• 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 method of assembling (S) a planet carrier (16) comprising the following steps: - to realize (S1) separately the cage (20) and the cage holder (30) by providing an extra thickness at level of one of the following elements: the through holes (23, 25) of at least one upright (21) of the cage (20) or the through hole (32) of a finger (31) of the holder cage (30), and / or at one of the following: a bearing surface (26) or a bearing surface (41, 42), - assembling (S2) the cage (20) and the carrier cage (30) and fix them (S3) so as to produce a one-piece assembly, - determine (S4) a position of a reference axis (Y1, Y2) connected to the cage (20), to the cage carrier (30) ) and / or to the shaft (40) and - taking into account the position of the reference axis (Y1, Y2), machining (S5) all or starting from the extra thicknesses.
    公开号:FR3052213A1
    申请号:FR1655203
    申请日:2016-06-07
    公开日:2017-12-08
    发明作者:Julie Lemoine；Guillaume Julien Beck
    申请人:Hispano Suiza SA；
    IPC主号:
    专利说明:

    Method of assembling a planet carrier
    FIELD OF THE INVENTION The invention relates to the field of turbomachines, and more particularly the reducers of turbofan engines configured to introduce a reduction ratio between the speed of the fan and that of the low pressure turbine.
    BACKGROUND
    A turbofan engine 1 generally comprises, upstream to downstream in the direction of the gas flow, a ducted fan 2 housed in a fan casing, an annular primary flow space and an annular flow space. secondary. The air mass sucked by the fan is thus divided into a primary flow, which flows in the primary flow space, and a secondary flow, which is concentric with the primary flow and flows in the flow space. secondary. The primary flow space passes through a primary body comprising one or more stages of compressors, for example a low-pressure compressor 3a and a high-pressure compressor 3b, a combustion chamber 4, one or more turbine stages, for example a turbine high pressure 5a and a low pressure turbine 5b, and a gas exhaust nozzle.
    Typically, the high-pressure turbine 5a rotates the high-pressure compressor 3b through a first shaft, called the high-pressure shaft, while the low-pressure turbine 5b rotates the low-pressure compressor 3a and the fan 2 by via a second shaft 6, said low pressure shaft. The low pressure shaft 6 is generally housed in the high pressure shaft.
    In order to improve the propulsive efficiency of the turbojet engine 1 and to reduce its specific consumption as well as the noise emitted by the fan 2, it has been proposed turbojet engines having a rate of dilution ("bypass ratio" in English, which corresponds to the ratio between the flow rate of the secondary flow (cold) and the flow rate of the primary flow (hot, which passes through the primary body)) high. By high dilution rate, here will be understood a dilution ratio greater than 10, for example between 12 and 18.
    To achieve such dilution rates, a reduction ratio is introduced between the speed of the fan 2 and that of the low-pressure turbine 5b, thus allowing to independently optimize their respective speed of rotation. This can be achieved in particular by means of a reduction gear 10 such as an epicyclic or planetary reduction mechanism, placed between the upstream end (with respect to the direction of flow of the gases in the turbojet engine 1) of the shaft. 6 blower and the blower 2. The blower 2 is then driven by the low pressure shaft 6 through the reduction mechanism and an additional shaft, said blower shaft 2, which is fixed between the reduction mechanism 10 and the fan disk 2.
    This reduces the rotational speed and the pressure ratio of the fan 2 ("fan pressure ratio" in English), which increases the power extracted by the low-pressure turbine 5b.
    A reduction mechanism 10 usually comprises: - a sun gear 12, centered on the main axis X of the reduction mechanism 10, which drives the low-pressure shaft 6 (input shaft), - a ring gear, centered on the main axis X, - satellites 14, placed between the sun gear 12 and the crown, whose teeth cooperate with those of the sun gear 12 and the ring gear, and - a planet carrier 16, on which the satellites 14 are mounted, generally via satellite bearings 15.
    The crown and the axis of the satellites 14 can be fixed while the planet carrier 16 rotates about the main axis X of the reduction mechanism 10: it is called epicyclic reduction mechanism. In this case, the fan shaft 2 (output shaft) is generally fixed on the planet carrier 16. In a variant, the planet carrier 16 can be fixed, while the planet wheel and the satellites 14 rotate around a planet. respective axis of revolution: this is called a planetary reduction mechanism. In this case, the fan shaft 2 is generally fixed on the ring.
    The planet carrier can be monobloc, or alternatively be in two parts and comprise a cage and a cage-carrier connected together with connection pins which are shrunk on the cage. For this purpose, the cage comprises a series of amounts distributed circumferentially around the axis of revolution of the cage and each having an inner bridge and an external bridge. The inner bridge and the outer bridge are separated by a housing adapted to receive an associated finger of the cage holder. The inner bridge, the external bridge and the finger each comprise coaxial through holes which extend opposite when the cage is mounted on the cage holder. In order to fix the cage on the cage carrier, a connection pin is introduced through these holes by being hooped on the inner bridge and the outer bridge of the cage. A ball is further interposed between the connection axis and the walls of the hole formed in the finger to form a flexible connection decoupling the deformations of the cage carrier and cage that can result from the transmission of torque through the planet carrier and misalignment of the fan.
    The mounting of a two-part planet carrier is however very difficult to achieve because of its hyperstatism resulting from the large number of fingers and bridges to be assembled using the flexible link (= generally equal to the number of satellites) . The bores of the plain bearings in the cage must also be located precisely with respect to the axis of revolution of the cage carrier to ensure proper operation of the teeth of the satellites. It has therefore been proposed to make a very precise rating of the different parts taken separately (with a tolerance of the order of a tenth of a micron) to ensure the assembly of said parts despite the hyperstatism of the planet carrier. Such precision is however very difficult to obtain and involves a significant increase in the cost of manufacturing parts that makes this procedure difficult to implement.
    SUMMARY OF THE INVENTION
    An object of the invention is therefore to allow a mounting of a planet carrier comprising a cage and a cage holder in a precise and robust manner despite its hyperstatism, which is simpler to implement and does not require tolerances of manufacturing as strict as in the prior art.
    For this, the invention proposes a method of manufacturing a planet carrier, said planet carrier having an axis of revolution and comprising: an annular cage comprising: a series of amounts distributed circumferentially around the axis of revolution each upright comprising an inner bridge and an external bridge in each of which a through hole is formed; - bearing spans defining bores configured to receive a landing of a satellite; - an annular cage carrier comprising: a series of fingers axial axes distributed circumferentially around the axis of revolution in each of which is formed a through hole, each axial finger being configured to be housed between the inner bridge and the external bridge of an amount of the cage, a shaft coaxial with the axis of revolution and having at least one bearing surface, said shaft being fixed on the cage carrier, the assembly method comprises nt the following steps: - separately realize the cage and the cage-carrier by providing an extra thickness at one of the following elements: the through orifice of the inner bridge and the through orifice of the external bridge of at least one amount the cage, or the through orifice of at least one finger of the cage holder, and / or at the level of one of the following elements: at least one bearing surface or the at least one bearing surface, assemble the cage and the cage holder by placing each axial finger of the cage holder between an inner bridge and an external bridge of the cage, - position the cage with respect to the cage holder and fix together the cage and the cage holder of in order to produce a one-piece assembly, - to determine a position of at least one reference axis connected to the cage, to the cage holder and / or to the shaft and - taking into account the position of at least one of the reference axes, machining everything or starting with extra thickness to ensure alignment between the through holes of each inner bridge and each external bridge with the through hole of the associated axial finger on the one hand, and / or bearings of the cage with the bearing surface on the other.
    Some preferred but non-limiting characteristics of the manufacturing process are the following, taken individually or in combination: during the step of producing the cage and the cage holder, the extra thickness is formed at the through orifice of the internal bridge and external bridge and / or at the bearing surfaces, the through-hole of the axial fingers and the at least one bearing surface being devoid of excess thickness, - the reference axes comprise an axis of revolution of the through orifice of at least one axial finger of the cage holder and / or a bearing axis, said bearing axis being defined as an axis of symmetry of the at least one bearing surface of the shaft; of revolution and the rolling axis are determined by three-dimensional metrology of the through hole of the axial finger and the at least one rolling surface, respectively, for example by probing, - the cage and the cage carrier each comprise a central bore, said central bores being coaxial with the axis of revolution of the planet carrier, and wherein the assembling step comprises a sub-step during which the cage and the door -cage are positioned so as to axially and radially align their central bore and / or to index them angularly, - the step of assembling the cage and the cage holder is performed by introducing a tool into the central bore the cage and the cage carrier and fixing said tooling in said central bores so as to lock the cage and the cage holder relative to a fixed frame, the tooling comprises: a first support configured to be introduced with adjustment into the central bore of the cage holder and a second support configured to be fit-fitted into the central bore of the cage, and wherein the step of positioning and securing the cage and of the cage carrier comprises the following substeps: (i) determining the dimensions of the central bore of the cage and the central bore of the cage holder, (ii) machining the first support and the second support according to the determined dimensions of the central bore of the cage and the cage holder so as to ensure a fitting assembly of said supports with the corresponding central bore, (iii) introducing the first support and the second support into the central bore of the carrier. cage and in the central bore of the cage, respectively, and (iv) block the cage and the cage holder so as to make them monoblock by fixing the first support relative to the second support, or vice versa, - the method comprises in in addition to a step of fixing the first support and the second support relative to the frame, and / or - the tooling further comprises at least two pins configured to penetrate cavities formed in the cage and / or in the cage holder, and the step of positioning and fixing the cage and the cage holder further comprises a sub-step during which the pins are introduced into the corresponding cavities to angularly index the cage and the cage holder.
    BRIEF DESCRIPTION OF THE DRAWINGS Other features, objects and advantages of the present invention will appear better on reading the detailed description which follows, and with reference to the appended drawings given by way of non-limiting examples and in which:
    FIG. 1 is a sectional view of an exemplary embodiment of a turbomachine comprising a reduction mechanism between the blower of the low-pressure shaft,
    FIG. 2 is a partial exploded view in perspective of an example of a carrier for a reduction mechanism, which can be assembled using an assembly method according to the invention,
    FIG. 3 is a detailed view of a finger of the cage holder of the planet carrier of FIG. 2,
    FIG. 4 is a partial view of the cage of the planet carrier of FIG. 2,
    FIG. 5 is a sectional view of a finger inserted between an internal bridge and an external bridge of the planet carrier of FIG. 2,
    FIG. 6 is a sectional view of the carrier of FIG. 2,
    FIG. 7 is an exemplary embodiment of a tool that can be used in an assembly method according to the invention,
    FIG. 8 is a perspective view of a part of the tool of FIG. 7 positioned on the cage carrier of the planet carrier of FIG. 2, on which a portion has been cut in order to visualize pins introduced into a pre-existing cavity,
    FIG. 9 is a partial perspective view of part of the tool of FIG. 7 positioned on the cage of the planet carrier of FIG. 2;
    FIG. 10 is a detailed view of a pre-existing cavity of the cage carrier of the planet carrier of FIG. 2, and
    Fig. 11 is a flowchart illustrating steps of a method of assembling a carrier for a reduction mechanism according to the invention.
    DETAILED DESCRIPTION OF AN EMBODIMENT
    In the following, a method of assembling a planet carrier 16 for a reduction mechanism 10 of the epicyclic type will now be described with reference to the accompanying figures. This is however not limiting, the invention also applying to the assembly of a planet carrier 16 of a reduction mechanism 10 of the planetary type.
    The planet carrier 16 has an axis of revolution X, configured to correspond to the axis of rotation of a reduction mechanism 10 in which it is intended to be integrated.
    The planet carrier 16 further comprises an annular cage and an annular cage holder, integrally secured together, and a drive shaft configured to be connected to the fan.
    The cage 20 comprises a first and a second platform together defining a space configured to receive a central sun gear 12 and satellites 14. The first and second platforms are fixed via a series of uprights 21 distributed circumferentially around the axis of revolution X, each upright 21 comprising an inner bridge 22 and an external bridge 24. A through hole 23 is formed in each inner bridge 22 and in each external bridge 24. The through orifices 23, 25 of the bridges 22, 24 the same amount 21 are placed next to define a passage configured to receive a connection axis.
    Openings are formed in the second platform of the cage 20, between the inner bridge 22 and the outer bridge 24 of each post 21, to allow the fixing of the cage 20 on the cage holder 30.
    The cage 20 further comprises a series of bearing lands 26, formed in the inner platform and in the outer platform and defining in pairs two bores 27 configured to each receive a bearing 15 of a satellite 14 associated.
    Finally, a central bore 28, coaxial with the axis of revolution X, is formed in the second platform of the cage 20.
    The cage carrier 30 comprises a substantially annular platform on which are fixed a series of axial fingers 31 distributed circumferentially around the axis of revolution X. Each finger 31 is configured to be inserted into an associated opening formed in the cage 20 in order to to be housed between an internal bridge 22 and an external bridge 24 of a given amount 21.
    A through hole 32 is formed in each finger 31. Each through hole 32 of the fingers 31 is configured to come into contact with the through orifices 23, 25 of the inner bridge 22 and the external bridge 24 of the associated upright 21, on the passage of the connection axis, to allow the fixing of the cage 20 on the cage holder 30 by means of the connection axis. More precisely, for each upright 21 and for each finger 31, a connection axis is introduced into the three through orifices 23, 32, 25 facing each other and engaged in this position on the inner bridge 22 and on the external bridge 24.
    A ball is further interposed between each connection axis and the associated finger 31 to form a flexible connection between the cage 20 and the cage holder 30. For this, the ball is fretted on the finger 31 and fixed by sliding adjustment on the associated connection axis.
    Finally, a central bore 33, coaxial with the axis of revolution X, is formed in the platform of the cage carrier 30. The drive shaft 40 is fixed integrally on the platform of the cage carrier 30 so that the drive shaft 40, the bore of the cage 20 and the bore of the cage carrier 30 are coaxial. The shaft 40 also has at least one bearing surface 41, generally two bearing surfaces 41, 42. These bearing surfaces 41, 42 are, in a manner known per se, parallel to the axis of rotation of the shaft. (which is confused with the axis of revolution X of the planet carrier 16).
    In order to achieve an assembly of the cage 20 and the cage holder 30 (pre-equipped with the drive shaft) in a robust and precise manner, the invention proposes an assembly method S comprising the following steps: ) S1 separate the cage 20 and the cage carrier 30 by providing an extra thickness at one of the following elements: the through hole 23 of the inner bridge 22 and the through hole 25 of the external bridge 24 of at least an upright 21 of the cage 20, or the through hole 32 of at least one finger 31 of the cage carrier 30, and / or at the level of one of the following elements: at least one of the bearing surfaces 26 or bearing bearing (s) 41, 42, (ii) assembling S2 the cage 20 and the cage holder 30 by placing each axial pin 31 of the cage holder 30 between an inner bridge 22 and an external bridge 24 of the cage 20 (iii) positioning S3 the cage 20 relative to the cage holder 30 and fasten together the cage 20 and the cage holder 30 of my to make a one-piece assembly, (iv) to determine S4 a position of at least one reference axis Y1, Y2 linked to the cage 20, to the cage carrier 30 and / or to the shaft and (v) taking into account of the position of at least one of the reference axes, machining S5 all or leaving the extra thicknesses so as to ensure alignment between the through orifices 23, 25 of each inner bridge 22 and each external bridge 24 with the through hole 32 of the associated axial finger 31 on the one hand, and / or bearing surfaces 26 of the cage 20 with the bearing surface 41, 42 on the other hand.
    For this, during a first step S1, the cage 20 and the cage holder 30 are made separately.
    During this step S1, an excess thickness is left (or created) at a portion of the through holes 23, 25, bearings 26 of the bearings.
    As we shall see later, these extra thicknesses form a local surplus of material allowing subsequent rectification of the orifices 23, 25 and bearing seats 26 in order to adapt their shape, their positioning and their dimensions to the final tolerances required, depending in particular the shape, the positioning and the dimensions of the through-orifice 32 of the finger 31 and / or the rolling bearings 41, 42.
    Where appropriate, the through hole 32 of the finger 31 (or fingers 31) and / or the bearing surfaces 41, 42 may also have an excess thickness forming a local surplus of material. However, their grinding is performed before the step S2 of assembling the cage 20 and the cage holder 30 so as to give them the dimensions, the shape and the positioning in accordance with the final tolerances required.
    By final tolerances, here will be understood the tolerances referred to at the end of the assembly process S. It may be the final tolerances referred to during assembly of the parts before the (conventional) nitriding step, or final tolerances referred to during their final assembly after the nitriding step.
    During a second step S2, the cage 20 and the cage holder 30 are assembled.
    For this, the fingers 31 of the cage carrier 30 are introduced into the associated opening formed in the second platform of the cage 20 to bring each finger 31 between an inner bridge 22 and an external bridge 24. The cage 20 and the The cage carriers 30 are then brought together until the associated through-holes 23, 32, 25 of the external bridge 24, the finger 31 and the inner bridge 22 are substantially aligned.
    During a third step S3, the cage 20 is positioned relative to the cage holder 30, then the cage 20 and the cage holder 30 are fixed together in this position so as to produce a one-piece assembly.
    For example, the cage 20 and the cage holder 30 can be fixed on the same tooling 50. An example of adapted tooling 50 has been illustrated in FIGS. 7 to 9. Note that this is only a proposed non-limiting, and that other tools 50 can be developed to implement the third step S3.
    Here, the tooling 50 comprises a first support 51 configured to be inserted without play-free fit into the central bore of the cage holder 30 and a second support configured to fit into the central bore of the cage 20.
    The first support 51 comprises a first slab 51 of cylindrical shape of revolution, the external diameter of which is substantially equal to the internal diameter of the central bore of the cage holder 30. This first slab 51 is configured to fit into the bore with adjustment central 33 to come into continuous contact with its walls, so that the position of the wafer makes it possible to accurately determine the position of the cage holder 30.
    In order to obtain the fit between the first support 51 and the walls of the central bore 33, the first support 51 can be rectified in order to adapt its configuration (shape, dimensions and orientation) to that of the central bore 33 For this, the walls of the central bore 33 may in particular be palpated (any other method of three-dimensional metrology may of course be considered) after grinding to determine the shape, dimensions and orientation with precision.
    After this grinding step, the first wafer 51 of the first support 51 and the central bore 33 fit perfectly then.
    The second support 52 also comprises a second wafer 52 of cylindrical shape of revolution whose outer diameter is substantially equal to the internal diameter of the central bore 28 of the cage 20 to fitly fit into said central bore 28 to determine accurately the position of the cage 20.
    Similarly to the first support 51 the second wafer 52 can be rectified to obtain a perfect interlocking of the two parts.
    It will be noted that the grinding of the supports 51, 52 makes it possible, in addition to ensuring a perfect assembly of the tooling 50 with the cage 20 and the cage holder 30, to improve the robustness of the method S by ensuring design continuity. central bores 28, 33 of the cage 20 and the cage holder 30.
    In addition, this configuration of the tooling 50 allows access to all parts of the cage 20 and the cage holder 30, especially during machining operations. A control of the size and shape of the supports 51, 52 can then be carried out to allow possible rework.
    The first support 51 is preferably fixed on the second support 52 so as to ensure a determined height between the cage 20 and the cage holder 30. For example, additional wafers 53 of suitable thickness may be interposed to adjust said height. These slabs 53 thus make it possible to adjust the distance between the central bore 33 of the cage holder 30 and the central bore 28 of the cage 20 during the positioning and fixing of the cage holder 30 and the cage 20.
    The first and the second support 51, 52 can then be introduced into the corresponding central bore 33, 28 and thus provide an axial alignment (along the axis of revolution X of the planet carrier 16) and radial alignment of the central bore 28 of the cage 20 with the central bore 33 of the cage holder 30.
    In order to adjust the angular position of the cage 20 relative to the cage holder 30 and to guarantee their concentricity, the tooling 50 may further comprise angular indexing members 54. For example, the tooling 50 may comprise two pins 54, namely at least one pin 54 for the cage 20 and at least one pin 54 for the cage holder 30, extending from the first support 51 and / or the second support 52 and configured to cooperate with as many cavities 29, 34 formed in the cage 20 and in the cage holder 30 so that, during the assembly of the cage 20 and / or the cage holder 30, the pins 54 penetrate into the cavities 29, 34 and thus correct the relative orientation of the cage 20 and the cage holder 30. The diameter of the pins 54 is adapted to the diameter of the cavities 29, 34 to make a mounting without play and allow the repeatability of the assembly.
    Preferably, pre-existing cavities 29, 34 in the cage 20 and in the cage holder 30 are used, for example a hole 29 configured to receive a pin formed in the cage 20 near its central bore 28, or two vertices a substantially triangular hole 34 formed near the central bore 33 of the cage holder 30. In the case of using these examples of cavities 29, 34, the first support 51 then comprises two pins 54 (see FIG. 8), configured to enter the hole 34 at its two vertices, while the second support 52 comprises a pin 54 configured to enter the hole 29 of the cage 20 (see Figures 4 and 9).
    In order to lock in position the cage 20 and the cage holder 30, the first support 51 and the second support 52 are then immobilized relative to a frame 55, for example a mounting table. For this, in one embodiment, the tooling 50 can be fixedly mounted relative to the frame 55.
    For example, the tooling 50 can comprise a rod 56, fixed on the frame 55 and comprising a threaded free end, and a plate 57 configured to be threaded onto the rod 56. The rod 56 extends in a direction substantially perpendicular to the frame 55 and has a length greater than a length of the shaft 40 along the axis of revolution X.
    The cage holder 30 can then be placed on the frame 55 via the shaft 40, so that the rod 56 extends substantially coaxially with its axis of rotation. The length of the rod 56 is chosen so that, in this configuration, its free end protrudes from the central bore 33 of the cage holder 30. The first support 51 is then threaded onto the rod 56 and fitted into the bore central 33 of the cage carrier 30. Where appropriate, the pins 54 of the first support 51 are inserted into an associated cavity 34 formed in the cage holder 30 in order to angularly index the first support 51, for example in the triangular hole 34 The first support 51 is further placed on the rod 56 so as to be flush with the surface of the platform.
    The additional wafers 53 are then threaded successively on the rod 56 to reach a height equal to the desired spacing between the cage 20 and the cage holder 30. In order to allow the immobilization of the tool 50, the additional wafer 53 in contact with the first support 51 is dimensioned so as to bear against the platform of the cage holder 30 so as to form a stop.
    The second support 52 is then threaded on the rod 56, coaxially with the first support 51, then the cage 20 is engaged on the first support 51. Where appropriate, the pin 54 of the second support 52 is inserted into an associated cavity 29 formed in the cage holder 30, for example in the hole 29, in order to angularly position the cage 20 relative to the cage holder 30, via the second support 52 and the first support 51. At this stage, the cage 20 and the cage carrier 30 are perfectly coaxial.
    Finally, the plate 57 can be threaded over the second support 52 and applied against the cage 20, then a nut 58 can be screwed onto the free end of the rod 56 so as to clamp the plate 57 against the cage 20 in order to to immobilize the assembly relative to the frame 55.
    In one embodiment, the first support 51, the additional wafer 53 and the second support 52 are monoblock, for example formed integrally and in one piece. The first support 51, the additional wafer 53 and the second support 52 are then placed at the same time between the cage holder 30 and the cage 20.
    The first support 51 and the second support 52 are then hooped in this position.
    The cage 20 and the cage holder 30 are thus accurately positioned relative to one another by means of the tooling 50 and are aligned axially, radially and angularly. They also form, with the tooling 50, a one-piece assembly, which makes it possible to dimension one of the parts (for example the cage 20) relative to the other of the parts (for example the cage carrier 30), which greatly simplifies their machining. Their positioning and alignment is then controlled.
    During a fourth step S4, the position of at least one reference axis Y1, Y2, for example of two reference axes, is then determined. This position can in particular be carried out in any one of the referential of the tooling 50, the reference frame of the cage 20 or the reference frame of the cage carrier 30, insofar as these three reference frames are now confused thanks to the third S3 step of positioning and fixing.
    In a first embodiment, the reference axis corresponds to an axis of revolution Y1 of the through hole 32 of the finger 31 which has no extra thickness (see Figure 5). It is recalled that this through hole 23 has been machined to the required final tolerances.
    The position of the axis of revolution Y1 of the through hole 23 can be determined by three-dimensional metrology, for example by palpating the through hole 23 and applying the least squares method to the measurements thus obtained.
    In a second embodiment, the reference axis is a bearing axis Y2 and corresponds to the common axis formed by the bearing surfaces 41, 42 (see FIG. 5). Here again, the rolling axis Y2 can be determined by three-dimensional metrology, and in particular by palpating at least one of the rolling bearings 41, 42 over all or part of the circumference of the shaft 40 and applying the least squares method to the measurements thus obtained. Preferably the bearing axis Y2 is determined from the two bearing surfaces 41,42.
    In the following, the method S will be described in the case where both the axis of revolution Y1 of the through hole 23 and the rolling axis Y2 are determined. This is however not limiting, the invention also applies in the case where only one of these axes Y1, Y2 is determined, especially when only the through orifices 23, 25 of the uprights 21 are ground (in which case the reference axis corresponds to the axis of revolution of the through hole 32 of a finger 31) or when only the bearing surfaces 26 are ground (in which case the reference axis corresponds to the rolling axis Y2) .
    During a fifth step S5, the remaining extra thicknesses at the through holes 23, 25 and bearing seats 26 are machined.
    For a given amount 21, the machining of the extra thicknesses of the through holes 23, 25 of each inner bridge 22 and of each external bridge 24 is made taking into account the axis of revolution Y1 of the through hole 32 of the associated finger 31 . It is recalled in fact that the through hole 32 of the finger 31 is already ground (first step S1) and meets the final tolerances required, so that the rectification of the through holes 23, 25 of the bridges 22, 24 can be performed accurately, starting from its axis of revolution Y1. Note that, in this embodiment, a reference axis (the axis of revolution Y1) is determined for each through hole 23 of each finger 31, so that the through hole 23 of the inner and outer bridge 22, 24 are rectified according to a dedicated reference axis.
    As a variant, all the through orifices 23, 25 of the uprights 21 may be machined according to a single reference axis corresponding to the axis of revolution Y1 of only one of the fingers 31. In this case, it is possible to feel that one of the through holes 32 of the fingers 31 during the third step S3 of the method S. Moreover, an extra thickness can be formed during the first step S1 at the through holes 23, 25 of the other fingers 31 these extra thicknesses being then machined during the fifth step S5, taking into account the position of the reference axis Y1 in order to grind the other through orifices 32.
    Similarly, for a bearing bearing 26 given, the machining of the associated extra thickness is made taking into account the bearing axis Y2 of bearing surfaces 41, 42. It is recalled that the bearing surfaces 41, 42 are already ground (first step S1) and meet the required final tolerances, so that the grinding of the bearing surfaces 26 can be performed accurately, starting from the bearing axis Y2. It should be noted that here only one reference axis (the rolling axis Y2) is used to correct all bearing spans 26.
    权利要求:
    Claims (9)
    [1" id="c-fr-0001]
    1. A method of assembling (S) a planet carrier (16), said planet carrier (16) having an axis of revolution (X) and comprising: - an annular cage (20) comprising: - a series of uprights (21) circumferentially distributed about the axis of revolution (X), each upright (21) comprising an internal bridge (22) and an external bridge (24) in each of which is formed a through hole (23, 25), - Bearing bearings defining bores configured to receive a bearing of a satellite, - An annular cage carrier (30) comprising: a series of axial fingers (31) distributed circumferentially around the axis of revolution (X) in each of which is formed a through hole (32), each axial finger (31) being configured to be housed between the inner bridge (22) and the outer bridge (24) of a post (21) of the cage (20), a shaft (40) coaxial with the axis of revolution (X) and having at least one rolling surface (41, 42), said shaft (40) being fastened to the cage carrier (30), the assembly method (S) being characterized in that it comprises the following steps: - producing (S1) separately the cage (20) and the cage carrier (30) providing an extra thickness at one of the following: the through hole (23) of the inner bridge (22) and the through hole (25) of the outer bridge (24) d at least one upright (21) of the cage (20), or the through hole (32) of at least one finger (31) of the cage carrier (30), and / or at one of the the following elements: at least one bearing surface (26) or the at least one bearing surface (41, 42), - assembling (S2) the cage (20) and the cage carrier (30) by placing each finger ( 31) of the cage carrier (30) between an inner bridge (22) and an external bridge (24) of the cage (20), - position (S3) the cage (20) relative to the cage carrier (30) and fasten together the cage (20) and the cage holder (30) so as to realize a set monoblock, - determining (S4) a position of at least one reference axis (Y1, Y2) connected to the cage (20), to the cage carrier (30) and / or to the shaft (40) and - taking into account the position of at least one of the reference axes (Y1, Y2), machining (S5) all or starting from the extra thicknesses so as to ensure alignment between the through orifices of each inner bridge (22) and each external bridge (24) with the through hole (23, 25) of the associated axial finger (31) on the one hand, and / or bearing surfaces (26) of the cage (20) with the bearing surface ( 41, 42) on the other hand.
    [2" id="c-fr-0002]
    2. Assembly method (S) according to claim 1, wherein, during the step (S1) of producing the cage (20) and the cage holder (30), the extra thickness is provided at the level of the through hole (23, 25) of the inner bridge (22) and the outer bridge (24) and / or at the bearing surfaces (26), the through hole (32) of the axial fingers (31) and the at least one bearing surface (41,42) being devoid of extra thickness.
    [3" id="c-fr-0003]
    3. Assembly method (S) according to claim 2, wherein the reference axes (Y1, Y2) comprise an axis of revolution (Y1) of the through hole (32) of at least one finger (31). axial axis of the cage carrier (30) and / or a bearing axis (Y1), said bearing axis (Y2) being defined as an axis of symmetry of the at least one bearing surface (41, 42) of the tree (40).
    [4" id="c-fr-0004]
    4. Assembly method (S) according to claim 3, wherein the axis of revolution (Y1) and the rolling axis (Y2) are determined by three-dimensional metrology of the through hole (32) of the finger (31). ) and the at least one bearing surface (41, 42), respectively, for example by probing.
    [5" id="c-fr-0005]
    5. Assembly method (S) according to one of claims 1 to 4, wherein the cage (20) and the cage holder (30) each comprise a central bore (28, 33), said central bores (28), , 33) being coaxial with the axis of revolution (X) of the planet carrier (16), and wherein the assembling step (S2) comprises a sub-step in which the cage (20) and the cage carriers (30) are positioned to axially and radially align their central bore (28, 33) and / or index them angularly.
    [6" id="c-fr-0006]
    6. Assembly method (S) according to claim 5, wherein the assembly step (S2) of the cage (20) and the cage holder (30) is performed by introducing a tool (50). in the central bore (28, 33) of the cage (20) and the cage holder (30) and fixing said tooling (50) in said central bores (28, 33) so as to lock the cage (20) and the cage holder (30) relative to a fixed frame (55).
    [7" id="c-fr-0007]
    The assembly method (S) according to claim 6, wherein the tooling comprises: - a first support (51) configured to be fitably inserted into the central bore (33) of the cage carrier (30) and - a second support (52) configured to be inserted with fit into the central bore (28) of the cage (20), wherein the step (S3) for positioning and fixing the cage (20) and the door -cage (30) comprises the following substeps: (i) determining the dimensions of the central bore (28) of the cage (20) and the central bore (33) of the cage carrier (30), ( ii) machining the first support (51) and the second support (52) according to the determined dimensions of the central bore (28, 33) of the cage (20) and the cage carrier (30) so as to provide a fitting said supports (51, 52) with the corresponding central bore (28, 33), (iii) introducing the first support (51) and the second support (52) into the bore (c). entral (28) of the cage holder (30) and in the central bore (33) of the cage (20), respectively, and (iv) locking the cage (20) and the cage holder (30) so as to make them monobloc by fixing the first support (51) relative to the second support (52), or vice versa.
    [8" id="c-fr-0008]
    8. The assembly method (S) according to one of claims 6 or 7, further comprising a step of fixing the first support (51) and the second support (52) relative to the frame (55).
    [9" id="c-fr-0009]
    9. The assembly method (S) according to one of claims 6 to 8, wherein the tool (50) further comprises at least two pins (54) configured to penetrate cavities (29, 34) formed in the cage (20) and / or in the cage holder (30), and the step (S3) for positioning and fixing the cage (20) and the cage holder (30) further comprises a sub-step during which the pins (54) are introduced into the corresponding cavities (29, 34) in order to angularly index the cage (20) and the cage holder (30).
    类似技术:
    公开号 | 公开日 | 专利标题
    EP3464955B1|2020-09-23|Method for assembling a planet carrier
    WO2014053728A1|2014-04-10|Combustion chamber comprising a flame tube fixed by means of three centring members
    EP2738356A1|2014-06-04|Vane of a turbomachine, vane assembly of a turbomachine, and corresponding assembly method
    EP1674761A1|2006-06-28|Transmission assembly with planetary gear
    FR3046951A1|2017-07-28|PROCESS FOR MANUFACTURING A PIECE OF A TURBOMACHINE AND PIECE PRODUCED THEREBY
    EP3561266B1|2021-03-10|Method for assembling a epicycloidal or planetary transmission
    FR3047776B1|2019-07-19|TURBOMACHINE AND METHOD OF MOUNTING
    EP3561267B1|2022-02-16|Method for assembling a transmission
    EP3682138A1|2020-07-22|Pivot for a sliding bearing
    FR3021097A1|2015-11-20|REVERSE FLOW COMBUSTION CHAMBER COMPRISING AN OPTIMIZED ELBOW WALL
    EP3362706B1|2019-08-14|Ring gear for an epicyclic reduction gear
    EP3464954B1|2020-09-09|Equipment for disassembling a planet carrier into two parts and associated planet carrier
    EP3736428A1|2020-11-11|Offset seal groove for coupling by meshing
    WO2020169896A1|2020-08-27|Blade pivot of adjustable orientation and of reduced bulk for a turbomachine fan hub
    EP3803159A1|2021-04-14|Method for assembling a reduction gear and facility for implementing the method
    FR3084697A1|2020-02-07|Improved balancing system for aircraft turbomachines
    WO2021115996A1|2021-06-17|Auxiliary power unit comprising a gas generator in direct-drive connection with an electric generator, and an accessories housing
    FR3052212A1|2017-12-08|EPICYCLOIDAL OR PLANETARY REDUCER MOUNTING TOOL AND ASSOCIATED METHOD
    FR3068750A1|2019-01-11|EPICYCLOIDAL OR PLANETARY REDUCER CROWN FOR A TURBOMACHINE
    FR3068749A1|2019-01-11|EPICYCLOIDAL OR PLANETARY REDUCER CROWN FOR A TURBOMACHINE
    FR3101373A1|2021-04-02|Turbomachine fan assembly comprising a roller bearing and a double row angular contact ball bearing
    FR3067393A1|2018-12-14|ROTATING PIECE HAVING MECHANICAL BONDING INTERFACE PROVIDED WITH AXIAL POSITIONING MEANS
    FR3065806A1|2018-11-02|METHOD FOR MANUFACTURING A DEVICE FOR MEASURING CHARACTERISTICS OF AN AIR FLOW
    同族专利:
    公开号 | 公开日
    EP3464955B1|2020-09-23|
    CN109416117B|2021-08-17|
    EP3464955A2|2019-04-10|
    WO2017212166A2|2017-12-14|
    US20190301593A1|2019-10-03|
    US10801609B2|2020-10-13|
    WO2017212166A3|2018-05-24|
    CN109416117A|2019-03-01|
    FR3052213B1|2018-05-18|
    引用文献:
    公开号 | 申请日 | 公开日 | 申请人 | 专利标题
    WO1994029614A1|1993-06-11|1994-12-22|United Technologies Corporation|Geared drive system for a bladed propulsor|
    US20130023378A1|2006-07-05|2013-01-24|United Technologies Corporation|Method of Assembly for Gas Turbine Fan Drive Gear System|EP3557097A1|2018-04-20|2019-10-23|hofer powertrain innovation GmbH|Planet carrier for a epicyclic gear, such as for a planetary gear drive and corresponding support method|
    WO2020021188A1|2018-07-26|2020-01-30|Safran Transmission Systems|Cage for a turbomachine speed reducer with planetary gear set|
    FR3092884A1|2019-02-20|2020-08-21|Safran Transmission Systems|PLANETARY REDUCER ASSEMBLY FOR A TURBOMACHINE|JPS59126165A|1983-01-10|1984-07-20|Fuji Tekkosho:Kk|Planetary gear device|
    US6206800B1|1998-08-21|2001-03-27|Thomson Industries, Inc.|Universally adaptable carrier and swing arm for planetary gear assembly|
    WO2003066359A2|2002-02-07|2003-08-14|Euclid-Hitachi Heavy Equipment, Ltd.|Axle assembly|
    US7081062B2|2002-11-25|2006-07-25|Delbert Tesar|Standardized rotary actuator|
    FR2853382B1|2003-04-04|2006-04-28|Hispano Suiza Sa|FLEXIBLE BONDING SYSTEM BETWEEN A SATELLITE HOLDER AND THE FIXED SUPPORT IN A SPEED REDUCER|
    JP2007127165A|2005-11-02|2007-05-24|Sumitomo Heavy Ind Ltd|Supporting structure of planetary rotator|
    US7704178B2|2006-07-05|2010-04-27|United Technologies Corporation|Oil baffle for gas turbine fan drive gear system|
    US8205432B2|2007-10-03|2012-06-26|United Technologies Corporation|Epicyclic gear train for turbo fan engine|
    US10151248B2|2007-10-03|2018-12-11|United Technologies Corporation|Dual fan gas turbine engine and gear train|
    BE1017854A3|2007-11-21|2009-09-01|Hansen Transmissions Int|PLANET CARRIER OF THE CAGE FORM.|
    WO2011100499A1|2010-02-12|2011-08-18|The Timken Company|Epicyclical gear transmission with improved load carrying capability|
    WO2012109344A1|2011-02-08|2012-08-16|General Electric Company|Cylindrical roller bearing apparatus|
    US20130269479A1|2012-04-11|2013-10-17|General Electric Company|Gearbox and support apparatus for gearbox carrier|
    ITMI20121712A1|2012-10-11|2014-04-12|Danieli Off Mecc|PLANETARY REDUCER|
    US20150354694A1|2014-06-09|2015-12-10|Caterpillar Inc.|System and method for assembling a planet carrier|
    JP6635502B2|2014-09-17|2020-01-29|ジーイー・アーヴィオ・ソチエタ・レスポンサビリタ・リミタータＧｅ Ａｖｉｏ Ｓｒｌ|Planetary carrier for planetary gear set, and planetary gear set provided with the planetary carrier|
    FR3058493B1|2016-11-07|2018-11-16|Safran Transmission Systems|SATELLITE CARRIER FOR AN EPICYCLOIDAL TRAIN SPEED REDUCER|
    US10005623B1|2017-03-30|2018-06-26|Karen Sue Svejkovsky|Adjustable gate|
    FR3065773B1|2017-04-27|2020-03-06|Safran Transmission Systems|CAGE SATELLITE HOLDER FOR AN EPICYCLOIDAL SPEED REDUCER|US11105395B2|2019-10-23|2021-08-31|Pratt & Whitney Canada Corp.|Planetary gear assembly and method of operating same|
    法律状态:
    2017-04-27| PLFP| Fee payment|Year of fee payment: 2 |
    2017-12-08| PLSC| Search report ready|Effective date: 20171208 |
    2018-06-05| PLFP| Fee payment|Year of fee payment: 3 |
    2018-08-17| CD| Change of name or company name|Owner name: SAFRAN TRANSMISSION SYSTEMS, FR Effective date: 20180717 |
    2020-05-20| PLFP| Fee payment|Year of fee payment: 5 |
    2021-05-19| PLFP| Fee payment|Year of fee payment: 6 |
    优先权:
    申请号 | 申请日 | 专利标题
    FR1655203A|FR3052213B1|2016-06-07|2016-06-07|METHOD FOR ASSEMBLING A SATELLITE HOLDER|
    FR1655203|2016-06-07|FR1655203A| FR3052213B1|2016-06-07|2016-06-07|METHOD FOR ASSEMBLING A SATELLITE HOLDER|
    US16/307,879| US10801609B2|2016-06-07|2017-06-06|Method of assembling a planet carrier|
    PCT/FR2017/051425| WO2017212166A2|2016-06-07|2017-06-06|Method for assembling a planet carrier|
    EP17742468.6A| EP3464955B1|2016-06-07|2017-06-06|Method for assembling a planet carrier|
    CN201780041899.3A| CN109416117B|2016-06-07|2017-06-06|Method for assembling planet carrier|
    [返回顶部]