• 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 invention relates to a casing for rotating machines, in particular for turbomachines, comprising a chamber (2) for housing a turbine, and a conduit (3) for gas flow opening into said chamber. According to the invention, the casing has at least one recess (4) surrounding at least a portion of the gas circulation duct (3).
    公开号:FR3040733A1
    申请号:FR1558277
    申请日:2015-09-07
    公开日:2017-03-10
    发明作者:Frederic Impellizzeri；Stephane Abed
    申请人:Poly Shape SAS；
    IPC主号:
    专利说明:

    Carter for rotating machines and in particular for turbomachines
    The present invention relates to a casing for rotating machines and in particular for turbomachines. It also relates to machines provided with such a housing and a method of manufacturing the housing. The invention finds applications in the production or the equipment of turbomachines such as turbojets or turbochargers. It can advantageously be used in the manufacture of aircraft thrusters or for the equipment of combustion engines of motor vehicles. However, a casing according to the invention can be adapted to any rotating machine having a turbine or a rotary element capable of being driven at high rotational speeds and to generate significant mechanical and thermal stresses.
    STATE OF THE PRIOR ART The state of the art can be illustrated by turbocharger housings for motor cars. In order to increase the power of the heat engines, they may be provided with a turbine housed in a housing and placed in the flow of the exhaust gas exiting said engine. The turbine is driven at high speed by the gases. The turbine is connected to a compressor, preferably of the rotary type, arranged in the intake duct of the heat engine. The compressor comprises a second turbine connected to the first through a shaft. In this way, the turbocharger comprises a first driving turbine rotated by the flow of the exhaust gas emitted by the internal combustion engine and a second compression turbine fixed in rotation with the first. This device increases the pressure of the air admitted into the engine and, consequently, the power of the latter.
    Currently, turbocharger housings used on combustion engines, are manufactured by traditional methods of the metal foundry type.
    These housings, as well as those used in other technical fields have a number of disadvantages and limitations.
    Among these we can mention a relatively high weight due to significant material thicknesses of their outer skin. This thickness of material is provided so as to withstand high mechanical stresses and so as to contain, if necessary, the splinters of the turbine in the event of explosion of the latter.
    Another difficulty encountered with conventional housings is the evacuation of the heat that is generated, in particular by the passage of gas and the rotation of the turbine.
    The invention aims to provide a housing having improved mechanical and thermal characteristics to overcome these difficulties and to be implemented in rotating machines subject to high thermal and mechanical stresses. The invention also aims to provide a lighter housing and able to withstand, if necessary, a breakage of the turbine.
    Thus, the invention proposes a casing for rotating machines, in particular for turbomachines, comprising a chamber for housing a turbine, and a gas flow duct opening into said chamber. According to the invention, the casing comprises at least one recess surrounding at least a portion of the gas circulation duct.
    The casing may comprise one or more recesses, open or closed, communicating with each other or not. The recess or the recesses are preferably formed in a solid part of the casing, and in particular inside the housing casing, around the gas circulation duct. The recess may surround all or part of the gas duct according to its section, and all or part of its length. Preferably, the recess extends over more than half the length of the gas flow conduit and surrounds the conduit over more than half of its section. One of the functions of the recess is to lighten the housing. Thus, the recess can simply be in the form of a hollow chamber. However, and preferably, it can be provided that the recess contains a reinforcing structure, so that the recess does not weaken the housing, but strengthens it. The reinforcing structure may be a rigid mesh structure, or a honeycomb structure. The reinforcing structure can be made of the same material as the solid part of the housing. It can be made of steel, titanium, aluminum or alloys of these materials. This is, for example, a mesh of metal son.
    The reinforcing structure may also be made of a material different from that of the housing. This is, for example a compact structure in a lighter material, that is to say less dense than the material of the solid part of the casing housing.
    A fluid passage, in particular a heat transfer fluid, is preferably formed in the reinforcing structure. This is particularly the case when the reinforcement structure is made of a mesh or an open-cell structure. The fluid can then pass into the cells or in the days of the mesh.
    The reinforcing structure may have meshes or cells in a regular pattern of repetition, for example a honeycomb structure, or possibly an irregular pattern. In the latter case, the pattern may advantageously be tighter in high stress areas of the housing and looser in areas of lower stress. The recess in the housing can be a closed chamber. It can also be provided with one or more connections. The connectors can be used during the manufacture of the housing to introduce the reinforcement structure into the recess. This is, for example, a fluid of pulverulent material which fills the recess by clogging.
    Connections may also be provided for connecting one or more cooling circuits to the casing and circulating a coolant in the recess or recesses. For example, one or more inlet fittings and one or more outlet fittings may be provided. The use of a plurality of inlet and / or outlet connections may in particular be considered to independently control the temperature of several zones of the housing or to maintain inside the housing a heat transfer fluid of substantially uniform temperature. The invention also relates to a method of producing a housing according to the invention with one or more recesses, comprising a layer-by-layer additive manufacturing step.
    The manufacture of layered structures by layers is in itself known.
    A virtual model of the crankcase is created in three dimensions on a computer in order to generate 3D CAD data in three dimensions. These data are converted into two-dimensional layered manufacturing data. Finally, the two-dimensional layer data is used to deposit the material in thin layers, typically 20 to 100 micrometers.
    The formation of successive layers may comprise, for example, the deposition of powders and their fusion by laser. Finally, the invention relates to a turbomachine comprising a turbojet or a turbocharger with a housing according to the invention and a turbine housed in the housing.
    In particular, the turbomachine may comprise a turbocharger and an internal combustion engine with which the turbocharger is associated. In this case, the crankcase gas flow duct is connected to an exhaust gas outlet of the engine.
    The exhaust gas then drives a driving turbine which in turn can be coupled to a second turbine of a compressor, in a known manner.
    Brief description of the figures. Other features and advantages of the invention will become apparent from the following description, given by way of illustration. It refers to the figures of the appended drawings in which:
    Figure 1 is a front view in section, of a conventional turbocharger housing.
    Figure 2 is a front view in section of a first embodiment of a housing according to the invention.
    Figure 3 is a sectional view along the plane A-A 'of Figure 2.
    Figure 4 is a front view in section of a second embodiment of a housing according to the invention incorporating a lightweight mesh reinforcement structure.
    Figure 5 is a detail section, on a larger scale, of a portion of a housing similar to the housing of Figure 4 with a honeycomb reinforcement structure.
    Figure 6 is a perspective view in section of a third embodiment of turbocharger housing according to the invention.
    FIG. 7 is a detail view, on an enlarged scale, of part of FIG. 6.
    Detailed description of modes of implementation of the invention.
    Reference is made to the drawings to describe interesting examples, although in no way limiting, of crankcases for rotating machines made according to the invention.
    Figure 1 shows a housing 1 used for turbochargers of known type.
    It has, in its central part, a chamber 2 intended to accommodate a drive turbine T. A conduit or channel 3 of gas circulation, is formed in the mass of the housing 1, around the central chamber 2. In the case of a turbocharger the duct 3 is connected to the exhaust of an internal combustion engine M.
    This duct 3 has a spiral shape or a volute shape with an inlet end 3a. It opens into the chamber 2 and communicates with the turbine T shown very schematically.
    In the application to turbochargers for improving the power and efficiency of the heat engines, the input end communicates with the exhaust gas outlet of a motor M. The driving turbine T is then subjected to exhaust gas flow. It causes, for example, a compression turbine not shown that sucks and compresses the ambient air and sends it into the cylinders of the engine, thus improving the filling thereof, which increases the amount of air mixture fuel entering said cylinders.
    FIG. 2 illustrates an implementation possibility of the invention for a casing comparable to FIG. 1. Identical references are used to indicate identical or similar parts described with reference to FIG. 1 so that one can 'carry it forward. It can be observed that a recess 4 is formed in the part of the casing 1 which surrounds the duct or channel 3 for the circulation of the exhaust gases. In the transverse direction, this recess 4 extends over an angular distance approximately corresponding to the angular distance that the duct 3 travels around the chamber 2. The recess 4 is formed in a solid portion of the casing between an outer skin and an inner skin of the housing. It has a section which decreases towards the direction of flow of the gases in the duct 3.
    In the implementation illustrated in Figure 2, the recess 4 is a hollow chamber formed in a solid portion of the housing.
    The arrangement of the recess around the chamber 3, on at least a portion of its section, is also visible in FIG. 3. The recess 4 is extended to also surround part of the chamber 2.
    As shown in Figure 4, the recess 4 may contain a reinforcing structure 5. This is a mesh structure, rigid and lightweight. This rigid mesh structure may comprise a mesh formed by a crisscrossing of rigid metal son connected to each other in a regular pattern or not. It can be formed in the same material as the wall or the solid part of the casing 1. It can also be formed in a material lighter than the material of the housing.
    The reinforcing structure 5 ensures a good rigidity of the wall of the casing 1, without increasing the mass thereof. While improving the burst resistance of the turbine not shown, it allows, in case of bursting thereof, to absorb the energy that results. Thus, the blades and debris of the turbine remain confined in the body of the casing and lose their dangerousness.
    According to an alternative embodiment of the casing of FIG. 4, the reinforcing structure may also be an open or closed cell structure, for example a honeycomb structure, as shown in FIG. 5.
    Figure 6 shows a housing according to the invention in which recess is used to form a heat exchanger. Like the casing of Figure 4, the recess 4 is provided with a reinforcing structure 5. The reinforcing structure is a mesh structure which thereby provides a passage for a heat transfer fluid that can pass between the meshes. A coolant circulation circuit, represented symbolically with reference numeral 10, is connected to an inlet fitting 12a and to an outlet fitting 14, provided on the recess 4 along the gas channel 3. The coupling 12a input and the output connector 14 are provided in particular at the ends 4a and 4b of the recess 4. One or more intermediate inlet connections may be provided. Figure 6 shows an intermediate inlet fitting 12b. It makes it possible to prevent an increasingly hot heat transfer fluid from circulating along the recess 4. It should be noted that the reinforcing structure 5, through which the heat transfer fluid flows from the connection (s) input and to the outlet connection or connectors participates in a heat exchange function between the housing and the fluid.
    Figure 7 shows that the mesh of the reinforcement structure is not necessarily regular. The pattern of the structure may indeed be irregular so as to form meshes, or possibly cells, of different dimensions. The irregular nature of the structure can be advantageously used to create zones of greater or lesser mechanical strength, more or less strong heat exchange capacity or areas with more or less heat transfer fluid flow.
    权利要求:
    Claims (12)
    [1" id="c-fr-0001]
    1. Carter for rotating machines, in particular for turbomachines, comprising a chamber (2) for housing a turbine, and a conduit (3) for gas flow opening into said chamber, characterized by at least one recess (4) surrounding at least a portion of the gas flow conduit (3).
    [2" id="c-fr-0002]
    The housing of claim 1, wherein the recess contains a reinforcing structure (5).
    [3" id="c-fr-0003]
    3. Carter according to claim 2, wherein a fluid passage is formed in the reinforcing structure (5).
    [4" id="c-fr-0004]
    4. Carter according to one of claims 2 or 3 wherein the reinforcing structure (5) is selected from a honeycomb structure and a mesh structure.
    [5" id="c-fr-0005]
    5. Carter according to claim 4, wherein the reinforcing structure (5) has a repeating pattern selected from a regular pattern and an irregular pattern.
    [6" id="c-fr-0006]
    6. The housing of claim 2, wherein the recess (4) is formed in a solid portion of the housing, and wherein the reinforcing structure comprises a less dense material than the solid portion of the housing.
    [7" id="c-fr-0007]
    The housing of claim 1, wherein the recess is provided with at least one connector (12a, 12b, 14) for a fluid connection.
    [8" id="c-fr-0008]
    8. Housing according to claim 7, comprising at least one inlet fitting (12a, 12b) and at least one outlet fitting (14), the inlet fitting and the outlet fitting being connected to a circulation circuit ( 10) of a heat transfer fluid.
    [9" id="c-fr-0009]
    The housing of claim 1, wherein the recess forms a closed chamber.
    [10" id="c-fr-0010]
    10. A method of manufacturing a housing (1) according to any one of the preceding claims, characterized in that it comprises a layer-by-layer additive manufacturing step.
    [11" id="c-fr-0011]
    11. A turbomachine comprising one of a turbojet engine and a turbocharger equipped with a housing (1) according to one of claims 1 to 9, and a turbine housed in the housing.
    [12" id="c-fr-0012]
    Turbine engine according to Claim 11, comprising a turbocharger and an internal combustion engine (M), in which the gas circulation duct (3) of the casing (1) is connected to an exhaust gas outlet of the engine.
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    同族专利:
    公开号 | 公开日
    FR3040733B1|2018-08-31|
    WO2017042448A1|2017-03-16|
    引用文献:
    公开号 | 申请日 | 公开日 | 申请人 | 专利标题
    US4068612A|1976-01-26|1978-01-17|M & W Gear Company|Turbocharger housing construction for marine turbocharger and device for turbocharging a marine engine|
    DE102010042104A1|2010-10-07|2012-04-26|Bayerische Motoren Werke Aktiengesellschaft|Supercharger for combustion engine, has compressor housing comprising coolant channel that is integrated into coolant circuit and extended tangentially and radially around compressor screw arranged radially around compressor wheel|
    US20140321998A1|2013-04-24|2014-10-30|MTU Aero Engines AG|Housing section of a turbine engine compressor stage or turbine engine turbine stage|
    US20150030434A1|2013-07-23|2015-01-29|MTU Aero Engines AG|Damping device for being situated between a housing wall and a casing ring of a housing of a thermal gas turbine|
    US20150211383A1|2014-01-27|2015-07-30|Ford Global Technologies, Llc|Internal combustion engine with cooled turbine|EP3633155A1|2018-10-05|2020-04-08|United Technologies Corporation|Additively manufactured thermally insulating structure|
    DE102018130772A1|2018-12-04|2020-06-04|Man Energy Solutions Se|Turbocharger, method of manufacturing a turbocharger assembly and use|
    DE102018132414A1|2018-12-17|2020-06-18|Man Energy Solutions Se|Exhaust gas turbocharger with auxetic structures|
    DE102019106733A1|2019-03-18|2020-09-24|Man Energy Solutions Se|Cooling of the rotor and stator components of a turbocharger with the help of additively manufactured component-internal cooling channels|
    法律状态:
    2016-07-21| PLFP| Fee payment|Year of fee payment: 2 |
    2017-03-10| PLSC| Search report ready|Effective date: 20170310 |
    2017-09-25| PLFP| Fee payment|Year of fee payment: 3 |
    2018-09-25| PLFP| Fee payment|Year of fee payment: 4 |
    2019-09-25| PLFP| Fee payment|Year of fee payment: 5 |
    2020-09-25| PLFP| Fee payment|Year of fee payment: 6 |
    2021-09-27| PLFP| Fee payment|Year of fee payment: 7 |
    优先权:
    申请号 | 申请日 | 专利标题
    FR1558277A|FR3040733B1|2015-09-07|2015-09-07|CARTER FOR ROTATING MACHINES, ESPECIALLY FOR TURBOMACHINES.|FR1558277A| FR3040733B1|2015-09-07|2015-09-07|CARTER FOR ROTATING MACHINES, ESPECIALLY FOR TURBOMACHINES.|
    PCT/FR2016/052116| WO2017042448A1|2015-09-07|2016-08-24|Casing for rotary machines and in particular for turbomachines|
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