CN111769666A

CN111769666A - Rotor assembly and motor with same

Info

Publication number: CN111769666A
Application number: CN202010550859.5A
Authority: CN
Inventors: 左亚军; 李文瑞; 王洪晓; 李虎
Original assignee: Guangdong Welling Motor Manufacturing Co Ltd
Current assignee: Guangdong Welling Motor Manufacturing Co Ltd
Priority date: 2020-06-16
Filing date: 2020-06-16
Publication date: 2020-10-13

Abstract

The invention discloses a rotor assembly and a motor with the same, wherein the rotor assembly comprises a rotor core, a permanent magnet, a rotating shaft, a transmission part and a second end part vibration damping part, wherein the rotor core is provided with a magnet groove and a rotating shaft hole; the permanent magnet is arranged in the magnet groove; the rotating shaft is arranged in the rotating shaft hole, a gap is formed between the rotating shaft and the rotor core, and a first end and a second end of the rotating shaft extend out of the rotating shaft hole; the first end part vibration damping piece is arranged on the first end surface of the rotor core and is connected with the rotor core; the transmission piece is arranged in the first end part vibration damping piece and matched with the rotating shaft; the second end vibration reduction part is arranged on the second end face of the rotor core and is connected with the rotor core, the second end vibration reduction part is directly matched with the rotating shaft, and the rotor core drives the rotating shaft through the second end vibration reduction part and the first end vibration reduction part and the transmission part in sequence. The rotor assembly of the invention improves the material quantity of the vibration reduction piece, has good noise reduction and vibration reduction effects and high reliability.

Description

Rotor assembly and motor with same

Technical Field

The invention relates to the technical field of motors, in particular to a rotor assembly and a motor with the rotor assembly.

Background

With the increase of the power density of the motor, the energy density of the motor is increased, the magnetic field of the motor tends to be deeply saturated, and the electromagnetic noise is increased. In the related art, in order to reduce electromagnetic vibration and noise caused by torque fluctuation in the operation process of a motor, a damping material is filled between a rotor core and a rotating shaft or a shaft sleeve to absorb electromagnetic force waves, so that the noise of the motor is reduced, and vibration damping is realized. In the related art, the vibration damping material is filled between the rotor core and the rotating shaft or the shaft sleeve, so that the noise reduction and vibration damping effects are poor and need to be improved.

Disclosure of Invention

The present invention is based on the discovery and recognition by the inventors of the following facts and problems:

in the related technology, the vibration damping rotor assembly comprises a permanent magnet, an outer iron core, a rotating shaft, an injection molding body and a vibration damping ring, wherein the injection molding body comprises an upper end plate, a lower end plate and a plastic packaging connecting part for connecting the upper end plate and the lower end plate, an annular boss axially protrudes from the upper end plate and/or the lower end plate, the inner iron core is arranged on the rotating shaft and embedded into a groove of the annular boss, and the vibration damping ring is arranged between the inner iron core and the inner wall of the groove. On one hand, since the gap between the inner core and the inner wall of the recess is limited, the amount of material of the damper is limited, and the noise reduction and vibration damping effects are poor. On the other hand, the injection molding piece and the damping ring are made of different materials, the damping ring at the end part of the outer iron core is not connected, a gap is easy to appear on the boundary surface of the injection molding piece and the damping ring, the reliability problem caused by different coefficients such as thermal expansion and the like is easy to appear in the operation process, the damping of the injection molding piece is small, and the suppression effect on electromagnetic vibration noise is not obvious. On the other hand, the vibration reduction rotor assembly needs to perform two steps of injection molding and placing of vibration reduction rings in the production process, the process is complex, and the reject ratio is high during mass production.

The present invention is directed to solving at least one of the problems of the related art to some extent, and therefore, an embodiment of the present invention provides a rotor assembly capable of increasing the amount of material of a damping member, reducing noise and vibration, and having high reliability without affecting a magnetic path of an electromagnetic field.

An embodiment of another aspect of the invention also provides an electric machine.

A rotor assembly according to an embodiment of the first aspect of an embodiment of the present invention includes: a rotor core having a magnet slot and a rotating shaft hole; the permanent magnet is arranged in the magnet groove; the rotating shaft is arranged in the rotating shaft hole, a gap is formed between the rotating shaft and the rotor core, and a first end and a second end of the rotating shaft extend out of the rotating shaft hole; the first end part vibration damping piece is arranged on the first end surface of the rotor core and is connected with the rotor core; the transmission piece is arranged in the first end part vibration damping piece and matched with the rotating shaft; second end damping spare, second end damping spare is established on rotor core's the second terminal surface and with rotor core links to each other, second end damping spare with the pivot directly cooperates, rotor core passes through second end damping spare and loop through first end damping spare with the driving medium drive the pivot.

According to the rotor assembly provided by the embodiment of the invention, the first end part vibration reduction piece matched with the rotating shaft through the transmission piece is arranged on the first end surface of the rotor core, so that the rigid connection between the rotating shaft and the rotor core is avoided, the rotating effect of the rotating shaft is improved by the transmission piece, the vibration reduction piece is large in material quantity, good in noise reduction and vibration reduction effects, the problem of different thermal expansion coefficients is solved, the reliability of the rotor assembly is improved, the vibration reduction piece is only required to be arranged in the production process, the preparation process is simple, and the reject ratio of mass production is reduced.

In some embodiments, a portion of the first end vibration damper is directly engaged with the rotating shaft, and the rotor core drives the rotating shaft through the portion of the first end vibration damper and, in turn, through the first end vibration damper and the transmission member.

In some embodiments, the material of the first end vibration dampening member and the second end vibration dampening member are both viscoelastic materials.

In some embodiments, the viscoelastic material has a dissipation factor of 0.15 or greater.

In some embodiments, the viscoelastic material has a shore hardness of 20 degrees to 80 degrees.

In some embodiments, the transmission member includes a base and a boss protruding from the base toward the first end surface of the rotor core, and the rotating shaft penetrates through the base and the boss; the minimum distance between the boss and the first end face of the rotor core in the axial direction of the rotor core is L1, and L1 is larger than 0.5 mm.

In some embodiments, a minimum gap between the boss and the permanent magnet in a radial direction of the rotor core is L2, and L2 > 0.5 mm.

In some embodiments, a minimum gap between the base and the permanent magnet in the axial direction of the rotor core is L3, and L3 > 0.5 mm.

In some embodiments, the rotor assembly further comprises an outer connection damper, the rotor core has an axial through hole between adjacent magnet slots, the outer connection damper is disposed in the axial through hole, a first end of the outer connection damper is connected to the first end damper, and a second end of the outer connection damper is connected to the second end damper.

In some embodiments, the rotor assembly further includes an inner connection damper disposed in a gap between the rotating shaft and the rotor core, a first end of the inner connection damper is connected to the first end damper, and a second end of the inner connection damper is connected to the second end damper.

In some embodiments, the rotor assembly further comprises an intermediate connection damper, a gap is formed between the inner surface of the permanent magnet and the inner bottom surface of the magnet groove, the intermediate connection damper is arranged in the gap, a first end of the intermediate connection damper is connected with the first end damper, and a second end of the intermediate connection damper is connected with the second end damper.

In some embodiments, the rotor core is formed by stacking a plurality of rotor laminations in an axial direction of the rotor core, the rotor laminations include full bridge laminations and half bridge laminations, the rotor core has a first end, a second end and a middle section located between the first end and the second end, the first end and the second end are formed by stacking a plurality of full bridge laminations, and the middle section is formed by stacking a plurality of half bridge laminations.

In some embodiments, in the axially adjacent half-bridge laminations of the rotor core in the middle section, one half-bridge lamination rotates relative to the other half-bridge lamination by one magnetic pole in the circumferential direction of the rotor core.

In some embodiments, some of the inner magnetic bridges of the plurality of inner magnetic bridges of the half-bridge stamped steel are provided with magnetic bridge holes penetrating through the inner magnetic bridges along the circumferential direction of the rotor core, among the inner magnetic bridges of the axially adjacent half-bridge stamped steel of the rotor core, the inner magnetic bridge of one half-bridge stamped steel is provided with the magnetic bridge hole, the inner magnetic bridge of the other half-bridge stamped steel is not provided with the magnetic bridge hole, the magnetic bridge holes are internally provided with circumferential connection vibration damping members, and the adjacent intermediate connection vibration damping members are connected with each other through the circumferential connection vibration damping members.

In some embodiments, the first end vibration damper, the second end vibration damper, the inner connecting vibration damper, the outer connecting vibration damper, the intermediate connecting vibration damper, and the circumferential connecting vibration damper are integrally injection molded from a viscoelastic material.

In some embodiments, the peripheral wall of the transmission member is provided with transmission radial protrusions and transmission radial open grooves located between adjacent transmission radial protrusions, the end damping member has a central hole, the peripheral wall of the central hole is provided with damping radial protrusions and radial damping open grooves located between adjacent damping radial protrusions, the transmission radial protrusions are fitted in the damping radial open grooves, and the damping radial protrusions are fitted in the transmission radial open grooves.

An electric machine according to an embodiment of the second aspect of the invention comprises a rotor assembly as described in any of the embodiments above.

According to the motor provided by the embodiment of the invention, the first end part vibration reduction piece matched with the rotating shaft through the transmission piece is arranged on the first end surface of the rotor core in the rotor assembly, so that the rigid connection between the rotating shaft and the rotor core is avoided, the rotating effect of the rotating shaft is improved by the transmission piece, the material quantity of the vibration reduction piece is large, the noise reduction and vibration reduction effects are good, and the reliability is high.

Drawings

Fig. 1 is a disassembled perspective view of a rotor assembly according to one embodiment of the present invention.

Fig. 2 is an assembled state schematic view of the rotor assembly shown in fig. 1.

Fig. 3 is an axial cross-sectional view of the rotor assembly of fig. 2.

Fig. 4 is an enlarged schematic view of a portion a in fig. 3.

Fig. 5 is a cross-sectional view of the damped rotor shown in fig. 2.

Fig. 6 is a schematic view of a rotor core of a rotor assembly according to an embodiment of the present invention.

Fig. 7 is a perspective view of a transmission of a rotor assembly according to an embodiment of the present invention.

FIG. 8 is a plan view of a transmission of a rotor assembly according to an embodiment of the present invention.

Fig. 9 is a schematic view of a half-bridge punch of a rotor assembly according to an embodiment of the present invention.

Fig. 10 is a schematic view of a fully-bridged punch of a rotor assembly according to an embodiment of the present invention.

Fig. 11 is another axial cross-sectional view of the rotor assembly shown in fig. 1.

Fig. 12 is a side view of the rotor assembly shown in fig. 1.

FIG. 13 is another perspective view of a transmission of a rotor assembly according to an embodiment of the present invention.

Fig. 14 is a comparison of the damping ratio of a rotor assembly according to an embodiment of the present invention with the prior art.

Reference numerals:

the rotor assembly 100 is provided with a rotor assembly,

a rotor core 10, a rotation shaft hole 101, a magnet groove 102, an axial through hole 103, a magnetic bridge hole 104, a gap 105,

a full bridge punching sheet 110, a half bridge punching sheet 120, a punching sheet body part 111, an outer magnetic bridge 112, an inner magnetic bridge 113, a magnetic pole 114, a protrusion 115,

the permanent magnet (20) is provided with,

a damping member 60, a first end damping member 61, a plate portion 610, a boss portion 611, an opening 612, a first damping radially inner open groove 615, a first damping radially inner protrusion 616, a first center hole 617, a second end damping member 62, an outer connecting damping member 63, an intermediate connecting damping member 64, an inner connecting damping member 65, a circumferential connecting damping member 66,

driving piece 51, driving radial protrusion 510, driving radial opening groove 511, base body 513 and boss 514.

Detailed Description

Reference will now be made in detail to embodiments of the present invention, examples of which are illustrated in the accompanying drawings. The embodiments described below with reference to the drawings are illustrative and intended to be illustrative of the invention and are not to be construed as limiting the invention.

As shown in fig. 1 to 10, a rotor assembly 100 according to an embodiment of the present invention includes a rotor core 10, a permanent magnet 20, a rotation shaft 30, a vibration damping member 60, and a transmission member 51.

The rotor core 10 has a magnet groove 102 and a rotating shaft hole 101. As shown in fig. 1 and 6, the rotating shaft hole 101 is provided at a substantially central position of the rotor core 10 and penetrates the rotor core 10 in the axial direction (the left-right direction in fig. 1 and 6) of the rotor core 10. The magnet grooves 102 are provided in plural, and the plural magnet grooves 102 are arranged at regular intervals around the rotation shaft hole 101 in the circumferential direction of the rotor core 10.

The permanent magnets 20 are disposed in the magnet slots 102. As shown in fig. 1 and 6, the permanent magnet 20 is plural, and one permanent magnet 20 is installed in each magnet slot 102, so that the plural permanent magnets 20 are arranged at intervals in the circumferential direction of the rotor core 10.

The rotating shaft 30 is disposed in the rotating shaft hole 101, and there is a gap between the rotating shaft 30 and the rotor core 10, in other words, as shown in fig. 3, the diameter D1 of the inner circular hole of the rotor core 10 is larger than the diameter D2 of the rotating shaft, i.e., D1 > D2. The first end (the left end of the rotating shaft 30 in fig. 1 to 3) and the second end (the right end of the rotating shaft 30 in fig. 1 to 3) of the rotating shaft 30 protrude from the rotating shaft hole 101. As shown in fig. 1 to 3, the axial direction of the rotating shaft 30 is substantially coincident with the axial direction of the rotor core 10 and is inserted into the rotor core 10 through the rotating shaft hole 101.

The damper 60 includes a first end damper 61, and the first end damper 61 is provided on a first end surface (a left end surface of the rotor core 10 in fig. 1 to 3) of the rotor core 10 and connected to the rotor core 10.

The transmission member 51 is disposed in the first end damping member 61, the transmission member 51 is engaged with the rotating shaft 31, and the rotor core 10 drives the rotating shaft 30 at least through the first end damping member 61 and the transmission member 51 in sequence. In other words, since the rotor core 10 has a gap between the inner peripheral wall of the rotation shaft hole 101 and the rotation shaft 30, the rotor core 10 does not directly drive the rotation shaft 30 but drives the rotation shaft 30 to rotate at least through the first end vibration damper 61 and the transmission member 51.

The damper 60 further includes a second end damper 62, and the second end damper 62 is provided on a second end surface (a right end surface of the rotor core 10 in fig. 1 to 3) of the rotor core 10 and connected to the rotor core 10. As shown in fig. 1 and 3, the second end vibration damper 62 is directly engaged with the rotary shaft 30, and the rotor core 10 drives the rotary shaft through the second end vibration damper 62 and, in turn, through the first end vibration damper 61 and the transmission member 51.

According to the rotor assembly provided by the embodiment of the invention, the first end part vibration reduction piece matched with the rotating shaft through the transmission piece is arranged on the first end surface of the rotor core, so that the rigid connection between the rotating shaft and the rotor core is avoided, the transmission piece improves the rotating effect of the rotating shaft, and the vibration reduction piece is large in material quantity and good in noise reduction and vibration reduction effects; the problem of different thermal expansion coefficients does not exist, the reliability of the rotor assembly is improved, only the vibration damping piece needs to be arranged in the production process, the preparation process is simple, and the reject ratio of mass production is reduced.

In some embodiments, the material of the first end vibration dampening member 61 and the second end vibration dampening member 62 are both viscoelastic materials, such as rubber, thermoplastic materials, and the like. The vibration damping device can greatly absorb energy generated due to resonance by adopting the viscoelastic material, and achieves a vibration damping effect.

As shown in fig. 14, the rotor core end face is designed to be made of a full viscoelastic material, so that the rotor damping ratio can be greatly improved, and compared with an end structure of a common rotor (rigidly connected) and an end plate and a vibration damping ring, the damping ratio of the end structure made of the full viscoelastic material is larger.

In some specific embodiments, the loss factor of the viscoelastic material is greater than or equal to 0.15, thereby ensuring effective absorption and attenuation of electromagnetic waves during operation of the motor rotor.

Further, the shore hardness of the viscoelastic material is 20 degrees to 80 degrees, thereby improving the manufacturability of the motor. For example, shore hardness is 30 degrees, 40 degrees, 50 degrees.

In some embodiments, a portion of the first end damper 61 is directly engaged with the rotating shaft 30, and the rotor core 10 drives the rotating shaft 30 through the portion of the first end damper 61 and, in turn, through the first end damper 61 and the transmission member 51.

As shown in fig. 1, 3 and 4, the transmission member 51 is located on the left side of a portion of the first end damping member 61, the left end of the rotating shaft 30 sequentially penetrates through the rotor core 10, the portion of the first end damping member 61 and the transmission member 51 and extends out, and both the transmission member 51 and the portion of the first end damping member 61 are directly engaged with the rotating shaft 30, so that when the rotor core 10 rotates, the first end damping member 61 is driven to rotate, and the rotating shaft 30 is driven to rotate by the portion of the first end damping member 61 and the transmission member 51. The thickness of a part of the first end damper 61 in the axial direction of the rotating shaft 30 is L, wherein L is greater than or equal to 0.5 mm, thereby increasing the amount of damper material and making the connection of the damper to the rotor core more reliable.

In some embodiments, transmission member 51 includes a base 513 and a boss 514, boss 514 protrudes from base 513 toward the first end surface of rotor core 10, and rotating shaft 30 penetrates base 513 and boss 514.

As shown in fig. 1, 13 and 11, the boss 514 faces the left end face of the rotor core 10, the base 513 is fitted with the first center hole 617 of the first end damper 61, and the boss 514 is fitted inside the first end damper 61. Both the base 513 and the boss 514 are provided with through holes, and the rotating shaft 30 penetrates through the base 513 and the boss 514 through the corresponding through holes.

When the length of the permanent magnet extends out of the end face of the rotor core, the protrusions can be embedded into the central ring formed by circumferential arrangement of the permanent magnet along the axial direction of the rotor core, the torque transmission capacity of the transmission part and the fatigue reliability of the vibration damping part can be improved, the axial length of the rotor assembly can be further reduced, and the miniaturization design of the motor is facilitated.

In some embodiments, the minimum distance between the boss 514 and the first end face of the rotor core 10 in the axial direction of the rotor core 10 is L1, and L1 > 0.5 mm. Thereby, the connection of the damper to the rotor core is made more reliable while the amount of material of the damper is increased. In addition, the vibration damping performance of the rotor is improved, the flowability of the vibration damping material during injection molding and filling can be improved, and the manufacturability of the injection molding process is improved.

In some embodiments, as shown in fig. 12, the minimum gap between the boss 514 and the permanent magnet 20 in the radial direction of the rotor core 10 is L2, and L2 > 0.5 mm. Thereby, the connection of the damper to the rotor core is made more reliable while the amount of material of the damper is increased. In addition, the vibration damping performance of the rotor is improved, the flowability of the vibration damping material during injection molding and filling can be improved, and the manufacturability of the injection molding process is improved.

In some embodiments, as shown in fig. 11, the minimum gap between the base 513 and the permanent magnet 20 in the axial direction of the rotor core 10 is L3, and L3 > 0.5 mm. Thereby, the connection of the damper to the rotor core is made more reliable while the amount of material of the damper is increased. In addition, the vibration damping performance of the rotor is improved, the flowability of the vibration damping material during injection molding and filling can be improved, and the manufacturability of the injection molding process is improved.

It is to be understood that the transmission member 51 of the present application is not limited to that shown in fig. 13, for example, in other embodiments, as shown in fig. 7, the transmission member 51 is free of bosses.

In some embodiments, as shown in fig. 1 and 3, the damper 60 further includes an outer connection damper 63, the rotor core 10 has an axial through hole 103 between the adjacent magnet slots 102, the outer connection damper 63 is disposed in the axial through hole 103, a first end of the outer connection damper 63 (a left end of the outer connection damper 63 in fig. 1) is connected to the first end damper 61, and a second end of the outer connection damper 63 (a right end of the outer connection damper 63 in fig. 1) is connected to the second end damper 62.

As shown in fig. 1, the plurality of outer connection vibration dampers 63 are arranged at intervals in the circumferential direction of the rotor core 10, so that the amount of the vibration dampers is further increased, the noise reduction capability and the vibration reduction effect are improved, and the connection between the first end vibration damper and the rotor core and the connection between the second end vibration damper and the rotor core are more reliable.

In some embodiments, as shown in fig. 1 and 3, the damper 60 further includes an inner connection damper 65, the inner connection damper 65 is disposed in the gap between the rotating shaft 30 and the rotor core 10, a first end (a left end of the inner connection damper 65 in fig. 4) of the inner connection damper 65 is connected to the first end damper 61, and a second end (a right end of the inner connection damper 65 in fig. 4) of the inner connection damper 65 is connected to the second end damper 62.

As shown in fig. 1 and 3, the inner connection damper member 65 is connected between the first and second

end damper members

61 and 62, and the plurality of outer connection damper members 63 surround the outside of the inner connection damper member 65. The inner connection damper 65 surrounds the rotation shaft 30 and is directly engaged with the rotation shaft 30. Therefore, the material quantity of the vibration damper is further increased, the noise reduction capability and the vibration damping effect are improved, the internal connection vibration damper is directly matched with the rotating shaft, and the transmission reliability of the vibration damper is further improved.

In some embodiments, as shown in fig. 1, the damping member 60 further includes a middle connection damping member 64, a gap 105 is formed between the inner surface of the permanent magnet 20 and the inner bottom surface of the magnet slot 102, the middle connection damping member 64 is disposed in the gap 105, a first end of the middle connection damping member 64 (a left end of the middle connection damping member 64 in fig. 1) is connected to the first end damping member 61, and a second end of the middle connection damping member 64 (a right end of the middle connection damping member 64 in fig. 1) is connected to the second end damping member 62.

As shown in fig. 1, the intermediate connection damper 64 is plural, the plural intermediate connection dampers 64 are arranged at intervals in the circumferential direction of the rotor core 10, and the intermediate connection damper 64 is provided between the outer connection damper 63 and the inner connection damper 65. Thereby, the connection of the damper to the rotor core is made more reliable while the amount of material of the damper is increased.

In some embodiments, the rotor core 10 is formed by stacking a plurality of rotor laminations in an axial direction of the rotor core 10, the rotor laminations 10 include full bridge laminations 110 and half bridge laminations 120, the rotor core 10 has a first end portion, a second end portion, and a middle section located between the first end portion and the second end portion, the first end portion and the second end portion are formed by stacking a plurality of full bridge laminations 110, and the middle section is formed by stacking a plurality of half bridge laminations 120.

As shown in fig. 6, 9 and 10, the rotor punching sheet includes a punching sheet main body portion 111, an outer magnetic bridge 112, an inner magnetic bridge 113 and magnetic poles 114, the magnetic poles 114 are arranged at intervals along the circumferential direction of the rotor core 10, and at least part of the magnetic poles 114 are connected with the punching sheet main body portion 111 through the inner magnetic bridge 113. The multiple rotor laminations forming the rotor core 10 include the full bridge laminations 110 and the half bridge laminations 120, the full bridge laminations 110 are located at two end portions of the rotor core 10, and the half bridge laminations 120 are located in the middle of the rotor core 10.

As shown in fig. 9, among the plurality of magnetic poles 114 of the half-bridge lamination sheet 120, a part of the magnetic poles 114 is connected to the lamination sheet main body portion 111 through the inner magnetic bridge 113, and another part of the magnetic poles 114 is spaced apart from the lamination sheet main body portion 111 in the radial direction of the rotor core 10, wherein the part of the magnetic poles 114 and the another part of the magnetic poles 114 are alternately arranged along the circumferential direction of the rotor core 10. The outer magnetic bridges 112 of the half-bridge laminations 120 are broken between adjacent magnetic poles 114.

As shown in fig. 10, in a plurality of magnetic poles 114 of the full bridge stamped sheet 110, each magnetic pole 114 is connected to the stamped sheet body portion 111 through an inner magnetic bridge 113, and the outer magnetic bridge 112 of the half bridge stamped sheet 110 is closed.

In this embodiment, through setting up the full bridge punching piece at rotor core's tip, not only be favorable to the mould of injection moulding technology to seal the material, prevent that the liquid of moulding plastics from oozing and leading to the product after the shaping to have burr and overlap, can also promote rotor core's rigidity and intensity.

In some embodiments, among the adjacent half-bridge laminations 110 in the middle section, one half-bridge lamination 110 rotates relative to the other half-bridge lamination 110 by one magnetic pole 114 in the circumferential direction of the rotor core 10. Therefore, the inner magnetic bridge of the rotor core forms a structure of alternate connection and disconnection in the axial direction, the electromagnetic performance of the motor can be improved, and the energy consumption is reduced.

Some inner magnetic bridges 113 in the plurality of inner magnetic bridges 113 of the half-bridge stamped sheet 120 are provided with magnetic bridge holes 104 penetrating through the inner magnetic bridges 113 along the circumferential direction of the rotor core 10, in the inner magnetic bridges 113 of the axially adjacent half-bridge stamped sheet 120 of the rotor core 10, the inner magnetic bridge 113 of one half-bridge stamped sheet 120 is provided with a magnetic bridge hole 104, the inner magnetic bridge 113 of the other half-bridge stamped sheet 120 is not provided with a magnetic bridge hole 104, a circumferential connection damping piece 66 is arranged in the magnetic bridge hole 104, and the adjacent intermediate connection damping pieces 64 are connected with each other through the circumferential connection damping piece 66.

As shown in fig. 6, the inner magnetic bridge 113 of one half bridge punch 120 is provided with magnetic bridge holes 104, the inner magnetic bridge 113 of the other half bridge punch 120 is not provided with magnetic bridge holes 104, and the half bridge punch 120 provided with magnetic bridge holes 104 and the half bridge punch 120 without magnetic bridge holes 104 are alternately arranged. The circumferential connection dampers 66 are arranged in a plurality of rows arranged at intervals in the axial direction of the rotor core 10, each row including a plurality of circumferential connection dampers 66 arranged at intervals in the circumferential direction of the rotor core 10, wherein the plurality of circumferential connection dampers 66 of each row connect adjacent intermediate connection dampers 64.

In some embodiments, the first end damping member 61, the second end damping member 62, the inner connection damping member 65, the outer connection damping member 63, the intermediate connection damping member 64, and the circumferential connection damping member 66 are integrally injection-molded from a viscoelastic material. This application is through filling viscoelastic material in the magnetic bridge hole with rotor core inside, tip and rotor core, can promote rotor core's damping characteristic, further improves and falls to make an uproar and damping performance.

Moreover, the viscoelastic materials (the first end vibration damping piece 61 and the second end vibration damping piece 62) on the two sides of the end face of the rotor core are connected, and in the actual manufacturing process, the damping materials can be filled in the two side ends through integral molding by utilizing a mold, so that the manufacturability of the motor is improved. And the connection of the vibration damping piece and the rotor core is tight and reliable, and the vibration damping piece is not easy to separate from the rotor core, so that the stability is improved.

In some specific embodiments, the loss factor of the viscoelastic material is greater than or equal to 0.15, and the shore hardness of the viscoelastic material is 20 degrees to 80 degrees, so that the electromagnetic waves can be effectively absorbed and attenuated when the motor rotor operates, and the manufacturability of the motor can be improved. For example, shore hardness is 30 degrees, 40 degrees, 50 degrees.

In some embodiments, as shown in fig. 1, 2, 7 and 8, the peripheral wall of the transmission member 51 is provided with transmission radial projections 510 and transmission radial open grooves 511 between adjacent transmission radial projections 510. The first end damping part 61 has a first center hole 617, first damping radial protrusions 616 and first radial damping open grooves 615 between adjacent first damping radial protrusions 616 are provided on an inner peripheral wall of the first center hole 617, the transmission radial protrusion 510 is fitted in the first damping radial open groove 615, and the first damping radial protrusions 616 are fitted in the transmission radial open grooves 511.

As shown in FIGS. 1, 2, 7 and 8, the outer peripheral wall of the transmission member 51 is provided with a plurality of transmission radial protrusions 510 and a plurality of transmission radial open grooves 511, and the transmission radial open grooves 511 have a taper angle α of not less than 5 ° and taper radially outward. A plurality of transmission radial protrusions 510 are arranged at intervals along the circumferential direction of the rotor core 10, and a first transmission radial opening groove 511 is formed between every two adjacent transmission radial protrusions 510.

The first end damping part 61 has a plurality of first damping radial protrusions 616 and a plurality of first radially damping inward opening grooves 615 on a circumferential wall of a first center hole 617, the plurality of first damping radial protrusions 616 are arranged at intervals in the circumferential direction of the rotor core 10, and one first radially damping inward opening groove 615 is formed between every two adjacent first damping radial protrusions 616.

The transmission member 51 is disposed within the first end damping member 61 with the transmission radial projection 510 engaged within the first radially damping inwardly opening groove 615 and the first damping radial projection 616 engaged within the transmission radial opening groove 511.

In some embodiments, the length of the permanent magnet 20 in the axial direction of the rotor core 10 is greater than the axial length of the magnet slot 102, a first end of the permanent magnet 20 protrudes from the magnet slot 102 and is fitted in the first end damper 61, and a second end of the permanent magnet 20 protrudes from the magnet slot 102 and is fitted in the second end damper 62. The rotor subassembly of this embodiment has not only promoted the electromagnetic property of motor, has reduced the energy consumption, can also make the damping piece of rotor subassembly bear bigger moment of torsion.

In some embodiments, each of the first and

second end dampers

61 and 62 is provided with an opening 612 for exposing a portion of the rotor core 10.

As shown in fig. 1, each of the first end vibration damping member 61 and the second end vibration damping member 62 includes a plate portion 610 and a boss portion 611, an opening 612 is provided on an outer circumferential surface of the plate portion 610, the openings 612 may be multiple, and the openings 612 are arranged along a circumferential direction of the plate portion 610 at intervals, so that a left end portion of the rotor core is exposed, thereby solving a problem that a structural rigidity of the rotor assembly is insufficient when the rotor assembly is integrally magnetized, ensuring that the rotor assembly is not significantly deformed or loosened when the rotor assembly is integrally magnetized, thereby realizing the integral magnetization of the rotor assembly, and improving the magnetizing efficiency.

The first end vibration damper 61 is provided with a plurality of openings 612, the second end vibration damper 62 is provided with a plurality of openings 612, projections formed by the openings 612 arranged on the first end vibration damper 61 and the second end vibration damper 62 on the end surface of the rotor core 10 are overlapped, and the positioning piece installed through the openings 612 can be abutted against the rotor core 10, so that the rotor core 10 is fixed between the first end vibration damper 61 and the second end vibration damper 62.

Because the projections formed by the openings 612 on the first end vibration damping part 61 and the second end vibration damping part 62 on the end surface of the rotor core 10 are overlapped, the stress points of the first end surface and the second end surface of the rotor core 10 are the same, and the stress is more uniform.

The position of the opening 612 is not limited to the outer peripheral surface of the end vibration damper, and for example, in other embodiments, the opening 612 may be provided on the plate portion 610 or the boss portion 611 of the first end vibration damper 61 and the second end vibration damper 62, as long as a part of the rotor core 10 is exposed to facilitate the positioning member to abut against the rotor core 10.

Some specific exemplary rotor assemblies according to the present invention are described below with reference to fig. 1-10.

As shown in fig. 1 to 3, a rotor assembly 100 according to an embodiment of the present invention includes a rotor core 10, a plurality of permanent magnets 20, a rotating shaft 30, a transmission member 51, and a damping member 60.

The rotor core 10 has a rotation shaft hole 101, a plurality of magnet grooves 102, a plurality of axial through holes 103, and a plurality of bridge holes 104. The rotating shaft hole 101 is provided at a substantially central position of the rotor core 10 and penetrates the rotor core 10 in the axial direction of the rotor core 10. The plurality of magnet slots 102 are arranged at regular intervals around the rotation shaft hole 101 in the circumferential direction of the rotor core 10. An axial through hole 103 is provided between any adjacent magnet slots 102.

The rotor core 10 is formed by stacking a plurality of rotor laminations in the axial direction of the rotor core 10, wherein the full-bridge laminations 110 are located at the left end portion and the right end portion of the plurality of rotor laminations, and the half-bridge laminations 120 are located at the middle portion of the plurality of rotor laminations.

The rotor punching sheet comprises a punching sheet body part 111, an outer magnetic bridge 112, an inner magnetic bridge 113 and a magnetic pole 114. In a plurality of magnetic poles 114 of the full bridge stamped sheet 120, each magnetic pole 114 is connected with the stamped sheet main body 111 through an inner magnetic bridge 113, a plurality of protrusions 115 arranged at intervals are arranged on the periphery of the stamped sheet main body 111, a protrusion 115 is arranged between adjacent inner magnetic bridges 113, and the outer magnetic bridge 112 of the half bridge stamped sheet 110 is closed.

The outer magnetic bridges 112 of the half-bridge laminations 120 are broken between adjacent magnetic poles 114. Among the plurality of magnetic poles 114 of the half-bridge lamination sheet 120, a part of the magnetic poles 114 are connected with the lamination sheet main body portion 111 through the inner magnetic bridge 113, the other part of the magnetic poles 114 are spaced from the lamination sheet main body portion 111 in the radial direction of the rotor core 10, and the part of the magnetic poles 114 and the other part of the magnetic poles 114 are alternately arranged along the circumferential direction of the rotor core 10. In the adjacent half-bridge stamped sheets 110 in the middle, one half-bridge stamped sheet 110 rotates by one magnetic pole 114 relative to the other half-bridge stamped sheet 110 along the circumferential direction of the rotor core 10. Therefore, the inner magnetic bridge of the rotor core forms a structure of alternate connection and disconnection in the axial direction, the electromagnetic performance of the motor can be improved, and the energy consumption is reduced.

Some inner magnetic bridges 113 in the plurality of inner magnetic bridges 113 of the half-bridge stamped sheet 120 are provided with magnetic bridge holes 104 penetrating the inner magnetic bridges 113 along the circumferential direction of the rotor core 10, and in the inner magnetic bridges 113 of the axially adjacent half-bridge stamped sheet 120 of the rotor core 10, the inner magnetic bridge 113 of one half-bridge stamped sheet 120 is provided with a magnetic bridge hole 104, and the inner magnetic bridge 113 of the other half-bridge stamped sheet 120 is not provided with a magnetic bridge hole 104.

The plurality of permanent magnets 20 are respectively provided in the plurality of magnet slots 102 correspondingly such that the plurality of permanent magnets 20 are arranged at intervals in the circumferential direction of the rotor core 10. A gap 105 is provided between the inner surface of each permanent magnet 20 and the inner bottom surface of the corresponding magnet slot 102.

The axial direction of the rotating shaft 30 is substantially the same as the axial direction of the rotor core 10, and the rotating shaft hole 101 is formed in the rotor core 10, and a gap is formed between the rotating shaft 30 and the rotor core 10.

The damper member 6 includes a first end damper member 61, a second end damper member 62, an outer connection damper member 63, an intermediate connection damper member 64, an inner connection damper member 65, and a circumferential connection damper member 66.

First end damping piece 61 is connected at the left end face of rotor core 10, and second end damping piece 62 is connected at the right end face of rotor core 10, and first end damping piece 61, rotor core 10 and second end damping piece 62 are run through in proper order to pivot 30 along the direction from a left side to the right side, and the direct cooperation of the periphery of the partly internal periphery of first end damping piece 61 and pivot 30, and the direct cooperation of the internal periphery of second end damping piece 62 and the periphery of pivot 30.

The first end vibration damping member 61 and the second end vibration damping member 62 each include a plate portion 610 and a boss portion 611. The outer peripheral surface of the plate portion 610 is provided with an opening 612, and the opening 612 is plural, and the plural openings 612 are arranged at intervals in the circumferential direction of the plate portion 610. The boss portion 611 of the first end vibration damper 61 protrudes leftward from the left end surface of the first end vibration damper 61, and the boss portion 621 of the second end vibration damper 62 protrudes rightward from the right end surface of the second end vibration damper 62.

The inner connection damper 65 is provided in the gap between the rotary shaft 30 and the rotor core 10, and the left end of the inner connection damper 65 is connected to the first end damper 61, and the right end of the inner connection damper 65 is connected to the second end damper 62.

The outer connecting damper 63 is disposed in the axial through hole 103, and the left end of the outer connecting damper 63 is connected to the first end damper 61, and the right end of the outer connecting damper 63 is connected to the second end damper 62. Since the outer connection damper 63 is plural, the plural outer connection dampers 63 are arranged at intervals in the circumferential direction of the rotor core 10 and surround the outside of the inner connection damper 65.

The intermediate connection damper 64 is disposed in the gap 105, the left end of the intermediate connection damper 64 is connected to the first end damper 61, and the right end of the intermediate connection damper 64 is connected to the second end damper 62. The intermediate connection damper 64 is thus plural, the plural intermediate connection dampers 64 are arranged at intervals in the circumferential direction of the rotor core 10, and the intermediate connection damper 64 is provided between the outer connection damper 63 and the inner connection damper 65.

The circumferential connection dampers 66 are arranged in a plurality of rows arranged at intervals in the axial direction of the rotor core 10, each row including a plurality of circumferential connection dampers 66 arranged at intervals in the circumferential direction of the rotor core 10, wherein the plurality of circumferential connection dampers 66 of each row connect adjacent intermediate connection dampers 64.

The first end vibration damper 61, the second end vibration damper 62, the intermediate connection vibration damper 64, the outer connection vibration damper 63, the inner connection vibration damper 65, and the circumferential connection vibration damper 66 are integrally formed by injection molding, and are made of rubber or a thermoplastic elastomer. Therefore, the vibration damping piece has lower hardness and rigidity, a good vibration damping effect, close and reliable connection with the rotor core, difficulty in separation and improved stability.

The outer circumferential wall of the transmission member 51 is provided with a plurality of transmission radial protrusions 510 and a plurality of transmission radial opening grooves 511, the plurality of transmission radial protrusions 510 are arranged at intervals along the circumferential direction of the rotor core 10, and one transmission radial opening groove 511 is formed between every two adjacent transmission radial protrusions 510. The transmission member 51 is disposed within the first end damping member 61 with the transmission radial projection 510 engaged within the first radially damping inwardly opening groove 615 and the first damping radial projection 616 engaged within the transmission radial opening groove 511.

The first boss 514 faces the left end surface of the rotor core 10, the first base 513 is fitted with the first center hole 617 of the first end damper 61, and the first boss 514 is fitted inside the first end damper 61. The first base 513 and the first boss 514 are provided with first through holes, and the rotating shaft 30 penetrates through the first base 513 and the first boss 514 through the corresponding first through holes.

The minimum distance between the boss 514 and the first end face of the rotor core 10 in the axial direction of the rotor core 10 is L1, and L1 is greater than 0.5 mm. The minimum gap between the boss 514 and the permanent magnet 20 in the radial direction of the rotor core 10 is L2, and L2 is greater than 0.5 mm; the minimum gap between the base 513 and the permanent magnet 20 in the axial direction of the rotor core 10 is L3, and L3 > 0.5 mm.

The rotating shaft 30 sequentially penetrates through the transmission member 51, a part of the first end vibration damping member 61, the rotor core 10 and the second end vibration damping member 62 along the left-to-right direction, the transmission member 51, a part of the first end vibration damping member 61, the rotor core 10 and the second end vibration damping member 62 are directly matched with the rotating shaft 30, therefore, when the rotor core 10 rotates, the first end vibration damping member 61 and the second end vibration damping member 62 are driven to rotate, and the rotating shaft 30 is driven to rotate through the combined action of the part of the first end vibration damping member 61, the first transmission member 51 and the second end vibration damping member 62.

The specific process of the rotor assembly according to the embodiment of the present invention may be as follows:

respectively manufacturing a rotor iron core, a permanent magnet, a rotating shaft and a transmission part;

sleeving the rotor iron core on the rotating shaft through the rotating shaft hole;

putting the assembled rotor iron core, the rotating shaft and the transmission piece into a mold, positioning, and respectively and correspondingly inserting a plurality of permanent magnets into a plurality of magnet grooves of the rotor iron core;

the rotor core, the permanent magnet, the rotating shaft and the transmission piece are molded into an integrated plastic-coated structure by using rubber or thermoplastic elastomer materials through an injection molding process, wherein the structure formed by using the rubber or thermoplastic elastomer materials is the vibration damping piece.

A motor according to an embodiment of the present invention includes the rotor assembly 100 of any of the above embodiments.

According to the motor provided by the embodiment of the invention, the structure of the rotor assembly is improved, the vibration reduction piece and the transmission piece can be arranged at least at the end part of the rotor core, at least part of the vibration reduction piece can be directly matched with the rotating shaft, and other parts of the vibration reduction piece can be matched with the rotating shaft through the transmission piece, so that the rigid connection between the rotating shaft and the rotor core is avoided, meanwhile, the material quantity of the vibration reduction piece is increased, and the noise reduction and vibration reduction effects of the whole motor are improved.

In the description of the present invention, it is to be understood that the terms "central," "longitudinal," "lateral," "length," "width," "thickness," "upper," "lower," "front," "rear," "left," "right," "vertical," "horizontal," "top," "bottom," "inner," "outer," "clockwise," "counterclockwise," "axial," "radial," "circumferential," and the like are used in the orientations and positional relationships indicated in the drawings for convenience in describing the invention and to simplify the description, and are not intended to indicate or imply that the referenced devices or elements must have a particular orientation, be constructed and operated in a particular orientation, and are therefore not to be considered limiting of the invention.

Furthermore, the terms "first", "second" and "first" are used for descriptive purposes only and are not to be construed as indicating or implying relative importance or implicitly indicating the number of technical features indicated. Thus, a feature defined as "first" or "second" may explicitly or implicitly include at least one such feature. In the description of the present invention, "a plurality" means at least two, e.g., two, three, etc., unless specifically limited otherwise.

In the present invention, unless otherwise expressly stated or limited, the terms "mounted," "connected," "secured," and the like are to be construed broadly and can, for example, be fixedly connected, detachably connected, or integrally formed; may be mechanically coupled, may be electrically coupled or may be in communication with each other; they may be directly connected or indirectly connected through intervening media, or they may be connected internally or in any other suitable relationship, unless expressly stated otherwise. The specific meanings of the above terms in the present invention can be understood by those skilled in the art according to specific situations.

In the present invention, unless otherwise expressly stated or limited, the first feature "on" or "under" the second feature may be directly contacting the first and second features or indirectly contacting the first and second features through an intermediate. Also, a first feature "on," "over," and "above" a second feature may be directly or diagonally above the second feature, or may simply indicate that the first feature is at a higher level than the second feature. A first feature being "under," "below," and "beneath" a second feature may be directly under or obliquely under the first feature, or may simply mean that the first feature is at a lesser elevation than the second feature.

In the present disclosure, the terms "one embodiment," "some embodiments," "an example," "a specific example," or "some examples" and the like mean that a specific feature, structure, material, or characteristic described in connection with the embodiment or example is included in at least one embodiment or example of the present disclosure. In this specification, the schematic representations of the terms used above are not necessarily intended to refer to the same embodiment or example. Furthermore, the particular features, structures, materials, or characteristics described may be combined in any suitable manner in any one or more embodiments or examples. Furthermore, various embodiments or examples and features of different embodiments or examples described in this specification can be combined and combined by one skilled in the art without contradiction.

Although embodiments of the present invention have been shown and described above, it is understood that the above embodiments are exemplary and should not be construed as limiting the present invention, and that variations, modifications, substitutions and alterations can be made to the above embodiments by those of ordinary skill in the art within the scope of the present invention.

Claims

1. A rotor assembly, comprising:

a rotor core having a magnet slot and a rotating shaft hole;

the permanent magnet is arranged in the magnet groove;

the rotating shaft is arranged in the rotating shaft hole, a gap is formed between the rotating shaft and the rotor core, and a first end and a second end of the rotating shaft extend out of the rotating shaft hole;

the first end part vibration damping piece is arranged on the first end surface of the rotor core and is connected with the rotor core;

the transmission piece is arranged in the first end part vibration damping piece and matched with the rotating shaft;

second end damping spare, second end damping spare is established on rotor core's the second terminal surface and with rotor core links to each other, second end damping spare with the pivot directly cooperates, rotor core passes through second end damping spare and loop through first end damping spare with the driving medium drive the pivot.

2. The rotor assembly of claim 1 wherein a portion of the first end damper is directly engaged with the rotating shaft, the rotor core driving the rotating shaft through the portion of the first end damper and, in turn, through the first end damper and the transmission member.

3. The rotor assembly of claim 1 wherein the first end vibration dampener and the second end vibration dampener are each a viscoelastic material.

4. The rotor assembly of claim 3 wherein the loss factor of the viscoelastic material is 0.15 or greater.

5. The rotor assembly of claim 3, wherein the viscoelastic material has a shore hardness of 20-80 degrees.

6. The rotor assembly of claim 1 wherein the transmission comprises a base and a boss projecting from the base toward the first end face of the rotor core, the shaft extending through the base and the boss; the minimum distance between the boss and the first end face of the rotor core in the axial direction of the rotor core is L1, and L1 is larger than 0.5 mm.

7. The rotor assembly of claim 6 wherein the minimum clearance of the boss from the permanent magnet in the radial direction of the rotor core is L2, and L2 > 0.5 mm.

8. The rotor assembly of claim 6 wherein the minimum clearance of the base and the permanent magnets in the axial direction of the rotor core is L3, and L3 > 0.5 mm.

9. The rotor assembly of claim 1 further comprising an outer link damper, the rotor core having an axial through bore between adjacent magnet slots, the outer link damper being disposed within the axial through bore, a first end of the outer link damper being connected to the first end damper, and a second end of the outer link damper being connected to the second end damper.

10. The rotor assembly of claim 9, further comprising an inner connection damper disposed in a gap between the rotating shaft and the rotor core, wherein a first end of the inner connection damper is connected to the first end damper and a second end of the inner connection damper is connected to the second end damper.

11. The rotor assembly of claim 10 further comprising an intermediate link damper, wherein a gap is provided between the inner surface of the permanent magnet and the inner bottom surface of the magnet slot, wherein the intermediate link damper is disposed within the gap, wherein a first end of the intermediate link damper is coupled to the first end damper, and wherein a second end of the intermediate link damper is coupled to the second end damper.

12. The rotor assembly of claim 11, wherein the rotor core is formed by stacking a plurality of rotor laminations in an axial direction of the rotor core, the rotor laminations include full bridge laminations and half bridge laminations, the rotor core has a first end portion, a second end portion and a middle section between the first end portion and the second end portion, the first end portion and the second end portion are formed by stacking a plurality of full bridge laminations, and the middle section is formed by stacking a plurality of half bridge laminations.

13. The rotor assembly of claim 12, wherein one of the axially adjacent half-bridge laminations in the intermediate section rotates one pole relative to the other half-bridge lamination in a circumferential direction of the rotor core.

14. The rotor assembly of claim 12, wherein a portion of the inner magnetic bridges of the plurality of inner magnetic bridges of the half-bridge stamped steel are provided with magnetic bridge holes penetrating through the inner magnetic bridges along the circumferential direction of the rotor core, the inner magnetic bridges of the axially adjacent half-bridge stamped steel of the rotor core are provided with the magnetic bridge holes in the inner magnetic bridge of one half-bridge stamped steel, the inner magnetic bridges of the other half-bridge stamped steel are not provided with the magnetic bridge holes, circumferential connection damping pieces are arranged in the magnetic bridge holes, and the adjacent intermediate connection damping pieces are connected with each other through the circumferential connection damping pieces.

15. The rotor assembly of claim 14 wherein the first end snubber member, the second end snubber member, the inner connection snubber member, the outer connection snubber member, the intermediate connection snubber member, and the circumferential connection snubber member are integrally injection molded from a viscoelastic material.

16. The rotor assembly of claim 1 wherein the peripheral wall of the drive member has drive radial projections and drive radial open slots between adjacent drive radial projections, the end damping member has a central bore, the peripheral wall of the central bore has damping radial projections and radial damping open slots between adjacent damping radial projections, the drive radial projections fit within the damping radial open slots, and the damping radial projections fit within the drive radial open slots.

17. An electrical machine comprising a rotor assembly as claimed in any one of claims 1 to 16.