• 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:
    Ball joint device (10) for suspending a turbine engine at a pylon or the suspension of equipment at the body of a turbomachine, comprising a first member (12), one end bearing a ball joint (14) and is interposed between the two lugs (16, 17) of a second member (18), the ball having a bore (28) for passage of an axis (30) whose ends pass through the orifices (20, 22) of the ears , characterized in that a first (16) of the ears comprises or carries first means (52) for axially retaining the axis on the side opposite the patella, and a second (17) ear comprises or carries second means (38) axially retaining the axis of the opposite side to the patella.
    公开号:FR3021373A1
    申请号:FR1454559
    申请日:2014-05-21
    公开日:2015-11-27
    发明作者:Nicolas Marc Florent；Marc Patrick Tesniere
    申请人:SNECMA SAS；
    IPC主号:
    专利说明:

    [0001] The present invention relates to a ball joint device for the suspension of a turbine engine to a pylon or the suspension of equipment to the body of a turbomachine. STATE OF THE ART A turbomachine is generally suspended from a pylon by means of a "yoke" which is fixed on the body of the turbomachine, at its intermediate casing. This yoke comprises yokes on which are articulated ends of rods whose other ends are connected to the suspension means of the turbine engine to the pylon. Each rod is generally articulated on a yoke by a ball joint device.
    [0002] In the current technique, each rod has an end which carries a ball joint and which is interposed between the two ears of a yoke, the ball having a bore for passage of an axis whose ends pass through the ear holes of the yoke. The devices of this type currently used are however not entirely satisfactory from a safety point of view. An important safety criterion is that the connection of a connecting rod to a yoke is maintained especially in case of rupture of the axis passing through the ball joint carried by the connecting rod. In each of the applications FR-A1-2 879 695 FR-A1-2 923 460 for example, in the event of breakage of the axis, the broken parts of the shaft can come out of the openings of the ears, which would result in a rupture of the connection of the connecting rod to the screed. The present invention is intended in particular to provide a simple, effective and economical solution to this problem. DESCRIPTION OF THE INVENTION The invention proposes a ball joint device for the suspension of a turbine engine to a pylon or the suspension of equipment to the body of a turbomachine, comprising a first member, one end of which carries a ball joint. and is interposed between the two lugs of a second member, the ball having a bore for passage of an axis, the ends of which pass through orifices of the ears, characterized in that a first ear comprises or carries first retaining means axial axis of the axis of the opposite side to the ball joint, and a second of the ears comprises or carries second axial retaining means of the axis of the opposite side to the ball joint. The device according to the invention is therefore equipped with means for ensuring axial retention of the axis so that it does not dissociate ears. Thus, even in the event of rupture of the axis, these broken parts are maintained and do not dislodge the orifices of the ears, which makes it possible to maintain the connection of the first and second members. Advantageously, the first retaining means comprise a cover which is fixed, for example by at least one screw, on the first lug and which covers one end of the axis.
    [0003] Preferably, an elastically deformable member in compression, such as a Belleville washer, is mounted tightly axially between the cover and said end of the axis to axially bias the latter on the opposite side to the cover. The lid may be generally annular in shape and includes an outer peripheral portion that extends around said end of the shaft and is applied and secured to an outer lateral surface of the first ear. The axis can pass through a first bushing which is mounted in the orifice of the first lug, said end of the axle comprising an outer annular flange which bears axially on one end of this first bushing which comprises at its opposite end a external annular flange. The cover can be fixed on the axis or be integrally formed with the axis. An elastically deformable compression member may be mounted axially tightly between the cover and a first bushing traversed by the axis and mounted in the orifice of the first lug, for axially biasing the first bushing in a direction opposite to the cover.
    [0004] The elastically deformable member may be directly or indirectly in axial bearing on one end of the first sleeve, said first sleeve comprising at its opposite end an outer annular flange. In the mounting position, an axial clearance can be provided between the first ear and the outer annular flange of the first socket. Advantageously, the second retaining means comprise a second bushing which is mounted in the orifice of the second lug and which is traversed by the axis, this second bushing comprising at a first end, located on the side opposite the patella, a flange annular internal axial retention of the axis. In the mounting position, the ball is preferably clamped between the first and second sockets. The second bushing may comprise at a second end an outer annular support flange on an internal lateral face of the first lug.
    [0005] In the mounting position, axial clearance can be provided between the axis and the inner annular flange of the second bushing. The first member may be a connecting rod and the second member may be a clevis, or vice versa. The present invention also relates to a turbomachine, such as a turbojet engine or an airplane turboprop, characterized in that it is equipped with at least one device as described above. DESCRIPTION OF THE FIGURES The invention will be better understood and other details, characteristics and advantages of the invention will become apparent on reading the following description given by way of nonlimiting example and with reference to the appended drawings, in which: FIG. 1 is a diagrammatic view in axial section of an embodiment of the ball joint device according to the invention; FIG. 2 is a diagrammatic view in axial section of the ball joint device of FIG. 2, the axis being here broken, - Figures 3 to 6 are schematic perspective views of the ball joint device of Figure 2, and - Figure 7 is a schematic axial sectional view of another embodiment of the ball joint device according to the invention. DETAILED DESCRIPTION FIGS. 1 to 6 show a first embodiment of the ball joint device according to the invention. This device 10 comprises a connecting rod 12 whose end carries a ball 14 and is interposed between the two lugs 16, 17 of a yoke 18. In the case of the suspension of a turbine engine to a pylon, the yoke 18 is typically formed with or attached to a motor housing. The yoke 18 is of the female type and its two lugs 16, 17 are flat and parallel to each other, these lugs 16, 17 having orifices 20, 22 that are coaxial and have cylindrical internal walls. The rod 12 is connected to suspension means to the pylon and its visible end in the drawing is flat and comprises an orifice 24 with an internal cylindrical wall for mounting a cage 26 which is crimped into the orifice and whose internal spherical wall receives the ball 14 which is free to rotate in the cage 26. The ball 14 comprises a cylindrical bore 28 traversed by a shaft 30 having a cylindrical body whose ends pass through the orifices 20, 22 of the lugs 16, 17. comprises at one end an outer annular flange 32. In the example shown, two bushes 36, 38 are respectively mounted in the orifices 20, 22 of the ears. These bushes 36, 38 are coaxial and each comprise a tubular cylindrical body. A first bushing 36 is engaged in the orifice 20, from the inner side of the lug 16, and comprises at its inner end (located on the side of the ball 14) an outer annular flange 40 which is opposite the lateral face. internal 42 of the ear 16 (and more exactly which extends opposite the peripheral portion of the face 42 extending around the orifice 20). As can be seen in FIG. 1, in the mounting position, the flange 40 is separated from the face 42 by an axial clearance A1. The first bushing 36 is supported by its flange 40 on the ball 14. Furthermore, the flange 32 of the axis 30 bears axially on the outer end (located on the side opposite to the ball) of the bushing 36 and is separated from the outer face 44 of the ear by an axial clearance A2. The second sleeve 38 is engaged in the orifice 22 from the inner side of the lug 16, and comprises at its inner end (located on the side of the ball) an outer annular rim 46 which is opposite the internal lateral face 48. of the ear (and more exactly which extends opposite the peripheral portion of the face 48 extending around the orifice 22). As can be seen in FIG. 1, in the mounting position, the flange 46 bears axially against the face 48. The second bushing 38 is supported by its flange 46 on the ball joint.
    [0006] The second bushing 38 comprises at its outer end (located on the opposite side to the ball) an inner annular flange 50 axially retaining the axis 30, towards the outside of the ear 18. As can be seen in FIG. in the mounting position, the flange 50 is separated from the axis 30 by an axial play A3, so that no axial support is generated between the axis 30 and the second bushing 38. Such axial support would indeed risk compromise the axial support of the axis 30 on the first sleeve 36 and thus compromise the tightening of the ball 14 between the two sockets. In the event of a break in the axis 30 (see FIG. 2), the portion 30a of the spindle extending in the second bushing 38 may bear axially on the flange 50 of this bushing 38 and thus be retained and prevented from dissociate from the ear 17.
    [0007] The sleeve 38 thus forms retaining means of the shaft 30, these means being carried by the lug 17, as is clear from the drawings. The device 10 according to the invention comprises other means of retaining the axis 30, these means being carried by the other lug 16 and here comprising a lid 52 which is attached and fixed to the lug 16.
    [0008] In the example shown, the cover 52 has an annular shape and covers the end of the axis 30 having the rim 32. The cover 52 is disposed outside the lug 16 and its outer periphery 54 extends around the edge 32 of the axis 30 and is applied and fixed on the outer face 44 of the lug 16. The cover 52 here comprises at its periphery 54 four holes 56 of screw passage 58 which are directly screwed from the outside The screws 58 extend here substantially parallel to the axis 30.
    [0009] A member 62 elastically deformable in compression is mounted tightly axially between the cover 52 and the end of the axis 30 having the flange 32. This member 62 is prestressed once the cover 52 attached to the lug 16, and axially solicits the 30 axis towards the opposite side to the cover 52. The member 62 is here a Belleville washer whose outer periphery bears on the axis 30 and is surrounded by a cylindrical rim 64 of the axis 30 which serves to center the washer vis-à-vis the axis and guide its compression. In the mounting position, the axis 30 is thus separated from the cover 52 by an axial clearance A4 at which the member 62 extends.
    [0010] In this first embodiment, the fact of disposing the washer 62 between the axis 30 and the cover 52 has a notable advantage. Indeed, the washer may have more or less the same diameter as the axis, a substantial difference between the two diameters being however possible, and further the axial clearance A4 may be more or less large by adapting the axial dimension of the lid 52 for this purpose. Thus, by taking a commercially available washer with a diameter more or less close to the diameter of the axis 30, the cylindrical rim 64 will be adapted to the end of the axis according to the diameter of the selected washer and provision will be made for a set Axial A4 suitable for the height of the washer. This saves development costs that would be required if the washer were to be given specific dimensions that are not found in the commercial washers. As can be seen in FIGS. 3 to 6, the lugs 16, 17 of the yoke 18 are interconnected by stiffening walls 66 which extend substantially parallel to the axis 30.
    [0011] The device 10 according to the invention can be mounted in the following manner. The bushes 36, 38 are mounted in the orifices 20, 22 of the lugs 16, 17 of the yoke 18 from the inside of the lugs, as described in the foregoing. The ball 14 carried by the connecting rod 12 is engaged between the lugs and disposed between the bushes 36, 38 so that its bore 28 is aligned with the bores of the sockets. The engagement of the ball 14 is facilitated by the clearance A1 which makes it possible to increase the inter-bushing distance 36, 38 beyond the axial dimension of the ball joint 14. The pin 30 is then engaged in the socket 36, the bore of the ball 14, then the sleeve 38, until its flange 32 bears on the sleeve 36. The member 62 is placed on the axis 30, then the cover 52 is mounted on the member 62 and is attached to the lug 16 by means of the screws 58. The tightening of the screws 58 causes the compression of the member 62 and the holding in abutment of the rim 32 of the shaft 30 on the bushing 36, as well as the tightening the ball 14 between the sleeves 36, 38. Figure 7 shows another embodiment of the device 10 'ball joint according to the invention. The elements of the device 10 'already described in the foregoing in relation to the device 10 are referenced by the same numbers in FIG. 7.
    [0012] It is found that, in this embodiment, the axial retaining means of the axis 30 ', carried by the ear 17, comprise a sleeve 38 identical to that of the first embodiment. The retaining means carried by the lug 16 here comprise a cover 52 'which covers at least partly an end of the axis 30'. The cover 52 'is on the one hand fixed to the axis 30', here by a screw 68 coaxial with the axis 30 'and screwed into a tapped hole 70 of the end of the axis, and secondly at the ear 16, by screws 58 similar to those described in the foregoing. Alternatively, the cover 52 'could be formed in one piece with the axis 30'. In the example shown in FIG. 7, the assembly formed by the cover 52 'and the screws 58 ensures the axial retention of the axis 30' on the side of the lug 16 opposite to the ball joint 14. In the variant mentioned above, it would be the screws 58 only which would ensure the axial retention of the axis 30 'in this direction. The member 62 'elastically deformable in compression is here mounted tightly axially between the cover 52' and the sleeve 36 mounted in the orifice 20 of the ear 16. The member 62 'extends here around the axis 30 . The member 62 'axially urges the bushing 36 in a direction opposite to the cover 52'. The elastically deformable member 62 'may be directly in axial bearing on one end of the sleeve 36. On the contrary, in the example shown, the elastically deformable member 62 is indirectly in axial bearing on this end of the sleeve 36 because a ring 72 is interposed between the member 62 'and this end. This member 62 'may also be a Belleville washer.
    [0013] The member 62 'is here dimensioned so that its inner diameter is very slightly greater than the diameter of the axis 30'. This embodiment makes it possible to remove the assembly comprising the cover 52 ', the axis 30', and the member 62 'with the ring 72, in a single block at disassembly once the screws 58 for fixing the cover 52 'are removed from the screed.
    权利要求:
    Claims (11)
    [0001]
    REVENDICATIONS1. Ball joint device (10, 10 ') for suspending a turbine engine at a pylon or the suspension of equipment at the body of a turbomachine, comprising a first member (12), one end bearing a ball joint ( 14) and is interposed between the two lugs (16, 17) of a second member (18), the ball having a bore (28) for passage of an axis (30, 30 '), the ends of which pass through orifices ( 20, 22) of the ears, characterized in that a first (16) of the ears comprises or carries first axial retaining means (52, 58, 52 ') of the axis opposite to the patella, and a second (17) ears comprises or carries second means (38) for axially retaining the axis of the opposite side to the patella.
    [0002]
    2. Device (10, 10 ') according to claim 1, characterized in that the first retaining means comprise a cover (52, 52') which is fixed, for example by at least one screw (58), on the first ear (16) and which covers at least partly an end of the axis (30, 30 ') or is formed in one piece with the axis.
    [0003]
    3. Device (10) according to claim 2, characterized in that a member (62) elastically deformable in compression, such as a Belleville washer, is mounted tightly axially between the cover (52) and said end of the axis. (30) for axially biasing the latter in a direction opposite to the lid.
    [0004]
    4. Device (10) according to claim 3, characterized in that the cover (52) has a generally annular shape and comprises an outer peripheral portion (54) which extends around said end of the axis (30, 30). ') and which is applied and fixed on an outer lateral face (44) of the first ear (16).
    [0005]
    5. Device (10) according to one of claims 2 to 4, characterized in that the axis (30) passes through a first sleeve (36) which is mounted in the orifice (20) of the first lug (16) , said end of the axis comprising an outer annular flange (32) which bears axially on one end of this first bushing which comprises at its opposite end an outer annular flange (40).
    [0006]
    6. Device (10 ') according to claim 2, characterized in that the cover (52') is fixed on the axis (30 ') or is integrally formed with the axis, and in that an element (62') ) elastically deformable in compression is mounted tightly axially between the cover (52 ') and a first sleeve (36) traversed by the axis and mounted in the orifice (20) of the first lug (16), to axially solicit the first socket in a direction opposite to the cover.
    [0007]
    7. Device (10 ') according to claim 6, characterized in that the member (62') elastically deformable is directly or indirectly in axial bearing on one end of the first sleeve (36), said first sleeve comprising at its end opposite an outer annular flange (40).
    [0008]
    8. Device (10, 10 ') according to claim 5 or 7, characterized in that, in the mounting position, an axial clearance (A1) is provided between the first lug (16) and the outer annular flange (40) of the first socket (36).
    [0009]
    9. Device (10, 10 ') according to one of the preceding claims, characterized in that the second retaining means comprise a second sleeve (38) which is mounted in the orifice (22) of the second lug (17). and which is traversed by the axis (30, 30 '), the second sleeve having at a first end, located on the opposite side to the ball joint, an inner annular flange (50) axially retaining the axis.
    [0010]
    Device (10, 10 ') according to claim 9, characterized in that, in the mounting position, an axial clearance (A3) is provided between the axis (30, 30') and the inner annular flange (50). of the second socket (38).
    [0011]
    11. Turbomachine, such as a turbojet engine or an airplane turboprop, characterized in that it is equipped with at least one device (10, 10 ') according to one of the preceding claims.
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    法律状态:
    2015-05-12| PLFP| Fee payment|Year of fee payment: 2 |
    2015-11-27| PLSC| Search report ready|Effective date: 20151127 |
    2016-05-06| RM| Correction of a material error|Effective date: 20160404 |
    2016-05-13| PLFP| Fee payment|Year of fee payment: 3 |
    2017-04-26| PLFP| Fee payment|Year of fee payment: 4 |
    2018-02-02| CD| Change of name or company name|Owner name: SAFRAN AIRCRAFT ENGINES, FR Effective date: 20170719 |
    2018-04-23| PLFP| Fee payment|Year of fee payment: 5 |
    2019-04-19| PLFP| Fee payment|Year of fee payment: 6 |
    2020-04-22| PLFP| Fee payment|Year of fee payment: 7 |
    2021-04-21| PLFP| Fee payment|Year of fee payment: 8 |
    优先权:
    申请号 | 申请日 | 专利标题
    FR1454559A|FR3021373B1|2014-05-21|2014-05-21|JOINT HINGE DEVICE FOR A TURBOMACHINE.|FR1454559A| FR3021373B1|2014-05-21|2014-05-21|JOINT HINGE DEVICE FOR A TURBOMACHINE.|
    EP15725837.7A| EP3146218B1|2014-05-21|2015-05-07|Ball-joint device for turbomachine|
    PCT/FR2015/051222| WO2015177431A1|2014-05-21|2015-05-07|Ball joint device for a turbine engine|
    US15/312,168| US10626913B2|2014-05-21|2015-05-07|Ball joint device for a turbine engine|
    CN201580031494.2A| CN106460916B|2014-05-21|2015-05-07|Globe joint equipment for turbogenerator|
    CA2949603A| CA2949603A1|2014-05-21|2015-05-07|Ball joint device for a turbine engine|
    RU2016148630A| RU2669502C2|2014-05-21|2015-05-07|Ball joint device for gas turbine engine|
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