• 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:
    There is provided a device (10) for centering and guiding in rotation a turbomachine shaft (12), in which the outer ring (18) of a bearing is retained axially upstream and downstream. by retention means (52, 72) cooperating with a bearing support (20) and with connecting means (29) comprising elastically deformable means (32) connecting the outer ring to the bearing support, these retention means being distinct from a hoop (28) of the device. It is also proposed a method of assembling such a device, wherein the retention means (52, 72) are preassembled to the connection means (29) before the final assembly of the connection means to the bearing support (20). ). The device and method have the combined advantages of axial retention of the outer ring in two opposite directions, and particularly simple assembly.
    公开号:FR3013760A1
    申请号:FR1361629
    申请日:2013-11-26
    公开日:2015-05-29
    发明作者:Regis Eugene Henri Servant；Serge Louis Antunes；Julie Bellay；Fabrice Cretin；Damien Lourit
    申请人:SNECMA SAS；
    IPC主号:
    专利说明:

    [0001] The present invention relates to the field of turbomachines, in particular for aircraft, and more particularly relates to a device for the purpose of rotating and guiding a rotor of a turbomachine comprising improved means for retaining the outer ring. centering and guiding in rotation of a turbomachine shaft, comprising a bearing of the type commonly called "soft bearing". In a bearing of this type, the means for connecting the outer ring of the bearing to the bearing support comprise a fixing flange mounted on the bearing support and elastically deformable means connecting the outer ring of the bearing to the fixing flange. The invention is particularly applicable to the bearings damped by means of an oil film, also called "squeeze film". The invention also relates to a method of assembling such a device. STATE OF THE PRIOR ART In a turbomachine, the occurrence of an event such as the loss of a fan blade or seizing a bearing due to lack of oil induces very large forces on the bearings of the turbomachine. Such forces may cause a rupture of the elastically deformable means connecting the outer ring of a "soft" type bearing to the flange for fixing the bearing on the bearing support. These elastically deformable means generally consist of a part commonly referred to as "flexible cage" or "squirrel cage". When they break, the elastically deformable means stop ensuring that the bearing ring is held in place, whether axially or tangentially. If appropriate means are not provided, the rolling function is no longer ensured, which causes rapid degradation of the bearing and surrounding parts. The bearing can no longer ensure the operation of the engine, especially in reel or "windmilling" phase.
    [0002] To ensure the axial retention of the outer ring of the bearing relative to the support of the bearing even when the elastically deformable means which connect the outer ring of the bearing to the bearing support are broken, various solutions have been proposed. A known solution consists in interposing means for axial retention of the outer ring between the bearing support and an upstream end of the ring. These axial retention means take the form of a plurality of radial tabs mounted by bolts on an upstream end of the bearing support, and forming axial stops for an upstream end of the outer ring. This technical solution is criticizable in that it causes congestion and a large overall mass, particularly because of the need to extend the outer bearing ring upstream, to provide an abutment surface to the radial tabs carried by the bearing support. Indeed, this ring extension upstream is justified by the need for it to extend beyond the ferrule in which it is housed, in order to receive the radial tabs carried by the bearing support surrounding the fret.
    [0003] This extension upstream of the outer bearing ring is sometimes even impossible to achieve, because of congestion problems in this already dense area of the turbomachine. Another solution proposed in the document FR 2960907 consists in ensuring the axial retention of the outer ring of a bearing by means of pins jointly engaged in a groove of the outer ring and in orifices of a downstream extension of the bearing hoop. (see for example Figure 3 of the aforementioned document). However, the latter solution requires a complex assembly procedure. Indeed, the pins must be mounted in the radial direction from inside to outside. The mounting of the pins can be achieved only after mounting the outer ring of the bearing in its support, and the size of the latter then complicates the task. Similarly, for disassembly, it is necessary to tear the pins before being able to remove the outer ring of the bearing from its support, which presents a risk of damage to these elements. Moreover, to make the pins captive, it is necessary to turn the outer ring of the bearing in its support, while it is already in its final axial position. Such an operation prohibits a tight fitting of the outer ring in its support, which is nevertheless desirable. DISCLOSURE OF THE INVENTION The invention aims in particular to provide a simple, economical and effective solution to at least some of these problems.
    [0004] It proposes for this purpose a device for centering and guiding in rotation of a turbomachine shaft, comprising: a rolling bearing comprising an outer ring; a bearing support surrounding the outer ring; a hoop interposed between the outer ring and the bearing support; means for connecting the outer ring to the bearing support, the connecting means comprising an annular fixing flange mounted on the bearing support and elastically deformable means connecting the outer ring to the fixing flange; and retention means for axially retaining the outer ring in case of rupture of said elastically deformable means. According to the invention, the retention means comprise first distinct means of the hoop and having a radially internal portion engaged in at least one recess formed in a radially outer surface of the outer ring, and a radially outer portion projecting radially outwardly relative to the radially outer surface of the outer ring so that: - the fixing flange opposes an axial displacement of said radially outer portion of the first means in a first direction in case of rupture of the means elastically deformable, and - the bearing support opposes an axial displacement of said radially outer portion of the first means in a second direction opposite to the first direction in case of rupture of the elastically deformable means. The device according to the invention thus makes it possible to ensure axial retention of the outer bearing ring in the event of rupture of the elastically deformable means in both directions, while being particularly simple to assemble because the first means are distinct from each other. the hoop and cooperate with the fastening flange belonging to the connecting means and with the bearing support. Preferably, the retention means further comprise a retaining ring distinct from the hoop and having a radially inner portion extending away from the outer ring and forming a stop opposing the axial displacement of said radially outer portion of the first means in said first direction in case of rupture of the elastically deformable means, and a radially outer portion axially interposed between the bearing support and the fixing flange. The retention ring advantageously has a radially outer end mounted tightly in an annular surface of the fastening flange defined axially by an annular shoulder of the fastening flange opposing axial displacement of the retention ring in said first direction. .
    [0005] Alternatively, the radially outer portion of the retaining ring may be provided with orifices through which fastening means of the fastening flange to the bearing support. Furthermore, in a preferred embodiment of the invention, the first means take the form of a plurality of retention pins each having a radially inner portion mounted tightly in a corresponding orifice of the outer ring, and a radially outer portion protruding from the radially outer surface of the outer ring so as to extend axially facing the radially inner portion of the retaining ring. In this case, the radially outer portion of each of the retention pins is advantageously positioned between two corresponding lugs integral with the bearing support, so that the lugs limit the rotation of the outer ring in case of rupture of the elastically deformable means. In another preferred embodiment of the invention, the first means take the form of an annular element having a radially inner portion engaged in an annular groove of the outer ring, and a radially outer portion projecting from the radially outer surface. the outer ring so as to extend axially opposite the radially inner portion of the retention ring. In yet another preferred embodiment of the invention, the first means take the form of a ring formed of at least two ring sectors circumferentially mounted end-to-end and having a radially internal portion engaged in a groove. annular of the outer ring, and a radially outer portion provided with orifices through which fastening means of the fastening flange to the bearing support.
    [0006] The invention also relates to a turbomachine comprising at least one device of the type described above. The invention also relates to a method of assembling a device according to any one of the preceding claims, comprising at least the steps of: providing a first solid assembly formed by the bearing support and the hoop previously mounted in the latter, - make available the outer ring and the connection means integral with the outer ring; moving said first means radially from the outside towards the inside with respect to an axis of revolution of the outer ring, so as to insert said radially inner portion of the first means in the or each corresponding recess formed in the outer ring, and thus obtaining a second solid assembly comprising the outer ring, the connecting means and the first means, then - moving the second solid assembly with respect to said first solid assembly until the outer ring is surrounded by the bearing support, then - Fix said fixing flange on the bearing support. The first means, and more generally the retention means, are thus preassembled to the integral connection means of the outer ring, so as to form an indissociable assembly, the latter assembly can then be assembled in a conventional manner to said first set, in particular to the bearing support. The invention thus provides a particularly simple method of assembly. In addition, the pre-assembly of the retention means to the connection means can be operated by a first entity, such as a spare parts manufacturer, while the final assembly can be operated by a second entity, such as a manufacturer of turbomachines. In this case, the invention allows the second entity to maintain a conventional final assembly method. Where appropriate, the method advantageously comprises the step of placing the retaining ring around the outer ring before the step of moving and inserting the first means in the outer ring, so that said portion radially internal of the retaining ring is arranged axially between at least a portion of the fastening flange and the or each recess for receiving the radially inner portion of the first means. BRIEF DESCRIPTION OF THE DRAWINGS The invention will be better understood, and other details, advantages and characteristics thereof will appear on reading the following description given by way of nonlimiting example and with reference to the appended drawings in which: Figure 1 is a schematic half-view in axial section of a device for centering and guiding in rotation of a turbomachine shaft, according to a first preferred embodiment of the invention; FIG. 2 is an enlarged view of detail II of FIG. 1; FIG. 3 is a schematic half-view in axial section of a first assembly formed by a bearing support and a hoop, during the assembly of the device of FIG. 1; FIG. 4 is a schematic half-view in axial section of a second assembly formed by an outer bearing ring and means for connecting the outer ring to the bearing support, during the assembly of the device of the figure 1 ; FIG. 5 is a partial schematic half-view in axial section of a device for centering and guiding in rotation of a turbomachine shaft, according to a second preferred embodiment of the invention; FIG. 6 is a partial schematic half-view in axial section of a device for centering and guiding in rotation of a turbomachine shaft, according to a third preferred embodiment of the invention; FIG. 7 is a partial schematic half-view in axial section of a device for centering and guiding in rotation of a turbomachine shaft, according to a fourth preferred embodiment of the invention; FIG. 8 is a partial schematic half-view in axial section of a device for centering and guiding in rotation of a turbomachine shaft, according to a fifth preferred embodiment of the invention; - Figure 9 is a partial schematic front view of two ring sectors for forming a ring of the device of Figure 8. In all of these figures, identical references may designate identical or similar elements. DETAILED DESCRIPTION OF PREFERRED EMBODIMENTS FIG. 1 illustrates a part of a device 10 for centering and guiding in rotation a shaft 12 in a turbomachine, according to a first preferred embodiment of the invention. In the following description, the "upstream" and "downstream" directions are defined with respect to a general direction of gas flow parallel to an axis 13 of the shaft 12 corresponding to an axis of the turbomachine, and the radial directions "Inwards" and "outwards" are defined relative to the axis 13. This device 10 comprises a bearing formed of an inner ring 14 integral with the shaft 12, a bearing 16, and a ring outer 18 secured to a bearing support 20 of generally annular shape. The bearing support 20 comprises a frustoconical wall 22 intended to be connected to a casing of the turbomachine or to another bearing support extending coaxially with the shaft 12, an annular flange 24 extending radially inwardly from an upstream end of the frustoconical wall 22, and a cylindrical upstream portion 26 of revolution extending upstream from a radially inner end of the annular flange 24. The device 10 comprises a band 28 mounted tightly in the upstream portion 26 of the bearing support 20. The device 10 further comprises means 29 for connecting the outer ring 18 to the bearing support 20. These means comprise an annular fixing flange 30 fixed, for example by means of bolts 31, to the annular flange. 24 of the bearing support, and elastically deformable means 32 consist of an annular row of tabs or "balusters" 34 U-shaped open upstream, forming a set of the type commonly referred to as "soft cage" or "squirrel cage". These tabs 34 have an upper upstream end 36 connected to the fastening flange 30, and a lower upstream end 38 connected to the outer ring 18 of the bearing. In the example illustrated, the outer ring 18 is formed of two coaxial parts, namely an annular support 40 connected to the lower upstream end 38 of the tongues 34, and a rolling track 42 mounted tightly in the annular support 40. Alternatively, the outer ring 18 can be made in one piece, as will become clearer in the following. The outer ring 18 has a radially outer annular surface 44 of generally cylindrical shape of revolution, and provided with two grooves 46 in which are respectively housed two annular sealing segments 48 defining axially an annular space 49 intended to receive a film of oil . In the illustrated example, the two grooves 46 are formed in the annular support 40 of the outer ring 18 and are arranged between two annular bearing surfaces 50 of the outer ring, commonly called "abutment bearings", at the right of which the clearance between the outer ring 18 and the ferrule 28 defines the radial stroke of the flexible bearing. This clearance is less than the thickness of the oil film but sufficient to maintain the damping function thereof until the flexible bearing is in abutment under radial force. The device 10 further comprises retention means for axially retaining the outer ring 18 in case of rupture of the elastically deformable means 32, in particular in case of rupture of one or more tongues 34. FIG. 2 illustrates on a larger scale the said retention means. According to the present invention, these retention means comprise first means 52 distinct from the hoop 28 and having a radially inner portion 54 engaged in at least one recess 56 formed in the radially outer surface 44 of the outer ring 18, and a portion radially outer portion 58 extending radially outwardly relative to the radially outer surface 44 of the outer ring 18. In the first preferred embodiment of the invention, the first means 52 is in the form of an annular row. retention pins 60 each having a radially inner portion 62 mounted tightly in the outer ring 18, and a radially outer portion 64 projecting from the radially outer surface 44 of the outer ring 18. Specifically, the radially inner portion 62 of each retention pin 60 extends through a corresponding orifice 66 of the annular support 40, and presents a radially inner end inserted in a corresponding hole 68 of the raceway 42. This keeps in place the raceway 42 in the annular support 40 even in the event of loss of clamping between these two parts. Each orifice 68 of the rolling track 42 has a diameter in section slightly smaller than the diameter in section of the corresponding orifice 66 of the annular support 40, and the radially inner portion 62 of each retention pin 60 has a narrowing of its diameter. section so as to block the retention pin 60 in the radial inward direction, to prevent the retention pin 60 from coming out of its housing in the event of loss of clamping between the retention pin 60 and the orifice 66, in order to it will not damage the bearing.
    [0007] The respective radially outer portions 64 of the retention pins 60 extend in an annular space delimited by a shoulder 70 formed at the base of the annular flange 24 of the bearing support. In the first preferred embodiment of the invention, the retention means further comprise a retaining ring 72 distinct from the band 28 and having a radially internal portion 74 extending away from the outer ring 18 and forming a stop opposing the axial displacement of the radially outer portion 58 of the first means 52 upstream, and a radially outer portion 76 interposed axially between the bearing support 20 and the attachment flange 30. The retention pins 60 extend thus axially facing the radially inner portion 74 of the retaining ring 72. Thus, it is clear that in case of rupture of the elastically deformable means 32, the fastening flange 30 opposes an axial displacement of the part radially outer 58 first means 52 in a first direction D1, in this case facing downstream, while the annular flange 24 of the bearing support 20 opposes a dep axially locating the radially outer portion 58 of the first means 52 in a second direction D2 opposite to the first direction D1, in this case facing upstream. Of course, the aforementioned directions can be reversed by reversing the configuration of the device 10 according to the invention.
    [0008] In the illustrated example, the retaining ring 72 has a radially outer end 78 mounted tightly in an annular surface 80 of the fastening flange 30 delimited axially by an annular shoulder 82 of the fastening flange opposing axial displacement. of the retention ring 72 in said first direction D1, in this case downstream.
    [0009] In the first preferred embodiment of the invention, an annular row of lugs 84 integral with the bearing support 20 is arranged such that the radially outer portion 64 of each of the retention pins 60 is positioned between two lugs 84. In the example illustrated, the lugs 84 form the end of an extension 86 downstream of the hoop 28. The cooperation of the lugs 84 with the retention pins 60 thus makes it possible to limit the rotation of the outer ring 18 by case of rupture of the elastically deformable means 32. The extension 86 of the hoop 28 comprises at least one recess 88 cooperating with a keying pin 90 mounted tightly in an orifice 92 formed in the shoulder 70 of the bearing support 20. The polarizing pin 90 makes it possible to index the angular position of the hoop 28, and thus of the lugs 84, with respect to the bearing support 20. Preferably, each polarizing pin 90 is substantially aligned with one of the retention pins 60, which thus prevents it from leaving its housing even in the event of loss of tightness with the orifice 92, so that it can not go to damage the bearing. Furthermore, the angular indexing of the pins 60 with respect to the bearing support 20 is ensured by referencing orifices 94 of the fastening flange 30 belonging to the connection means 29 with orifices 96 of the annular flange 24 belonging to to the bearing support 20. Some of the orifices 94 and 96 are intended for the passage of the bolts 31 while others of these orifices may be intended for the passage of lubricant supply channels or ventilation channels, or intended to cooperate with each other. with tools to facilitate the separation of the connecting means 29 and the bearing support 20 during the disassembly of the device 10.
    [0010] The device 10 of Figures 1 and 2 can be assembled as follows. On the one hand, the keying pin 90 is inserted into the orifice 92 of the bearing support 20 and is for example made integral with the bearing support 20 by a thermal expansion / contraction technique, then the ferrule 28 is mounted tightly in the housing. bore 30 formed by the upstream portion 26 of the bearing support 20, for example by thermal expansion / contraction. The establishment of the band 28 is effected by moving it upstream, that is to say in the second direction D2, while making sure to angularly align the recess 88 with the polarizing pin 90, until the polarizing pin 90 engages in the recess 88. A first solid assembly 98 visible in FIG. 3 and comprising the bearing support 20 and the ferrule 28 is thus obtained. On the other hand, the outer ring 18 is secured to the connecting means 29. In the particular example described above, the outer ring 18 is formed of two parts, namely the annular support 40 which is made of a single holding with the connecting means 29, and the rolling track 42 which is mounted shrunk in the bore of the annular support 40, for example by thermal expansion / contraction. Then, the retaining ring 72 is moved axially downstream around the outer ring 18 and is then mounted tightly in the annular surface 80 of the fastening flange 30, for example also by thermal expansion / contraction.
    [0011] At this moment, the radially inner portion 74 of the retaining ring 72 is arranged axially between the annular shoulder 82 of the fastening flange 30 and each recess 56 intended to receive the radially inner portion 54 of the first means 52. Next, the retention pins 60 are moved radially from the outside to the inside and the respective radially inner portions 62 of the retention pins 60 are mounted in the orifices 66, 68, for example by thermal expansion / contraction. On the other hand, the sealing segments 48 are, if necessary, put into place in the grooves 46 of the outer ring 18.
    [0012] Then, a second solid assembly 100 formed by the outer ring 18, the connecting means 29, the retaining ring 72, the retention pegs 60 and the sealing segments 48 (FIG. 4) is positioned angularly so as to make corresponding the orifices 94 of the fastening flange 30 with the orifices 96 of the annular flange 24 of the bearing support 20. Then this second solid assembly 100 is moved axially upstream until the outer ring 18 is surrounded by the upstream portion 26 of the bearing support 20. When the attachment flange 30 is applied to the annular flange 24 of the bearing support 20, these two flanges are fixed to each other by means of the bolts 31 (Figure 1) . It should be noted that one or more of thermal expansion / contraction assemblies may alternatively be replaced by assemblies by gluing, crimping, screwing, or by welding. FIG. 5 illustrates a second preferred embodiment of the invention broadly similar to the first embodiment described above, but in which the band 28 has no downstream extension, and therefore pins that can block the retention pions in the tangential direction. In addition, in the example illustrated in FIG. 5 as well as in the following examples, the outer race 18 is formed in one piece having the radially outer annular surface 44 and a radially inner surface 102 forming a raceway. In this case, the recess or recesses 56 may be through or blind. In the example of FIG. 5, for the sake of simplicity of manufacture, the recesses 56 take the form of through orifices provided with a narrowing of section 103 making it possible to guarantee retention of the retention pins 60 in the radial direction towards inside.
    [0013] In addition, in this example, the retaining ring 72 comprises an axial flange 104 making it possible to reinforce its connection with the connection means 29. Finally, in the example illustrated in FIG. 5 as well as in the following examples, the means resiliently deformable tongues 32 comprise a reinforcing ring 106 connecting the respective downstream ends of the tongues 34. Such a reinforcing ring could of course equip the device of FIG. 1. It should be noted that the orifice 94a of the fastening flange 30 and the orifice 96a of the annular flange 24 visible in FIG. 5 are not through holes for a bolt 31 but circulation holes for oil intended to form the film of oil between the ferrule 28 and the ring outside 18.
    [0014] FIG. 6 illustrates a third preferred embodiment of the invention, generally similar to the first embodiment described above, but in which the first means 52 do not take the form of an annular row of retention pins but take the shape of an annular element 108 having a radially inner portion 110 engaged in an annular groove 112 of the outer ring 18, and a radially outer portion 114 projecting from the radially outer surface 44 of the outer ring so as to extend axially facing the radially inner portion 74 of the retention ring 72.
    [0015] The annular element 108 takes for example the form of an elastic ring, that is to say a split and prestressed metal ring. The annular element 108 is then mounted by opening this element for the time it is moved downstream around the outer ring 18, then releasing the annular element when the latter is in the right position. of the annular groove 112 so that the annular element engages in the annular groove 112. In addition, to limit the risk of disengagement of the annular element 108, the ferrule 28 has an extension 116 downstream, which covers a radially outer end of the annular element 108 when the latter is engaged in the annular groove 112. FIG. 7 illustrates a fourth preferred embodiment of the invention, generally similar to the third embodiment described above, but wherein the radially outer portion 76 of the retaining ring 72 is provided with orifices 118 traversed by the bolts 31 for securing the fastening flange 30 to the bearing support 20. A e illustrative, the radially outer portion 76 of the retaining ring 72 extends radially outwardly to a radially outer end of the attachment flange 30.
    [0016] In the example shown, the band 28 has no downstream extension similar to the extension 116 of FIG. 6. The assembly of the device according to this fourth embodiment is carried out in a similar manner to the assembly of the device according to the third embodiment of the invention, except with regard to the retention ring 72 which is not tight in the fastening flange 30, but which is simply arranged around the outer ring 18, close of the fixing flange 30, preferably in contact with the latter, before the first means 52 are engaged in the recess 56. In the example illustrated, the engagement of the first means 52 consists in the engagement of the radially inner portion 110 of the annular element 108 in the annular groove 112 of the outer ring 18. The first means 52 then allow to retain axially retaining ring 72 as the second solid assembly above is not attached to the first solid assembly by means of the bolts 31.
    [0017] FIG. 8 illustrates a fifth preferred embodiment of the invention, generally similar to the fourth embodiment described above, but in which the first means 52 take the form of a ring 120 formed of at least two sectors of 122a, 122b ring (FIG. 9) circumferentially mounted end-to-end and having a radially internal portion 124 engaged in the annular groove 112 of the outer ring 18 (FIG. 8), and a radially outer portion 126 provided with orifices 128 traversed by the fixing members of the fastening flange 30 to the bearing support 20, that is to say in the example illustrated, by the bolts 31. The device 10 according to this fifth embodiment is therefore devoid of a ring of independent retention of the first means 52. The ring 120 forming the first means fulfills both the retention function of the outer ring 18 and retention vis-à-vis the bearing support 20 and the flange of fi The assembly of the device 10 of FIG. 8 is broadly similar to the assembly of the devices described above, but the placement of the first means 52 comprises the positioning of the ring sectors. 122a, 122b around the outer ring 18 so as to engage these ring sectors in the annular groove 112 while angularly positioning the ring sectors so as to align their orifices 128 with corresponding holes 94 of the fastening flange 30 Then the bolts 31, or fasteners of any suitable type, are inserted through the orifices 94 and 128 to radially retain the ring sectors 122a, 122b. The second solid assembly thus formed can then be assembled to the bearing support 20 in the manner described above.
    [0018] In all of the embodiments of the invention described above, the aforementioned retention means make it possible to ensure retention of the outer ring 18 in the two opposite axial directions D1, D2. Since these retention means do not include the ferrule 28 integral with the bearing support, the assembly of the device can be operated in a particularly simple and effective manner.
    权利要求:
    Claims (11)
    [0001]
    REVENDICATIONS1. Device (10) for centering and guiding in rotation a turbomachine shaft (12), comprising: a rolling bearing comprising an outer ring (18); a bearing support (20, 24, 26) surrounding the outer ring; a hoop (28) interposed between the outer ring and the bearing support; means for connecting the outer ring to the bearing support, the connecting means comprising an annular fixing flange (30) mounted on the bearing support (20) and elastically deformable means (32) connecting the outer ring (18). at the fastening flange (30); and retention means for axially retaining the outer ring (18) in case of rupture of said elastically deformable means (32); characterized in that the retention means comprise first means (52) separate from the hoop (28) and having a radially inner portion (54) engaged in at least one recess (56) formed in a radially outer surface (44) of the outer ring, and a radially outer portion (58) projecting radially outwardly with respect to the radially outer surface (44) of the outer ring so that: - the mounting flange (30) is opposes axial displacement of said radially outer portion (58) of the first means in a first direction (D1) in case of rupture of the elastically deformable means (32), and - the bearing support (24) opposes a axial displacement of said radially outer portion (58) of the first means in a second direction (D2) opposite the first direction in case of rupture of the elastically deformable means (32).
    [0002]
    2. Device according to claim 1, wherein the retention means further comprises a retaining ring (72) separate from the hoop (28) and having a radially inner portion (74) extending at a distance from the outer ring ( 18) and forming a stop opposing the axial displacement of said partieradialement external (58) first means in said first direction (D1) in case of rupture of the elastically deformable means (32), and a radially outer portion (76) interposed axially between the bearing support (24) and the attachment flange (30).
    [0003]
    3. Device according to claim 2, wherein the retaining ring (72) has a radially outer end (78) tightly mounted in an annular surface (80) of the fastening flange (30) delimited axially by an annular shoulder ( 82) of the fastening flange opposing axial displacement of the retention ring in said first direction (D1).
    [0004]
    4. Device according to claim 2, wherein the radially outer portion (76) of the retaining ring (72) is provided with orifices (118) traversed by members (31) for fixing the fastening flange (30). ) to the bearing support (24).
    [0005]
    The device of any one of claims 2 to 4, wherein the first means (52) is in the form of a plurality of retention pegs (60) each having a radially inner portion (62) tightly mounted in an orifice corresponding (66, 68) of the outer ring (18), and a radially outer portion (64) projecting from the radially outer surface (44) of the outer ring so as to extend axially facing the radially inner portion (74) of the retention ring (72).
    [0006]
    6. Device according to claim 5, wherein the radially outer portion (64) of each of the retention pins (60) is positioned between two corresponding lugs (84) integral with the bearing support (20), so that the lugs ( 84) limit the rotation of the outer ring (18) in case of rupture of the elastically deformable means (32).
    [0007]
    7. Device according to any one of claims 2 to 4, wherein the first means (52) take the form of an annular element (108) having a radially inner portion (110) engaged in an annular groove (112) of the outer ring (18), and a radially outer portion (114) projecting from the radially outer surface (44) of the outer ring (18) so as to extend axially facing the radially inner portion (74) of the retention ring (72).
    [0008]
    8. Device according to claim 1, wherein the first means (52) take the form of a ring (120) formed of at least two ring sectors (122a, 122b) mounted end-to-end circumferentially and having a radially inner portion (124) engaged in an annular groove (112) of the outer ring (18), and a radially outer portion (126) provided with orifices (128) traversed by members (31) for fixing the flange fastening (30) to the bearing support (24).
    [0009]
    9. Turbomachine, characterized in that it comprises at least one device according to any one of the preceding claims.
    [0010]
    10. A method of assembling a device (10) according to any one of claims 1 to 8 characterized in that it comprises at least the steps of: - providing a first solid assembly (98) formed by the bearing support (20, 24, 26) and the hoop (28) previously mounted in the latter, - providing the outer ring (18) and the connecting means (29) integral with the outer ring; moving said first means (52) radially from the outside towards the inside with respect to an axis of revolution (13) of the outer ring, so as to insert said radially inner portion (54) of the first means in the or each recess (56) formed in the outer ring, and thereby obtain a second solid assembly (100) comprising the outer ring (18), the connecting means (29) and the first means (52), then moving the second set solid (100) with respect to said first solid assembly (98) until the outer ring (18) is surrounded by the bearing support (26), and - securing said attachment flange (30) on the bearing support (24).
    [0011]
    The method of claim 10 of assembling a device according to claim 2, further comprising the step of placing the retaining ring (72) around the outer ring (18) prior to the step for moving and inserting the first means (52) in the outer ring, so that said radially inner portion (74) of the retaining ring is arranged axially between at least a portion (82) of the attachment flange ( 30) and the or each recess (56) for receiving the radially inner portion (54) of the first means.
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    WO2013114032A1|2013-08-08|Method for repairing wear marks on a rotor supporting the fan of a bypass engine
    FR2949138A1|2011-02-18|Turbomachine e.g. turbopropeller, for airplane, has snap ring cooperating with anti-rotation collar by axial abutment, where collar has grooves co-operating with complementary grooves of nut and ring to immobilize rotation of collar
    EP3610136B1|2021-04-21|Device for centring and rotationally guiding a turbomachine shaft comprising means for an axial retention of outer ring of a bearing
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    同族专利:
    公开号 | 公开日
    WO2015079156A1|2015-06-04|
    US9708931B2|2017-07-18|
    EP3074611B1|2018-10-24|
    JP6464168B2|2019-02-06|
    CN105765173B|2018-08-10|
    US20160290161A1|2016-10-06|
    CA2931044A1|2015-06-04|
    EP3074611A1|2016-10-05|
    FR3013760B1|2015-12-25|
    CN105765173A|2016-07-13|
    JP2016540923A|2016-12-28|
    RU2016125485A|2018-01-09|
    RU2664726C1|2018-08-22|
    引用文献:
    公开号 | 申请日 | 公开日 | 申请人 | 专利标题
    US20030039538A1|2001-08-27|2003-02-27|Allmon Barry Lynn|Methods and apparatus for bearing outer race axial retention|
    EP1630357A2|2004-08-27|2006-03-01|General Electric Company|Apparatus for centering rotor assembly bearings|
    FR2960907A1|2010-06-02|2011-12-09|Snecma|BEARING BEARING FOR AIRCRAFT TURBOJET ENGINE WITH IMPROVED AXIAL RETENTION MEANS FOR ITS OUTER RING|FR3042215A1|2015-10-13|2017-04-14|Snecma|STRUCTURE FOR TURBOMACHINE COMPRISING AXIAL RETAINING ROLLS FOR EXTERIOR BEARING BEARING BEARING|
    EP3163106A1|2015-10-28|2017-05-03|United Technologies Corporation|Integral centering spring and bearing support and method of supporting multiple damped bearings|
    US9879720B2|2016-05-05|2018-01-30|General Electric Company|Bearing damper with external support spring systems and methods|
    WO2020053504A1|2018-09-13|2020-03-19|Safran Aircraft Engines|System for the axial retention of a ring of a rolling element bearing|
    US10746050B2|2017-12-21|2020-08-18|Safran Aircraft Engines|Variable stiffness bearing suspension device|JPS5148545U|1974-10-09|1976-04-12|
    JPH1182498A|1997-09-16|1999-03-26|Nissan Motor Co Ltd|Bearing device|
    US6413046B1|2001-01-26|2002-07-02|General Electric Company|Method and apparatus for centering rotor assembly damper bearings|
    FR2866069A1|2004-02-06|2005-08-12|Snecma Moteurs|SOLIDARITY BLOWER TURBOREACTOR OF A DRIVE SHAFT SUPPORTED BY A FIRST AND A SECOND BEARING|
    RU2265728C1|2004-04-29|2005-12-10|Открытое акционерное общество "Научно-производственное объединение "Сатурн" |Turbomachine rotor thrust-damper support|
    US9777592B2|2013-12-23|2017-10-03|Pratt & Whitney Canada Corp.|Post FBO windmilling bumper|FR3066550B1|2017-05-18|2019-07-12|Safran Aircraft Engines|DEVICE FOR THE CENTERING AND ROTATION GUIDING OF A TURBOMACHINE TREE COMPRISING AXIAL RETAINING RINGS OF EXTERNAL BEARING RING|
    FR3088672B1|2018-11-16|2020-12-18|Safran Aircraft Engines|DEVICE FOR CENTERING AND GUIDING IN ROTATION OF A ROTATING PART WITH INTERLACED ARMS|
    CN111740538B|2020-07-31|2021-05-25|江苏友孚汽车部件科技有限公司|Locating part of high-speed motor bearing|
    法律状态:
    2015-11-04| PLFP| Fee payment|Year of fee payment: 3 |
    2016-11-08| PLFP| Fee payment|Year of fee payment: 4 |
    2017-10-20| PLFP| Fee payment|Year of fee payment: 5 |
    2017-11-10| CD| Change of name or company name|Owner name: SNECMA, FR Effective date: 20170713 |
    2018-10-24| PLFP| Fee payment|Year of fee payment: 6 |
    2019-10-22| PLFP| Fee payment|Year of fee payment: 7 |
    2020-10-21| PLFP| Fee payment|Year of fee payment: 8 |
    2021-10-20| PLFP| Fee payment|Year of fee payment: 9 |
    优先权:
    申请号 | 申请日 | 专利标题
    FR1361629A|FR3013760B1|2013-11-26|2013-11-26|DEVICE FOR THE CENTERING AND ROTATION GUIDING OF A TURBOMACHINE SHAFT COMPRISING IMPROVED MEANS FOR RETAINING EXTERNAL BEARING RING|FR1361629A| FR3013760B1|2013-11-26|2013-11-26|DEVICE FOR THE CENTERING AND ROTATION GUIDING OF A TURBOMACHINE SHAFT COMPRISING IMPROVED MEANS FOR RETAINING EXTERNAL BEARING RING|
    RU2016125485A| RU2664726C1|2013-11-26|2014-11-25|Device for centring and guiding rotation of turbine engine shaft including improved means for retaining external bearing ring|
    EP14821737.5A| EP3074611B1|2013-11-26|2014-11-25|Device for centring and guiding the rotation of a turbine engine shaft including improved means for retaining the external bearing ring|
    US15/037,889| US9708931B2|2013-11-26|2014-11-25|Device for centring and guiding the rotation of a turbine engine shaft including improved means for retaining the external bearing ring|
    JP2016534187A| JP6464168B2|2013-11-26|2014-11-25|Apparatus for centering and guiding the rotation of a turbine engine shaft including improved means for retaining an outer bearing ring|
    PCT/FR2014/053020| WO2015079156A1|2013-11-26|2014-11-25|Device for centring and guiding the rotation of a turbine engine shaft including improved means for retaining the external bearing ring|
    CN201480064694.3A| CN105765173B|2013-11-26|2014-11-25|To the equipment that the rotation of propeller for turboprop arbor is felt relieved and is oriented to, including the improved device for fixing external bearings ring|
    CA2931044A| CA2931044A1|2013-11-26|2014-11-25|Device for centering and guiding in rotation with a turbomachine shaft and comprising methods for retaining the bearing outer race|
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