• 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 the field of support interfaces, and in particular such a support interface (30a, 30b) for a motor housing (90) comprising a coupling part (50), a first plurality of bolts (80) and a plurality of pawns (70). The coupling piece (50) comprises an outer face (52), having a cavity (42) adapted to receive a support arm (20a, 20b), and an inner face (51), adapted to be mounted on an outer face (93) of the motor housing (90), and a first plurality of orifices (53) between the outer face (52) and the inner face (51) of the coupling piece (50). The bolts (80) each comprise a threaded rod (82) received in an orifice (53) of the first plurality of orifices (53) and a head (81) capable of pressing on the outer face (52) of the piece of coupling (50). Each pin (70) comprises a threaded orifice (71) in which is engaged, through a first end of the pin (70), the threaded rod (82) of one of the bolts (80) of the first plurality of bolts ( 80), and a second enlarged end, adapted to press on an inner face (92) of the motor housing (90).
    公开号:FR3041376A1
    申请号:FR1558744
    申请日:2015-09-17
    公开日:2017-03-24
    发明作者:Margaux Justine Emma Dubois；Nelson Caetano；Alexandre Christophe Adrien Demoulin
    申请人:SNECMA SAS；
    IPC主号:
    专利说明:

    Background of the invention
    The present invention relates to a support interface. More particularly, the invention relates to a support interface for a crankcase, in particular an aeronautical engine such as a turbojet, which is adapted to be used during the manufacture or handling of the engine. The invention also relates to a support device comprising such an interface, an assembly comprising a motor housing and such a support interface, and a method of mounting such an interface on a motor housing.
    When assembling or handling engines, it is often necessary to support the engine in an elevated position to allow easier access to its various components. For this, it is known to form in the outer casing of an engine, and in particular turbine engines turbine, at least two diametrically opposite receiving cavities for receiving each end of a support arm integral with a frame . To support the motor, a support arm is thus introduced into each cavity and fixed to the housing, keeping the motor in a desired position.
    With such a configuration, to ensure a good maintenance of each arm, it is necessary that each cavity has a sufficient useful depth.
    To obtain such a depth, the housing is generally provided with local extra thicknesses, also called bosses, in which the receiving cavities for the arms are machined.
    These extra thicknesses lead to a considerable increase in the weight of the engine. However, for obvious reasons of efficiency, it is desirable that the weight of the engine is minimized and, in particular, it is not impacted by parts having no utility in operation.
    In order to solve this problem, support interfaces have been proposed comprising a coupling part with an external face and an internal face, the external face of this coupling piece having a cavity able to receive a support arm, and the internal face. of this coupling piece being adapted to be mounted on an outer face of the motor housing.
    However, even if these support interfaces of the prior art make it possible to avoid at least partially the excess weight which would result from forming bosses directly on the crankcase, the fixing of these support interfaces on the crankcase is relatively complex and can require the incorporation of fastening means to the housing which also weigh it.
    Object and summary of the invention
    The present disclosure relates to a crankcase support interface for further reducing the additional crankcase mass required for attachment, while allowing for easier attachment with precise positioning on the crankcase. For this, in at least one embodiment, this support interface comprises a coupling part, a first plurality of bolt bodies, and a plurality of pins. The coupling part has an outer face, having a cavity adapted to receive a support arm, and an inner face, adapted to be mounted on an outer face of the motor housing, and a first plurality of orifices between its outer faces. and internal. Each bolt body of the first plurality of bolt bodies includes a threaded shank received in an orifice of the first plurality of orifices and a head adapted to press on the outer face of the coupling member, and each peg of the plurality of pions comprises a threaded orifice in which is engaged, through a first end of the pin, the threaded rod of one of said body of bolts, and a second enlarged end, adapted to press on an inner face of the motor housing.
    The pins at the same time facilitate the positioning and fixing of the coupling piece to the crankcase by the bolt bodies, without having to directly tap holes on the crankcase or use nuts whose access from the inner face of the crankcase. could be difficult.
    To also ensure reliable transmission of forces in at least one plane transverse to one of the bolt bodies, at least one orifice of said first plurality of orifices may have an inner surface complementary to an outer surface of the first end of corresponding pawn. More specifically, at least two orifices of said first plurality of orifices may each have an axisymmetric inner surface complementary to an outer surface of the first end of the corresponding pin, thereby forming together two sliding pivot type links cooperating to immobilize the support interface in all directions relative to the housing.
    Furthermore, to ensure a more reliable support, the coupling piece may have a second plurality of orifices, each orifice of the second plurality of orifices being threaded and opening on the outer face of the coupling piece. The orifices of this second plurality will thus be able to offer an additional mechanical connection, in particular in traction, to a support arm whose end is received in the cavity on the external face of the coupling piece, in particular to avoid an accidental release of this end of the support arm of the cavity in which it is received.
    The present disclosure also relates to a support device comprising a first support interface of the aforementioned type and a first support arm connected to a frame and one end of which is received in the cavity of the coupling part of the first support interface. The interface and the support arm can thus provide a stable connection between the frame and the crankcase. In particular, the coupling piece may have a second plurality of orifices, each orifice of this second plurality of orifices being threaded and opening onto the outer face of the support piece, the device then further comprising a second plurality of bodies. bolts connecting the support arm to the coupling part through the threaded holes of the second plurality of orifices, to avoid in particular an accidental exit of the support arm of the cavity in which it is received.
    Furthermore, the support device may also comprise a second support interface of the same type and a second support arm connected to a frame and one end of which is received in the cavity of the coupling part of the second support interface.
    The present disclosure also relates to an assembly comprising at least one crankcase and a support interface of the aforementioned type, in which the pins are received in orifices passing through an internal face to an external face of the crankcase, with their second ends extended. resting on the inner face of the crankcase. To facilitate assembly of this assembly, the pins can be received under pressure in said holes of the crankcase. Thus, this pressure mounting of the pins prevents their rotation during the engagement of the threaded rods of the bolt bodies of the first plurality in the tapped holes of the pins, thereby facilitating this operation.
    Finally, the present disclosure also relates to a method of mounting a support interface of the above-mentioned type on an engine crankcase, comprising the following steps: introduction, from an internal face of the crankcase, into orifices passing through an inner face to an outer face of the motor housing, each of the pins to its second enlarged end; placing the coupling piece with its inner face on the outer face of the motor housing and the orifices of the first plurality of orifices aligned with the pins; engaging the threaded rods of the first plurality of bolt bodies, through the first plurality of orifices, in the tapped holes of the pins, to immobilize the coupling member with respect to the motor housing.
    BRIEF DESCRIPTION OF THE DRAWINGS The invention will be better understood and its advantages will appear better on reading the detailed description which follows, of an embodiment shown by way of non-limiting example. The description refers to the accompanying drawings in which: - Figure 1 is an overview of an engine, supported by a support device according to an embodiment of the invention; FIG. 2A shows a detail of the support device of FIG. 1, fixed to the crankcase; FIG. 2B shows a cross section of the crankcase, with a part of the support device of FIG. 1, along the plane IIB-IIB in FIG. 2A; - Figure 3A illustrates a first step of a mounting method of the support device of Figure 1, wherein pins are inserted into through holes of the motor housing from an inner face of the motor housing; FIG. 3B illustrates subsequent steps of the mounting method of the support device of FIG. 1, in which a coupling piece is placed on an external face of the motor casing and immobilized thereon with a first plurality of bolts in engagement. with the pawns; and FIG. 3C illustrates final steps of the mounting method of the support device of FIG. 1, in which a support arm is received in a cavity on an external face of the coupling part, and again connected to this piece of support. coupling by a second plurality of bolts.
    Detailed description of the invention
    FIG. 1 shows a support device 100 according to an exemplary embodiment of the invention in cooperation with an annular fan casing 90 of a turbofan engine M. However, such a support device 100 may be applied similarly to any other type of engine comprising a housing.
    In the example, the support device 100 comprises a frame 28, two support arms 20a, 20b connected to the frame and extending along respective longitudinal axes Xa, Xb horizontal, two support interfaces 30a, 30b each provided with a receiving cavity 42 for one of the support arms 20a, 20b.
    Each support interface 30a, 30b is thus intended to connect the housing 90 to a support arm 20a, 20b. In the mounted position on the support device 100, and as will be described in more detail below, the housing 90 is supported by the arms 20a, 20b, through the two support interfaces 30a, 30b.
    Displacement means (not shown) allow the displacement of each arm 20a, 20b, in particular along its longitudinal axis Xa, Xb.
    As illustrated in Figure 1, the support arms 20a, 20b are positioned substantially face to face and so as to provide between them a sufficient reception space for the motor housing 90. In the example, more particularly, the two arms 20a, 20b are coaxial.
    Each arm 20a, 20b comprises, in the example, a distal portion 22 of cylindrical constant section, here circular profile, extending from its end.
    Each arm 20a, 20b further comprises, at a distance from its distal end, an outer collar 24 provided with fixing orifices 26, the function of which will be better apparent from the remainder of this description.
    The first support interface 30a is shown in greater detail in FIGS. 2A and 2B. As illustrated in FIGS. 2A and 2B, each support interface 30a, 30b comprises a coupling piece 50 and means for temporary assembly of this coupling piece 50 on the casing 90. In the example illustrated, the coupling piece 50 comprises an inner face 51, an outer face 52, in which the cavity 42 is formed, and a first plurality of orifices 53 extending from the inner face 51 to the outer face 52, whereas the temporary assembly means comprise a plurality of pins 70 and a first plurality of bolt bodies 80. The second support interface 30b is similar to the first in all respects, with its cavity 42 arranged symmetrically with respect to that of the first support interface 30a, although the configuration geometric coupling part 50, and in particular holes 53 thereon may be different in order to adapt to geometric constraints that may be different from each side casing 90.
    Each pin 70 comprises a threaded orifice 71, opening on a first end 73 of the pin 70, and an enlarged second end forming a flange 72. Each pin 70 is permanently installed in a through hole 91 of the casing 90, with the collar 72 in bearing on an inner face 92 of the housing 90 and the first end 73 projecting from an outer face 93 of the housing 90. The pins 70 are received under pressure in the orifices 91, so as to retain these pins 70 axially and in rotation relative to the housing 90. Each bolt body 80 has a head 81 and a threaded rod 82. The heads 81 bear against the outer face 52 of the coupling member 50, while the threaded rod 82 of each bolt body 80 is complementary to the threaded orifice 71 of a corresponding pin 70 and engaged in this threaded orifice 71 through a corresponding orifice 53 of said first plurality of orifices 53 of the coupling piece 5 0. For this, these orifices 53 are aligned with the pins 70 and the orifices 91 of the housing 90 in which the pins 70 are installed.
    The pins 70 and the bolt bodies 80 thus cooperate to axially retain the coupling piece 50 with its inner face 51 pressed against an outer face 93 of the casing 90. In the embodiment illustrated, each pin 70, whose first end 73, projecting, is in contact with an inner surface of the corresponding orifice 53, also takes forces transverse to the axes of the bolt bodies 80. For this, this inner surface of the orifice 53 and the outer surface of the first end 73 of the corresponding pawn 70 are complementary. They may in particular both be axisymmetrical, in particular cylindrical or conical, so as to form a sliding pivot type connection. Two such connections can thus be enough to immobilize in all directions a coupling piece 50 with respect to the casing 90.
    Moreover, the coupling piece 50 also comprises a second plurality of orifices 54 arranged around the cavity 42. These orifices 54 are threaded and aligned with the fixing orifices 26 of the outer collar 24 of the arm 20a, 20b, so that to be able to receive, through these fixing orifices 26, the threaded rods of bolts 85 connecting the outer collar 24 of the arm 20a, 20b to the coupling piece 50 and taking up tensile forces to prevent an accidental release of the end of the arm 20a, 20b of the cavity 42. It is not necessary that the bolts 85 are tightly tightened, and it may even be preferable to leave some clearance between the heads of the bolts 85 and the outer collar 24 of the arm 20a, 20b corresponding.
    A method of mounting this support device 100 may be described with reference to FIGS. 3A-3C. In a first step of this method, the pins 70 are inserted into pressure in the orifices 91 of the housing 90, from the inner face 92 of the housing 90. It should be noted that this step can be performed before the assembly of the housing 90 around of the turbojet engine M, thus facilitating access to the inner face 92 for the insertion operation of the pins 70.
    In a second step, illustrated in FIG. 3B, the coupling piece 50 is placed on the outer face 93 of the casing 90, with the surfaces 51a, 51b of the internal face 51 of the coupling piece 50 cooperating with the complementary surfaces 93a. 93b of the outer face 93 of the housing 90, and the orifices 53 of its first plurality of orifices of the coupling part 50 aligned with the pins 70 and the orifices 91 receiving them.
    Then, in a third step, also illustrated in Figure 3B, the threaded rods 82 of the bolts 80 are engaged in the threaded holes 71 of the pins 70 through the orifices 53 of the coupling piece 50 and tightened to immobilize the coupling piece 50 relative to the housing 90.
    Once the coupling pieces 50 are thus immobilized with respect to the housing 90 to form the support interfaces 30a, 30b, a fourth step, illustrated in FIG. 3C, for moving each arm 20a, 20b for its insertion into the corresponding cavity 42. Finally, in a fifth step also illustrated in FIG. 3C, the threaded rods of the bolts 85 are engaged in the threaded orifices 54 of each coupling piece 50 through the fastening orifices 26 of the outer collar 24 of the corresponding arm 20a, 20b. to retain each arm 20a, 20b with respect to the corresponding coupling piece 50 and thus prevent accidental disengagement of the arms 20a, 20b. The turbofan engine M can thus be supported by the frame 28 through the arms 20a, 20b, the support interfaces 30a, 30b and the housing 90.
    Each of the second to fifth steps is reversible in reverse order. Thus, if it is desired to separate the turbofan engine M from the frame 28, we first remove the bolts 85, then extract the arms 20a, 20b cavities 42 corresponding. The bolts 80 and the coupling pieces 50 can then be removed to leave on the casing 90 only the pins 70, permanently installed in the orifices 91.
    Although the present invention has been described with reference to a specific exemplary embodiment, it is obvious that various modifications and changes can be made to this example without departing from the general scope of the invention as defined by the claims. Therefore, the description and drawings should be considered in an illustrative rather than restrictive sense.
    权利要求:
    Claims (10)
    [1" id="c-fr-0001]
    A support interface (30a, 30b) for a crankcase (90), comprising: a coupling member (50) with an outer face (52), having a cavity (42) adapted to receive a support arm (20a, 20b), and an inner face (51), adapted to be mounted on an outer face (93) of the motor housing (90), and a first plurality of orifices (53) between the outer face (52) and the inner face (51) of the coupling piece (50); a first plurality of bolt bodies (80), each comprising a threaded rod (82) received in an orifice (53) of the first plurality of orifices (53) and a head (81) capable of pressing on the outer face ( 52) of the coupling piece; and a plurality of pins (70), each comprising a threaded orifice (71) in which is engaged, through a first end (73) of the pin (70), the threaded rod (82) of one of the bolt bodies (80) of the first plurality of bolt bodies (80), and a second enlarged end adapted to press on an inner face (92) of the motor housing (90).
    [2" id="c-fr-0002]
    The support interface (30a, 30b) according to claim 1, wherein at least one orifice (53) of said first plurality of orifices (53) has an inner surface complementary to an outer surface of the first end (73). ) of the corresponding pin (70).
    [3" id="c-fr-0003]
    The support interface (30a, 30b) according to claim 2, wherein at least two orifices (53) of said first plurality of orifices (53) each have an axisymmetric inner surface complementary to an outer surface of the first end (73) of the corresponding pawn (70).
    [4" id="c-fr-0004]
    The support interface (30a, 30b) according to any one of the preceding claims, wherein the coupling piece (50) has a second plurality of orifices (54), each orifice (54) of this second plurality of orifices (54) being threaded and opening on the outer face (52) of the coupling piece (50).
    [5" id="c-fr-0005]
    A support device (100) for a crankcase (90), comprising at least a first support interface (30a, 30b) according to any one of claims 1 to 3, and a first support arm (20a, 20b) ) connected to a frame (28) and one end of which is received in the cavity (42) of the coupling piece (50) of the first support interface (30a, 30b).
    [6" id="c-fr-0006]
    The support device (100) for a crankcase (90) according to claim 5, wherein the coupling part (50) has a second plurality of orifices (54), each orifice (54) of this second plurality of the orifices (54) being threaded and opening on the outer face (52) of the coupling member (50), the support device (100) further comprising a second plurality of bolt bodies (85) connecting the first support (20a, 20b) to the coupling piece (50) through the orifices (54) of this second plurality of orifices (54).
    [7" id="c-fr-0007]
    A support device (100) for a crankcase according to any one of claims 5 or 6, comprising a second support interface (30a, 30b) according to any one of claims 1 to 4, and a second support arm support (20a, 20b) connected to a frame (28) and one end of which is received in the cavity (42) of the coupling piece (50) of the second support interface (30a, 30b).
    [8" id="c-fr-0008]
    8. An assembly comprising at least one crankcase (90) and a support interface (30a, 30b) according to any one of claims 1 to 4, wherein the pins (70) are received in orifices (91) passing through an inner face (92) to an outer face (93) of the motor housing (90), with their second widened ends bearing against the inner face (92) of the motor housing (90).
    [9" id="c-fr-0009]
    9. The assembly of claim 8, wherein the pins (70) are received under pressure in said orifices (91) of the motor housing (90).
    [10" id="c-fr-0010]
    10. A method of mounting a support interface (30a, 30b) according to any one of claims 1 to 4 on a motor housing (90), comprising the steps of: introduction from an inner face (92) of the housing motor (90), in orifices (91) passing from an inner face (92) to an outer face (93) of the motor housing (90), each of the pins (70) to its widened second end; placing the coupling piece (50) with its inner face (51) on the outer face (93) of the motor housing (90) and the orifices (53) of the first plurality of orifices (53) aligned with the pins ( 70); engaging the threaded rods (82) of the first plurality of bolt bodies (80) through the first plurality of orifices (53) in the threaded holes (71) of the pins (70) to immobilize the workpiece coupling (50) relative to the crankcase (90).
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    同族专利:
    公开号 | 公开日
    CN108138586B|2020-09-01|
    WO2017046536A1|2017-03-23|
    US10697327B2|2020-06-30|
    CN108138586A|2018-06-08|
    EP3350420A1|2018-07-25|
    FR3041376B1|2017-11-17|
    EP3350420B1|2022-01-12|
    US20180283215A1|2018-10-04|
    引用文献:
    公开号 | 申请日 | 公开日 | 申请人 | 专利标题
    US4202539A|1978-11-15|1980-05-13|Avco Corporation|Engine work stand|
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    FR3085710A1|2018-09-12|2020-03-13|Safran Aircraft Engines|REMOVABLE SUPPORT INTERFACE FOR TURBOMACHINE ANNULAR HOUSING|WO2000009861A2|1998-08-12|2000-02-24|ETN Präzisionstechnik GmbH|Support devices for the vanes of power units|FR3017112B1|2014-02-03|2017-09-29|Snecma|TRANSPORT AND HINGING STRUCTURE FOR TURBOMACHINE|
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    法律状态:
    2016-09-08| PLFP| Fee payment|Year of fee payment: 2 |
    2017-03-24| PLSC| Publication of the preliminary search report|Effective date: 20170324 |
    2017-05-15| PLFP| Fee payment|Year of fee payment: 3 |
    2018-08-22| PLFP| Fee payment|Year of fee payment: 4 |
    2018-09-14| CD| Change of name or company name|Owner name: SAFRAN AIRCRAFT ENGINES, FR Effective date: 20180809 |
    2019-08-20| PLFP| Fee payment|Year of fee payment: 5 |
    2020-08-19| PLFP| Fee payment|Year of fee payment: 6 |
    2021-08-19| PLFP| Fee payment|Year of fee payment: 7 |
    优先权:
    申请号 | 申请日 | 专利标题
    FR1558744A|FR3041376B1|2015-09-17|2015-09-17|INTERFACE AND SUPPORT DEVICE FOR CRANKCASE|FR1558744A| FR3041376B1|2015-09-17|2015-09-17|INTERFACE AND SUPPORT DEVICE FOR CRANKCASE|
    US15/760,930| US10697327B2|2015-09-17|2016-09-15|Support interface and device for an engine casing|
    EP16785191.4A| EP3350420B1|2015-09-17|2016-09-15|Engine crankcase supporting device and interface|
    CN201680058721.5A| CN108138586B|2015-09-17|2016-09-15|Engine crankcase support apparatus and interface|
    PCT/FR2016/052341| WO2017046536A1|2015-09-17|2016-09-15|Engine crankcase supporting device and interface|
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