• 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 bearing of a lubricated pale foot comprising a coating of chemical compound lamellar structure.
    公开号:FR3045561A1
    申请号:FR1562656
    申请日:2015-12-17
    公开日:2017-06-23
    发明作者:Abdelounis Houcine Ben；Eric Gard
    申请人:NTN SNR Roulements SA；
    IPC主号:
    专利说明:

    FIELD OF THE INVENTION The invention relates to the field of bearings of a blade root, in particular bearings of a blade root comprising a coating of chemical compound lamellar structure and a lubricant.
    Context of the invention
    A standard bearing comprises an inner ring fixed on a shaft, and an outer ring, concentric, between which is formed a raceway. Rolling bodies are arranged in this raceway. Conventionally the outer ring is fixed and the inner ring rotates, the opposite mounting being possible. Rolling bodies have very little contact with the inner and outer rings to scrub as little as possible and limit warming.
    The bearing also includes a lubricant, usually a grease or an oil. Lubrication is an essential element for the proper functioning of the bearing. 70% of bearing damage is due to lubrication problems. The purpose of the lubrication is to interpose a lubricant film (called an oil film) between the rolling bodies and the raceway, in order to limit the metal-to-metal contact, the heating, the wear and the seizing of the elements. contact. The lubricant can also provide protection against oxidation and external pollution.
    The bearing of a blade root is one of the different existing bearings used in the field of aeronautics. Applications FR2862609 and FR2817233 describe such a bearing.
    This bearing is used to orient the blades of a propeller motor, depending on the phase of flight (take-off, cruise, landing, ...). H is positioned eccentrically with respect to the axis of rotation of the motor rotor and is constantly rotating about the axis of rotation of the rotor. Due to this eccentric position relative to the axis of rotation of the rotor, the rolling of a blade root is subjected to a large centrifugal force and high applied forces. The centrifugal force and the high applied forces will subject the rolling of a blade root to a high contact pressure, of the order of 3 GPa.
    As for the blade, it slowly moves around its longitudinal axis over a small angular range (-30 °, + 90 °) through the inner ring and the outer ring of the bearing. If the relative movement of the two rings is limited, the vibrations oscillate permanently both rings with very small deflections generating oscillating conditions.
    This high contact pressure and the oscillating conditions have the effect of driving the lubricant contained in the bearing outside the contact zones. In addition, the centrifugal forces applied to the bearing result in a projection of the lubricant towards the outside of the bearing, particularly over the high operating range in temperature. These projections cause a loss of lubrication and consequently the deterioration of the rolling of one foot of pale and decreasing its life.
    In addition to this high contact pressure and the oscillating conditions, the rolling of a blade root is subjected to a large temperature range that can range from -55 ° C (outdoor temperature at altitude) to + 170 ° C (because the location near the engine). The bearing of a blade root must be lubricated over this wide temperature range.
    The bearing must therefore be lubricated over a wide range of temperatures under severe conditions involving imposed contact pressure and oscillating conditions. These conditions are antinomic because for the bearing to be well lubricated, it is necessary that the lubricant is capable of re-energizing the contact over the entire temperature operating range, without freezing at the minimum temperatures or being expelled to the maximum temperatures under the effect of centrifugal efforts. On the other hand, to resist the contact pressure and the centrifugal forces, the lubricant must be as viscous as possible even at the high temperatures encountered during engine speeds generating the largest centrifugal forces.
    Surprisingly, the Applicant has found a complex tribological system for optimizing the operation of a rolling blade foot. This complex tribological system employs a blade root bearing comprising a lamellar chemical compound coating and a lubricant. In fact, the combination of the lamellar structure chemical compound and the lubricant allows the rolling of a blade root to be lubricated despite the high contact pressure and oscillations, and for the wide range of temperatures at which it is submitted.
    Thus, the subject of the invention is, according to a first aspect, a rolling of a blade root extending in a longitudinal direction between a proximal end and a distal end, the rolling of a blade root comprising a ring an outer surface having an inner surface and an outer surface opposite to the inner surface, the inner surface of the outer ring having an outer raceway, - an inner ring having an inner surface and an outer surface opposite the inner surface, the outer surface of the inner race having an inner raceway, - a single interior space being defined between the inner surface of the outer race and the outer surface of the inner race, the single interior space extending between a proximal end where it is closed by a proximal sealing system between the outer ring and the inner ring and a distal end where it is closed by a distal sealing system between the outer ring and the inner ring, said single inner space containing a lubricant, - a row of rolling bodies having a contact surface mounted in the inner space single, rolling on the outer and inner races, and characterized in that at least one of the raceways and / or the contact surface of the rolling bodies is (are) covered (s) with a chemical compound coating with lamellar structure. The invention also relates to a rolling of a blade root extending in a longitudinal direction between a proximal end and a distal end, the bearing allowing an oscillation of the foot about an axis extending in the longitudinal direction relative to a housing, the bearing of a blade root comprising: - a single outer ring having an inner surface and an outer surface opposite to the inner surface, the inner surface of the outer ring having a first proximal outer raceway and a second distal outer raceway, the first and second outer raceways being offset relative to each other in the longitudinal direction, - a first inner race having an inner surface and an outer surface opposite the inner surface, the outer surface of the first inner ring having a first proximal inner raceway and a distal seat, the first inner raceway and the seat being offset relative to each other in the longitudinal direction, - a second inner race having an inner surface and an opposing outer surface on the inner surface, the outer surface of the second inner race having a second distal inner race, the second inner race being fitted on the seat and being held axially abutting against the first inner race, - a single interior space being defined between the inner surface of the outer ring and the outer surface of the first and second inner rings, the single inner space extending between a proximal end where it is closed by a proximal sealing system between the outer ring and the first ring inner and one distal end wherein it is closed by a distal sealing system between the outer ring and the second inner ring, said single inner space containing a lubricant, - a first proximal row of rolling bodies having a contact surface mounted in the single inner space, on the first proximal outer and inner raceways and a second distal row of rolling bodies having a contact surface mounted in the single interior space, rolling on the second outer and inner distal raceways, the first and second rows of rolling bodies being spaced from each other along the longitudinal axis, - the inner surface of the first inner ring comprising an assembly shoulder to a blade root, - the outer surface of the single outer ring comprising a shoulder assembly to a housing. and characterized in that at least one of the raceways and / or the contact surface of the rolling bodies of one of the rows of rolling bodies is (are) covered (s) with a coating of chemical compound lamellar structure.
    According to a second aspect, the invention also relates to a lubricant for rolling a blade root characterized in that it comprises a chemical compound lamellar structure.
    According to a third aspect, the invention also relates to a use of a lubricant comprising a chemical compound with lamellar structure for lubricating the rolling of a blade root.
    According to a fourth aspect, the subject of the invention is a method for manufacturing a bearing of a blade root, characterized in that it comprises a step of depositing a chemical compound coating with a lamellar structure and a step of application of a lubricant.
    Description of figures
    Figure 1 is a block diagram in perspective of a rotor.
    Figure 2 is a sectional view of a particular embodiment of a blade foot bearing.
    Figure 3 shows two microscopies of traces of wear after a tribological test on: the surface of a plate not covered with a coating of WS2 and lubricated (surface SI, above), and - the surface of a covered plate a WS2 coating and lubricated (surface S2, bottom).
    Detailed description of the invention
    According to a first aspect, the present invention relates to a bearing of a blade root extending in a longitudinal direction between a proximal end and a distal end, the bearing of a blade root comprising - an outer ring having an inner surface and an outer surface opposite to the inner surface, the inner surface of the outer ring having an outer raceway, - an inner ring having an inner surface and an outer surface opposite to the inner surface, the outer surface of the inner ring having an inner raceway, - a single interior space being defined between the inner surface of the outer ring and the outer surface of the inner ring, the single inner space extending between a proximal end where it is closed by a system of Proximal seal between the outer ring and the ring in and a distal end where it is closed by a distal sealing system between the outer ring and the inner ring, said single inner space containing a lubricant, - a row of rolling bodies having a contact surface mounted in the inner space single, rolling on the outer and inner races, and characterized in that at least one of the raceways and / or the contact surface of the rolling bodies is (are) covered (s) with a chemical compound coating with lamellar structure.
    A chemical compound with a lamellar structure is a compound whose crystalline structure consists of two-dimensional sheets (along the x and y axes) stacked along the third dimension (along the z axis). The bonds between the atoms within the layers are strong, whereas those between the atoms of two layers are weak.
    The chemical compound with a lamellar structure is chosen from fluorine carbides, graphite, M0S 2, WS 2 WSe 2, NB, ZnO, ZnS and SnS, preferably chosen from graphite, M0S 2 and WS 2, more preferably still the chemical compound with lamellar structure. is WS2. WS2 is preferred because it is chemically inert, it is particularly compatible with solvents, fuels, oils, bases and acids. In addition, it is not intrinsically hard, thus, in the case where particles of WS2 detach from the coating of chemical compound lamellar structure, these particles would not hinder the smooth operation of the bearing of a blade root. The difference in the bond strength between the atoms gives the lamellar chemical compound a lubricating property.
    Advantageously, this lubrication property is present over a wide temperature range. For example, WS2 can lubricate a bearing from -188 ° C to + 538 ° C. The chemical compound coating with lamellar structure, in particular WS2, advantageously makes it possible to lubricate the rolling of a blade root, in particular the rolling bodies with respect to the coated raceway, over the entire range of temperatures at which the rolling of a blade root is subjected.
    The solid WS2 coating remains lubricant up to a contact pressure of the order of 3 GPa. Thus, a chemical compound coating with lamellar structure, in particular WS2, advantageously makes it possible to lubricate the rolling of a blade root, in particular the rolling bodies with respect to the coated raceway, irrespective of the stress which said bearing is subjected during the use for which it is designed.
    In addition, the chemical compound coating lamellar structure strongly adheres to the surface of the raceway on which it is present. The coating of chemical compound with lamellar structure does not come off despite the high contact pressure and the oscillating conditions to which the rolling of a blade root is subjected.
    According to one embodiment, the thickness of the coating is from 0.2 μm to 2 μm, in particular from 0.5 μm to 1.75 μm, more particularly from 0.8 μm to 1.5 μm.
    In one embodiment, the lubricant is a grease comprising a base oil and a thickener. The base oil of a grease contributes to the lubricating power of the grease, its thermal resistance, its resistance to the load and, consequently, its service life. A synthetic ester oil, polyalphaolefme, perfluoropolyether, used alone or in admixture, are particularly suitable as the base oil for the grease of the lubricant of the present invention. These synthetic oils are those usually used in the grease field and known to those skilled in the art. The thickener confers its structure on the grease by fixing the base oil, determines the behavior of the grease in terms of heat resistance, resistance to the load, water, its consistency and its flow capacities. It also helps to form the lubrication film. Depending on the fat used, the thickeners may be soapy or non-soapy type. The soapy thickeners used may be metal soaps (lithium) or complex metal soaps (aluminum, lithium, calcium, sodium) and non-soap thickeners may be organic or non-organic compounds (bentonite, bentone, polyresin, silica, polyurea, etc.). .). Polyurea, a lithium complex metal soap, and a sodium complex metal soap are particularly suitable as the lubricant grease thickener of the present invention.
    In particular, the grease comprises an ester-perfluoropolyether and polyurea mixture; polyalphaolefins and a lithium complex metal soap; an ester-polyalphaolefin mixture and a sodium complex metal soap; or a synthetic oil and a lithium complex metal soap. Preferably, the fat comprises a mixture of polyalphaolefins and lithium complex metal soap or a mixture of synthetic oil and complex metal soap.
    The grease may also include additives such as anti-corrosion additives, extreme pressure additives, antioxidants.
    The operating temperature range of the grease ranges from a lower temperature limit to a higher temperature performance limit. The lower temperature limit is the lowest temperature at which the grease allows the ride to start without difficulty. Below this limit, lubrication is insufficient and may cause bearing failure. Above the upper temperature performance limit, the grease breaks down uncontrollably and its service life is no longer guaranteed.
    The lower temperature limit of the grease of the lubricant according to the invention can be from -70 ° C. to -20 ° C., in particular from -60 ° C. to -30 ° C., more particularly from -55 ° C. to -40 ° C. ° C.
    The upper temperature performance limit of the lubricant grease according to the invention may be greater than or equal to 170 ° C, in particular from 170 ° C to 210 ° C, more preferably from 175 ° C to 200 ° C.
    Advantageously, these temperature ranges allow the lubricant to have a lubricating property for lubricating the rolling of a blade root over the entire range of temperatures to which said bearing is subjected.
    According to one embodiment, the grease has a drop point of 200 ° C. to 350 ° C., in particular of 220 ° C. to 300 ° C., more particularly of 240 ° C. to 285 ° C. as measured by the NF method. T 60-627.
    According to the NF T 60-627 method, the drop point corresponds to the temperature at which a heated grease sample begins to flow through a standardized orifice.
    Advantageously, the drop point of the grease is greater than the maximum temperature of the temperature range at which the rolling of a blade root is subjected. The grease of the lubricant according to the invention does not liquefy in this temperature range and will not be easily projected outwardly of the bearing of a blade root in which the lubricant is used, but on the contrary, will allow lubricating said bearing to the elevated temperatures to which it may be subjected.
    The NLGI grade, established by the National Lubricating Grease Institute, is a widely used classification for fats. It is measured by the ASTM D217 method. It allows to classify the fats in nine grades according to their consistency.
    A grease having a NLGI grade greater than 0, in particular from 1 to 5, more particularly from 2 to 3 as measured by the ASTM D217 method, is particularly suitable for the lubricant according to the invention. In fact, a grease having a NLGI grade in these ranges of values has the best ratio between the resistance to the stresses undergone and the friction generation of the surfaces in contact in the rolling of a blade root, so it is more resistant to the stresses undergone. by the lubricant and limits the risk of projection of said lubricant according to the invention to the outside of said bearing.
    According to one embodiment, the base oil exhibits a kinematic viscosity at 40 ° C. of greater than or equal to 40 mm 2 s -1, in particular of 45 mm 2 s -1 to 250 mm 2 s -1, more particularly from 50 mm2.s4 to 220 mm2.s "1 as measured by the method NF T 60-100.
    Kinematic viscosity is the measurement of the resistance of a fluid to the flow. Since the kinematic viscosity varies according to the temperature, it is measured at 40 ° C., in accordance with the NF T 60-100 method.
    Advantageously, a base oil having a kinematic viscosity in the ranges above allows the lubricant according to the invention to have a lubricating property such that surfaces in contact in the bearing of a blade root do not rub. too much, which promotes the life of said bearing.
    The lubricant may further comprise the chemical compound having a lamellar structure of the coating.
    As explained above, in connection with the coating, the lamellar structure chemical has a lubricating property over a wide temperature range. Advantageously, the combination of the lubricant and the lamellar structure chemical allows the lubricant to exhibit a lubricating property over the entire range of temperatures at which a blade root bearing is subjected.
    Without wishing to be bound by any theory, the inventors believe that the chemical compound with a lamellar structure included in the lubricant interacts with the lamellar structure chemical compound coating in order to reform it in the event that said coating is damaged during use. of the rolling of a blade root. Advantageously, this interaction increases the life of the coating.
    According to one embodiment, the content of chemical compound with a lamellar structure in the lubricant is from 1% to 10% by weight, in particular from 2% to 7% by weight, more particularly from 3% to 5% by weight. relative to the weight of the fat.
    Levels of chemical compound with lamellar structure out of the ranges below can destabilize the lubricant according to the invention, that is to say make it lose its lubricating property.
    In order to improve the lubrication of the bearing of a blade root, the coating of chemical compound with lamellar structure may preferentially cover the two raceways. In order to facilitate the deposition of the coating, said coating may, more preferably still, be deposited on the entire inner surface of the outer ring and / or on the entire outer surface of the inner ring. The contact surface of the rolling bodies can also be covered with the lamellar chemical compound coating.
    According to one embodiment, the surface of the raceway covered by the coating is rough.
    The chemical compound coating with lamellar structure follows the shapes of the roughness of the surface to which it is applied. Advantageously, the roughness of the surface allows the formation of surface crevices in which the lubricant and any wear particles of the rolling of a blade root or said coating can be trapped. This surface roughness allows retention of the lubricant in the contact zone despite the oscillating conditions. This surface roughness also reduces the risk that the wear particles play a role of abrasive particles altering the operation of the bearing of a blade root. The surface roughness therefore increases the life of the bearing of a blade root.
    According to one embodiment, the metallurgical characteristics of one of the surfaces of a race covered by the coating can be improved, in particular the residual stresses can be increased, thus increasing the life of the bearing of a foot of blade.
    According to one embodiment, the material of the outer ring and the material of the inner ring are selected from the grades of rolling steels, independently of one another, among OOCr0, M50, M50NlL, 32CrMoV13 nitrided, 16NiCrMol3 cemented, in particular is M50NÎL.
    According to one embodiment, the material of the rolling bodies is selected from M50, 1000 * 6, S3N4, in particular is M50.
    The present invention also relates to a rolling of a blade root extending in a longitudinal direction between a proximal end and a distal end, the bearing allowing an oscillation of the foot about an axis extending in the longitudinal direction relative to a housing, the bearing of a blade root comprising: - a single outer ring having an inner surface and an outer surface opposite to the inner surface, the inner surface of the outer ring having a first proximal outer raceway and a second distal outer raceway, the first and second outer raceways being offset relative to each other in the longitudinal direction, - a first inner race having an inner surface and an outer surface opposite the inner surface, the outer surface of the first inner ring pr sensing a first proximal inner raceway and a distal seat, the first inner raceway and the seat being offset relative to each other in the longitudinal direction, - a second inner race having an interior surface and a surface outer surface opposite to the inner surface, the outer surface of the second inner race having a second distal inner race, the second inner race being fitted on the seat and being held axially abutting against the first inner race, - a single interior space being defined between the inner surface of the outer ring and the outer surface of the first and second inner rings, the single inner space extending between a proximal end where it is closed by a proximal sealing system between the outer ring and the outer ring. first inner ring and one end distal tee where it is closed by a distal sealing system between the outer ring and the second inner ring, said single inner space containing a lubricant, - a first proximal row of rolling bodies having a contact surface mounted in the inner space single, rolling on the first proximal outer and inner raceways and a second distal row of rolling bodies having a contact surface mounted in the single interior space, rolling on the second distal outer and inner raceways, the first and second rows of rolling bodies being spaced from one another along the longitudinal axis, - the inner surface of the first inner ring comprising an assembly shoulder to a blade root, - the outer surface of the single outer ring comprising an assembly shoulder to a housing. and characterized in that at least one of the raceways and / or the contact surface of the rolling bodies of one of the rows of rolling bodies is (are) covered (s) with a coating of chemical compound lamellar structure.
    The lamellar structure chemical compound coating and the lubricant of this particular blade foot bearing are as described above.
    A detailed discussion of this particular blade foot bearing, with reference to FIGS. 1 and 2, is presented below.
    Figure 1 shows schematically in three-dimensional perspective an example of a rotating system 1 according to an exemplary implementation of the invention. The rotating system 1 comprises a hub (not shown) of axis A around which is rotatably mounted a rotor 2. The rotor 2 rotates relative to the hub about the axis A. The rotor 2 comprises a main body 3, for example symmetrical revolution about the axis A. The rotor 2 also comprises one or more blades 4 (in the example, three blades 4), each extending radially relative to the hub. Each blade 4 extends along a longitudinal axis B. A blade can have a very complex shape, it is difficult to very precisely define the longitudinal axis B, except that it corresponds to the main direction of the blade 4. Also, when we say that the blade 4 extends "radially", it does not necessarily imply that the axis B intersects the axis A or extends in a plane perpendicular to the axis A, but the general direction of the blade 4 is radial.
    The blade 4 extends between one end, called blade root 4a, where it is assembled to the main body 3, and an opposite end 4b free. The blade 4 is mounted, at its foot 4a, in a housing 5 integral with the main body 3. The blade 4 is oscillatingly mounted in the housing 5 via a bearing (described in detail below) mounted between the blade root 4a and the housing 5. The bearing in question has a rolling axis, and the oscillation of the blade 4 relative to the housing 5 is allowed with respect to this axis. The axis in question is clearly defined and extends substantially along the axis B. To fix the ideas, we can consider that the axis B corresponds to the axis of the bearing and, subsequently, we will call B the bearing axis.
    In operation, the blade 4 will rotate relative to the housing 5 around the axis B, but a priori on an angular stroke less than 360 °. By cons, the blade 4 will oscillate relative to the housing 5 around the axis B by controlled back and forth movements, according to the forces transmitted by the blade to the fluid (air) surrounding.
    The housing 5 is any component allowing this implementation.
    As explained above, the bearing is therefore eccentric with respect to the axis A, and is therefore subjected to strong centrifugation around this axis A during the implementation of the rotating system 1.
    The present invention is applicable to other bearings oscillating about a radial axis and centrifuged about an axial axis.
    In what follows, the term "axial" refers to the axis B of this bearing 7, parallel to the direction (B) shown. The term "proximal" refers to the proximity of a component to axis A, while the term "distal" refers to the distance of a component from axis A.
    The bearing 7 thus comprises a proximal side 8 and a distal side 9, opposite to the proximal side 8.
    The bearing 7 defines an inner bore 10 in which the blade root 4 is intended to be mounted.
    In what follows, the term "inside" is used to designate the proximity to the B axis, while the term "outside" is used to designate the distance from the B axis.
    The bearing 7 comprises a first inner ring 11, a second inner ring 12, and a single outer ring 13. The inner rings 11 and 12 are so called because they each comprise an inner race for rolling bodies, and the outer ring 13 is so called because it has outer raceways for rolling bodies, as will be explained more in detail thereafter.
    The first inner ring 11 includes an inner surface 14 and an outer surface 15 opposite the inner surface 14. The inner surface 14 is used for mounting the bearing 7 on the blade root. The inner surface 14 has a minimum shaft diameter. The first inner ring 11 extends axially from the proximal side 8 towards the distal side 9, over a great majority of the axial length of the bearing 7.
    In the distal half of the bearing 7, the outer surface 15 defines a distal seat 16 for receiving the second inner ring 12. The distal seat 16 comprises an axial abutment surface 17 facing the distal side 9, and a cylindrical surface of receiving 18 facing outwards, and extending from the axial abutment surface 17.
    In the proximal half of the bearing 7, the outer surface 15 defines a first proximal raceway 23.
    The first inner ring 11 has a proximal end surface 19. The inner surface 14 of the first inner ring 11 comprises a shoulder 20 of assembly to a blade root. The shoulder 20 comprises a cylindrical surface 21 extending from the proximal end surface 19 towards the distal end, an axial abutment surface 22 facing the proximal side 8, and extending from the cylindrical surface 21 to the bore 10.
    The first inner ring 11 has a distal end surface 27 opposite to the axial abutment surface 22 and facing the distal side 9.
    The second inner ring 12 comprises an inner surface 24 and an outer surface 25 opposed to the inner surface 24. The inner surface 24 is used for mounting the second inner ring 12 in the seat 16 of the first inner ring by fitting. The inner surface 24 therefore faces, complementary to, the cylindrical receiving surface 18. The second inner ring 12 extends axially from a first axial abutment surface 26 facing the proximal side 8 towards the distal side 9, about one half distal of the axial length of the bearing 7.
    The outer surface 25 defines a second distal raceway 28.
    The second inner ring 12 has a distal end surface 29. The inner surface 24 of the second inner ring 11 includes a pre-load shoulder 30. The shoulder 30 includes a cylindrical surface 31 extending from the distal end surface 29 toward the proximal end, an axial abutment surface 32 facing the distal side 9, and extending from the cylindrical surface 31 to the cylindrical receiving surface 18.
    The outer ring 13 includes an inner surface 33 and an outer surface 34 opposite to the inner surface 33. The outer surface 34 is used to mount the bearing 7 to the housing. The outer ring 13 extends axially from the proximal side 8 to the distal side 9, over the entire axial length of the bearing 7.
    In the proximal half of the bearing 7, the inner surface 33 defines a second proximal raceway. In the distal half of the bearing 7, the inner surface 33 defines a second distal race 36.
    The outer ring 13 has a proximal end surface 37 and a opposed distal end surface 38. The outer surface 34 includes a shoulder 39 for assembly to the housing. The shoulder 39 includes a cylindrical surface 40 extending from the distal end surface 38 toward the proximal end, an axial abutment surface 41 facing the distal side 9, and extending from the cylindrical surface 40 to a second cylindrical surface 42. The second cylindrical surface 42 extends from the axial abutment surface 41 to the proximal end surface 37.
    A single interior space 43 is defined between the inner surface 33 of the outer ring 13 and the outer surface 15, 25 of the first and second inner rings 11, 12, the single inner space 43 extending between a proximal end 44 where it is closed by a proximal sealing system 45 between the outer ring 13 and the first inner ring 11 and a distal end 46 where it is closed by a distal sealing system 47 between the outer ring 13 and the second inner ring 12.
    At the single interior space 43, the first proximal outer and inner raceways 23, 35 face each other, and the second distal outer and inner raceways 28, 36 face each other.
    A first proximal row of rolling bodies 48 having a contact surface is mounted in the single interior space, rolling on the first proximal outer and inner raceways 23, 35. A second distal row of rolling bodies 49 having a contact surface is mounted in the single interior space, rolling on the second distal outer and inner raceways 28, 36. The first and second rows of rolling bodies 48, 49 are spaced from one another along the longitudinal axis B .
    The rolling bodies of the same row are optionally spaced from each other by a cage 50, as shown in Figure 2 for the proximal row.
    The bearing 7 comprises a loading system 51 adapted to hold the second inner ring 12 axially abutting against the first inner ring 11.
    The loading system 51 comprises an annular plate 52 having a bearing surface 53 in contact with the second inner ring 12 and biasing the second inner ring 12 in the axial direction, the annular plate 52 being held integral with the first inner ring 11 by screwing with the aid of screws 54. More specifically, the plate 52 is screwed on the inner ring 51 by screws passing through bores 55 of the plate 52 and bores 56 of the first inner ring 11 matched with the bores. 55. The bearing surface 53 presses on the axial abutment surface 32, thus urging the second inner ring 12 towards the proximal side, these clamping forces being found at the level of the contact between the axial abutment surface 17 of the first inner ring 11 and the axial abutment surface 26 of the second inner ring 12. The screws are tightened until a loading force is applied
    Preload · The shoulder 39 of the assembly to the housing, in particular the axial abutment surface 41 thereof, provided on the outer surface 34 of the single outer ring 13, is arranged axially (in the direction (B)) between the first and second rows of rolling bodies, that is to say substantially in the middle, axially, of the length of the bearing 7. The shoulder 20 assembly at the blade root, provided on the inner surface 14 of the first Inner ring 12 is disposed more proximal than the first proximal row 48 of rolling bodies.
    Thus, the axial forces experienced by the bearing are essentially supported by the first proximal row 48 of rolling bodies.
    In the example above, the rolling bodies of the two rows of rolling bodies have the same type of geometry. Instead of the rollers, other types of rolling bodies could be used, for example balls.
    In order to improve the lubrication of the bearing of a blade root 7 described above, the coating of chemical compound with lamellar structure can cover at least two raceways, preferably at least three raceways, more preferably all the raceways. In order to facilitate the deposition of the coating, said coating may, more preferably still, be deposited on the whole of the inner surface of the single outer ring, on the whole of the outer surface of the first inner ring and / or on the outside. set of the outer surface of the second outer ring. The contact surface of the rolling bodies of the first proximal row and / or the contact surface of the second distal row may also be covered with the lamellar structure chemical coating.
    According to a second aspect, the present invention also relates to a lubricant for rolling a blade root characterized in that it comprises a chemical compound lamellar structure.
    The lubricant is as described above in the section devoted to the rolling of a blade root.
    As explained above, in connection with the rolling coating of a blade root, the chemical compound with lamellar structure has a lubricating property over a wide temperature range. Advantageously, the combination of the lubricant and the lamellar chemical compound allows the lubricant to exhibit a lubricating property over the entire temperature range at which a blade foot bearing is subjected.
    According to one embodiment, the content of chemical compound with a lamellar structure in the lubricant is from 1% to 10% by weight, in particular from 2% to 7% by weight, more particularly from 3% to 5% by weight. relative to the weight of the fat.
    Levels of chemical compound with lamellar structure out of the ranges below can destabilize the lubricant according to the invention, that is to say make it lose its lubricating property.
    According to a third aspect, the present invention relates to the use of the lubricant comprising a chemical compound with lamellar structure for lubricating the rolling of a blade root.
    As explained above, in the lubricant section, the combination of the lubricant and the lamellar structure chemical compound allows the lubricant to have a lubricating property regardless of the stress and temperature at which a rolling of a foot of blade is subject. This combination can therefore be used to lubricate a bearing of a blade root.
    In particular, the lubricant can be used to lubricate the bearing of a blade root object of the invention.
    Without wishing to be bound by any theory, the inventors believe that the chemical compound with a lamellar structure included in the lubricant interacts with the lamellar structure chemical compound coating in order to reform it in the event that said coating is damaged during use. of the rolling of a blade root. Advantageously, this interaction increases the life of the coating.
    In particular, the lubricant can be used to lubricate the rolling bodies with respect to the rolling path of the blade foot bearing. The invention also relates to a manufacturing method of the rolling of a blade root described above, characterized in that it comprises the following steps: a) deposition of a coating of chemical compound lamellar structure on one of the paths and / or on the contact surface of the rolling bodies, and b) applying a lubricant in the single interior space.
    The lamellar chemical compound coating and the lubricant of this particular blade foot bearing are as described in the bearing section.
    The chemical compound coating with lamellar structure can be deposited by any deposition techniques on a surface known to those skilled in the art. In particular, the coating may be deposited by propulsion in a conditioned gas of the chemical compound with lamellar structure on the surface to be coated. Such a technique is very advantageous because it allows cold deposition, at high speed, without heat input or polymerization. It is therefore economical and fast.
    The lubricant is applied in the single interior space of the bearing by any lubricant deposition techniques known to those skilled in the art. Lubricant can be applied manually, by a grease gun or an automatic lubricator. In particular, the lubricant may be applied to the chemical compound coating with lamellar structure deposited on one of the raceways and / or on the contact surface of the rolling bodies.
    According to one embodiment, the method may further comprise a preliminary step of treating the surface having the raceway on which the coating is deposited during step a).
    This preliminary stage of treatment of the surface increases the roughness of said surface. It can be performed by any techniques known to those skilled in the art for increasing the roughness of a surface. In particular this preliminary step is carried out by shot blasting. Advantageously, shot peening also improves the metallurgical characteristics, in particular by increasing the residual stresses, of the treated surface, thus improving the life of the rolling of a blade root.
    According to one embodiment, the method may comprise a tribofinishing step in order to adjust the roughness obtained during the preliminary surface treatment step.
    Examples
    Example 1: Tribological test of a surface covered with a chemical compound coating lamellar structure.
    The surface, SI, of a plate (in M50NIL) is subjected to a tribological test using a ball (in M50) according to the parameters of Table 1 below.
    To study the impact of the WS2 coating, the surface, S2, of a WS2-coated (M50NiL) plate is subjected to the same test.
    After the tests, the state of the SI and S2 surfaces is analyzed.
    Table 1: Parameter of the tribological test
    As illustrated in FIG. 3, the wear trace on the surface S1 is wider and deeper than that on the surface S2. The WS2 coating therefore makes it possible to better lubricate the area of contact between the surface and the ball. The WS2 coating therefore makes it possible to extend the service life of a bearing of a blade root.
    EXAMPLE 2 Tribological Test of a Shot-Milled Surface Coated with a Lamellar Structure Chemical Coating
    The surface, S3, of a plate (M50NIL) treated by shot blasting then covered with a WS2 coating, is subjected to a tribological test using a ball (in M50) according to the parameters of table 1 above. .
    After the test, the state of the surfaces S3 and S2 is analyzed.
    The wear trace on the surface S3 is less extensive and shallower than that on the surface S2 of Example 1. The shot blasting treatment combined with the WS2 coating therefore makes it possible to better lubricate the contact zone between the surface and the surface. the ball that the coating in WS2 alone. This combination therefore makes it possible to extend the life of a bearing of a blade root.
    权利要求:
    Claims (15)
    [1" id="c-fr-0001]
    1. Bearing of a blade root (7) extending in a longitudinal direction between a proximal end and a distal end, the bearing of a blade root (7) comprising - an outer ring (13) having a surface interior (33) and an outer surface (34) opposite to the inner surface (33), the inner surface (33) of the outer ring (13) having an outer raceway, - an inner ring (11, 12) having an inner surface (14, 24) and an outer surface (15, 25) opposite to the inner surface (14, 24), the outer surface (15, 25) of the inner ring (11, 12) having a raceway interior, - a single interior space (43) being defined between the inner surface (33) of the outer ring (13) and the outer surface (15, 25) of the inner ring (11, 12), the single interior space (43) extending between a proximal end (44) where it is closed by a s proximal sealing system (45) between the outer ring (13) and the inner ring (11, 12) and a distal end (46) where it is closed by a distal sealing system (47) between the outer ring ( 13) and the inner ring (11, 12), said single inner space (43) containing a lubricant, - a row of rolling bodies (balls or rollers) (48, 49) having a contact surface mounted in the interior space single (43), rolling on the outer and inner races, and characterized in that at least one of the raceways and / or the contact surface of the rolling bodies is (are) covered (s) with a coating in chemical compound with lamellar structure.
    [2" id="c-fr-0002]
    2. Bearing a blade root (7) extending in a longitudinal direction between a proximal end and a distal end, the bearing allowing oscillation of the foot about an axis extending in the longitudinal direction relative to a housing (5), the rolling of a blade root (7) comprising: - a single outer ring (13) having an inner surface (33) and an outer surface (34) opposite to the inner surface (33), the inner surface (33) of the outer race (13) having a first outer race (35) proximal and a second outer race (36) distal, the first and second outer races being offset one by relative to each other in the longitudinal direction, - a first inner race (11) having an inner surface (14) and an outer surface (15) opposite to the inner surface (14), the outer surface (15) of the first inner race (11) having a first proximal inner race (23) and a distal seat (16), the first inner race and the seat being offset relative to one another in the longitudinal direction a second inner race (12) having an inner surface (24) and an outer surface (25) opposite to the inner surface (24), the outer surface (25) of the second inner race (12) having a second path inner race (28) distal, the second inner race (12) being fitted on the seat (16) and being held axially in abutment with the first inner race (11), - a single interior space (43) being defined between the inner surface (33) of the outer ring (13) and the outer surface (15, 25) of the first and second inner rings, the single inner space (43) extending between a proximal end (44) where it is closed by a proximal sealing system (45) between the outer ring (13) and the first inner ring (11) and a distal end (46) where it is closed by a distal sealing system (47) between the outer ring (13) and the second inner ring (12), said single inner space (43) containing a lubricant, - a first proximal row of rolling bodies (48) having a contact surface mounted in the single inner space ( 43), rolling on the first proximal outer and inner raceways (23, 35) and a second distal second row of rolling bodies (49) having a contact surface mounted in the single interior space (43), rolling on the second outer and inner distal races (28, 36), the first and second rows of rolling bodies (48, 49) being spaced apart from each other along the longitudinal axis, - the inner surface (14) of the first inner ring (11) comprising a shoulder (20) for joining to a blade root (4a), - the outer surface (34) of the single outer ring (13) comprising a shoulder (20) for assembly to a housing . and characterized in that at least one of the raceways and / or the contact surface of the rolling bodies of one of the rows of rolling bodies is (are) covered (s) with a coating of chemical compound lamellar structure.
    [3" id="c-fr-0003]
    3. Bearing of a blade root (7) according to claim 1 or claim 2, wherein the chemical compound lamellar structure is selected from fluorine carbides, graphite, M0S2, WS2 WSe2, NB, ZnO, ZnS and SnS preferably selected from graphite, M0S2 and WS2, more preferably still the chemical compound with lamellar structure is WS2.
    [4" id="c-fr-0004]
    4. A blade root bearing (7) according to any one of claims 1 to 3 wherein the lubricant is a grease comprising a base oil and a thickener, the base oil being selected from an ester-ester mixture. perfluoropolyether, polyalphaolefins, an ester-polyalphaolefin mixture and a synthetic compound, and the thickener being selected from polyurea, a lithium complex metal soap and a sodium complex metal soap.
    [5" id="c-fr-0005]
    The blade root bearing (7) according to any one of claims 1 to 4, wherein the grease has an operating temperature range having a lower temperature limit of -70 ° C to -20 ° C. in particular from -60 ° C to -30 ° C, more preferably from -55 ° C to -40 ° C, and a higher temperature performance limit greater than or equal to 170 ° C, in particular from 170 ° C to 210 ° C, more preferably 175 ° C to 200 ° C.
    [6" id="c-fr-0006]
    The blade foot bearing (7) according to any one of claims 1 to 5, wherein the lubricant further comprises the lamellar structure chemical compound of the coating,
    [7" id="c-fr-0007]
    7. A blade root bearing (7) according to claim 6, wherein the content of chemical compound with lamellar structure is from 1% to 10% by weight, in particular from 2% to 7% by weight, more particularly still 3% to 5% by weight relative to the weight of the fat.
    [8" id="c-fr-0008]
    8. Bearing of a blade root (7) according to any one of claims 1 to 7, wherein the surface having the raceway covered by the coating is rough.
    [9" id="c-fr-0009]
    9. Bearing of a blade root (7) according to any one of claims 1 to 8 wherein the material of the outer ring (13) and the material of the inner ring (11, 12) are selected independently of one of the other, among 100Cr6, M50, M50NiL, 32CrMoV13 nitrided, 16NiCrMol3 cemented, in particular is M50NÎL.
    [10" id="c-fr-0010]
    10. Bearing of a blade root (7) according to any one of claims 1 to 9, wherein the material of the rolling bodies is selected from M50, 10OCrô, S3N4, in particular is M50.
    [11" id="c-fr-0011]
    11. Lubricant combination for rolling a blade root (7) comprising a lubricant and a chemical compound with lamellar structure.
    [12" id="c-fr-0012]
    12. Use of a lubricating combination as defined in claim 11 for lubricating a bearing of a blade root (7), in particular the rolling of a blade root (7) as defined in any one Claims 1 to 10.
    [13" id="c-fr-0013]
    13. Use according to claim 12 for lubricating the rolling bodies with respect to the blade foot race (7).
    [14" id="c-fr-0014]
    14. A method of manufacturing a bearing of a blade root (7) as defined in any one of claims 1 to 10, characterized in that it comprises the following steps: a) deposition of a coating in a lamellar structure chemical compound on at least one of the raceways and / or on the contact surface of the rolling bodies, and b) applying a lubricant in the single interior space (43).
    [15" id="c-fr-0015]
    The method of claim 14, further comprising a preliminary step of treating the surface having the race on which the coating is deposited in step a).
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    同族专利:
    公开号 | 公开日
    FR3045561B1|2020-06-05|
    CN106895078A|2017-06-27|
    EP3184418A1|2017-06-28|
    CA2952112A1|2017-06-17|
    CN106895078B|2020-07-03|
    US20170175814A1|2017-06-22|
    EP3680168A1|2020-07-15|
    US10125821B2|2018-11-13|
    EP3184418B1|2020-06-17|
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    KR100602059B1|2003-05-16|2006-07-14|셰플러코리아|dual seal assembly for bearing|
    FR2862609B1|2003-11-21|2007-03-09|Roulements Soc Nouvelle|DEVICE FOR MOUNTING A BLADE WITH VARIABLE INCIDENCE ANGLE|
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    法律状态:
    2016-10-28| PLFP| Fee payment|Year of fee payment: 2 |
    2017-06-23| PLSC| Publication of the preliminary search report|Effective date: 20170623 |
    2017-12-21| PLFP| Fee payment|Year of fee payment: 3 |
    2018-12-19| PLFP| Fee payment|Year of fee payment: 4 |
    2019-12-19| PLFP| Fee payment|Year of fee payment: 5 |
    2020-12-23| PLFP| Fee payment|Year of fee payment: 6 |
    2021-12-24| PLFP| Fee payment|Year of fee payment: 7 |
    优先权:
    申请号 | 申请日 | 专利标题
    FR1562656|2015-12-17|
    FR1562656A|FR3045561B1|2015-12-17|2015-12-17|BEARING OF A LUBRICATED BLADE FOOT|FR1562656A| FR3045561B1|2015-12-17|2015-12-17|BEARING OF A LUBRICATED BLADE FOOT|
    US15/377,526| US10125821B2|2015-12-17|2016-12-13|Lubricated rolling bearing for blade roots|
    EP16204444.0A| EP3184418B1|2015-12-17|2016-12-15|Lubricated blade root bearing|
    CA2952112A| CA2952112A1|2015-12-17|2016-12-15|Roulement d'un pied de pale lubrifie|
    EP20159632.7A| EP3680168A1|2015-12-17|2016-12-15|Lubricated blade root bearing|
    CN201611166809.7A| CN106895078B|2015-12-17|2016-12-16|Lubricated rolling bearing for blade root|
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