• 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:
    The modular turbocharger shaft (4) comprises a tubular bearing portion (5) having a first axial end portion and a second axial end portion; a wheel part (6) arranged at the first axial end portion of the tubular bearing portion (5); and a driving portion (7) arranged at the second axial end portion of the tubular bearing portion (5). The tubular bearing part (5) is made of a hard material, and the wheel part (6) and / or the driving part (7) is / are made of a relatively soft material with respect to the material hard of the tubular bearing portion (5). The wheel part (6) and / or the driving part (7) extends / extends at least partially in the tubular bearing part (5) and is / are firmly connected to the part of tubular bearing (5). The tubular bearing part (5), the wheel part (6) and the driving part (7) are configured so that the radial deformations occurring during the assembly of the wheel part (6) and or from the driving part (7) to the tubular bearing part (5), are essentially limited to the driving part (7) and / or to the wheel part (6).
    公开号:FR3055677A1
    申请号:FR1658169
    申请日:2016-09-02
    公开日:2018-03-09
    发明作者:Yves Rosson；Patrice Bonnefoi
    申请人:Danfoss Silicon Power GmbH；
    IPC主号:
    专利说明:

    ® FRENCH REPUBLIC
    NATIONAL INSTITUTE OF INDUSTRIAL PROPERTY © Publication number: 3,055,677 (to be used only for reproduction orders) (© National registration number: 16 58169
    COURBEVOIE © Int Cl 8 : F 04 D 25/06 (2017.01), F 04 D 29/056
    A1 PATENT APPLICATION
    ©) Date of filing: 02.09.16. © Applicant (s): DANFOSS SILICON POWER GMBH (© Priority: - OF. @ Inventor (s): ROSSON YVES and BONNEFOI PATRICE. (43) Date of public availability of the request: 09.03.18 Bulletin 18/10. ©) List of documents cited in the report preliminary research: Refer to end of present booklet (© References to other national documents ® Holder (s): DANFOSS SILICON POWER GMBH. related: ©) Extension request (s): © Agent (s): CABINET GERMAIN & MAUREAU.
    P4) MODULAR TURBOCHARGER SHAFT.
    FR 3 055 677 - A1 (gr) The modular turbocharger shaft (4) comprises a tubular bearing part (5) having a first axial end part and a second axial end part; a wheel part (6) arranged at the first axial end part of the tubular bearing part (5); and a drive part (7) arranged at the second axial end part of the tubular bearing part (5). The tubular bearing part (5) is made of a hard material, and the impeller part (6) and / or the drive part (7) is / are made of a material that is relatively flexible compared to the material hard of the tubular bearing part (5). The impeller part (6) and / or the drive part (7) extends / extend at least partially in the tubular bearing part (5) and is / are firmly connected to the part of tubular bearing (5). The tubular bearing part (5), the impeller part (6) and the drive part (7) are configured so that the radial deformations, occurring during assembly of the impeller part (6) and / or from the drive part (7) to the tubular bearing part (5), are essentially limited to the drive part (7) and / or to the impeller part (6).

    Field of the invention
    The present invention relates to a rotor shaft for a turbocharger, and in particular for a high speed turbocharger.
    Background of the invention
    Document US4063850 discloses a gas turbine engine with a turbocharger comprising in particular:
    - a turbocharger shaft, also called a rotor shaft, comprising:
    - a tubular bearing part having a first axial end part and a second axial end part opposite to the first axial end part,
    a part of the impeller arranged at the level of the first part of the axial end of the part of the tubular bearing, and
    - a drive part arranged at the level of the second axial end part of the tubular bearing part,
    - at least one compression stage configured to compress a refrigerant, the at least one compression stage comprising at least one impeller connected to the impeller part of the turbocharger shaft,
    a radial bearing arrangement configured to support in rotation the tubular bearing part, and
    - an axial bearing arrangement configured to limit axial movement of the turbocharger shaft during operation.
    According to document US4063850, the tubular bearing part and the drive part are formed in one piece, and are connected to the impeller part by an annular fusion junction.
    Although such a turbocharger shaft is less expensive to manufacture compared to monolithic turbocharger shafts, the manufacture of such a turbocharger shaft is still expensive and takes time due to the hard material used to manufacture the drive part. . Indeed, such a hard material is difficult to machine, because of its high surface hardness.
    In addition, the disclosed fusion junction configuration of the connection between the tubular bearing part and the impeller part can lead to a rupture of said connection and can therefore affect the reliability of such a turbocharger shaft, in particular when the turbocharger shaft is driven at very high speeds. These fusion junctions can also be expensive to manufacture, due to the addition of special materials and necessary precise control of temperature profiles during the joining process.
    Summary of the invention
    It is an object of the present invention to provide an improved turbocharger shaft which can overcome the disadvantages encountered in conventional turbocharger shafts.
    Another object of the present invention is to provide a modular turbocharger shaft which is reliable, and easier and less expensive to manufacture.
    According to the invention, such a modular turbocharger shaft comprises:
    - a tubular bearing part having a first axial end part and a second axial end part opposite to the first axial end part,
    a part of the impeller arranged at the level of the first part of the axial end of the part of the tubular bearing, and
    - a drive part arranged at the second axial end part of the tubular bearing part, in which the tubular bearing part is made of a hard material, and the impeller part and / or the part of drive is / are made of a relatively flexible material compared to the hard material of the tubular bearing part, in which the impeller part and / or the drive part extends / extend at least partially in the tubular bearing part and is / are firmly connected to the tubular bearing part, and in which the tubular bearing part, the impeller part and the drive part are configured so that the radial deformations, When assembling the impeller part and / or the drive part to the tubular bearing part, are essentially limited to the drive part and / or the impeller part.
    Such a configuration of the modular turbocharger shaft reduces the machining costs, since only the tubular bearing part, which has to meet low tolerances and increased wear resistance, is made of a hard material. The other shaft parts made of more flexible (and less rigid) materials are easier to machine, and absorb the major part of the radial deformations, which occur during the assembly process (for example heat shrinkage) of the modular turbocharger shaft. Thus, the tolerances of the external surfaces of the impeller part and / or of the drive part can be increased without risk of excessive stress on the tubular bearing part.
    In addition, the softer shaft parts absorb deformations occurring during compressor operation, caused by different coefficients of thermal expansion of hard and flexible materials.
    Therefore, the deformations of the tubular bearing part occurring during the assembly of the modular turbocharger shaft and occurring during operation are limited. This results in an improvement in the reliability of the axial and radial bearings supporting the modular turbocharger shaft, in particular when gas bearings are used as they require a very small play to be stable while requiring sufficient play to avoid a bearing seizure.
    Therefore, the modular turbocharger shaft according to the present invention is more reliable, lighter and easier and less expensive to manufacture than conventional turbocharger shafts.
    The turbocharger shaft may also have one or more of the following characteristics, taken alone or in combination.
    According to one embodiment of the invention, the impeller part and the drive part extend at least partially in the tubular bearing part and are firmly connected to the tubular bearing part, the tubular bearing part, the impeller part and the driving part being configured so that the radial deformations, occurring during the assembly of the impeller part and the driving part to the tubular bearing part, are essentially limited to the part drive and spinning part.
    According to one embodiment of the invention, the impeller part and / or the drive part is / are connected to the tubular bearing part by pressure adjustment or by contraction adjustment, the tubular bearing part , the impeller part and the drive part being configured so that the radial deformations, occurring during assembly by adjustment by contraction or by pressure adjustment of the impeller part and / or the drive part to the tubular bearing part, are essentially limited to the drive part and / or to the impeller part.
    According to one embodiment of the invention, the impeller part and / or the drive part is / are connected to the tubular bearing part by heat shrinking adjustment.
    According to one embodiment of the invention, the impeller part and / or the drive part is / are radially deformable during the assembly of the impeller part and / or the drive part to the tubular bearing part.
    According to one embodiment of the invention, the ratio between the Vickers hardness of the hard material of the tubular bearing part and the Vickers hardness of the relatively flexible material of the impeller part is greater than 3.
    According to one embodiment of the invention, the ratio between the Vickers hardness of the hard material of the tubular bearing part and the Vickers hardness of the relatively flexible material of the drive part is greater than 3.
    According to one embodiment of the invention, the tubular bearing part comprises:
    - a tubular cylindrical part having an external surface configured to cooperate with a radial bearing arrangement of a turbocharger, and
    a part in the form of a flat disc having an external diameter greater than the external diameter of the tubular cylindrical part, the part in the form of a flat disc having a first axial end face and a second axial end face opposite the first axial end face, the first and second axial end faces being configured to cooperate with an axial bearing arrangement.
    According to one embodiment of the invention, the drive part is firmly connected to the tubular cylindrical part.
    According to an embodiment of the invention, the impeller part is firmly connected to the tubular cylindrical part and to the part in the form of a flat disc.
    According to an embodiment of the invention, the flat disc-shaped part has a central opening having a diameter corresponding essentially to the internal diameter of the tubular cylindrical part.
    According to an embodiment of the invention, the tubular cylindrical part and the flat disc-shaped part are formed in one piece or as two separate parts.
    According to an embodiment of the invention, the tubular bearing part is made of a high-resistance material having a high surface hardness.
    According to one embodiment of the invention, the tubular bearing part is made of tungsten carbide or of ceramic materials.
    According to one embodiment of the invention, the hard material of the tubular bearing part has a Vickers hardness greater than 1500HV.
    According to an embodiment of the invention, the relatively flexible material of the impeller part has a Vickers hardness less than 500HV.
    According to an embodiment of the invention, the impeller part is made of titanium alloys or aluminum alloys.
    According to one embodiment of the invention, the drive part comprises:
    - a mounting part arranged inside the tubular bearing part, and
    - a rotor fixing part for fixing a rotor of the turbocharger.
    According to an embodiment of the invention, the mounting part of the drive part is arranged inside the tubular cylindrical part.
    According to one embodiment of the invention, the mounting part of the drive part is arranged inside the tubular bearing part by adjustment by contraction or by adjustment by pressure.
    According to an embodiment of the invention, the mounting part of the drive part has a cylindrical external surface.
    According to one embodiment of the invention, the rotor fixing part comprises an axial bore extending over at least part of the length of the rotor fixing part, the axial bore being configured to receive the rotor.
    According to an embodiment of the invention, the rotor can comprise permanent magnets and can be adjusted firmly, for example adjusted by pressure or adjusted by contraction, in the axial bore of the rotor fixing part.
    According to one embodiment of the invention, the rotor fixing part is tubular.
    According to an embodiment of the invention, the mounting part of the driving part has an axial hole extending over at least part of the length of the mounting part of the driving part. Such a configuration of the drive part reduces the weight of the latter, and therefore of the turbocharger shaft.
    According to one embodiment of the invention, the axial hole provided on the drive part extends at least partially in the tubular bearing part. Such a configuration of the drive part increases the flexibility of the mounting part of the drive part, and thus makes it possible to further limit the radial deformations of the tubular bearing part occurring during assembly of the shaft. turbocharger.
    According to one embodiment of the invention, the drive part is made of a titanium alloy or another non-magnetic material.
    According to one embodiment of the invention, the relatively flexible material of the drive part has a Vickers hardness less than 500HV.
    According to one embodiment of the invention, the impeller part comprises:
    - a mounting part arranged at least partially inside the tubular bearing part, and
    - a spinning wheel fixing part for fixing at least one spinning wheel.
    According to one embodiment of the invention, the mounting part of the impeller part is arranged at least partially inside the tubular cylindrical part.
    According to an embodiment of the invention, the mounting part of the impeller part is connected to the tubular bearing part by adjustment by contraction or by adjustment by pressure.
    According to an embodiment of the invention, the mounting part of the impeller part has an essentially cylindrical external surface.
    According to one embodiment of the invention, the mounting part of the impeller part has an axial hole extending over at least part of the length of said mounting part. Such a configuration of the impeller part reduces the weight of the latter, and therefore of the turbocharger shaft.
    According to one embodiment of the invention, the axial hole provided on the impeller part extends at least partially in the tubular bearing part. Such a configuration of the impeller part increases the flexibility of the mounting part of the impeller part, and therefore makes it possible to further limit the radial deformations of the tubular bearing part occurring during the assembly of the turbocharger shaft. .
    According to one embodiment of the invention, the part in the form of a flat disc is connected to the mounting part of the impeller part, and is arranged around said mounting part.
    According to an embodiment of the invention, the flat disc-shaped part is adjacent to an axial end of the tubular cylindrical part.
    According to one embodiment of the invention, the part in the form of a flat disc extends radially outwards relative to the mounting part of the impeller part.
    According to an embodiment of the invention, the tubular bearing part, the impeller part and the drive part extend along the same longitudinal axis.
    According to one embodiment of the invention, the turbocharger shaft is configured to be supported axially and radially by gas bearing arrangements formed at the external surfaces of the tubular bearing part.
    The present invention also relates to a centrifugal turbocharger comprising a modular turbocharger shaft according to the present invention.
    According to one embodiment of the invention, the centrifugal turbocharger further comprises:
    - at least one compression stage configured to compress a refrigerant, the at least one compression stage comprising at least one impeller connected to the impeller part of the turbocharger shaft,
    - an electric motor configured to drive the turbocharger shaft in rotation about an axis of rotation, the electric motor comprising a stator and a rotor, the rotor being connected to the drive part of the pressurized shaft r.
    According to an embodiment of the invention, the centrifugal turbocharger further comprises a radial bearing arrangement configured to support in rotation the tubular bearing part.
    According to one embodiment of the invention, the radial bearing arrangement is a gas bearing arrangement.
    8
    According to one embodiment of the invention, the radial bearing arrangement is configured to cooperate with an external surface of the tubular cylindrical part.
    According to an embodiment of the invention, the radial bearing arrangement comprises a radial bearing extending over at least part of the length of the tubular cylindrical part.
    According to one embodiment of the invention, the centrifugal turbocharger further includes an thrust bearing arrangement configured to limit axial movement of the turbocharger shaft during operation.
    According to an embodiment of the invention, the thrust bearing arrangement is located between the electric motor and the first compression stage.
    According to an embodiment of the invention, the thrust bearing arrangement is configured to cooperate with the first and second faces of axial ends of the part in the form of a flat disc.
    According to an embodiment of the invention, the thrust bearing arrangement is a gas bearing arrangement.
    According to one embodiment of the invention, the thrust bearing arrangement comprises a first annular thrust bearing element having a first thrust bearing surface, and a second annular thrust bearing element having a second bearing surface thrust, the first and second thrust bearing surfaces being configured to cooperate respectively with the first and second faces of axial ends of the part in the form of a flat disc.
    These advantages, as well as others, will appear on reading the following description taking into account the attached drawing which represents, by way of a nonlimiting example, an embodiment of a turbocharger shaft according to the invention .
    Brief description of the drawings
    The following detailed description of an embodiment of the invention is better understood when read in conjunction with the accompanying drawings, it being understood, however, that the invention is not limited to the specific embodiment disclosed.
    Figure 1 is a longitudinal sectional view of a centrifugal turbocharger having a turbocharger shaft according to the invention.
    Figure 2 is a longitudinal sectional view of the turbocharger shaft of Figure 1.
    Figure 3 is an exploded perspective view of the turbocharger shaft of Figure 1.
    Detailed description of the invention
    FIG. 1 represents a centrifugal turbocharger 2, and in particular a two-stage centrifugal turbocharger. The centrifugal turbocharger 2 comprises a hermetic housing 3, and a turbocharger shaft 4 arranged in rotation in the hermetic housing 3 and extending along a longitudinal axis A.
    As best shown in Figures 2 and 3, the turbocharger shaft 4 has a tubular bearing part 5, a impeller part 6 arranged at a first axial end part 5a of the tubular bearing part 5, and a drive part 7 arranged at a second axial end part 5b of the tubular bearing part 5. The
    0 impeller part 6 and the driving part 7 extend partially in the tubular bearing part 5 and are firmly connected to the tubular bearing part 5, by pressure adjustment or by contraction adjustment. In particular, the tubular bearing part 5, the impeller part 6 and the drive part 7 are defined so that the radial deformations, occurring during assembly by adjustment by contraction or by pressure adjustment of the part impeller 6 and the drive part 7 to the tubular bearing part 5, are essentially limited to the drive part 7 and to the impeller part 6.
    The tubular bearing part 5 comprises a tubular cylindrical part 8 having an external surface 9 configured to cooperate with a radial bearing arrangement configured to support in rotation and radially the turbocharger shaft 4.
    According to the embodiment shown in the figures, the radial bearing arrangement comprises at least one radial bearing 11, such as a radial sleeve bearing, located in the hermetic housing 3 and having an internal surface 12 configured to cooperate with the external surface 9 of the cylindrical ίο · tubular part 8. The or each radial bearing 11 may be a fluid radial bearing, and for example a gas radial bearing. According to the embodiment shown in the figures, the radial bearing arrangement comprises a plurality of radial bearings 11, for example two, distributed over the entire axial length of the tubular cylindrical part 8. However, the radial bearing arrangement can have only one radia bearing! 11 extending along the tubular cylindrical part 8.
    The tubular bearing part 5 further comprises a flat disc-shaped part 13 which extends coaxially with the tubular cylindrical part 8. The flat disc-shaped part 13 has an external diameter greater than the external diameter of the tubular cylindrical part 8, and comprises a first axial end face 13a and a second axial end face 13b opposite the first axial end face 13a. The first and second axial end faces 13a, 13b are configured to cooperate with an axial bearing arrangement, also called thrust bearing arrangement, configured to limit an axial movement of the turbocharger shaft 4 during operation. According to the embodiment shown in the figures, the axial bearing arrangement comprises a first annular thrust bearing element 14 and a second annular thrust bearing element 15 located in the sealed housing 3. The first thrust bearing element ring 14 has a first thrust bearing surface 16 configured to cooperate with the first axial end face 13a of the flat disc-like part 13, and the second annular thrust bearing element 15 has a second bearing surface stop 17 configured to cooperate with the second axial end face 13b of the flat disc-shaped part 13.
    According to the embodiment shown in the figures, the flat disc-shaped part 13 is adjacent to an axial end of the tubular cylindrical part 8 which is opposite to the drive part 7, and has a central opening 18 having a diameter essentially corresponding to the internal diameter of the tubular cylindrical part 8. In addition, according to the embodiment shown in the figures, the tubular cylindrical part 8 and the flat disc-shaped part 13 are formed as two separate parts. However, according to another embodiment of the invention, the tubular cylindrical part 8 and the flat disc-shaped part 13 can be formed in one piece.
    Advantageously, the tubular bearing part 5 (that is to say the tubular cylindrical part 8 and the flat disc-shaped part 13) is made of a hard material having a Vickers hardness greater than 1500HV. According to one embodiment of the invention, the tubular bearing part 5 is made of a high-strength material having a high surface hardness. For example, the tubular bearing part 5 can be made of tungsten carbide or of ceramic materials. Tungsten carbide is particularly preferred, due to its relatively low coefficient of thermal expansion combined with relatively high thermal conductivity, which is advantageous for controlling clearance in gas bearings and for removing heat during operation of the compressor. Thus, the risk of bearing seizures is further reduced.
    As best shown in Figure 2, the drive portion 7 includes a mounting portion 19 and a tubular rotor attachment portion
    Each extending along the longitudinal axis A of the turbocharger shaft 4. The mounting part 19 is arranged inside the cylindrical tubular part 8 of the tubular bearing part 5, and has a surface cylindrical outer configured to cooperate with the inner surface of the tubular bearing part 5. In addition, the mounting part 19 of the drive part 7 has an axial hole 21 extending over at least part of the length of the mounting part 19 and opening into an end face of the mounting part 19 opposite the rotor fixing part
    20. Advantageously, the axial hole 21 extends in the tubular cylindrical part 8.
    The tubular rotor fixing part 20 has an axial bore 22 opening into an end face of the tubular rotor fixing part 20 opposite the impeller part 6. The axial bore 22 can also lead into the axial hole 21 .
    According to the embodiment shown in the figures, the drive part 7 is in the form of a single piece. However, according to another embodiment of the invention, the mounting part 19 and the tubular rotor fixing part 20 can be formed as two separate parts connected together.
    Advantageously, the drive part 7 is made of a relatively flexible material compared to the hard material of the tubular bearing part
    5. According to one embodiment of the invention, the relatively flexible material '
    of drive part 7 has a Vickers hardness of less than 500HV. For example, the drive part 7 is made of a titanium alloy or another non-magnetic material.
    The impeller part 6 comprises a mounting part 23 and a impeller fixing part 24 each extending along the longitudinal axis A of the turbocharger shaft 4. The mounting part 23 is partially arranged at the inside of the tubular cylindrical part 8, and has an essentially cylindrical external surface and configured to cooperate with the internal surface of the tubular cylindrical part 8. In addition, the mounting part 23 of the impeller part 6 has an axial hole 25 s extending over at least part of the length of the mounting part 23 and opening into an end face of the mounting part 23 opposite the impeller fixing part 24. Advantageously, the axial hole 25 extends partially in the tubular cylindrical part 8.
    It should be noted that the flat disc-shaped part 13 is firmly connected to the mounting part 23 of the impeller part 6 by pressure adjustment or by contraction adjustment, and extends radially outward relative to the mounting part 23 of the impeller part 6.
    According to the embodiment shown in the figures, the impeller part 6 is in the form of a single piece. However, according to another embodiment of the invention, the mounting part 23 and the impeller fixing part 24 can be formed as two separate parts interconnected.
    Advantageously, the impeller part 6 is made of a relatively flexible material compared to the hard material of the tubular bearing part
    5. According to one embodiment of the invention, the relatively flexible material of the impeller part 6 has a Vickers hardness of less than 500HV. For example, the impeller part 6 is made of titanium alloys or aluminum alloys.
    The centrifugal refrigeration compressor 2 further comprises a first compression stage 26 and a second compression stage 27 configured to compress a refrigerant. The first compression stage 26 has a fluid inlet 28 and a fluid outlet 29, while the second compression stage 27 has a fluid inlet 31 and a fluid outlet 32, the fluid outlet 29 of the first compression stage 26 being fluidly connected to the fluid inlet 31 of the second compression stage 27.
    The hermetic housing 3 therefore comprises a low pressure chamber situated upstream of the first compression stage 26, a high pressure chamber situated downstream of the second compression stage 27 and an intermediate pressure chamber provided between the fluid outlet 29 of the first compression stage 26 and the fluid inlet 31 of the second compression stage 27.
    The first and second compression stages 26, 27 respectively comprise a first impeller 33 and a second impeller 34. The first and second impellers 33, 34 are connected to the impeller fixing part 24. According to the embodiment shown in the figures , the first and second impellers 33, 34 are provided on a impeller 35 attached to the impeller attachment portion 24, and are arranged in a back-to-back configuration, so that the directions of fluid flow at the fluid inlet 28, 31 of the first and second compression stages 26, 27 are opposite one another.
    Each of the first and second impellers 33, 34 has a front side provided with a plurality of vanes configured to accelerate, during the rotation of the turbocharger shaft 4, the refrigerant entering the respective stage of the first and second compression stages 26, 27, and for delivering the accelerated refrigerant to a diffuser arranged at the level of the external radial edge of the respective impeller of the first and second impellers 33, 34.
    According to one embodiment of the invention, the centrifugal turbocharger 2 is configured so that part of the refrigerant compressed by the first and second compression stages 26, 27 is used as lubrication fluid in the radial bearing arrangement gas and the thrust bearing arrangement.
    The centrifugal refrigeration compressor 2 further comprises an electric motor 36 configured to rotate the turbocharger shaft 4 around its longitudinal axis A. According to the embodiment shown in the figures, the electric motor 36 is arranged in the lower chamber pressure defined by the hermetic housing 3.
    The electric motor 36 comprises a stator 37 and a rotor 38. Advantageously, the rotor 38 comprises permanent magnets, and is adjusted firmly, for example adjusted by pressure or adjusted by contraction, in the axial bore 22 of the fixing part of rotor 20. According to the embodiment shown in the figures, the thrust bearing arrangement is located between the electric motor 36 and the first compression stage 26.
    The different parts of a rotor shaft according to the invention are optimized with regard to their function, manufacturability and costs:
    The bearing part: Light weight, high strength, low dimensional tolerances and high hardness on the external surface for gas bearings, low coefficient of thermal expansion, good thermal conductivity for heat dissipation,
    The drive part: high resistance to receive a rotor at high speed, non-magnetic, good thermal conductivity for heat dissipation, easy to machine due to larger tolerances, relatively flexible to limit the stress during a connection with the rotor and the bearing part,
    The impeller part: high resistance to receive at least one impeller at high speed, easy to machine due to larger tolerances, relatively flexible to limit the stress when connected with the impeller and the bearing parts.
    Of course, the invention is not limited to the embodiment described above by way of nonlimiting example, but on the contrary it encompasses all of its embodiments.
    权利要求:
    Claims (16)
    [1" id="c-fr-0001]
    1. Modular turbocharger shaft (4) comprising:
    - a tubular bearing part (5) having a first axial end part (5a) and a second axial end part (5b) opposite the first axial end part (5a),
    - a wheel part (6) arranged at the level of the first axial end part (5a) of the tubular bearing part (5), and
    a drive part (7) arranged at the level of the second axial end part (5b) of the tubular bearing part (5), in which the tubular bearing part (5) is made of a hard material, and the impeller part (6) and / or the drive part (7) is / are made of a material which is relatively flexible compared to the hard material of the tubular bearing part (5), characterized in that the impeller part (6) and / or the drive part (7) extends / extend at least partially in the tubular bearing part (5) and is / are firmly connected to the part of tubular bearing (5), and in that the tubular bearing part (5), the impeller part (6) and the drive part (7) are configured so that the radial deformations occurring during the assembly of the impeller part (6) and / or the drive part (7) to the tubular bearing part (5), are essentially limited to the the drive part (7) and / or the impeller part (6).
    [2" id="c-fr-0002]
    2. Modular turbocharger shaft (4) according to claim 1, in which the impeller part (6) and / or the drive part (7) is / are connected to the tubular bearing part (5) by pressure adjustment or by contraction adjustment, the tubular bearing part (5), the impeller part (6) and the drive part (7) being configured so that the radial deformations occurring during the assembly by adjustment by contraction or by pressure adjustment of the impeller part (6) and / or of the drive part (7) to the tubular bearing part (5), are essentially limited to the drive part ( 7) and / or to the impeller part (6).
    [3" id="c-fr-0003]
    3. Modular turbocharger shaft (4) according to claim 1 or 2, wherein;
    the ratio between the Vickers hardness of the hard material of the tubular bearing part (5) and the Vickers hardness of the relatively flexible material of the impeller part (6) is greater than 3, and / or
    - The ratio between the Vickers hardness of the hard material of the tubular bearing part (5) and the Vickers hardness of the relatively flexible material of the drive part (7) is greater than 3.
    [4" id="c-fr-0004]
    4. Modular turbocharger shaft (4) according to any one of claims 1 to 3, in which the tubular bearing part (5) comprises:
    - a tubular cylindrical part (8) having an external surface (9) configured to cooperate with a radial bearing arrangement of a turbocharger (2), and
    - a flat disc-shaped part (13) having an external diameter larger than the external diameter of the tubular cylindrical part (8), the flat disc-shaped part (13) having a first axial end face (13a ) and a second axial end face (13b) opposite the first axial end face (13a), the first and second faces of axial ends (13a, 13b) being configured to cooperate with an axial bearing arrangement.
    [5" id="c-fr-0005]
    5. Modular turbocharger shaft (4) according to claim 4, wherein the flat disc-shaped part (13) has a central opening (18) having a diameter corresponding essentially to the internal diameter of the tubular cylindrical part (8).
    [6" id="c-fr-0006]
    6. Modular turbocharger shaft (4) according to claim 4 or 5, wherein the tubular cylindrical part (8) and the flat disc-shaped part (13) are formed in one piece or as two separate parts.
    [7" id="c-fr-0007]
    7. Modular turbocharger shaft (4) according to any one of claims 1 to 6, in which the hard material of the tubular bearing part (5) has a Vickers hardness greater than 1500HV.
    [8" id="c-fr-0008]
    8. Modular turbocharger shaft (4) according to any one of claims 1 to 7, in which:
    - the relatively flexible material of the impeller part (6) has a Vickers hardness of less than 500HV, and / or
    - the relatively flexible material of the drive part (7) has a Vickers hardness of less than 500HV.
    [9" id="c-fr-0009]
    9. Modular turbocharger shaft (4) according to any one of claims 1 to 8, in which the drive part (7) comprises:
    - a mounting part (19) arranged inside the tubular bearing part (5), and
    - a rotor fixing part (20) for fixing a rotor (38) of the turbocharger.
    [10" id="c-fr-0010]
    10. Modular turbocharger shaft (4) according to claim 9, wherein the rotor fixing part (20) has an axial bore (22) configured to receive the rotor (38).
    [11" id="c-fr-0011]
    11. Modular turbocharger shaft (4) according to claim 9 or 10, wherein the mounting part (19) of the drive part (7) has an axial hole (21) extending over at least part of the length of the mounting part (19) of the drive part (7).
    [12" id="c-fr-0012]
    12. Modular turbocharger shaft (4) according to any one of claims 1 to 11, in which the impeller part (6) comprises:
    - a mounting part (23) arranged at least partially inside the tubular bearing part (5), and
    - a spinning wheel fixing part (24) for fixing at least one spinning wheel.
    [13" id="c-fr-0013]
    13. Modular turbocharger shaft (4) according to claim 12, in which the mounting part (23) of the impeller part (6) has an axial hole (25) extending over at least part of the length of the mounting part (23) of the impeller part (6).
    [14" id="c-fr-0014]
    14. Centrifugal turbocharger (2) comprising a modular turbocharger shaft (4) according to any one of claims 1 to
    13.
    [15" id="c-fr-0015]
    15. Centrifugal turbocharger (2) according to claim 14, further comprising:
    - at least one compression stage (26, 27) configured to compress a refrigerant, the at least one compression stage (26, 27) comprising at least one impeller (33, 34) connected to the impeller part (6 ) the turbocharger shaft (4),
    5 - an electric motor (36) configured to rotate the turbocharger shaft (4) about an axis of rotation, the electric motor (36) comprising a stator (37) and a rotor (38), the rotor (38) being connected to the drive part (7) of the turbocharger shaft (4).
    10
    [0016]
    16. Centrifugal turbocharger (2) according to claim 14 or 15, further comprising:
    a radial bearing arrangement configured to rotatably support the tubular bearing part (5), and
    - a thrust bearing arrangement configured to limit movement
    15 axial of the turbocharger shaft (4) during operation.
    1/1
    类似技术:
    公开号 | 公开日 | 专利标题
    FR3055677A1|2018-03-09|MODULAR TURBOCHARGER SHAFT
    FR3034460B1|2019-07-19|ROTOR AND ROTOR TURBOMACHINE ASSEMBLY AT VERY HIGH SPEEDS INCLUDING SUCH A ROTOR ASSEMBLY
    CA2885650C|2020-09-15|Turbomachine casing and impeller
    FR3055678A1|2018-03-09|AXIAL BEARING ARRANGEMENT FOR A DRIVE SHAFT OF A CENTRIFUGAL COMPRESSOR
    CA2861738C|2019-04-30|Bearing bracket for a turbine engine
    FR3037110B1|2019-11-01|CENTRIFUGAL REFRIGERATING COMPRESSOR
    FR2856440A1|2004-12-24|TURBOMACHINE COMPRESSOR AND COMPRESSOR WHEEL
    FR3038665A1|2017-01-13|
    FR3021693B1|2019-11-01|PLATFORM FOR AUBAGEE WHEEL
    FR2921408A1|2009-03-27|Annular sealing and vibration dampening ring for turbomachine rotor in e.g. automobile field, has square, rectangular or circular shaped section, where ring is made of super-elastic metal material such as shape memory alloy material
    EP2959107A1|2015-12-30|Wheel of a turbine, compressor or pump
    FR3078363A1|2019-08-30|MOBILE SEAL RING
    FR3066552A1|2018-11-23|ASSEMBLY ON A TURBOMACHINE SHAFT OF A MONOBLOCK AUBING DISC AND A LOW PRESSURE COMPRESSOR ROTOR WITH AT LEAST TWO FLOORS OF MOBILE AUBES
    FR3014141A1|2015-06-05|FIXED TURBOMACHINE RECEIVER PART COMPRISING WITHIN A FIXED FIXTURE AN ASSEMBLY INCLUDING SERVITUDES
    FR3082250A1|2019-12-13|Plain bimetallic sleeve bearing with additive manufacturing
    FR3063776A1|2018-09-14|BEARING ARRANGEMENT FOR A DRIVE SHAFT OF A TURBOMACHINE, AND A TURBOMACHINE HAVING SUCH A BEARING ARRANGEMENT
    FR3068741B1|2019-08-23|DRIVE SHAFT FOR A TURBOMACHINE
    FR3055754A1|2018-03-09|ROTOR FOR A HIGH SPEED ELECTRIC MOTOR
    EP2631490B1|2016-12-14|Radial-flow impeller with radially free base ring
    FR3063777A1|2018-09-14|DUAL-STAGE WHEEL ARRANGEMENT FOR A DOUBLE-STAGE CENTRIFUGAL TURBOCHARGER
    FR3025559B1|2019-09-13|ASSEMBLY OF ELEMENTS FOR A TURBOMACHINE
    WO2017137701A1|2017-08-17|System for rotating a fan of a turbojet engine
    FR3063778A1|2018-09-14|CENTRIFUGAL TURBOCHARGER
    FR3042215B1|2019-09-13|STRUCTURE FOR TURBOMACHINE COMPRISING AXIAL RETAINING ROLLS FOR EXTERIOR BEARING BEARING BEARING
    WO2016034804A1|2016-03-10|Rotational assembly provided with a wedging device
    同族专利:
    公开号 | 公开日
    DE112017004422T5|2019-07-25|
    FR3055677B1|2020-05-29|
    CN109790847B|2021-02-05|
    WO2018041938A1|2018-03-08|
    CN109790847A|2019-05-21|
    US10794390B2|2020-10-06|
    US20190249682A1|2019-08-15|
    引用文献:
    公开号 | 申请日 | 公开日 | 申请人 | 专利标题
    WO1998034324A1|1997-01-29|1998-08-06|Turbocorp Limited|Improvements in high speed rotor shafts|
    DE102008056061A1|2008-08-04|2010-02-11|Mtu Friedrichshafen Gmbh|Turbosupercharger for internal-combustion engine, has sleeve provided in radial bearing, and axial-thrust bearing disk frictionally clamped with sleeve through screwing shaft stubs by set of threading parts|
    DE2554353A1|1975-12-03|1977-06-16|Motoren Turbinen Union|GAS TURBINE ENGINE|
    AUPO478297A0|1997-01-24|1997-02-20|Commonwealth Scientific And Industrial Research Organisation|Improvements in high speed electric motors|
    JP2002213385A|2001-01-19|2002-07-31|Ebara Corp|Canned motor and canned motor pump|
    US6866478B2|2002-05-14|2005-03-15|The Board Of Trustees Of The Leland Stanford Junior University|Miniature gas turbine engine with unitary rotor shaft for power generation|
    JP2007092646A|2005-09-29|2007-04-12|Jtekt Corp|Supercharger for fuel cell|
    JP4961485B2|2010-03-30|2012-06-27|本田技研工業株式会社|Dynamic pressure type foil type gas bearing|
    CN102322448B|2011-09-02|2013-02-27|西安交通大学|Cooling structure of motor-driven high-speed centrifugal air compressor|
    US9028220B2|2011-10-24|2015-05-12|Hamilton Sundstrand Corporation|Tie rod|
    FR3034460B1|2015-04-01|2019-07-19|Liebherr-Aerospace Toulouse Sas|ROTOR AND ROTOR TURBOMACHINE ASSEMBLY AT VERY HIGH SPEEDS INCLUDING SUCH A ROTOR ASSEMBLY|
    CN105889096B|2016-05-06|2019-10-18|同济大学|The two-stage series connection pressurization of fuel battery engines is straight to drive centrifugal air compressor|FR3063778A1|2017-03-08|2018-09-14|BD Kompressor GmbH|CENTRIFUGAL TURBOCHARGER|
    FR3085188B1|2018-08-22|2020-12-25|Danfoss As|A TURBOCHARGER PROVIDED WITH AN AXIAL BEARING COOLING SYSTEM|
    FR3101208A1|2019-09-23|2021-03-26|IFP Energies Nouvelles|Hybrid transient magnet rotor|
    法律状态:
    2017-08-24| PLFP| Fee payment|Year of fee payment: 2 |
    2018-03-09| PLSC| Search report ready|Effective date: 20180309 |
    2018-08-23| PLFP| Fee payment|Year of fee payment: 3 |
    2019-08-29| PLFP| Fee payment|Year of fee payment: 4 |
    2019-12-27| TP| Transmission of property|Owner name: DANFOSS A/S, DK Effective date: 20191119 |
    2020-08-26| PLFP| Fee payment|Year of fee payment: 5 |
    2021-08-26| PLFP| Fee payment|Year of fee payment: 6 |
    优先权:
    申请号 | 申请日 | 专利标题
    FR1658169|2016-09-02|
    FR1658169A|FR3055677B1|2016-09-02|2016-09-02|MODULAR TURBOCHARGER SHAFT|FR1658169A| FR3055677B1|2016-09-02|2016-09-02|MODULAR TURBOCHARGER SHAFT|
    CN201780060808.0A| CN109790847B|2016-09-02|2017-08-31|Modular turbo-compressor shaft|
    DE112017004422.7T| DE112017004422T5|2016-09-02|2017-08-31|Modular turbocompressor shaft|
    US16/329,332| US10794390B2|2016-09-02|2017-08-31|Modular turbo compressor shaft|
    PCT/EP2017/071849| WO2018041938A1|2016-09-02|2017-08-31|Modular turbo compressor shaft|
    [返回顶部]