• 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 rotor (1) of an electromagnetic motor or generator having a body comprising an internal hub (2) concentric with a central axis (7) of rotation of the rotor (1), branches (3) extending radially with respect to the central axis (7) of rotation from the internal hub (2) towards a hoop (8) forming a circular external periphery of the rotor (1), at least one magnet structure (10 ) being housed in each space delimited between two adjacent branches (3). The body consists of several superimposed layers of composite containing fibers bonded by a resin, the fibers of each layer being oriented in a predetermined direction (F1, F2) different for two superimposed layers. A radial covering skin is located on each of two opposite faces of the rotor body, being made up of several superimposed layers of composite containing fibers bonded by a resin.
    公开号:FR3086465A1
    申请号:FR1801010
    申请日:2018-09-24
    公开日:2020-03-27
    发明作者:Loic Mayeur；Romain Ravaud
    申请人:Whylot SAS；
    IPC主号:
    专利说明:

    "Rotor for electromagnetic motor or generator with hub body and branches in composite layers with fibers of different orientations"
    The present invention relates to a rotor for an axial flow electromagnetic motor or generator having a hub body and branches in layers of composite with fibers of different orientations. The invention also relates to an electromagnetic motor or generator equipped with such a rotor.
    The present invention finds an advantageous but non-limiting application for an electromagnetic motor delivering a high power with a high rotational speed of the rotor, which is obtained by the specific characteristics of the rotor according to the present invention. Such a motor can be used, for example, as an electromagnetic motor in a fully electric or hybrid motor vehicle.
    Advantageously but not limited to, the electromagnetic motor or generator can comprise at least one rotor framed by two stators, these elements being able to be superposed relative to each other by being separated by at least one air gap on the same shaft.
    In high speed applications, it is necessary to have very good mechanical strength of the rotating part, that is to say the rotor, in order to improve the reliability of the system.
    For an electromagnetic axial flow machine, the rotor comprises a body in the form of a discoidal support for magnets having two circular faces connected by a thickness, the disc being delimited between an external crown formed by a hoop and an internal periphery delimiting a recess for a rotation shaft.
    The magnets are each held in the disc support by holding means, an interval being left between the magnets.
    Axial flux motors are often used as an engine having higher torque than radial flux motors. They can therefore be used in low speed applications.
    For high-speed applications, the design of the rotor in an axial flow motor is more delicate since the forces due to centrifugal effects cause fairly significant mechanical stresses in the rotor. Furthermore, eddy current losses become preponderant both in the magnets and also in the rotor part when this is made with electrically conductive materials.
    For a rotor which must rotate at high rotational speeds, the main disadvantage of a motor at high rotational speed lies in the high probability of detachment of the magnet or magnets from the rotor as well as at least partial breakage of the rotor. . The rotor of such an engine must therefore be able to withstand high rotational speeds.
    The state of the art pushes the skilled person to stiffen the disc support of the magnet or magnets to combat centrifugal force. This requires a specific material for the disc support and to increase its size by thickening it so that the disc support is more rigid.
    This was not entirely satisfactory because the engine or generator thus provided with a discoidal support has a higher weight as well as an increased manufacturing price.
    One solution may be to make meshes of elongated unit magnets in fibrous and resinous structures, so as to reduce the eddy currents and to use a body of composite material for the rotor which does not conduct electricity, ideally a fiberglass rotor, with a hoop placed at the periphery of the rotor so as to maintain the forces due to centrifugal effects.
    However, for applications where the linear speeds become very high, the mechanical stresses become such that it is necessary to reduce the mass of magnet in order to access these speeds of rotation. However, the torque that an electric machine must provide is proportional to the area of magnets interacting with the magnetic fields produced by the stators. A reduction in the surface of the magnets therefore results in a reduction in the torque and therefore the power of the machine.
    The problem underlying the present invention is to design a rotor for the support of several permanent magnets provided with a hoop for an electromagnetic machine with axial flux, the rotor having a body grouping a hub and branches which can, from on the one hand, to maintain the permanent magnets between its branches effectively by preventing the magnets from detaching from the rotor while effectively compensating for the centrifugal force and, on the other hand, having a mechanical resistance such that the rotor can rotate at very high speeds.
    To this end, the present invention relates to a rotor of an electromagnetic motor or generator having a body comprising an internal hub concentric with a central axis of rotation of the rotor, branches extending radially with respect to the central axis of rotation from the internal hub to a hoop forming a circular external periphery of the rotor, at least one magnet structure with a plurality of unit magnets being housed in each space delimited between two adjacent branches, characterized in that:
    the body consists of several superimposed layers of composite containing fibers bonded by a resin, the fibers of each layer being oriented in a different predetermined direction for two superimposed layers,
    - A radial covering skin is located on each of two opposite faces of the rotor body, consisting of several superimposed layers of composite containing fibers bonded by a resin.
    The composite according to the present invention does not contain iron.
    The configuration of the rotor according to the present invention is based on the observation that the maximum stresses applying at very high speed on a rotor are made at the level of the hub surrounding the median axis of rotation of the rotor. It is therefore necessary to solidify this internal portion of the rotor.
    The Applicant has found that the superposition of layers of composition each having a single predetermined direction of orientation with different directions of orientation for each layer stiffens the body and the rotor. This is not equivalent to having a single layer of composite with fibers extending in two different directions, which is more difficult to manufacture, the fibers in two different directions in the same layer being able to move during injection. a binder like resin.
    For applications where the linear speeds become very important, typically from 160 meters per second or 180 meters per second, the mechanical stresses become such that the mass of magnet has to be reduced in order to access these speeds of rotation. . This has the great disadvantage that the torque that an electric machine must provide is proportional to the area of magnets interacting with the magnetic fields produced by the stators. A reduction in the surface of the magnets therefore results in a reduction in the torque and therefore the power of the machine.
    According to the invention, the body makes the hub and the branches in one piece. This increases the mechanical resistance of the assembly and consequently of the rotor.
    The skins or covering discs are arranged on each circular face of the rotor. The hoop can be made of glass or carbon fibers or carbon fibers. The composite hoop circumferentially surrounds large magnets or magnet structures at an outer periphery of the rotor. The hoop contributes, if necessary, to the radial retention of the magnets in addition to that guaranteed by the external coating layer of composite.
    Advantageously, the fibers of a composite layer of the body are oriented perpendicular to the fibers of an adjacent superimposed composite layer.
    Advantageously, the fibers of a composite layer of the body are oriented with an offset of 30 ° to 45 ° relative to the fibers of an adjacent superimposed composite layer.
    Advantageously, the number of layers of composite of the body is determined according to an axial thickness of each magnet structure and the covering skins have a thickness of between 0.3 and 2 mm.
    Advantageously, each branch has a decreasing width away from the internal hub to end with a tapered tip against the hoop. The tapered tips of the branches may or may not be secured to the hoop.
    The Applicant has taken into account that, in the case of an axial flow machine, the torque is proportional to the cube of the radius of the rotor. Therefore, it makes more sense to add magnet area to the periphery of the rotor than in more internal portions of the rotor. Hence an absence of a magnet near the axis of rotation can be easily compensated for by an addition of magnets at the periphery of the rotor, which can be obtained by configurations of branches decreasing in width the further one moves away from the center of the rotor until they are only tapered points with a width close to zero.
    It is therefore desirable to increase the surface area of the section of the rotor arms at their connection with the hub and to decrease this section gradually in order to increase the section of the magnet surfaces to maintain a high motor torque.
    This had never been envisaged by the state of the art which used only branches of constant width and hubs of small radius to make room for magnets. There was therefore a strong prejudice in reducing the distribution of the magnets on the rotor to increase the mechanical resistance of the rotor and the state of the art was oriented towards other solutions such as an increase in the axial direction of the branches and of the hub, this which increased the weight of the rotor without having a great beneficial effect on its resistance.
    Advantageously, the bases of two adjacent branches are separated by an intermediate portion of the internal hub, the intermediate portion being of concave shape rounded in the direction of the axis of the rotor, the internal hub having a radius equal to at least a quarter of a rotor radius.
    The inward curvatures of the intermediate portions between arms make it possible to reduce the mechanical stresses at the level of the thickest section of the arms bearing on the external periphery of the hub.
    Advantageously, each magnet structure has an increasing width as it moves away from the internal hub to end up against the hoop surrounding the rotor.
    Advantageously, each unit magnet of the plurality of unit magnets of the magnet structure is of polygonal shape or each unit magnet has an at least partially ovoid outline by comprising a first portion forming the body of the unit magnet having a larger section. and extending over a greater length of the unit magnet than at least a second longitudinal end portion pointing towards an associated longitudinal end of the unit magnet by decreasing in section as it approaches the longitudinal end.
    Advantageously, each magnet structure consists of a plurality of unit magnets secured by an insulating material reinforced with fibers, each unit magnet being of elongated shape extending in the axial direction of the rotor.
    This mainly applies to the use of covering skins. The large magnets used for the rotor according to the prior art dissipated a large amount of heat. This dissipation prevented the use of axial retention means in the form of skins or composite cover discs and the heat dissipation could have consequences on the behavior of the coating with accelerated aging of this coating as well as magnets.
    Composite cover discs were not frequently used in the prior art because they did not resist the heat dissipation generated by the magnets.
    As the present invention preferably uses a multitude of unitary magnets replacing a compact magnet of the state of the art, the heat dissipation is less and skins or covering discs can be used as axial holding means, these skins or discs advantageously replacing axial retention means between magnets and rotor body, necessitating if necessary modifications of the magnets or of their coating in order to produce additional fixing means with fixing means carried by the rotor.
    Another synergy provided by the present invention is that the rotor can have, between each branch, unitary magnets grouped together in a magnet structure. Each three-dimensional magnet structure consists of a plurality of unit magnets.
    This allows for a magnet structure having many unitary magnets. It has been revealed that a structure with such a plurality of unit magnets has a great power of not being sensitive to space harmonics or currents generated by the stator windings. Consequently, the losses generated in the magnet structures are very low, and the yields, particularly at high speed, are very high. Such a magnet structure can form a magnet pole or be a complete magnet.
    One of the preferred measures of the present invention is to decompose a magnet structure which may be a whole magnet or a magnetic pole according to the state of the art into a plurality of small or micro magnets. A large magnet is subject to greater eddy current losses than its equivalent in small or micro-magnets. The use of small magnets or micro-magnets therefore makes it possible to reduce these losses which are detrimental to the operation of the electromagnetic actuator.
    It is known that, in order to obtain a magnetic field of optimal intensity, the ideal volume of a magnet must approach a cube or a cylinder whose length is equal to the diameter. It is common knowledge that increasing the length of a magnet beyond it does not increase the magnetic field. The approach of the present invention in this preferred form, however, goes in the opposite direction of this prejudice.
    The length of a unitary magnet is appreciably increased compared to the diameter or to a diagonal of its planar longitudinal face compared to what the widely used practice recommends, this essentially to meet needs of mechanical resistance of the structure, which is the main object of the present invention.
    The Applicant has discovered that a plurality of unit magnets in a magnet structure gives a magnet structure having a much greater mechanical resistance while retaining magnetic properties almost similar to those of a single magnet having an equal surface. to n times the elementary surface of the n unit magnets when n unit magnets are present.
    Ovoid magnets can have facets. One thus obtains as unitary magnets crystals associated with each other which are not linked over the entire surface of facets or longitudinal faces but layers of resin and glue build a mesh network at the ends of the poly-faceted studs with zones of contact between magnets limited.
    As an alternative, for unit magnets of perfect ovoid shape with a first rounded portion, the contact between two adjacent unit magnets is more reduced by being able to be only punctual and corresponds substantially to an arc of circle of reduced size between the two magnets unitary. It can be dug a streak the size of the arc of a contact circle between two adjacent unit magnets to receive glue, preferably in the form of resin.
    Advantageously, the plurality of unit magnets of a magnet structure are secured by an insulating material reinforced with fibers, each unit magnet being of elongated shape extending in the radial direction of the rotor.
    Advantageously, each magnet structure incorporates at least one mesh having meshes each delimiting a housing for a respective unitary magnet, each housing having sufficient internal dimensions sufficient to allow a unitary magnet to be introduced into its interior while leaving a space between the housing and the unitary magnet filled with a fiber-reinforced resin, the meshes being made of insulating material reinforced with fibers.
    The mesh remains in place and can also be coated in a layer of composite. Such a mesh makes it possible to maintain unitary magnets during the manufacture of the magnet structure and has the advantage of representing an additional solidification element of the magnet structure, the mesh possibly also containing reinforcing fibers.
    For example, a honeycomb mesh is known to reinforce the resistance of an element, in this case a magnet structure. The unit magnets are inserted in hexagonal housings which ensure their maintenance. The walls of the housings serve as electrical insulation and the density of the housings in the magnet structure can be considerably increased. The honeycomb mesh can be made of an insulating composite material reinforced with fibers.
    Advantageously, each magnet structure between two adjacent branches is embedded in at least one layer of composite, the rotor also being embedded in at least one layer of composite including the structures of embedded magnets and the body made up of several layers of composite.
    Advantageously, the composite layers embedding the rotor and constituting the hub and the branches of the body are made of glass or carbon fibers cast in resin. These reinforcing fibers help to increase the resistance of the magnet structure and in particular the bending and buckling rigidity.
    The invention also relates to a method for manufacturing such a rotor, which comprises the following steps:
    - casting of a first layer of composite containing fibers bonded by a resin, the fibers of the first layer being oriented in the same predetermined direction,
    - casting of at least a second layer of composite containing fibers bonded by a resin, the fibers of the second layer being oriented in a predetermined direction different from the direction of the first layer,
    - hardening of the resin.
    This process is easy to implement and retains the orientation of the fibers more easily than if there were several different orientations of fibers per layer of composite.
    Advantageously, the width of each branch of the body of the hub at a point of its length extending radially from the external periphery of the hub to the internal periphery of the hoop is determined from an evaluation of an admissible mechanical stress capable of '' be applied to the rotor, with a maximum permissible speed of rotation of the rotor and a mechanical resistance of the material of the branch, a decrease in the width of each branch away from the hub being obtained by selecting for each branch a width for each point of its length making it possible to obtain an iso-stress inside the branch.
    Without being limiting, the maximum stress exerted on a branch towards its end connected to the hub can be evaluated at 120 mega Pascals. Obtaining this iso-stress makes it possible to minimize the width of the branch and therefore to put more surface area of large magnets or magnet structures, therefore in the latter case more unit magnets, which allows to obtain more torque and more to compensate for the loss of magnet surface towards the hub.
    The invention finally relates to an electromagnetic motor or generator with axial flow, characterized in that it comprises at least one such rotor, the electromagnetic motor or generator comprising at least one stator carrying at least one winding, the electromagnetic motor or generator comprising one or more air gaps between said at least one rotor and said at least one stator.
    Other characteristics, aims and advantages of the present invention will appear on reading the detailed description which follows and with regard to the appended drawings given by way of nonlimiting examples and in which:
    FIG. 1 is a schematic representation of a front view of a rotor intended for an electromagnetic machine with axial flow according to a first embodiment of the present invention, a body grouping together the hub and the branches of the rotor consisting of composite layers each with different 90 ° orientations of the fibers in two different layers,
    FIG. 2 is an enlarged schematic representation of a portion of the rotor shown in FIG. 1,
    FIG. 3 is a schematic representation of a front view of a rotor intended for an electromagnetic axial flow machine according to a first embodiment of the present invention, a body grouping together the hub and the branches of the rotor consisting of composite layers with each different orientation of 30 ° of the fibers in two different layers,
    FIG. 4 is an enlarged schematic representation of a portion of the rotor shown in FIG. 3,
    - Figures 5a, 5b and 5c are schematic representations for Figures 5a and 5b of a respective embodiment of a unitary magnet of ovoid shape and for Figure 5c of a magnet structure comprising unitary ovoid magnets , four unit ovoid magnets being shown spaced from the magnet structure.
    The figures are given by way of examples and are not limitative of the invention. They constitute schematic representations of principle intended to facilitate the understanding of the invention and are not necessarily at the scale of practical applications. In particular the dimensions of the different parts are not representative of reality.
    In what follows a single branch 3, a single base 3a and a single tapered point 3b of the branch 3 are referenced for all the branches in FIGS. 1 to 4. The same is true for a single magnet structure referenced 10 with internal faces 10a and external 10b, an intermediate portion 9 between two branches for all the intermediate portions and a single orientation of fiber F1 or F2 per layer of composite in FIGS. 2 and 4. In FIGS. 1 to 4, a single unitary magnet 4 is referenced for all the unit magnets in a magnet structure 10.
    Everything stated for one of these referenced elements applies to all similar unreferenced elements.
    Referring to all the figures and more particularly to Figures 1 to 4, these figures respectively show a rotor 1 and an enlargement of a portion of a rotor 1 according to the present invention with two branches 3 interposing between them a structure of magnet 10 composed of several unitary magnets 4 polygonal.
    This is not limiting and a single large magnet can be inserted between two branches 3, this single large magnet not being to be confused with the unit magnets 4 of a magnet structure 10 visible and referenced to Figure 2 and 4.
    Such a rotor 1 is used in an electromagnetic motor or generator, advantageously with axial flow. The rotor 1, advantageously substantially circular, has a body comprising an internal hub 2 concentric with a central axis 7 of rotation of the rotor 1 or longitudinal median axis of the rotor 1. Branches 3 extend radially in the rotor 1 relative to the central axis 7 of rotation from the internal hub 2 towards a hoop 8 forming a circular external periphery of the rotor 1.
    The hub 2 and the branches 3 are in one piece and form a rotor body 2, 3. At least one magnet, then a large magnet or a magnet structure 10 comprising a plurality of unit magnets 4 of small size is housed in each space delimited between two adjacent branches 3.
    According to the present invention, the body 2, 3 consists of several superimposed layers of composite containing fibers bonded by a resin, the fibers of each layer being oriented in a predetermined direction F1, F2 different for two superimposed layers.
    A covering skin or disc, not shown in the figures because radially covering a circular face of the rotor 1 is located on each of two opposite faces of the body 2, 3 of the rotor by being made up of several superimposed layers of composite containing fibers bonded by a resin. The skins or cover discs, not shown in the figures, can be arranged on each circular face of the rotor 1 to prevent axial movement of the magnet structures 10 or large magnets between two branches 3.
    All these characteristics taken in combination considerably stiffen the body 2, 3 of the rotor 1.
    Several embodiments of the composite layers can be envisaged. Non-limiting examples will now be given.
    As shown in Figures 1 and 2, the fibers of a composite layer of the body 2, 3 can be oriented perpendicular to the fibers of an adjacent superimposed composite layer, the directions F1 and F2 shown in Figure 2 being perpendicular.
    As shown in Figures 3 and 4, the fibers of a composite layer of the body 2, 3 are oriented with an offset of 30 ° to 45 ° relative to the fibers of an adjacent superimposed composite layer, to these figures of 30 °.
    There may be more than two layers of composite on top of each other. The number of layers of composite of the body 2, 3 is determined according to an axial thickness of the magnet structure 10 and the covering skins have a thickness of between 0.3 and 2 mm.
    As best shown in Figures 1 and 3, each branch 3 may have a decreasing width by moving away from the internal hub 2 to finish with a tapered tip 3b against the hoop 8.
    Each large magnet or magnet structure 10 may have an increasing width by moving away from the internal hub 2 to finish against the hoop 8 surrounding the rotor 1.
    The space lost for the magnets by increasing the width of the branches 3 towards their end portion or base 3a opposite the hub 2 and, if necessary, also by increasing the radius of the hub 2 is made up on the portions peripheral end of rotor 1.
    The fact of placing each large magnet or each magnet structure 10 with their greatest width oriented towards the external periphery of the rotor 1 makes it possible to increase the magnet parts placed at the periphery of the rotor 1 and therefore to increase the total magnetization surface.
    Still referring more particularly to FIGS. 1 and 3, the tapered tip 3b of each branch 3 can be at least two to four times less wide than a base 3a of the branch 3 connected to the internal hub 2.
    The bases 3a of two adjacent branches 3 can be separated by an intermediate portion 9 of the internal hub 2. This intermediate portion 9 can be of concave shape rounded in the direction of the axis of the rotor 1. The inner hub 2 can have a radius equal to at least a quarter of a radius of the rotor 1, which makes it a hub 2 more large than a hub 2 of the prior art. The radius of the rotor is equal to the radius of a branch 3 to which a hoop thickness 8 is added.
    The hub 2 and the branches 3 may be made of glass or carbon fibers cast in resin. Resistant plastic fibers can also be used in order to increase the resistance of the rotor 1 and in particular the bending and buckling rigidity.
    As previously mentioned, to solidify the rotor 1, the hub 2 and the branches 3 are in one piece by forming the composite body with fibers of different orientations F1, F2 according to the layer of composite which contains them. The branches 3 can be secured or not to the hoop 8 by their tapered end 3b.
    With particular reference to FIGS. 1, 3, 5a to 5c, each magnet structure 10 can consist of a plurality of unit magnets 4 secured by an insulating material reinforced with fibers, each unit magnet 4 being of elongated shape. by extending in the axial direction of the rotor 1. The unit magnets 4, only one of which is referenced by figure, are not to be confused with the magnet structures 10 nor with large magnets not shown in the figures.
    It follows that each magnet structure 10 can be three-dimensional and made up of a plurality of unit magnets 4.
    In FIGS. 1 to 4, each unit magnet 4 of the plurality of unit magnets 4 is of polygonal shape.
    In FIGS. 5a, 5b and 5c, each unitary magnet 4 can have an at least partially ovoid contour by comprising a first portion 4a forming the body of the unitary magnet 4 having a larger section and extending over a greater length of l unitary magnet 4 that at least a second portion 4b of longitudinal end pointing towards an associated longitudinal end of unitary magnet 4 by decreasing in section as it approaches the longitudinal end.
    In FIG. 5a, the unit magnet 4 has an almost perfect ovoid shape with a first portion 4a and two second portions 4b of rounded end and of convex shape. As can be seen in Figure 5c, the contact between two unitary magnets 4 adjacent and ovoid is substantially punctual or extends in a limited arc.
    In this case, the unitary magnet 4 can have an at least partially ovoid outer contour with the first portion 4a forming the body of the unitary magnet 4 having a larger section and extending over a greater length of the unitary magnet. 4 that said at least one second portion 4b.
    In FIG. 5b, the unitary magnet 4 can have at least a second portion 4b at at least one longitudinal end of the unitary magnet 4 as an extension of the first portion 4a. There may be two second portions 4b with a second portion 4b respectively at a longitudinal end of the unitary magnet 4.
    The second portion (s) 4b can point towards an associated longitudinal end of the magnet by decreasing in section by approaching the longitudinal end.
    As shown in FIG. 5b, the second portion (s) 4b of longitudinal end can be curved while being convex in shape. The second portion (s) 4b of longitudinal end may terminate at their longitudinal end associated with a median facet 11 forming the longitudinal end. In FIG. 5b, for the ovoid shape, this median facet 11 forming the longitudinal end is however curved and is only optional.
    In this FIG. 5b, the second longitudinal end portion (s) 4b can comprise lateral facets inclined towards a longitudinal axis of the unitary magnet 4 while approaching the associated longitudinal end of the unitary magnet 4.
    As shown in Figure 5c, in a magnet structure 10, the unit magnets 4 are directly adjacent to each other by being partially in contact. The unit magnets 4 are glued by depositing glue. The plurality of unit magnets 4 provides a mesh of magnets without interposing holding elements between them other than glue, the unit magnets 4 being in direct contact between adjacent magnets. The first portion 4a and the second portion 4b for a unitary magnet are also shown in this figure 5c.
    In Figures 2 and 4, the unit magnets 4 can be bonded against each other without mesh between them. The same is true for Figure 5c. The adhesive can be a layer of composite, a bonding resin, advantageously thermosetting or thermoplastic.
    Each large magnet or magnet structure 10 between two adjacent branches 3 can also be embedded in a layer of composite. The rotor can also be coated in a layer of composite in its entirety.
    There can therefore be superposition of at least a first layer of composite to surround the unitary magnets 4, of at least a second layer of composite to individually surround the magnet structures 10 and of at least a third layer of composite to coat the rotor 1, knowing that the body 2, 3, comprising the hub 2 and the branches of the rotor, also consists of layers of composite superimposed with fibers of different orientations depending on the layer.
    As not shown in the figures but by using the references which are already indicated in the figures for similar elements, each magnet structure 10 can integrate at least one mesh having meshes each delimiting a housing for a respective unitary magnet 4. Each housing can have sufficient internal dimensions sufficient to allow a unitary magnet 4 to be inserted into its interior while leaving a space between the housing and the unitary magnet 4 filled with a fiber-reinforced resin, the meshes being made of insulating material. fiber reinforced.
    The hoop 8 may be made of glass or carbon fibers or of carbon fibers. The composite hoop 8 circumferentially surrounds the magnet structures 10 or the large magnets at an outer periphery of the rotor 1. The hoop 8 contributes, if necessary, to the radial maintenance of the magnet structures 10 or large magnets pruning in addition to that guaranteed by the external composite coating layer. The tapered points 5b of the branches 3 can be joined or not to the hoop 8.
    The present invention relates to a method for manufacturing a rotor 1 with, for the manufacture of its body 2, 3 comprising a hub 2 and branches 3, the implementation of the following steps.
    The first step is a casting of a first layer of composite containing fibers bonded by a resin, the fibers of the first layer being oriented in the same predetermined direction F1.
    The second step is a casting of at least a second layer of composite containing fibers bonded by a resin, the fibers of the second layer being oriented in a predetermined direction F2 different from the direction F1 of the first layer.
    The third step is the hardening of the resin.
    The body 2, 3 is then ready for use to form the framework of the rotor 1.
    Advantageously, the invention also relates to a method of manufacturing such a rotor 1, in which the width I of each branch 3 at a point of its length extending radially from the external periphery of the hub 2 to the internal periphery of the hoop 8 at a known distance from the central axis 7 of rotation of the rotor 1 is determined from an evaluation of an admissible mechanical stress capable of being applied to the rotor 1, of a maximum admissible speed of rotation of the rotor 1 and a mechanical strength of the material of the branch.
    A decrease in the width of each branch 3 away from the hub 2 is obtained by selecting for each branch 3 a width for each point of its length allowing an iso-stress to be obtained inside the branch 3.
    It can be seen in FIGS. 1 and 3 that the width of the branches 3 decreases the more the radius therefore increases away from the central axis 7 of the rotor 1.
    Advantageously, the width of each branch at a point of its length extending radially is given by the following equation:
    O lyn = K - 9WT στη
    K being a constant varying according to a thickness of the hoop 8 and representative of the mechanical resistance of the material of the branch, p a density of the magnet structure 10, σΎη an admissible mechanical stress capable of being applied to the rotor 1 and consequently on the branch, θ an opening angle of each magnet or of each magnet structure 10 and W the maximum admissible speed of rotation of the rotor 1.
    Finally, the invention relates to an electromagnetic motor or generator with axial flow comprising at least one such rotor 1, the motor 5 or the electromagnetic generator comprising at least one stator carrying at least one coil, the electromagnetic motor or generator comprising one or more air gaps between said at least one rotor 1 and said at least one stator.
    The electromagnetic motor or generator may preferably comprise at least one rotor 1 associated with two stators.
    权利要求:
    Claims (15)
    [1" id="c-fr-0001]
    1. Rotor (1) of an electromagnetic motor or generator having a body (2, 3) comprising an internal hub (2) concentric with a central axis (7) of rotation of the rotor (1), branches ( 3) extending radially with respect to the central axis (7) of rotation from the internal hub (2) towards a hoop (8) forming a circular external periphery of the rotor (1), at least one magnet structure (10) with a plurality of magnets (4) being housed in each space delimited between two adjacent branches (3), characterized in that:
    • the body (2, 3) consists of several superimposed layers of composite containing fibers bonded by a resin, the fibers of each layer being oriented in a different predetermined direction (F1, F2) for two superimposed layers, • a skin of Radial covering is located on each of two opposite faces of the body (2, 3) of the rotor, being made up of several superposed layers of composite containing fibers bonded by a resin.
    [2" id="c-fr-0002]
    2. Rotor (1) according to claim 1, wherein the fibers of a composite layer of the body (2, 3) are oriented perpendicular to the fibers of an adjacent superimposed composite layer.
    [3" id="c-fr-0003]
    3. Rotor (1) according to claim 1, wherein the fibers of a composite layer of the body (2, 3) are oriented with a shift of 30 ° to 45 ° relative to the fibers of a layer of composite overlay adjacent.
    [4" id="c-fr-0004]
    4. Rotor (1) according to any one of the preceding claims, in which the number of layers of composite of the body (2, 3) is determined according to an axial thickness of the magnet structure (10) and the covering skins have a thickness between 0.3 and 2 mm.
    [5" id="c-fr-0005]
    5. Rotor (1) according to any one of the preceding claims, in which each branch (3) has a decreasing width away from the internal hub (2) to end with a tapered tip (3b) against the hoop (8 ).
    [6" id="c-fr-0006]
    6. Rotor (1) according to the preceding claim, wherein the bases (3a) of two adjacent branches (3) are separated by an intermediate portion (9) of the inner hub (2), the intermediate portion (9) being of shape concave rounded towards the axis of the rotor (1), the internal hub (2) having a radius equal to at least a quarter of a radius of the rotor (1).
    [7" id="c-fr-0007]
    7. Rotor (1) according to any one of the preceding claims, in which each magnet structure (10) has an increasing width as it moves away from the internal hub (2) to end up against the hoop (8) surrounding the rotor. (1).
    [8" id="c-fr-0008]
    8. Rotor (1) according to any one of the preceding claims, in which each unit magnet (4) of the plurality of unit magnets (4) of the magnet structure (10) is of polygonal shape or each unit magnet (4) has an at least partially ovoid contour, comprising a first portion forming the body of the unit magnet (4) having a larger section and extending over a greater length of the unit magnet (4) than at least a second longitudinal end portion pointing towards an associated longitudinal end of the unit magnet (4) by decreasing in section as it approaches the longitudinal end.
    [9" id="c-fr-0009]
    9. Rotor (1) according to the preceding claim, wherein the plurality of unit magnets (4) of a magnet structure (10) are secured by an insulating material reinforced with fibers, each unit magnet (4) being elongated shape extending in the radial direction of the rotor (1).
    [10" id="c-fr-0010]
    10. Rotor (1) according to the preceding claim, in which each magnet structure (10) incorporates at least one mesh having meshes each delimiting a housing for a respective unitary magnet (4), each housing having sufficient just internal dimensions. to allow introduction of a unitary magnet (4) therein while leaving a space between the housing and the unitary magnet (4) filled with a fiber-reinforced resin, the meshes being of insulating material reinforced with fibers.
    [11" id="c-fr-0011]
    11. Rotor (1) according to any one of the preceding claims, in which each magnet structure (10) between two adjacent branches (3) is embedded in at least one layer of composite, the rotor (1) also being coated in at least one layer of composite including the structures of embedded magnets and the body (2, 3) consisting of several layers of composite.
    [12" id="c-fr-0012]
    12. Rotor (1) according to the preceding claim, in which the composite layers embedding the rotor and constituting the hub (2) and the branches of the body (2, 3) are made of glass or carbon fibers cast in resin .
    [13" id="c-fr-0013]
    13. Method for manufacturing a rotor (1) according to any one of the preceding claims, which comprises the following steps:
    casting a first layer of composite containing fibers bonded by a resin, the fibers of the first layer being oriented in the same predetermined direction (F1),
    - casting of at least a second layer of composite containing fibers bonded by a resin, the fibers of the second layer being oriented in a predetermined direction (F2) different from the direction (F1) of the first layer,
    - hardening of the resin.
    [14" id="c-fr-0014]
    14. A method of manufacturing a rotor (1) according to the preceding claim, wherein the width of each branch (3) of the body (2, 3) of the hub (2) at a point of its length extending radially from the outer periphery of the hub (2) at the inner periphery of the hoop (8) is determined from an evaluation of an admissible mechanical stress capable of being applied to the rotor (1), with a maximum admissible speed of rotation of the rotor (1) and of a mechanical resistance of the material of the branch (3), a decrease in the width of each branch (3) away from the hub (2) being obtained by selecting for each branch (3) a width for each point of its length allowing to obtain an iso-stress inside the branch (3).
    [15" id="c-fr-0015]
    15.Engine or electromagnetic generator with axial flow, characterized in that it comprises at least one rotor (1) according to any one of claims 5 to 12, the motor or the electromagnetic generator comprising at least one stator carrying at least a winding, the motor or the electromagnetic generator comprising one or more air gaps between said at least one rotor (1) and said at least one stator.
    类似技术:
    公开号 | 公开日 | 专利标题
    EP3602740B1|2021-02-24|Motor or electromagnetic generator comprising a rotor with magnetised structures comprising unit magnets and a stator with concentric windings
    WO2019243996A1|2019-12-26|Rotor for an electromagnetic motor or generator with tapered branches
    EP3857677A1|2021-08-04|Axial-flux rotor with magnets and body made of layers of composite with fibers of different orientations
    EP3387742A1|2018-10-17|Rotor of an axial-flow electromagnetic motor having a corrugated-shape integral magnet
    EP3430706B1|2021-02-24|Rotor for axial flux electromagnetic motor or generator with semi-embedded magnets and axial holding means
    WO2005117244A1|2005-12-08|Polyphase rotating electrical machine for a motor vehicle
    WO2016116678A1|2016-07-28|Rotor for an axial flux electromagnetic machine rotating at high rotational speeds and electromagnetic machine equipped with such a rotor
    EP3743929A1|2020-12-02|Unitary magnet having an ovoid configuration, and magnet structure comprising multiple unitary magnets
    CA2999352C|2020-04-28|Dynamic stress generators including at least two ballasts and actuator including such generators
    FR3110767A1|2021-11-26|Magnet pole with several individual magnets of variable section
    WO2021250509A1|2021-12-16|Magnet pole with a plurality of unit magnets coated in a composite layer
    FR3076674A1|2019-07-12|ELECTROMAGNETIC ENGINE OR GENERATOR WITH TWO ROTORS AND FOUR STATORS AND INTEGRATED COOLING SYSTEM
    WO2019073128A1|2019-04-18|Reduced-stiffness rotor for an electromagnetic generator or motor
    FR3077413A1|2019-08-02|UNITARY MAGNET WITH FORWARD-LOOKING SHAPES INTENDED TO BE PART OF CONTACT AREAS BETWEEN ADJACENT MAGNETS
    FR3107999A1|2021-09-10|Rotor for electromagnetic axial flow machine
    FR3097913A1|2021-01-01|PLASTIC BEARING FOR ELECTRIC ROTATING MACHINE
    FR2919771A1|2009-02-06|MAGNETIC MOTOR WITH PERMANENT MAGNETS
    同族专利:
    公开号 | 公开日
    WO2020065488A1|2020-04-02|
    US20210265884A1|2021-08-26|
    JP2022500976A|2022-01-04|
    EP3857677A1|2021-08-04|
    FR3086465B1|2021-05-21|
    CN112640256A|2021-04-09|
    引用文献:
    公开号 | 申请日 | 公开日 | 申请人 | 专利标题
    FR1475501A|1966-04-13|1967-03-31|Deutsche Edelstahlwerke Ag|Permanent magnet poles for permanent magnet systems|
    EP0353042A1|1988-07-26|1990-01-31|The Turbo Genset Company Limited|Axial field electrical generator|
    US20030141721A1|2002-01-30|2003-07-31|Bartlett Lexington P.|Wind power system|
    DE102010039123A1|2010-08-10|2012-02-16|Bayerische Motoren Werke Aktiengesellschaft|Rotor for permanent magnet-energized transverse flux machine i.e. electric drive, of hybrid car, has rotor disk formed of plastic i.e. fiber-reinforced plastic, as injection moulding body in which permanent magnets is received|
    FR3014255A1|2013-12-02|2015-06-05|Renault Sa|DISCOID ROTOR WITH REINFORCED COMPOSITE STRUCTURE FOR AXIAL FLUX ELECTRIC MACHINE|FR3111244A1|2020-06-09|2021-12-10|Whylot|Magnet pole with several individual magnets encased in a layer of composite|
    FR3064423B1|2017-03-22|2019-11-15|Whylot Sas|ROTOR FOR MOTOR OR ELECTROMAGNETIC GENERATOR WITH ALVEOLAR STRUCTURE COMPRISING ALVEOLES FOR THE HOUSING OF RESPECTIVE MAGNETS|
    法律状态:
    2019-07-17| PLFP| Fee payment|Year of fee payment: 2 |
    2020-03-27| PLSC| Publication of the preliminary search report|Effective date: 20200327 |
    2020-09-15| PLFP| Fee payment|Year of fee payment: 3 |
    2021-09-10| PLFP| Fee payment|Year of fee payment: 4 |
    优先权:
    申请号 | 申请日 | 专利标题
    FR1801010A|FR3086465B1|2018-09-24|2018-09-24|ROTOR FOR ELECTROMAGNETIC MOTOR OR GENERATOR WITH HUB BODY AND BRANCHES IN COMPOSITE LAYERS WITH DIFFERENT ORIENTATION FIBERS|FR1801010A| FR3086465B1|2018-09-24|2018-09-24|ROTOR FOR ELECTROMAGNETIC MOTOR OR GENERATOR WITH HUB BODY AND BRANCHES IN COMPOSITE LAYERS WITH DIFFERENT ORIENTATION FIBERS|
    PCT/IB2019/058015| WO2020065488A1|2018-09-24|2019-09-23|Axial-flux rotor with magnets and body made of layers of composite with fibers of different orientations|
    US17/261,625| US20210265884A1|2018-09-24|2019-09-23|Axial-flux rotor with magnets and body made of layers of composite with fibers of different orientations|
    JP2021507000A| JP2022500976A|2018-09-24|2019-09-23|Axial flux rotor with magnet and body of composite layer with fibers in different directions|
    EP19778676.7A| EP3857677A1|2018-09-24|2019-09-23|Axial-flux rotor with magnets and body made of layers of composite with fibers of different orientations|
    CN201980056474.9A| CN112640256A|2018-09-24|2019-09-23|Axial flux rotor with magnets and body made of composite layers with differently oriented fibers|
    [返回顶部]