• 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 device for assembling a turbomachine, intended to center a shaft (4) of a second module with respect to a longitudinal axis (X) of a hollow central hub (21) placed in front of a first module (5), said first module (5) having a longitudinal cavity (20) along said axis (X), opening forwards into said hollow hub (21) and passing through the first module (5) along the axis longitudinal (X) to a rear end, said shaft (4) to be inserted into said longitudinal cavity (20) by said rear end, comprising a central axis centering element (21) configured to be in place in said hollow hub (21) by inserting it by a first of its ends (26 ') and cooperating with the latter to make its central axis coincide with said longitudinal axis (X), characterized in that it further comprises a guide tube (36) configured to enter at least a portion of the cavity longitudinal direction (20) of the first module (5), behind the hollow hub (21), and in that the device is arranged so that the guide tube (36) slides inside the centering element ( 25) along said central axis, between a first position, in which the guide tube (36) is entirely on the side of the centering element (25) with respect to said first end (26 '), and a rear position in which the guide tube (36) protrudes from said first end (26 ') so as to penetrate into the longitudinal cavity (20) when the centering element (25) is put into place in the hollow hub (21). ). The invention also relates to the assembly formed by the device and a calibration dummy, and a method of assembly using it.
    公开号:FR3072137A1
    申请号:FR1759371
    申请日:2017-10-06
    公开日:2019-04-12
    发明作者:Fernand Gastal Thierry；Bryan Antony Creuset Morgan；Louis Charles Petit Eric
    申请人:Safran Aircraft Engines SAS；
    IPC主号:
    专利说明:

    The invention relates to a device for assembling a turbomachine, intended to center a shaft (4) of a second module relative to a longitudinal axis (X) of a hollow central hub (21) placed in front of 'a first module (5), said first module (5) comprising a longitudinal cavity (20) along said axis (X), opening forward in said hollow hub (21) and passing through the first module (5) along the axis longitudinal (X) to a rear end, said shaft (4) to be inserted into said longitudinal cavity (20) by said rear end, comprising a centering element (21) with a central axis, configured to be put in place in said hollow hub (21) by inserting it by a first of its ends (26 ') and cooperating with the latter to make its central axis coincide with said longitudinal axis (X), characterized in that it further comprises a guide tube (36) configured to be able to enter at least part of the cav longitudinal ity (20) of the first module (5), behind the hollow hub (21), and in that the device is arranged so that the guide tube (36) slides inside the centering element ( 25) along said central axis, between a first position, in which the guide tube (36) is entirely on the side of the centering element (25) relative to said first end (26 '), and a rear position , in which the guide tube (36) protrudes from said first end (26 '), so as to penetrate into the longitudinal cavity (20) when the centering element (25) is placed in the hollow hub (21 ). The invention also relates to the assembly formed by the device and a calibration dummy, as well as to an assembly method using it.

    Device for assembling a turbomachine, and method using the device
    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 twin-body turbojet engine, with a front fan for example, comprises a high pressure body, called the HP body, and a low pressure body, called the BP body. The BP body, downstream of the HP body, rotates at a first speed and includes a low pressure turbine which drives the front fan. In this document, the upstream and downstream, respectively the front and the rear, are defined with respect to the general direction of the gas flow in the turbojet engine. The HP body rotates at a different speed from that of the low pressure 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 behind the turbine and in front of the high pressure compressor. The HP body shaft is guided in rotation by bearings supported by the fixed structure of the motor. In the type of turbojet engine concerned by the invention, there is no bearing at the rear of the HP body connecting the HP body shaft and the BP body shaft. The BP body shaft therefore freely crosses the HP body forward until it is held by the upstream bearings.
    Figure 1 shows a turbomachine of this type during assembly. This is a double-flow, double-body turbojet engine, comprising a front fan body 1, an HP body 2 with its shaft, not visible in FIG. 1, and the BP module 3, with its shaft 4, known as BP tree. The front fan body 1 and the HP body 2 are already assembled and form a module 5, called the first module. In the figure, we are in the process of docking the BP module 3 on the first module 5.
    By the term docking, here is meant all or part of the translational movement, along the longitudinal axis X of the first module 5, of the BP module 3 until the flange 6 of the outer casing thereof comes in contact with the corresponding flange 7 of the HP body 2.
    During the docking operation, the shaft BP 4 must pass through the body HP 2 without contact, typically with a minimum clearance of 0.5 mm at the level of the shaft, to guarantee that the anticorrosion coating of the shaft BP or the interior of the first module is not damaged, and a clearance of 0.08 mm at the level of the labyrinths. The labyrinths, not shown in FIG. 1, are sealing devices placed between the HP body 2 and the BP body 3, each comprising a rotating element with the HP body shaft and a rotating element with the BP shaft. These elements are assembled during docking, when the flanges 6 and 7 of the HP body 2 and the BP body 3 are in contact.
    In the example of FIG. 1, the docking is carried out horizontally. The first module 5 is suspended from a gantry 8 by means of a swing 60 so that its longitudinal axis X is horizontal. It can also be held by a cart or pedestal.
    The BP module 3, fixed to a lifter 12, is moved along the longitudinal axis X by means of a hoist 9 fixed movably to the gantry 8, to pass through the first module 5 until it comes into contact with the two flanges 6 and 7.
    In known manner, a shaft guide 10 is fixed at the end of the BP shaft 4 so as to extend it forward. This shaft guide 10 is thinner than the BP shaft 4 and can progress inside the first module 5 until it reaches a centralizer 11 placed at the front of the first module 5. Once in the centralizer 11, the guide shaft 10 can guide the progression of shaft BP 4 along the longitudinal axis X.
    During the progression of the shaft guide 10 and of the BP shaft 4 until the coupling of the flanges 6 and 7, it is necessary to ensure the precision of the guidance so that contacts of these elements with those of a internal part of the first module 5 does not lead to the degradation of the coating paint ensuring the non-corrosion of the material of the parts or of the shaft, or that the labyrinths are not damaged, or that too strong stresses are applied.
    However, the BP 3 module is heavy (typically 1200 kg) and the risk of rocking and misalignment of the BP 4 shaft during docking is major.
    Each pulse of the hoist 9 causes an uncontrolled movement of the BP module 3 by a swing effect. There is also a risk of misalignment in the vertical axis RZ (connection between the gantry 8 and the swing 60) by the mechanical play of the swing 60 supporting the module 5 and a risk of misalignment in the transverse horizontal axis Y, by the play between the module 5 holding pins and the swing 60.
    This leads to using, for centering, fairly heavy devices and long procedures including numerous manipulations to regularly correct the alignment of modules 5 and 3.
    There is therefore a need to have a tool making it possible to comply with the centering constraints while remedying the aforementioned problems.
    In addition, such a tool must be usable on different means of carrying the modules of the turbojet engine, whether in new assembly or repair.
    It is also interesting that the tooling makes it possible to carry out the compaction function of the BP module 3 on the first module 5 during docking, then a function of extracting the BP module 3 with its shaft 4, for example during '' disassembly for repair operations.
    Statement of the invention:
    To this end, the invention relates to a device for assembling a turbomachine, intended to center a shaft of a second module relative to a longitudinal axis of a hollow central hub placed in front of a first module, said first module comprising a longitudinal cavity along said axis, opening forward in said hollow hub and passing through the first module along the longitudinal axis to a rear end, said shaft to be inserted into said longitudinal cavity by said rear end, comprising a central axis centering element, configured to be placed in said hollow hub by inserting it by a first of its ends and cooperating with the latter to make its central axis coincide with said longitudinal axis, characterized in that it further comprises a guide tube configured to be able to enter at least part of the longitudinal cavity of the first module, at a rear of the hollow hub, and in that the device is arranged so that the guide tube slides inside the centering element along said central axis, between a first position, in which the guide tube is entirely of side of the centering element with respect to said first end, and a rear position, in which the guide tube projects from said first end, so as to enter the longitudinal cavity when the centering element is placed in the hollow hub.
    The first position of the guide tube makes it possible to insert the centering element in the hollow hub without risking damaging an internal coating of the first module by contact with the guide tube. The rear position of the guide tube allows the shaft or a shaft guide placed at the end of the shaft to be searched as far as possible in the second module, to limit the amplitude of the swings during movement. In addition, the additional guide length provided by the guide tube in which the shaft guide can slide makes it possible to obtain precise axial guidance of the shaft. In particular, at the end of docking, this ensures the engagement of labyrinths. The manipulations are thus clearly simplified by avoiding systematic checks of centering.
    Advantageously, in the rear position, the guide tube sinks at least in the middle of the HP body in a turbomachine as described in the introduction.
    Preferably, a first end of the guide tube is adapted to enter the centering element by a second end of the latter, opposite the first end along the central axis, so that the first position of the tube guide corresponds to its separation from the centering element.
    This makes it possible to reduce the weight and size of the element to be introduced first into the hollow hub, by limiting it to the centering element alone, and therefore to facilitate the handling of the different parts of the tooling.
    Advantageously, the centering element comprises first means intended to cooperate by contact with the hollow hub, situated at said first end of the centering element, and second means situated near an end opposite the first end according to the central axis and intended to cooperate by locking, for example a dog clutch, with the hollow hub.
    The distance between the first and second means makes it possible to take advantage of the length of the centering element to obtain the desired precision on the centering. The contact connection on the first end makes it possible to center the centering element and to maintain it in the hollow hub with ease, this end not being visible when the element is inserted. Furthermore, the limitation of the fixing means to only the two ends makes it possible to limit the surfaces to be adapted for the contacts and to treat the rest of the internal surface of the hollow hub with an anti-corrosion coating similar to the rest of the walls of the longitudinal cavity.
    Preferably, the device further comprises a shaft guide arranged to be able to be inserted by a first end into the guide tube and to be fixed to said shaft of the second module by a second end, the device being configured so that the guide tube cooperates with the shaft guide to maintain the latter on the central axis of the device when the shaft guide is moved forward, and the sum of the length of the guide tube and the length of the shaft guide being greater than the extension of the longitudinal cavity of the first module.
    The presence of the shaft guide, with an adequate length, makes it possible to avoid introducing the shaft inside the longitudinal cavity of the first module before the shaft has been correctly centered using the tube guide. This eliminates the risk of contact of the shaft with the walls of the longitudinal cavity in the first module.
    Advantageously, the shaft guide slides inside the guide tube until an axial stop of the shaft guide is in contact with said first end of the guide tube.
    The sliding of the shaft guide in the guide tube makes it easy to center the shaft guide and therefore the shaft during its progression. The stopper prevents the guide tube from coming into contact with the shaft.
    Advantageously, the shaft guide comprises a groove at a given distance from said axial stop and the guide tube comprises openings located substantially at the same distance from its first end, so as to give external radial access to the groove.
    The presence of the groove makes it possible to grip the tree guide to exert a longitudinal force during phases of docking where it is desired to compact the second module on the first module.
    Preferably, the device comprises longitudinal clamping means fixed to the centering element by a second end of the latter opposite to its first end, said clamping means comprising axial pins adapted to pass through the openings of the guide tube and to cooperate with the groove of the shaft guide in order to apply to the latter a force along the central axis.
    Advantageously, the clamping means are supported by a part which can be detached from the centering element.
    This makes it possible to limit the weight of the centering element when it is manipulated to install it in the hollow hub.
    Preferably, the device further comprises an element configured to be fixed to the centering element or a clamping element fixed to the centering element and a casing element of the first module, so as to prevent rotation of the device around the longitudinal axis.
    The invention also relates to a method for assembling a turbomachine using a device according to the preceding description, the turbomachine comprising at least a first module comprising a longitudinal cavity, opening out in a hollow hub and passing through the first module along an axis. longitudinal of the hollow hub to a rear end, and at least a second module with a shaft, said shaft to be engaged in said longitudinal cavity by said rear end to an assembly position, characterized in that it comprises the following steps:
    installation of the centering element in the hollow hub, the guide tube being in the first position or absent from the centering element;
    sliding the guide tube through the centering element to the rear position;
    docking of the second module to a position where a free end of the shaft or a shaft guide fixed to the shaft enters the rear end of the guide tube, so that the guide tube guides the shaft along the longitudinal axis of the hollow hub;
    longitudinal translation of the second module with a progression of the shaft centered on the longitudinal axis of the hollow hub by the guide tube, to the assembly position.
    As indicated previously, the modules can be other than those described in the introduction and the hollow hub can be a fixed or movable part in rotation.
    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 shows a turbomachine during the docking of a second module on a first module;
    FIG. 2 shows a longitudinal section of a first turbomachine module equipped with a tool according to the invention, with the shaft guide of FIG. 6 introduced at the rear;
    FIG. 3 shows a perspective view of a centering element belonging to the tool according to the invention:
    Figure 4 schematically shows the manipulation of the centering element of Figure 3 with a manipulation tool;
    Figure 5 shows in perspective a guide tube belonging to I Tooling according to the invention;
    Figure 6 shows in perspective a shaft guide used in the tooling according to the invention;
    Figure 7 shows in perspective a compacting key used in the tooling according to the invention;
    Figure 8 shows in perspective a detail of the fixing of the tamping key of Figure 7 on the centering element of Figure 3;
    Figures 9 and 10 show in perspective two positions of the guide tube of Figure 5 relative to the assembly formed of the centering member of Figure 3 and the packing key of Figure 7;
    Figure 11 shows an anti-rotation bar used in the tooling according to the invention;
    Figure 12 shows, with a longitudinal section, the result of a step of the method according to the invention in which the centering element of Figure 3 was installed on the first module of the turbomachine;
    Figure 13 shows the result of a process step according to the invention in which the tamping key of Figure 7 was installed on the centering element mounted as shown in Figure 12;
    Figure 14 shows a step in the method according to the invention in which the guide tube of Figure 5 is installed in the compacting key and the centering element mounted as shown in Figure 13;
    Figure 15 shows a step in the method according to the invention in which the anti-rotation bar of Figure 11 is installed on the elements of the tooling according to the invention mounted as shown in Figure 14;
    FIG. 16 shows, with a longitudinal section, the result of a step of the method according to the invention in which the shaft guide of FIG. 6 has passed through the elements of the tooling according to the invention forwards after having been introduced as shown in Figure 2;
    FIG. 17 shows a detail of FIG. 16 at the level of the interaction between the shaft guide of FIG. 6 and the settlement key of FIG. 7.
    Description of an embodiment:
    The tool according to the invention is intended to be able to be used in particular during an assembly phase illustrated in FIG. 1, already described in the introduction. Before describing the tool and how to use it, it is necessary to succinctly specify the type of turbomachine to which it applies.
    FIG. 2 shows the first module 5 as defined above, that is to say the upstream fan body 1 and the HP body 2 assembled, with the tooling installed for an assembly phase. The first module 5 comprises a fixed structure 13, here called the first casing, which supports the rotating parts 14 of the HP body 2, here the high pressure compressor 15 and the high pressure turbine 16, as well as the rotating parts 17 of the blower body upstream 1, intended to be driven by the BP shaft 4, here the blower 18 and the low pressure compressor 19. The BP module 3 is not shown in the figure. Only the front end of the low shaft BP 4 is shown, outside the rear of the first module 5.
    The elements of the first module 5 provide a longitudinal cavity 20, centered on the axis X of symmetry of the first module 5 and which passes right through it. In front of the module 5, the longitudinal cavity 20 ends in a hollow hub 21, which here is integral with the rotating parts 17 of the upstream fan body 1. Behind the hollow hub 21, coupling means 22 of these rotating parts 17 with the BP shaft 4 are installed in the longitudinal cavity 20. Behind these coupling means 22, the minimum diameter of the longitudinal cavity 20 is substantially greater than that of the BP shaft 4, so as to allow it to pass without friction. There is no bearing now the BP shaft in the longitudinal cavity 20 of the first module 5, between said coupling means 22 to the rotating parts of the upstream fan body 1 and the rear of the HP body 2. It will be noted here that the surfaces of the parts of the first module 5 delimiting the longitudinal cavity 20 are treated with an anti-corrosion coating which can be altered in the event of contact during the passage of the BP shaft 4 or of a shaft guide 10, during the mounting.
    The hollow hub in front of the coupling means has a significant longitudinal extension Lm. In the example, this extension Lm is at least as large as that of the mobile wheel of the fan 18. The internal part of the body of the hollow hub 21 is cylindrical, of diameter substantially larger than that of the longitudinal cavity 20 at the level said coupling means 22. The internal part of the hollow hub comprises, at its end opening onto the front, slots 23 intended to form the first elements of a connection by dog clutch with a part coming to be fixed at this location. The rear end of the internal part of the hollow hub 22 has a contact surface 24, here substantially cylindrical, intended to form a support for a part which is housed inside this contact surface to be centered on the axis longitudinal X. The geometries of the contact surface 24 and of the square elements 23 of the clutch connection are defined in connection with the longitudinal extension Lm of the hollow hub 21 so that the longitudinal axis X 'of a fixed part between these two means coincides with the longitudinal axis X of the first module 5 according to the precision required for the mounting operations. With reference to the figures cited in the introduction, this precision typically corresponds to a minimum clearance of 0.5 mm at the level of the BP 4 shaft and a clearance of 0.08 mm at the level of the labyrinths.
    It will also be noted that the internal surface of the hollow hub 21 is treated, like the whole of the longitudinal cavity 20 with an anticorrosion coating, with the exception of the elements 23 of the dog clutch and the contact surface 24. The elements 23 of the dog clutch are formed from aluminum. The contact surface 24 is covered with a material called "synthetic metal", formed from intrinsically conductive polymers.
    The tool according to the invention comprises several elements cooperating during the successive stages of docking but separable from each other.
    The first element 25, called the centering element, is a part intended to be installed in the internal part of the hollow hub 21, so as to center the other elements and the BP shaft 4 on the longitudinal axis X of the first module 5. With reference to FIG. 3, it is a tubular part of revolution around an axis X ′, having a cylindrical interior cavity, with a diameter De of value less than the smallest value of the diameter of the cavity central 20 of the first module 5. The central body of the element 25 has an outside diameter substantially smaller than that of the internal surface of the hollow hub 21. The element 25 comprises, at a longitudinal end 26 ′, an external contact surface 26 substantially cylindrical and of diameter equal to that of the contact surface 24 in the hollow hub 21 of the first module 5, and, at the opposite end, slots 27 forming interconnected connecting elements shaped in. ur cooperate with the slot elements 23 of the hollow hub 21, in order to form a dog clutch. These two means 26, 27 are spaced along the longitudinal axis X 'by a distance substantially equal to that existing between the corresponding means 23, 24, on the hollow hub 21 along the longitudinal axis X. In this way, the the centering element 25 can be inserted from the front of the first module 5 into the hollow hub 21 so that, when the clutch connection is formed between the corresponding elements 23 and 27, the contact surface 24 of the interior of the hub those 21 and that 26 of the exterior of the centering element 25 are in contact, maintaining the latter in a position where its axis X 'coincides with the longitudinal axis X of the first module 5 according to the desired precision.
    The contact surface 26 of the centering element 25 is treated with the same material called "synthetic metal" as the contact surface 24 of the hollow hub
    21. The means 27 cooperating with those 23 of the hollow hub 21 for the clutch connection are here made of aluminum, like the latter. As can be seen in FIG. 3, the slots 27 have stops 28 in rotation to stop the slots 27 of the centering element 25 opposite those of the slots 23 of the hollow hub 21 when the dog clutch is formed.
    The centering element 25 also includes a head, placed at its end in front of the means for the clutch connection. This head is intended to remain outside the hollow hub. It comprises radial arms 29 shaped to be able to be gripped by hand and exert a rotational force in order to lock the clutch connection, once the slots 27 are engaged behind those 23 of the corresponding means on the hollow hub 21. The head has also at its free end, in this example, a flat disc 30 carrying longitudinal pins 31 threaded circumferentially, and an external notch 32 at the periphery. This assembly forms means arranged to cooperate with those of a second part, described below, and form between them a "quarter-turn" connection which secures said second part to the centering element.
    Advantageously, the weight of the centering element 25 is limited so that it can be handled by a single operator. However, taking into account the constraints that it must bear, this weight, typically 12 kg, can cause significant leverage when it comes to holding the element by one end to introduce it into the hollow hub 21. Advantageously , with reference to FIG. 4, a complementary manipulation tool 33 can be used. It is a tool comprising a longitudinal rod 34 designed to be inserted inside the centering element 25, comprising at its end two arms 35 extending radially and intended for gripping. As shown in FIG. 4, the manipulation tool 33 makes it easy to keep the centering element 25 substantially horizontal in order to introduce it into the hollow hub 21.
    With reference to FIG. 5, the second element of the tool is a guide tube 36 arranged to slide inside the cylindrical cavity of the centering element 25 while remaining in contact therewith, so as to move longitudinally while remaining centered on the axis X 'of the first element 25. The outside diameter of the body of the guide tube 36 is therefore equal to that of the cylindrical cavity of the centering element 25. In addition, the one of its ends, called the rear end 37 has an outside diameter less than or equal to the tubular body, so that the guide tube 36 can be introduced into the centering element 25 by the front end of the latter. The guide tube 36 has a length Ltg defined so that it substantially protrudes from the rear end of the centering element 25 when it is slid backwards and that its opposite end, or front end, exceeds 1 'front end of the centering element 25. In the example considered, the length Ltg of the guide tube 36 is substantially greater than the distance separating the front end of the first module 5 and the front of the body HP 2, so as to approach the rear end of the first module 5.
    The guide tube 36 is hollow, of diameter Dtg, so as to receive by its rear end 37 a rod which slides therein so as to remain centered on the longitudinal axis X ”of the guide tube 36. The front end of the tube guide 36 here comprises a ring 38 of diameter greater than that of the tube, so as to form a longitudinal stop on the guide tube 36. At a determined distance Lta from its rear end 37, the guide tube 36 has slots 39 transverse , arranged to allow pins to pass radially.
    Advantageously, to avoid driving the BP shaft 4 into the first module 5, a shaft guide element 40, shown in FIG. 6, is intended to be fixed to said BP shaft
    4. The shaft guide 40 forms a rod adapted to be inserted by a front end 41 into the rear end 37 of the guide tube 36 and to slide inside the latter while remaining centered on its axis X ". Its rear end has a head 42 adapted to be fixed to the front of the BP shaft 4 and has an axial stop 43 intended to block the sliding of the shaft guide 40 in the guide tube 36. The length Lga of the shaft guide 40 , in correspondence with the design of the guide tube 36, is defined so that the length Ltg of the guide tube 36 added to that Lga of the shaft guide 40 is substantially greater than that of the first module 5 along the axis longitudinal X, so that the head 42 of the rear end of the shaft guide 40 protrudes from the rear end of the first module 5 while the front end 38 of the guide tube 36 protrudes from the front of the first module 5, when these elements are placed end to end in the longitudinal cavity 20. In addition, the shaft guide 40 has a groove 44 intended to cooperate with radial pins to block its longitudinal movement. This groove 44 is at a distance from the axial stop 43 substantially equal to that Lta which separates the lights 39 from the guide tube 36 from the rear end 37 of the latter, so that the groove 44 and the lights 39 are in correspondence when the shaft guide 40 comes into abutment on the rear 37 of the guide tube 36 and the lights 39 allow passage from the outside of the radial pins to the groove 44. It will be noted that this distance is substantially greater to the longitudinal extension of the centering element 25 so that the groove protrudes from the latter from the front when the shaft guide 40 is slid towards the front of the first module until its rear head 42 position behind the centering element 25 and brings the BP shaft 4 in front of the coupling means 22 with the rotating elements 17 of the front fan module 1. In this case, said pins supposed to block the axial movement of the g uid shaft 40 can be inserted from the outside of the centering element 25, in front of the first module 5.
    Advantageously, the tool also includes a so-called compacting key element 45 which is fixed to the front of the centering element 25 by the quarter-turn connection indicated above with the longitudinal pins 31 threaded. The tubular body 46 is then centered on the central axis X 'of the centering element 25. With reference to FIG. 7, this element 45 comprises a tubular body 46 supporting circumferential slots 47 arranged to cooperate with the longitudinal pins 31 of the front head 30 of the centering element 25, to form the quarter-turn connection, as shown in FIG. 8. With reference to FIG. 8, the compacting key 45 also includes an anti-rotation finger 48 which is engaged in the outer notch 32 of the centering element 25 when the longitudinal pins 31 are correctly positioned in the circumferential slots 47. The quarter-turn connection is then locked by nuts 49 tightened on the threaded longitudinal pins 31.
    The tubular body 46 of the compacting key 45 supports a capstan 50 with radial arms 51 arranged to be turned manually. The rotation of the capstan 50 allows it to impart a longitudinal movement forward or backward along the central axis X ’, relative to the tubular body 46.
    The tubular body 46 and the capstan 50 are designed to leave free a longitudinal cavity in the axis X ’of the centering element 25 and of sufficient diameter to allow the guide tube 36 to pass.
    The front end of the capstan 50 carries a system here comprising two pins 52 which are radially movable and which can be placed either in a "withdrawn" position, where they are at a distance from the central axis X 'equal to half the diameter of the central cavity of the centering element and leave the central longitudinal cavity free, either in an "engaged" position where they can be inserted into the groove 44 of the shaft guide 40 to block it longitudinally. The pins 52 are completed by a mechanical system 53 enabling them to be locked in order to exert a radial force on the external surface of the guide tube 36.
    Advantageously, the body 46 of the compacting key 45 comprises longitudinal slots 54 which make it possible to monitor the progress of the shaft guide 36 in the compacting key.
    In the example, the compacting key 45 is designed with a sufficiently low weight, typically 4 kg, to be able to be easily handled when it is fixed to the centering element 25.
    When the compacting key 45 is assembled with the centering element 25 and the pins 52 are in the withdrawn position, the assembly therefore forms a member through which the guide tube 36 and the shaft guide 40 can slide longitudinally, the along the axis X 'of the centering element 25. If we consider in particular the guide tube 36, the latter, once introduced at the front of this member by its rear end 37, may be in two remarkable positions between which it can slide. In a first position, called the waiting position, illustrated in FIG. 9, it is held in the member but its rear end does not protrude from the rear end 26 'of the centering element 25. In a second position , illustrated in FIG. 10, the guide tube 36 protrudes from the rear end 26 ′ of the centering element 25 and its head 38 located at the front end is in abutment on the pins 52 of the compacting key. 45. It will be noted that the guide tube 36 can be blocked in this position by tightening the pins 52 on its external surface by the mechanical means 53 provided for this purpose.
    Preferably, the hollow hub 21 on which the centering element 25 is to be fixed being movable in rotation, the tooling further comprises an element 55 preventing the rotation of the assembly. With reference to FIG. 11, this anti-rotation element 55 is here composed of a removable transverse bar 56. As illustrated in FIG. 15, the anti-rotation bar 56 has at one end a fixing 57 arranged to receive a pin 58 provided for this purpose on the compacting key 45 and, at its other end, a clamp 59 intended to hook the casing 13, at the periphery of the fan 18.
    Such a tool can be used to ensure correct centering of the second module 3 during docking in the first module 5. FIG. 1 described above illustrates an assembly in which the first module 5 is kept fixed, here under a gantry 8, with its longitudinal axis X horizontally and the second module 3 is held by a hoist 9 supported by said gantry 8, movable in translation so as to achieve docking.
    Preferably, the mounting method according to the invention begins with the equipment of the first module 5 with the corresponding elements of the tooling, the first module 5 being held horizontally under the gantry.
    In a first step, the centering element 25 is installed in the hollow hub 21 at the front of the first module 5. For this, the operator installs the handling tool 33 described above as shown in Figure 4 and introduced horizontally the centering element 25 in the hollow hub 21 until the slots 27 of the element pass through the corresponding slots 23 of the dog clutch on the hollow hub and that the contact surface 26 of the centering element 25 presses on the contact surface 24 of the hollow hub 21. Then, after removing the handling tool 33, the operator rotates the centering element 25 around the longitudinal axis X using the radial arms 29, until the stops 28 of the clutch connection block the movement. At the end of this step, as illustrated in FIG. 12, the centering element 25 is therefore fixed in the hollow hub 21 by the clutch connection with support of the contact surfaces 24, 26 and its longitudinal axis X 'coincides with the longitudinal axis X of the hollow hub 21.
    In a second step, the compacting key is installed on the centering element by locking the quarter-turn link 30, 31, 47, described above. At the end of this step, as illustrated in FIG. 13, the assembly formed by the centering element 25 and the compacting key 45 is fixed to the front of the hollow hub 21.
    In a third step, with reference to FIG. 14, the operator engages the guide tube 36 through its rear end 37 in the assembly formed by the centering element 25 and the compacting key 45, up to 1 'install in the waiting position described in figure 9.
    In a fourth step, the anti-rotation bar 56 is installed as illustrated in FIG. 15. It is first engaged in the corresponding pin 58 of the compacting key 45, then fixed at the periphery of the casing 13 by its clamp 59.
    In a fifth step, the guide tube 36 is slid backwards into the second position described in FIG. 10, with its head 38 in abutment on the pins 52 of the compacting key 45. The latter are supported on its outer surface, so as to block a sliding of the guide tube 36 forwards. At the end of this step, as illustrated in FIG. 2, the first module is equipped, ready to receive the shaft guide 40 for docking the second module 3.
    In a step which can be carried out in parallel with the preceding steps, the shaft guide 40 is fixed by its rear end to the front end of the BP shaft 4, of the second module 3.
    In a sixth step, illustrated in FIG. 1, the second module 3, supported here by a mobile hoist 9, is presented horizontally in front of the back of the first module
    5. An operator monitors and assists in the introduction of the shaft guide 40 into the longitudinal cavity 20 of the first module 5, so that the shaft guide 40 progresses horizontally in the longitudinal cavity 20 until its front end 41 enters the guide tube 36. As illustrated in FIG. 2, the shaft guide 40 is then centered on the longitudinal axis X of the first module 5 by the guide tube even though the shaft BP 4 of the second module 3 is not still inserted into the longitudinal cavity 20. Then the shaft guide 40 slides in the guide tube 36 until its axial stop 43 reaches the rear end 37 of the guide tube 36.
    In a seventh step, the pins 52 which block the guide tube 36 are unlocked and the second module 3 is advanced forward while keeping it centered on the longitudinal axis X of the first module 5. The shaft 4 of the second module 3 then pushes the shaft guide 40 and the guide tube 36 forward. The shaft guide being held on the longitudinal axis X by the guide tube 36, the assembly does not risk knocking against the walls of the longitudinal cavity 20 under the effect of swaying due to the progression of the second module 3. The progression is stopped when the groove 44 of the shaft guide 40 is opposite the pins 52 located on the capstan 50 of the packing key 45, as illustrated in FIG. 16. The head of the shaft 4 of the second module 3 is then also engaged in the coupling means 22 with the rotating elements 17 of the front fan module. The pins 52 are then inserted into the groove 44 of the shaft guide 40 to secure the latter with the capstan 50 along the longitudinal axis X, as illustrated in FIG. 17.
    In an eighth step, the last centimeters of longitudinal progression of the shaft 4 and of the second module 3 are made by manually actuating the capstan 50, to insert the head of the shaft in the coupling means 22 of the rotating elements 17 of the module fan before and to control the precise coupling of the elements of the sealing labyrinths at the interface of the first 5 and of the second 3 modules, until the flanges 6, 7, of said modules are fixed together.
    It will be noted here that the compacting key 45 can also be used in the opposite direction, during the disassembly of the engine, to decouple the two modules 3, 5, before separating them.
    The tooling, the elements of which can then be removed from the two modules, has thus made it possible to effect docking while respecting the desired centering precision and avoiding contacts liable to deteriorate elements of one or other of the two modules. As mentioned above, the tool can also be used during disassembly of the turbomachine, to avoid untimely contacts during the translation of the second module 3 relative to the first module 5.
    权利要求:
    Claims (10)
    [1" id="c-fr-0001]
    claims
    1. Device for assembling a turbomachine, intended to center a shaft (4) of a second module (3) relative to a longitudinal axis (X) of a hollow central hub (21) placed in front of 'a first module (5), said first module (5) comprising a longitudinal cavity (20) along said axis (X), opening forward in said hollow hub (21) and passing through the first module (5) along the axis longitudinal (X) to a rear end, said shaft (4) to be inserted into said longitudinal cavity (20) by said rear end, comprising a centering element (21) with central axis (X '), configured to be placed in said hollow hub (21) by inserting it by a first of its ends (26 ') and cooperate with the latter to make its central axis (X') coincide with said longitudinal axis (X), characterized in which it further comprises a guide tube (36) configured to be able to enter at least u part of the longitudinal cavity (20) of the first module (5), behind the hollow hub (21), and in that the device is arranged so that the guide tube (36) slides inside the centering element (25) along said central axis (X '), between a first position, in which the guide tube (36) is entirely on the side of the centering element (25) relative to said first end ( 26 '), and a rear position, in which the guide tube (36) protrudes from said first end (26'), so as to enter the longitudinal cavity (20) when the centering element (25) is put in place in the hollow hub (21).
    [2" id="c-fr-0002]
    2. Device according to the preceding claim, characterized in that a first end (37) of the guide tube (36) is adapted to enter the centering element (25) by a second end (30) of the latter, opposite the first end (26 ') along the central axis (X'), so that the first position of the guide tube corresponds to its separation from the centering element (25).
    [3" id="c-fr-0003]
    3. Device according to one of the preceding claims, wherein said centering element (25) comprises first means (26) intended to cooperate by contact with the hollow hub (21), located at said first end (26 ') of the centering element, and second means (27) located near an end (30) opposite the first end (26 ') along the central axis (X'). and intended to cooperate by locking, for example a clutch connection, with the hollow hub (21)
    [4" id="c-fr-0004]
    4. Device according to one of the preceding claims, further comprising a shaft guide (40) arranged to be inserted by a first end (41) in the guide tube (36) and to be fixed to said shaft (4) of the second module (3) by a second end (42), the device being configured so that the guide tube (36) cooperates with the shaft guide (40) to hold the latter on the central axis (X ') of the device when the shaft guide (40) is translated forward, and the sum of the length (Ltg) of the guide tube (36) and the length (Lga) of the shaft guide (40) being greater than the extension of the longitudinal cavity (20) of the first module (5).
    [5" id="c-fr-0005]
    5. Device according to the preceding claim, configured so that the shaft guide (40) slides inside the guide tube (36) until an axial stop (43) of the shaft guide (40) is in contact. with said first end (37) of the guide tube (36).
    [6" id="c-fr-0006]
    6. Device according to the preceding claim, wherein the shaft guide (40) comprises a groove (44) at a given distance (Lta) from said axial stop (43) and the guide tube (36) comprises lights (39) located substantially at the same distance (Lta) from its first end (37), so as to give external radial access to the groove (44).
    [7" id="c-fr-0007]
    7. Device according to the preceding claim, characterized in that it comprises longitudinal clamping means (45) fixed to the centering element (25) by a second end (30) of the latter opposite to its first end (26 '), said clamping means comprising axial pins adapted to pass through the openings (39) of the guide tube (36) and cooperate with the groove (44) of the shaft guide (40) in order to apply a force to the latter along the central axis (X ').
    [8" id="c-fr-0008]
    8. Device according to the preceding claim, characterized in that the clamping means are supported by a part which can be detached from the centering element (25).
    [9" id="c-fr-0009]
    9. Device according to one of the preceding claims comprising an element (55) configured to be fixed to the centering element (25) or a clamping element (45) fixed to the centering element (25) and an element casing (13) of the first module (5), so as to prevent rotation of the device around the longitudinal axis (X).
    [10" id="c-fr-0010]
    10. A method of assembling a turbomachine using a device according to one of the preceding claims, the turbomachine comprising at least a first module (3) comprising a longitudinal cavity (20), opening out forwards in a hollow hub (21) and passing through the first module (5) along a longitudinal axis (X) of the hollow hub (21) to a rear end, and at least a second module (3) with a shaft (5), said shaft (5) in front be inserted into said longitudinal cavity (20) by said rear end to an assembly position, characterized in that it comprises the steps:
    installation of the centering element (25) in the hollow hub (21), the guide tube (36) being in the first position or absent from the centering element (25);
    sliding the guide tube (36) through the centering member (21) to the rear position;
    docking of the second module (3) to a position where a free end of the shaft (4) or a shaft guide (40) fixed to the shaft (4) enters the rear end (37) of the tube guide (36), so that the guide tube (40) guides the shaft along the longitudinal axis (X) of the hollow hub 5 (21);
    longitudinal translation of the second module (3) with a progression of the shaft (4) centered on the longitudinal axis (X) of the hollow hub (21) by the guide tube (40), to the assembly position .
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    同族专利:
    公开号 | 公开日
    WO2019068985A1|2019-04-11|
    EP3692247A1|2020-08-12|
    FR3072137B1|2020-07-24|
    CA3077557A1|2019-04-11|
    US20200230754A1|2020-07-23|
    RU2020112947A|2021-11-08|
    EP3692247B1|2021-10-27|
    RU2020112947A3|2022-02-24|
    CN111164274A|2020-05-15|
    BR112020006591A2|2020-10-06|
    引用文献:
    公开号 | 申请日 | 公开日 | 申请人 | 专利标题
    EP1655457A1|2004-10-29|2006-05-10|General Electric Company|Gas turbine engine and method of assembling same|
    EP1752409A2|2005-08-12|2007-02-14|United Technologies Corporation|Assembly apparatus with four rails and method|
    EP1757777A1|2005-08-26|2007-02-28|Snecma|Method to assemble a turbomachine|
    US20090288291A1|2005-10-28|2009-11-26|Man Turbo Ag|Device for the Lateral Fitting and Removal of a Compressor Barrel|
    FR3016337A1|2014-01-15|2015-07-17|Dcns|MAT STRUCTURE, IN PARTICULAR FOR AN UNDERWATER VEHICLE WITH AN OPTIMIZED HEDGE RACE|
    FR3095492B1|2019-04-26|2021-05-07|Safran Aircraft Engines|TOOL FOR REMOVING A BLOWER DISK FROM A MODULE|
    FR3108660A1|2020-03-24|2021-10-01|Safran Aircraft Engines|Rotating actuator of a turbojet rotor for an inspection and / or maintenance operation|
    CN111376016B|2020-03-31|2021-03-02|中国航发动力股份有限公司|Positioning and guiding tool for low-pressure turbine of engine|
    法律状态:
    2019-04-12| PLSC| Publication of the preliminary search report|Effective date: 20190412 |
    2019-09-19| PLFP| Fee payment|Year of fee payment: 3 |
    2020-09-17| PLFP| Fee payment|Year of fee payment: 4 |
    2021-09-22| PLFP| Fee payment|Year of fee payment: 5 |
    优先权:
    申请号 | 申请日 | 专利标题
    FR1759371|2017-10-06|
    FR1759371A|FR3072137B1|2017-10-06|2017-10-06|DEVICE FOR ASSEMBLING A TURBOMACHINE, AND METHOD USING THE DEVICE|FR1759371A| FR3072137B1|2017-10-06|2017-10-06|DEVICE FOR ASSEMBLING A TURBOMACHINE, AND METHOD USING THE DEVICE|
    RU2020112947A| RU2020112947A3|2017-10-06|2018-09-24|
    PCT/FR2018/052328| WO2019068985A1|2017-10-06|2018-09-24|Device for assembling a turbine engine, and method using the device|
    CA3077557A| CA3077557A1|2017-10-06|2018-09-24|Device for assembling a turbine engine, and method using the device|
    CN201880064345.XA| CN111164274A|2017-10-06|2018-09-24|Apparatus for assembling a turbine engine and method of using the same|
    BR112020006591-9A| BR112020006591A2|2017-10-06|2018-09-24|device for mounting a turbomachinery, and process using the device|
    EP18783069.0A| EP3692247B1|2017-10-06|2018-09-24|Device for assembling a turbine engine, and method using the device|
    US16/652,594| US20200230754A1|2017-10-06|2018-09-24|Device for assembling a turbine engine, and method using the device|
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