• 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 turbomachine assembly comprising: a housing comprising: an inner hub (10), an outer shell (20) extending around and away from the inner hub (10), a hollow arm ( 30), provided with a longitudinal cavity (40) and connecting the inner hub (10) and the outer shell (20), • a tube (50) configured to extend within the longitudinal cavity (40) the hollow housing arm (30) and comprising a central support (60) comprising two resilient blades (61) and configured to exert pressure on the longitudinal cavity wall (42) when the tube (50) is extended to the interior of the longitudinal cavity (40). characterized in that the material (or materials) of the elastic blades (61) is (are) such that said elastic blades (61) have a stress curve between the minimum and maximum stress curves of Table A.
    公开号:FR3064302A1
    申请号:FR1752420
    申请日:2017-03-23
    公开日:2018-09-28
    发明作者:Patrick Jean Laurent Sultana；Sebastien Jean Laurent Prestel；Olivier Renon
    申请人:Safran Aircraft Engines SAS；
    IPC主号:
    专利说明:

    TECHNICAL AREA
    The invention relates to a set of parts for a turbomachine.
    The invention relates more specifically to structures with hollow arms that are found in turbomachines, as well as the pipes extending inside these hollow arms.
    STATE OF THE ART
    The operation of a conventional turbomachine involves the circulation of various fluids through said turbomachine. For example, these fluids can be air, oil, or oiled air.
    In order to route these fluids, it is known to have pipes in the structure of the turbomachine. Some of these pipes must connect radially external parts of the turbomachine to radially internal parts, and thus pass through the primary and secondary air flows. To do this, it is known to arrange these pipes, called service tubes, within hollow casing arms. For example, such tubes are found in the hollow arms of the turbine downstream casing, called TRF (Turbine Rear Frame). This example is not, however, limiting, since it is also possible to find such tubes in parts of turbomachines such as a TRV (downstream turbine rectifier, or "Turbine Rear Vane" according to the English terminology generally used ), a TCF (inter-turbine casing, or "Turbine Center Frame" according to the Anglo-Saxon terminology generally used) or a TVF (inter-turbine rectifier, or "Turbine Vane Frame" according to the Anglo-Saxon terminology generally used).
    Illustrated in FIG. 1 is an example of an assembly 1 of a turbomachine comprising a tube 2 disposed inside a longitudinal cavity 3 provided inside a hollow arm 4 connecting an internal hub 5 to an external ferrule 6 turbomachine housing.
    As can be seen in FIG. 1, it is known to introduce the tube 2 within the longitudinal cavity 3 of the hollow arm 4 at the junction between the hollow arm 4 and the outer ferrule 6. The tube 2 is then slid inside the cavity 3 until it fully extends there. The ends 8, 9 of tube 2 are then fixed respectively to the inner hub 5 and to the outer ferrule 6 in order to secure the tube to the hub 5 and to the ferrule 6. As a result, the ends 8, 9 of tube are assembled to tubes included in hydraulic circuits arranged in radially external or internal parts, so as to ensure fluid communication between radially external parts of the turbomachine and radially internal parts.
    In FIG. 1, it is also visible that, over the majority of the length of the tube 2, the external surface of the tube is not in contact with the longitudinal cavity wall 3. The tube 2 thus arranged is therefore free to vibrate .
    However, the tube 2 has natural frequencies of vibration. Tube 2 vibrates most violently when excited at these frequencies. This induces rapid fatigue which can go as far as rupture. These frequencies depend on the length of the tube 2, but also on the material which constitutes it, its thickness, or its temperature.
    The longer the tube 2, the lower the natural frequency, the lower the frequency of rotation of the low and high pressure bodies of the turbomachine. This leads to problems of robustness and safety within the turbomachinery. This is particularly true in the case of large motors.
    It is therefore known to add a central support system, integral with the tube, disposed in a position substantially equidistant from the two ends of the tube, so as to stabilize the tube within the hollow arm. This central support system generally has two complementary elastic blades arranged opposite one another so as to give the support a double U orthogonal section called "hurricane" in English terminology.
    Such a central support has a length of orthogonal section greater than the width of the longitudinal cavity. It is therefore known to compress the central support when inserting the central portion of the tube within the longitudinal cavity, so as to allow the passage of the entire tube. Once inserted, the central support system relaxes to exert pressure on the longitudinal cavity walls.
    However, in the central support systems of the prior art, the relaxation of the central support observed is not sufficient to come into contact with the walls of the longitudinal cavity.
    There is therefore a need for an assembly for a turbomachine comprising a tube disposed inside a longitudinal cavity of hollow arms connecting an internal hub to an external ferrule and not having the drawbacks mentioned above.
    BASIS OF THE INVENTION
    An object of the invention is to propose an assembly for a turbomachine making it possible to convey a fluid between two parts of turbomachinery which are radially distant in a robust and reliable manner.
    Another object of the invention is to propose an assembly for a turbomachine which is easy to assemble and thus reduces manufacturing and assembly costs.
    Another object of the invention is to propose an assembly for a turbomachine suitable for large turbomachinery.
    In this regard, the invention proposes an assembly for a turbomachine comprising:
    • a housing comprising:
    - an internal hub,
    - an external ferrule extending around and at a distance from the internal hub,
    - a hollow arm, provided with a longitudinal cavity and connecting the internal hub and the external ferrule, • a tube configured to extend inside the longitudinal cavity of the hollow arm of the casing and comprising a central support comprising two blades elastic and configured to exert pressure on the wall of the longitudinal cavity when the tube is extended inside the longitudinal cavity.
    characterized in that the material (s) of the elastic blades is (are) such that said elastic blades have a stress curve comprised between the minimum and maximum stress curves of table A.
    Alternatively, but optionally, the assembly according to the invention can also include the following characteristics:
    - the material (s) of the elastic blades have a Young's modulus at 20 ° C of between 180,000 MPa and 250,000 MPa,
    - the elastic blades are in forged inco718 or sheet metal (DMD0424),
    - the elastic blades are brazed to the tube or linked to a support configured to be attached to the tube,
    the thickness of the elastic blades is between 0.5 mm and 1.5 mm, preferably between 0.7 mm and 0.9 mm,
    - the length of the orthogonal section at rest of the central support is 12 mm to 30 mm greater than the width of the longitudinal cavity of the hollow casing arm,
    - the width of the elastic blades is between 30 mm and 50 mm,
    - the central support is placed in a substantially equidistant position from the two ends of the tube,
    - the assembly includes two supports, each comprising two elastic blades, the first support being disposed in a position distant from one of the ends by substantially one third of the distance separating the ends, and the second support being disposed in a position distant from the end of substantially two thirds of the distance between the ends.
    The invention also relates to a turbomachine comprising an assembly as described above.
    The invention also relates to a method of assembling an assembly as described above, the method comprising the steps of:
    • compression of the elastic blades of central support until plasticization of said blades, and • passage of the elastic blades of central support plasticized through a longitudinal cavity opening of hollow casing arms.
    QUICK DESCRIPTION OF THE FIGURES
    Other characteristics, objects and advantages of the present invention will appear on reading the detailed description which follows and with reference to the appended drawings given by way of non-limiting example and in which:
    FIG. 1, already described, illustrates a turbomachine assembly comprising an service tube without central support,
    FIG. 2 illustrates a part of a turbomachine assembly comprising an internal hub and an external ferrule connected by arms,
    FIG. 3 is a sectional view of the part of the turbomachine assembly illustrated in FIG. 2,
    - Figure 4 illustrates a part of a turbomachine assembly comprising a service tube provided with a central support type "hurricane";
    - Figure 5 illustrates the main dimensions of an elastic blade of central support type "hurricane",
    FIG. 6 illustrates a section of a “hurricane” type central support attached to a service tube in a plane orthogonal to the main direction of said tube,
    - Figure 7 illustrates the blocking of the central support type "hurricane" at rest at the entrance of the longitudinal cavity oblong hollow casing arm during the insertion of the service tube inside said cavity ,
    FIG. 8 illustrates the diagram of the prestresses undergone by the hurricane support during the assembly process, and
    - Figure 9 illustrates the minimum and maximum stress curves between which is included the stress curve of (or) material (s) of elastic blades of central support.
    DETAILED DESCRIPTION OF THE INVENTION
    With reference to the figures, a description will now be given of a turbomachine assembly which comprises an internal hub 10 and an external ferrule 20, each of annular shape, and extending around an axis X-X of the turbomachine.
    In the turbomachine, the described assembly can be placed at any location. For example, it can be downstream of the low pressure turbine.
    With reference to FIG. 2, the external ferrule 20 extends around and at a distance from the internal hub 10. The external ferrule 20 thus has a diameter greater than the internal hub 10. The external ferrule 20 and the internal hub 10 are moreover concentric .
    The internal hub 10 and the external ferrule 20 are connected by a set of arms 30 extending radially with respect to the axis X-X.
    With reference to FIG. 3, each of the arms 30 is hollow and includes a longitudinal cavity 40 which opens into the internal hub 10 through a first opening 11 and onto the external shell 20 by a boss 22 provided with a second opening 21.
    The assembly may also include a service tube 50 illustrated in FIG. 4, configured to convey a fluid such as air, oil, or oiled air. The tube 50 is also configured to extend into the longitudinal cavity
    40.
    In this configuration, a first tube end 51 passes through the first opening 11 so that it can be connected to the internal hub 10, for example by bolting. In addition, the tube 50 extends out of the outer shell 20 through the second opening 21 by a second end 52 which can, for example, take the form of an elbow. The second end 52 may, for example, further comprise a collar 521 provided with peripheral holes 522 to allow a connection by screwing on the boss 22 of the external ferrule 20.
    In this configuration, the two ends of the tube 51, 52 are therefore secured respectively to the internal hub 10 and to the external ferrule 20.
    In this configuration, the tube 50 extends within the longitudinal cavity 40 without the external surface of the tube 50 being in contact with a wall 42 of the longitudinal cavity 40. Thus, the tube 50 is able to vibrate during operation of the turbomachine. These vibrations can reach the natural frequencies of the tube 50 which can therefore enter into resonance and induce rapid fatigue which can go as far as breaking.
    The assembly can therefore also comprise a central support 60 attached to the tube 50. The central support 60 can be attached by direct soldering to the tube 50 or via a support itself configured to be attached to the tube 50.
    As illustrated in FIG. 5, the central support 60 comprises two elastic blades 61 of generally rectangular shape, and having a length L, a width I and a thickness e.
    As visible in FIG. 4, the elastic blades 61 envelop the tube 50. A section along a plane orthogonal to the main direction of the tube 50 of the tube / elastic blade assembly is visible in FIG. 6. As can be seen more precisely on the Figure 7, each blade 61 comprises a flat 610 from which extend two legs 611 curved. Each of the blades 61 then has a U shape. Once placed on the tube 50, the tube 50 extends into the hollow of the U formed by each of the blades 61.
    In a privileged manner, the central support 60 comprises two elastic bands 61 complementary arranged opposite one another and successively along the main direction of the tube 50. The central support 60 thus has a general shape in double U , the tube 50 extending in the successive hollows of the two complementary elastic blades 61. The length L ′ of orthogonal section of hurricane support 60 is also illustrated in FIG. 6, and corresponds to the distance separating the opposite ends from the complementary elastic blades 61. The double U structure of the support 60 recalling the shape of a cyclone, the English terminology uses the term "hurricane" to designate such a central support 60.
    The hurricane support 60 is therefore configured, when the tube 50 is inserted into the longitudinal cavity 40 of the hollow casing arm 30, to exert sufficient pressure on the walls 42 of said cavity 40 to prevent vibrations of the tube 50 during operation of the turbomachine. In this regard, it is known to place the hurricane support 60 in a position substantially equidistant from the ends 51, 52 of the tube 50, so as to maintain the central part of the tube 50.
    As a variant, the central support 60 comprises two pairs of two elastic blades 61 forming two hurricane supports 60. In this case, the first hurricane support 60 can be disposed in a position distant from one of the ends 51, 52 by substantially a third of the distance separating the ends 51, 52. The second hurricane support 60 is then placed in a position distant from the end 51, 52 by substantially two thirds of the distance separating the ends 51, 52.
    As will be understood from what has been described above, the hurricane support 60 is attached to the tube 50 before the tube 50 is placed inside the central cavity 40.
    However, as can be seen in FIG. 7, the dimensions of the hurricane support 60 are such that the passage of the portion of tube 50 carrying the hurricane support 60 through the second opening 21 of the longitudinal cavity 40 is made impossible.
    In this regard, a method of assembling the assembly described above comprises a step of compressing the hurricane support 60 when passing the second opening 21 of the longitudinal cavity 40, until the support 60 is plasticized, so allowing the entire tube 50 to extend within the longitudinal cavity 40 of the hollow arm 30 of the casing.
    As can be seen in FIG. 3, the longitudinal cavity portion 40 located near the second opening 21, called oblong 41, has a width less than the rest of the longitudinal cavity 40. Consequently, the hurricane support is kept in compression as long that the entire hurricane support 60 has not exceeded the oblong 41. Subsequently, the hurricane support 60 relaxes and exerts pressure on the walls 42 of the longitudinal cavity 40.
    FIG. 8 shows the diagram of the prestresses undergone by the hurricane support 60 during an assembly process. There are three stages of prestressing as a function of the time of insertion of the tube 50 within the longitudinal cavity.
    During a first step, the hurricane support 60 is compressed by mechanical means such as pliers, or manually, so as to reduce the orthogonal section length L ′ of the hurricane support 60 until it reaches the width of oblong
    41. This compression results in the plasticization of the hurricane support 60.
    In a second step, the hurricane support 60 passes the oblong 41, and the orthogonal section length L ’of the hurricane support 60 is kept constant substantially equal to the width of oblong 41.
    During a last step, the hurricane support 60 extends again by elastic return phenomenon, until it reaches a length of orthogonal section substantially equivalent to the width of the longitudinal cavity 40 and thus exert pressure on the walls. 42 of said cavity 40.
    Thereafter, the tube ends 51, 52 are fixed respectively to the inner hub 10 and to the outer ferrule 20.
    In order to optimize the operation of the hurricane support 60 previously described, it is possible to design elastic blades of particular dimensions.
    In this regard, the orthogonal section length L ’, the width I, and the thickness e of the elastic blades 61 have been dimensioned.
    With regard to the thickness e, the dimensioning meets two opposite constraints:
    the thickness e must be as large as possible to increase the natural frequency of the tube 50, and
    - the thickness e must be as small as possible to facilitate assembly of the assembly, in particular when the hurricane support 60 passes at the level of the oblong 41.
    In this regard, the Applicant has found that an optimal thickness e is between 0.5 and 1.0 mm, preferably between 0.7 and 0.9 mm, and even more preferably is 0.7 mm.
    With regard to the width I of the elastic blades 61, the dimensioning must also respond to mounting constraints. To do this, the Applicant has found that an optimal total width of urrican support 60 (i.e. by summing the successive widths I of elastic blades 61 joined) is between 30 mm and 50 mm.
    The last support dimension 60 is the length of orthogonal section L ’at rest. The Applicant has found that an orthogonal section length L ′ at optimum rest is between the width of the longitudinal cavity 40 to which is added 6 mm on each side of the cavity 40, and the width of the longitudinal cavity 40 to which is added 15 mm on each side of the cavity.
    In order to optimize the hurricane support 60 previously described, it is also possible to provide elastic blades 61 made of a material having particular properties.
    The material must be such that the plasticization of the elastic blades 61 is sufficient for the passage of the oblong 41 so that the elastic return is greater than the difference in width between the oblong 41 and the longitudinal cavity 40 of the arm 30 .
    For this, the Applicant has found that an optimal material has a Young's modulus at 20 ° C of between 180,000 MPa and 250,000 MPa.
    Furthermore, the elastic blades 61 can comprise one or more material (s) having the stress-strain characteristics in accordance with the following table A:
    Table A
    Deformation(%) Min associated stress (MPa) Max associated stress (MPa) 0.5 800 1250 1 850 1300 2 900 1400 5 950 1470 7.5 1000 1500
    As illustrated in FIG. 9, the material (s) of the elastic blades 61 is can (can) be such that said elastic blades 61 have a stress curve comprised between the minimum and maximum stress curves of table A.
    These measurements are carried out on tensile test benches well known to those skilled in the art. By way of nonlimiting example, these tests can be carried out on a traction machine using test pieces comprising a material to be tested.
    The assembly described above therefore offers the advantage of reducing the resonance vibrations of the service tube 50 by proposing a hurricane support 60 whose elastic return after plasticization is sufficient to ensure permanent contact with the walls 42 of the longitudinal cavity 40 of the arm 30 crankcase.
    The properties of elastic blades 61 of hurricane support 60 previously described have a range between:
    - a dynamic status which requires hurricane support 60 which is as thick as possible, and
    - ease of assembly which requires hurricane support 60 which is as thin as possible.
    Finally, it is possible to provide a deburring or a slight radius on the hurricane support 60 so as to minimize scratches on the walls 42 of the longitudinal cavity 40 when the tube 50 is inserted.
    权利要求:
    Claims (11)
    [1" id="c-fr-0001]
    1. Turbomachine assembly comprising:
    • a housing comprising:
    - an internal hub (10),
    - an external ferrule (20) extending around and at a distance from the internal hub (10),
    - a hollow arm (30), provided with a longitudinal cavity (40) and connecting the internal hub (10) and the external ferrule (20), • a tube (50) configured to extend inside the longitudinal cavity (40) of the hollow arm (30) of the casing and comprising a central support (60) comprising two elastic blades (61) and configured to exert pressure on the wall (42) of longitudinal cavity (40) when the tube ( 50) is extended inside the longitudinal cavity (40).
    characterized in that the material (s) of the elastic blades (61) is (are) such that said elastic blades (61) have a stress curve comprised between the minimum and maximum stress curves of the table AT.
    [2" id="c-fr-0002]
    2. The assembly of claim 1, wherein the (or) material (s) of the elastic blades (61) have a Young's modulus at 20 ° C between 180,000 MPa and 250,000 MPa.
    [3" id="c-fr-0003]
    3. Assembly according to one of claims 1 or 2, in which the elastic blades (61) are made of forged inco718 or sheet metal (DMD0424).
    [4" id="c-fr-0004]
    4. Assembly according to one of claims 1 to 3, wherein the elastic blades (61) are brazed to the tube (50) or linked to a support configured to be attached to the tube (50).
    [5" id="c-fr-0005]
    5. Assembly according to one of claims 1 to 4, wherein the thickness of the elastic blades (61) is between 0.5 mm and 1.5 mm, preferably between 0.7 mm and 0.9 mm.
    [6" id="c-fr-0006]
    6. Assembly according to one of claims 1 to 5, in which the length of the orthogonal section at rest of the central support (60) is greater by 12 mm to 30 mm than the width of the longitudinal cavity (40) of the arm (30) crankcase hollow.
    [7" id="c-fr-0007]
    7. Assembly according to one of claims 1 to 6, in which the width of the elastic blades (61) is between 30 mm and 50 mm.
    [8" id="c-fr-0008]
    8. Assembly according to one of claims 1 to 7, wherein the central support (60) is placed in a position substantially equidistant from the two ends (51, 52) of the tube (50).
    [9" id="c-fr-0009]
    9. Assembly according to one of claims 1 to 7, comprising two supports (60), each comprising two elastic blades (61), the first support (60) being disposed in a position distant from one of the ends (51, 52 ) of substantially one third of the distance separating the ends (51, 52), and the second support (60) being arranged in a position distant from the end (51, 52) of substantially two thirds of the distance separating the ends ( 51, 52).
    [10" id="c-fr-0010]
    10. Turbomachine comprising an assembly according to one of claims 1 to 9.
    [11" id="c-fr-0011]
    11. Method for assembling an assembly for a turbomachine according to one of claims 1 to 9, the method comprising the steps of:
    • compression of the elastic blades (61) of central support (60) until the plasticization of said elastic blades (61), and • passage of the elastic blades (61) of central support (60) plasticized through an opening (21) of longitudinal cavity (40) of hollow casing arms (20).
    1/8
    2/8
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    同族专利:
    公开号 | 公开日
    EP3601746A1|2020-02-05|
    FR3064302B1|2019-06-07|
    US11136894B2|2021-10-05|
    WO2018172715A1|2018-09-27|
    EP3601746B1|2022-01-12|
    US20210108526A1|2021-04-15|
    CN110546350A|2019-12-06|
    引用文献:
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    法律状态:
    2018-02-19| PLFP| Fee payment|Year of fee payment: 2 |
    2018-09-28| PLSC| Publication of the preliminary search report|Effective date: 20180928 |
    2020-02-20| PLFP| Fee payment|Year of fee payment: 4 |
    2021-02-19| PLFP| Fee payment|Year of fee payment: 5 |
    2022-02-21| PLFP| Fee payment|Year of fee payment: 6 |
    优先权:
    申请号 | 申请日 | 专利标题
    FR1752420A|FR3064302B1|2017-03-23|2017-03-23|CENTRAL SUPPORT OF TUBES SERVITUDE WITH ELASTIC RETURN|
    FR1752420|2017-03-23|FR1752420A| FR3064302B1|2017-03-23|2017-03-23|CENTRAL SUPPORT OF TUBES SERVITUDE WITH ELASTIC RETURN|
    CN201880024536.3A| CN110546350A|2017-03-23|2018-03-23|Center support with elastic return for an auxiliary conduit|
    EP18715226.9A| EP3601746B1|2017-03-23|2018-03-23|Central support for auxiliary tubes with elastic return|
    PCT/FR2018/050707| WO2018172715A1|2017-03-23|2018-03-23|Central support for auxiliary tubes with elastic return|
    US16/496,368| US11136894B2|2017-03-23|2018-03-23|Central support for auxiliary tubes with elastic return|
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