuttering segment (4, 5), the radial shuttering segments (4, 5) in the area of the respective tab (7) are exclusively connected to the housing to be shuttered, the radial shuttering segments (4 , 5) outside the respective bracket (7) exclusively with the axial shuttering segments ( 2, 3) are connected.
    [2]
    2. Formwork according to claim 1, characterized in that the radial formwork segments (4, 5) a first section (4a, 5a) extending between the axial formwork segments (2, 3) and one adjacent to an axial formwork segment (2, 3rd ) have a second section (4b, 5b), the slot-like material cutouts (6) extending from the second section (4b, 5b) into the first section (4a, 5a) of the respective radial shuttering segment (4, 5).
    [3]
    3. Formwork according to claim 2, characterized in that first fastening means (8), via which the radial formwork segments (4, 5) in the area of the respective tab (7) are connected to the housing to be formworked, by the second section (4b , 5b) of the respective radial shuttering segment (4, 5).
    [4]
    4. Formwork according to claim 2 or 3, characterized in that second fastening means, via which the radial formwork segments (4, 5) outside the respective tab (7) with the respective axial formwork segment (2, 3) are connected by the second Extend section (4b, 5b) of the respective radial shuttering segment (4, 5).
    [5]
    5. Formwork according to one of claims 2 to 4, characterized in that the respective axial formwork segment (2, 3) in the projection of the first fastening means (8) has a radially outwardly open material recess (10).
    [6]
    6. Formwork according to one of claims 2 to 5, characterized in that the slot-like material recesses (6) which delimit the tabs (7) in the region of the first section (4a, 5a) of the respective radial formwork segment (4, 5) Have widening (6a).
    CH 714 607 A2
    [7]
    7. Formwork according to claim 6, characterized in that the widening (6a) is formed at the end of the respective slot-like material recess (6) in the region of the first section (4a, 5a) of the respective radial formwork segment (4, 5).
    [8]
    8. Formwork according to claim 6 or 7, characterized in that the widenings (6a) of such slot-like material cutouts (6), each of which delimit a tab (7), face away from one another.
    [9]
    9. Connecting element for a casing (1) according to one of claims 1 to 8, characterized in that the connecting element slot-like material recesses (6) are introduced, with two adjacent slot-like material recesses (6) each delimiting a tab (7) and the separate Connection element in the area of the respective tab (7) is connected exclusively to the housing to be clad.
    [10]
    10. turbocharger, with a turbine for expanding a first medium, with a compressor for compressing a second medium using energy obtained in the turbine when expanding the first medium, a turbine housing of the turbine and a compressor housing of the compressor each having one between the same arranged bearing housing are connected, with a turbine casing and / or the compressor housing and / or the bearing housing radially outside and axially outside at least partially surrounding casing (1), characterized in that the casing (1) is designed according to one of claims 1 to 8 ,
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    同族专利:
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    DE102018105827A1|2018-03-14|2019-09-19|Man Energy Solutions Se|Formwork of a turbocharger and turbocharger|DE102018105827A1|2018-03-14|2019-09-19|Man Energy Solutions Se|Formwork of a turbocharger and turbocharger|
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    法律状态:
    优先权:
    申请号 | 申请日 | 专利标题
    DE102018100937.2A|DE102018100937A1|2018-01-17|2018-01-17|Formwork of a turbocharger and turbocharger|
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