• 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:
    Device (10) for assembling a turbomachine (1), the turbomachine having at least two modules (3) assembled by inserting a shaft of one of the modules in a housing of the other modules, the device comprising: - means (11) for supporting a first one of the modules, and - means (20, 21) for suspending a second one of the modules, and for moving this second module along an axis of displacement (Z) , characterized in that it further comprises: - a laser beam emitter (30) intended to be fixed to said first module and configured to emit a laser beam (31) coinciding with a longitudinal axis (X) of this first module, and a target (40) intended to be fixed to said suspension and displacement means, so that it can be displaced along said axis of displacement, and at least two axial positions distant on this axis, a task (41) of said laser beam is located at the center of said target.
    公开号:FR3068078A1
    申请号:FR1755886
    申请日:2017-06-27
    公开日:2018-12-28
    发明作者:Remy LE GALL
    申请人:Safran Aircraft Engines SAS；
    IPC主号:
    专利说明:

    Device and method for assembling a turbomachine
    Field of the invention:
    The present invention relates to the field of turbomachinery and is aimed in particular at multi-body gas turbine engines. It relates to the assembly operations of the engines and in particular to the mounting of the low pressure turbine module on a high pressure body.
    State of the art:
    A double-body turbojet engine, with a front fan for example, comprises a high pressure HP body and a low pressure BP body. The LP body rotates at a first speed and includes a BP turbine downstream of the HP body, which drives the front fan. The HP body rotates at a different speed from that of the BP turbine. The shafts of the two bodies are concentric and the body shaft BP crosses inside the body shaft HP. The BP body shaft is guided in rotation by bearings supported by the fixed structure of the engine, located respectively downstream of the turbine and upstream of the high pressure compressor. The HP body shaft is guided in rotation by bearings supported by the fixed motor structure upstream and by the BP body shaft downstream, by means of an inter-shaft bearing. This latter bearing is of the roller type and located, at least according to a known motor, between the high pressure turbine and the low pressure turbine. Such a bearing includes an inner ring fitted with rollers held by a cage on the shaft of the LP body and an outer ring, generally mounted with cold clamping in the shaft of the HP body. The mounting of this bearing, that is to say the assembly of the outer ring with the assembly formed of the rollers, the cage and the inner ring, is carried out at the same time as the low pressure turbine is approached during which the shaft previously mounted with the low pressure turbine is guided in the HP body. By the term docking, here is meant all or part of the translational movement of the low pressure turbine module until the flange of the external casing thereof comes into contact with the corresponding flange of the module constituting the HP body.
    It follows that the mounting of the inter-shaft bearing is carried out blind. The operator has no visibility to monitor, in particular, the engagement of the rollers in the rotor of the HP body and then in the outer ring. This operation involves strong risks of degradation of the bearing if the conditions are not controlled. The main risk for the bearing is hard contact of the rollers against the retaining nut of the outer ring and the ring itself.
    It is known, for example from document FR-A1-2 890 110, to use techniques allowing controlled heating of the part supporting the outer ring to facilitate the introduction of the contactless rollers.
    However, even with the expansion of the outer ring, it is necessary to ensure precise positioning of the BP body shaft to avoid contact. The known practice of centering the shaft of the BP body with the rule lacks precision and leads to mounting incidents which can lead to non-qualities or even damage to parts which must then be changed by at least partially dismantling modules of the assembled turbomachine. In document FR-A1-2 890 110, it is proposed to use laser measurements with instruments mounted on a removable support which is positioned relative to the HP body, but the instrumentation is expensive and complex to implement.
    There is therefore a need for a simple technique for positioning the shaft of the LP module with respect to the outer ring of the module of the HP body with sufficient precision to minimize the risk of hard contact on the elements of the inter-shaft bearing. . More generally, there is a need to have a simple technique for assembling a turbomachine comprising at least two modules assembled by inserting a shaft of one of the modules in a housing of the other of the modules.
    Statement of the invention:
    To this end, the invention relates to a device for assembling a turbomachine, the turbomachine comprising at least two modules assembled by inserting a shaft of one of the modules in a housing of the other of the modules, the device comprising:
    - means for supporting a first of the modules, and
    - means for suspending a second module, and for moving this second module along an axis of movement, characterized in that it further comprises:
    a laser beam emitter intended to be fixed to said first module and configured to emit a laser beam coincident with a longitudinal axis of this first module, and
    - A target intended to be fixed to said suspension and displacement means, so that it can be displaced along said axis of displacement, and that at least two distant axial positions on this axis, a task of said beam laser is located in the center of said target.
    The function of the laser beam is to simulate the longitudinal axis of the first module. This axis must be substantially parallel to the axis of movement to allow the assembly of the modules and in particular to avoid any contact during docking. To guarantee this parallelism, it is necessary that in at least two distinct axial positions of the target along the axis of movement, the task of the laser beam is centered on the target. The invention can therefore use a single laser emitter and a single target.
    The device may include one or more of the following characteristics taken in isolation from one another or in combination with one another;
    - Said support means are configured to allow adjustment of the positioning of said first module in at least one direction substantially perpendicular to said longitudinal axis of said first module;
    - Said support means are configured to allow adjustment of the positioning of said first module in two directions substantially perpendicular to each other and to said longitudinal axis of said first module;
    - Said suspension and displacement means comprise at least one hoist which is attached to a beam and which is capable of being displaced along this beam defining said axis of displacement;
    - said first module is the module comprising said housing;
    - said transmitter is housed in said housing of said first module;
    - The distance between said first and second axial positions is greater than or equal to 1 meter, and for example between 2 and 3 meters.
    The invention also relates to a method of assembling a turbomachine, by means of a device as described above, comprising the steps of:
    a) positioning of said first module on said support means,
    b) fixing of said target to said suspension and displacement means,
    c) determination of a first axial position of said target, for which a spot of said laser beam is located in the center of said target,
    d) displacement of said target along said axis of displacement, and
    e) determination of a second axial position of said target, for which a task of said laser beam is located on the center of said target, in order to validate the parallelism between said longitudinal axis of said first module and said axis of movement.
    Step a) can be carried out before or after step b).
    The method can include the following steps:
    f) disassembly of said target from said suspension and displacement means,
    g) fixing of said second module to said suspension and displacement means, and
    h) insertion of said first and second modules one into the other, by displacement of said second module along said axis of displacement.
    Preferably, said first axial position is located near said first module.
    Advantageously, the process comprises, between steps d) and e), sub-steps of:
    - verification of the position of said task on said target, and
    - Adjustment of the position of said first module so that said task is located in the center of said target.
    Brief description of the figures:
    The present invention will be better understood and other details, characteristics and advantages of the present invention will appear more clearly on reading the description of a nonlimiting example which follows, with reference to the appended drawings in which:
    Figure 1 is a schematic side view of a device for assembling a turbomachine according to the invention; two modules of the turbomachine being mounted on the device;
    Figure 2 is another schematic perspective view of the device of Figure 1, one of the modules being mounted on the device and a target also mounted on the device in place of the other module, Figure 3 is another view schematic side of the device of Figure 1 equipped with the target and one of the modules here in axial section;
    Figure 4 is a schematic front view of a module mounted on support means of the device of Figure 1; and FIG. 5 is a schematic exploded perspective view of means for adjusting the support means of FIG. 4.
    Description of several embodiments:
    FIG. 1 shows a turbomachine 1 during assembly, at the start of the docking operation defined above. This is a double flow, double body turbojet engine. It comprises a front fan 2 and a high pressure module, called the first module 3, constituted by the high pressure body with its shaft 3a, called the first shaft, visible in FIG. 3. These elements are already assembled.
    Here we are mounting the low pressure turbine module, said second module 4, whose shaft 5, said second shaft, must be engaged in the high pressure body following the arrow F, parallel to the longitudinal axis X of the first module 3. This longitudinal axis X is substantially horizontal during assembly.
    In the following description, the assembly of the second module 4 is therefore described in the first module 3. The upstream and downstream are noted along the longitudinal axis X as a function of the main direction of the flow of gases, therefore from the high pressure body to the low pressure turbine.
    At its downstream end, the first module 3 comprises a housing 6 into which the shaft 5 of the second module 4 is intended to be inserted. This shaft 5 extends along the longitudinal axis Y of the second module 4.
    The drawings show an exemplary embodiment of a device 10 for assembling the turbomachine 1. The device 10 comprises means 11 for supporting the first module 3, and means for suspending the second module 4, and for moving this second module 4 along an axis of movement Z.
    The support means 11 are visible in FIGS. 1, 2 and 4. They comprise a first support 11a from the downstream end of the first module 3 and a second support 11b from the upstream end of the first module 3. The supports 11a, 11b are like legs that rest on the ground.
    The first support 11a can comprise means 12a for adjusting the positioning of the first module 3, preferably in a first vertical direction (double arrow f1). The second support 11b can comprise means 12b for adjusting the positioning of the first module 3, preferably in a first vertical direction (double arrow f 1) and in a second horizontal direction (double arrow f2).
    Figures 4 and 5 show an embodiment of the adjustment means 12b.
    The vertical adjustment ability of the means 12b, as well as the means 12a, can be obtained by means of threaded rods 13 oriented vertically and which can be screwed or unscrewed to adjust the height of means 12c for fixing to the first module 3. In addition , the ability for horizontal adjustment of the means 12b can be obtained by means of another threaded rod 14 oriented horizontally and which can be screwed into the fixing means 12c or unscrewed from these fixing means, to adjust the position of the first module in a horizontal plane. The threaded rod 14 has one end engaged in a threaded orifice of the fixing means 12c and an opposite end connected to a crank flywheel 15. This crank flywheel 15 is mounted on a plate 16 which is removably fixed to a head of a threaded rods 13. The plate 16 has an L shape, one branch of which carries the flywheel 15 which can rotate about its axis, and the other branch of which is horizontal and comprises a horizontal series of holes 17. The above-mentioned head of the threaded rod 13 includes a through hole 18 for passage of a pin 19 which is intended to be engaged through this hole into one of the holes 17 of the plate. One of the holes 17 of the plate is aligned with the hole 18 for mounting the pin 19, depending on the desired position of the fixing means in the horizontal direction. This cooperation allows a rough adjustment of the horizontal position of the fixing means 12c and therefore of the first module 3, and the screwing / unscrewing of the threaded rod 14 in the fixing means 12c allows a more precise adjustment of this position.
    The suspension and displacement means comprise a horizontal beam 20 to which a hoist 21 is fixed. The hoist 21 is able to move along the beam 20 which defines an axis Z of movement of the hoist 21.
    The second module 4 is intended to be fixed to the hoist 21. It is suspended from the hoist 21 so that its axis Y is parallel to the axis Z. To assemble the modules 3, 4 of the turbomachine 1, the shaft of the module 4 must be inserted into the housing 6 of the module 3. For this, the axes X and Y must be parallel. Knowing that the Y axis is parallel to the Z axis, it is therefore necessary that the X and Z axes are parallel.
    The present invention enables this objective to be achieved quickly and reliably. The assembly device includes:
    a laser beam emitter 30 intended to be fixed to said module 3 and configured to emit a laser beam 31 coinciding with the X axis, and
    - A target 40 intended to be fixed to the suspension and displacement means, so that it can be displaced along the Z axis.
    The transmitter 30 is for example inserted into the housing 6 of the module 3 and immobilized in this housing 6 by appropriate means. It is mounted in the housing from the downstream end of the module 3 and is oriented so that its laser beam 31 is oriented downstream.
    The target 40 is fixed to the hoist 21 in place of the second module 4 and can therefore be moved along the Z axis. To guarantee parallelism between the X and Z axes, at least two distant axial positions are required P1, P2 of the target 40 exist, for which a task 41 of the laser beam is located at the center 42 of the target 40. Indeed, in the case where two axial positions of the target 40 are identified as meeting this criterion, this means that all the intermediate positions between these positions P1, P2 meet this criterion and that the axes X and Z are parallel.
    In practice, the positions P1, P2 are at a distance D of 2 to 3 meters from each other. The first position P1 is an axial position of the target 40 as close as possible to the first module 3. The target is then positioned just downstream from the module 3 and then it is checked that the beam task is centered on the target 40. If this is not is not the case, the position of the first module 3 is adjusted until the task is located in the center of the target. The adjustment is carried out with the means 12a, 12b.
    The target 40 is then moved by means of the hoist 21 to the position P2 and the position of the beam task on the target is checked. If it is not centered, the position of the first module 3 is adjusted until the task is located in the center of the target. The adjustment is carried out with the means 12a, 12b. In such a case, it may be necessary to check again that the beam task is indeed centered on the target when the latter is in the position P1.
    权利要求:
    Claims (10)
    [1" id="c-fr-0001]
    claims
    1. Device (10) for assembling a turbomachine (1), the turbomachine comprising at least two modules (3, 4) assembled by insertion of a shaft (5) of one of the modules in a housing (6 ) of the other of the modules, the device comprising:
    - means (11) for supporting a first of the modules, and
    - means (20, 21) for suspending a second module, and for moving this second module along an axis of movement (Z), characterized in that it further comprises:
    a laser beam emitter (30) intended to be fixed to said first module and configured to emit a laser beam (31) coincident with a longitudinal axis (X) of this first module, and
    - a target (40) intended to be fixed to said suspension and displacement means, so that it can be displaced along said displacement axis, and that at least two distant axial positions (P1, P2) on this axis, a spot (41) of said laser beam is located in the center of said target.
    [2" id="c-fr-0002]
    2. Device (10) according to the preceding claim, characterized in that said support means (11) are configured to allow adjustment of the positioning of said first module (3) in at least one direction (f1) substantially perpendicular to said longitudinal axis ( X) of said first module.
    [3" id="c-fr-0003]
    3. Device (10) according to claim 1 or 2, characterized in that said support means (11) are configured to allow adjustment of the positioning of said first module (3) in two directions (f 1, f2) substantially perpendicular between them and to said longitudinal axis (X) of said first module.
    [4" id="c-fr-0004]
    4. Device (10) according to one of the preceding claims, characterized in that said suspension and displacement means comprise at least one hoist (21) which is attached to a beam (20) and which is capable of being moved the along this beam defining said axis of movement (Z).
    [5" id="c-fr-0005]
    5. Device (10) according to one of the preceding claims, characterized in that said first module (3) is the module comprising said housing (6).
    [6" id="c-fr-0006]
    6. Device (10) according to the preceding claim, characterized in that said transmitter (30) is housed in said housing (6) of said first module (3).
    [7" id="c-fr-0007]
    7. Method for assembling a turbomachine (1), by means of a device (10) according to one of the preceding claims, comprising the steps of:
    a) positioning of said first module (3) on said support means (11),
    b) fixing of said target (40) to said suspension and displacement means,
    c) determination of a first axial position (P1) of said target, for which a task (41) of said laser beam (31) is located in the center of said target,
    d) displacement of said target along said axis of displacement (Z), and
    e) determining a second axial position (P2) of said target, for which a spot of said laser beam is located on the center of said target, in order to validate the parallelism between said longitudinal axis (X) of said first module and said axis of displacement.
    [8" id="c-fr-0008]
    8. Method according to the preceding claim, in which it comprises the following steps:
    f) disassembly of said target (40) from said suspension and displacement means,
    g) fixing of said second module (4) to said suspension and displacement means, and
    h) insertion of said first and second modules (3, 4) one into the other, by displacement of said second module along said axis of displacement.
    [9" id="c-fr-0009]
    9. The method of claim 7 or 8, wherein said first axial position (P1) is located near said first module (3).
    [10" id="c-fr-0010]
    10. Method according to one of claims 7 to 9, in which it comprises, between steps d) and e), sub-steps of:
    - verification of the position of said task (41) on said target (40), and
    - adjustment of the position of said first module (3) so that said task
    5 is located in the center of said target.
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    同族专利:
    公开号 | 公开日
    US20210148253A1|2021-05-20|
    FR3068078B1|2021-06-25|
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    CN110785551A|2020-02-11|
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    引用文献:
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    EP1752409A2|2005-08-12|2007-02-14|United Technologies Corporation|Assembly apparatus with four rails and method|
    KR20130078698A|2011-12-30|2013-07-10|두산중공업 주식회사|A measuring apparatus for rotor alignment of driving portion and passive portion at a gas turbine engine|
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    DE102015214667A1|2015-07-31|2017-02-02|MTU Aero Engines AG|Assembly system for mounting, demounting and / or servicing a gas turbine|
    FR2890110B1|2005-08-26|2007-11-02|Snecma|METHOD FOR ASSEMBLING A TURBOMACHINE|GB201901396D0|2019-02-01|2019-03-20|Rolls Royce Plc|System and method for assembling components of a gas turbine engine|
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    FR3111831A1|2020-06-24|2021-12-31|Safran Aircraft Engines|LASER POSITIONING DEVICE FOR TURBOMACHINE|
    法律状态:
    2018-12-28| PLSC| Search report ready|Effective date: 20181228 |
    2020-05-20| PLFP| Fee payment|Year of fee payment: 4 |
    2021-05-19| PLFP| Fee payment|Year of fee payment: 5 |
    优先权:
    申请号 | 申请日 | 专利标题
    FR1755886A|FR3068078B1|2017-06-27|2017-06-27|DEVICE AND METHOD FOR ASSEMBLING A TURBOMACHINE|
    FR1755886|2017-06-27|FR1755886A| FR3068078B1|2017-06-27|2017-06-27|DEVICE AND METHOD FOR ASSEMBLING A TURBOMACHINE|
    PCT/FR2018/051478| WO2019002725A1|2017-06-27|2018-06-20|Method for assembling a turbomachine|
    US16/626,856| US20210148253A1|2017-06-27|2018-06-20|Method for assembling a turbomachine|
    EP18737695.9A| EP3645847B1|2017-06-27|2018-06-20|Method for assembling a turbomachine|
    CN201880042182.5A| CN110785551A|2017-06-27|2018-06-20|Method for assembling a turbomachine|
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