CN104165132B - Compressor - Google Patents

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Publication number
CN104165132B
CN104165132B CN201410378180.7A CN201410378180A CN104165132B CN 104165132 B CN104165132 B CN 104165132B CN 201410378180 A CN201410378180 A CN 201410378180A CN 104165132 B CN104165132 B CN 104165132B
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China
Prior art keywords
rotor
hole
guide plate
end plates
compressor
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CN104165132A (en
Inventor
向东
杨泾涛
郑立宇
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Guangdong Meizhi Precision Manufacturing Co Ltd
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Guangdong Meizhi Precision Manufacturing Co Ltd
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Abstract

The invention discloses a compressor which comprises a shell, a compression mechanism, a motor and a rotor end plate. The compression mechanism is arranged in the shell, the motor is arranged in the shell and connected with the compression mechanism, and the motor comprises a stator and a rotor. A first through hole is formed in the rotor, an end plate of the rotor is arranged at the end, away from the compression mechanism, of the rotor, and a second through hole communicated with the first through hole is formed in the end plate of the rotor. The side wall, adjacent to the center of the end plate of the rotor, of the second through hole is provided with a guiding plate for guiding an oil and gas mixture in the first through hole out in the direction towards the side wall of the shell. According to the compressor, due to the fact that the guiding plate is arranged on the end plate of the rotor, oil and mist separation can be effectively conducted, so that the oil output amount, especially the oil output amount generated in high-frequency operation of the compressor, of the compressor is reduced, refrigerating machine oil is limited in the compressor, and the energy efficiency and reliability of the compressor are improved. In addition, the structure of the end plate of the rotor is simple, and machining and assembling are convenient.

Description

Compressor
Technical field
The present invention relates to art of refrigeration units, especially relate to a kind of compressor.
Background technology
Point out in correlation technique, the Main Function of the refrigerator oil in compressor is lubrication, sealing etc., however, in compression Machine run in, particularly frequency-changeable compressor high frequency run when, because extraction flow is larger, refrigerator oil easily with coolant along Exhaustor is discharged to outside compressor, thus leading to the internal oil starvation of compressor, causes lack of lubrication, the reliability of impact compressor operating Property, simultaneously excessive refrigerator oil enters system (such as air conditioning system), reduces the heat exchange property of air conditioning system, lead to air-conditioning The efficiency of system reduces.The mode that tradition reduces oil spitting amount of compressor is increase oil guard between rotor and exhaustor, or Person is to increase oil guard etc. between stator and upper shell, but due to introducing baroque oil guard, thus increasing Compressor processed complex degree and cost, simultaneously because introducing the accessories such as oil guard, and then reduce the reliability of compressor And safety.
Content of the invention
It is contemplated that at least solving one of technical problem present in prior art.For this reason, it is an object of the invention to A kind of compressor is proposed, described compressor can be effectively reduced oil spitting amount.
Compressor according to embodiments of the present invention, including:Housing;Compression mechanism, described compression mechanism is located at described housing Interior;Motor, described motor is located in described housing and is connected with described compression mechanism, and described motor includes stator and rotor, The first through hole of insertion is formed with described rotor;And rotor end plates, described rotor end plates be located at described rotor away from institute State one end of compression mechanism, described rotor end plates are formed with the second through hole being connected with described first through hole, wherein said The side wall at the center of neighbouring described rotor end plates of two through holes is provided with guide plate with by the air-fuel mixture in described first through hole The direction of the side wall towards described housing for the thing is derived.
Compressor according to embodiments of the present invention, by arranging guide plate in rotor end plates, such that it is able to carry out effectively Ground mist of oil separate, and then reduce compressor oil spitting amount, especially reduce compressor high frequency run when oil spitting amount, by fridge Oil is limited in compressor, improves efficiency and the reliability of compressor.In addition, the structure of rotor end plates is simple, be easy to processing and Assembling.
Alternatively, described guide plate is located at the side away from described rotor of described rotor end plates, and described guide plate from The interior direction being directed away from described rotor to outward extends.
Specifically, described guide plate is directed away from direction straight line, curve or the broken line extension of described rotor from inside to outside.
Further, the distance between center of the one end in the circumference of described guide plate and described rotor end plates is more than institute State the distance between the other end in the circumference of guide plate and center of described rotor end plates.Thus, make flow process away from rotor The stress of heart axis direction increases, and lifts mist of oil separating effect.
Alternatively, described second through hole is that multiple and the plurality of second through hole is circumferentially spaced along described rotor end plates Distribution, described guide plate is multiple, and the plurality of guide plate is corresponded with the plurality of second through hole.
Further, described rotor is formed with towards described rotor end plates side open wide cavity, described cavity with Described first through hole all connects with described second through hole.Thus, it is possible to improve mist of oil separating effect further.
Alternatively, described guide plate stretches in described cavity, and described guide plate is directed away from described compression from inside to outside The direction of mechanism extends.Thus, it is possible to improve the safety and reliability of compressor.
Specifically, described guide plate and the diapire of described cavity are spaced apart from each other.
Alternatively, described cavity is formed on the rotor core of described rotor, the height H of wherein said cavity1Meet: 0.05×H2≤H1≤0.5×H2, wherein, described H2Height for described rotor core.
Specifically, the center of described rotor end plates is formed with the through hole of insertion.Thus, meet processing technique to require.
The additional aspect of the present invention and advantage will be set forth in part in the description, and partly will become from the following description Obtain substantially, or recognized by the practice of the present invention.
Brief description
Fig. 1 is the profile of compressor according to embodiments of the present invention;
Fig. 2 is the profile of the rotor shown in Fig. 1, rotor end plates and balance weight;
Fig. 3 is the profile of the rotor shown in Fig. 2 and balance weight;
Fig. 4 is the top view of the rotor shown in Fig. 3;
Fig. 5 is the top view of the rotor end plates shown in Fig. 2;
Fig. 6 is the profile of compressor in accordance with another embodiment of the present invention;
Fig. 7 is the profile of the rotor shown in Fig. 6, rotor end plates and balance weight;
Fig. 8 is the profile of the rotor shown in Fig. 6 and balance weight;
Fig. 9 is the top view of the rotor shown in Fig. 8;
Figure 10 is the profile of the rotor shown in Fig. 9;
Figure 11 is the profile of the compressor according to further embodiment of the present invention;
Figure 12 is the profile of the rotor shown in Figure 11;
Figure 13 is the profile of the compressor according to another embodiment of the present invention;
Figure 14 is the profile of the rotor shown in Figure 13, rotor end plates and balance weight.
Reference:
100:Compressor;
1:Housing;11:Upper shell;111:Exhaustor;12:Main casing;13:Lower house;
2:Motor:21:Stator;211:Line bag;
22:Rotor core;221:Magnet;222:First through hole;223:Cavity;
224:Installing hole;225:First rivet hole;
23:Rotor end plates;231:Guide plate;232:Second through hole;
233:Through hole;234:Second rivet hole;
24:Rotor bottom plate;241:Third through-hole;
251:Upper balance weight;252:Lower balance weight;
26:Rivet;
3:Compression mechanism;31:Base bearing;32:Supplementary bearing;33:Cylinder.
Specific embodiment
Embodiments of the invention are described below in detail, the example of described embodiment is shown in the drawings, wherein from start to finish The element that same or similar label represents same or similar element or has same or like function.Below with reference to attached The embodiment of figure description is exemplary it is intended to be used for explaining the present invention, and is not considered as limiting the invention.
Below with reference to Fig. 1-Figure 14, compressor 100 according to embodiments of the present invention is described, wherein, compressor 100 can be Vertical compressor 100 or horizontal compressor 100, in explained below of the present invention, with compressor 100 for vertical rotating formula pressure Illustrate as a example contracting machine 100.
As shown in figure 1, compressor 100 according to embodiments of the present invention, including:Housing 1, compression mechanism 3, motor 2 and Rotor end plates 23.
Specifically, with reference to Fig. 1, housing 1 can be by upper shell 11, main casing 12 and lower house 13 be sequentially connected with group The cylindrical shape sealed shell of tank becoming, compression mechanism 3 and motor 2 are respectively provided in main casing 12, and wherein motor 2 includes rotor and stator 21, stator 21 is fixed on the top in main casing 12, and rotor includes rotor core 22 and Magnet 221, and Magnet 221 vertically plugs In rotor core 22, Magnet 221 is interacted with stator 21, so that rotor is rotatably arranged at the inner side of stator 21.
As shown in figure 1, compression mechanism 3 can include bent axle (not shown), base bearing 31, supplementary bearing 32 and cylinder 33, cylinder 33 is located between base bearing 31 and supplementary bearing 32 and is respectively positioned on the lower section of motor 2, and the upper end of bent axle and rotor are fixed, The lower end of bent axle sequentially passes through base bearing 31, cylinder 33 and supplementary bearing 32, thus base bearing 31, cylinder 33 and supplementary bearing 32 Jointly limit compression chamber, bent axle has eccentric part, eccentric part is arranged with piston, piston is located at compression intracavity, works as rotor When driving crank rotation, piston can be able to roll along the inwall of compression chamber, and cylinder 33 is formed with the vane slot radially extending, slide plate It is provided with reciprocating slide plate, the inner (i.e. adjacent to the one end at cylinder 33 center) of slide plate is stopped with the periphery wall phase of piston in groove Support, bent axle passes through eccentric part band piston in compression intracavity eccentric motion, thus pressing to the coolant entering into compression intracavity Contracting, the top of upper shell 11 is set as the exhaustor 111 running through, and the coolant after compression discharges compressor 100 from exhaustor 111.
Further, rotor end plates 23 be located at rotor the one end away from compression mechanism 3 (upper for example shown in Fig. 2 End).For example in the figure 2 example, rotor core 22 is vertically arranged, and the upper surface of rotor core 22 is provided with rotor end plates 23, The top of rotor end plates 23 is provided with balance weight 251, analogously, the lower surface of rotor core 22 can also be provided with rotor End plate 24, the bottom of rotor bottom plate 24 is provided with lower balance weight 252.Wherein, rotor core 22 and rotor end plates 23 can be passed through The mode that rivet 26 connects is fixed together, referring for example to Fig. 4 and Fig. 5, the first rivet that rotor core 22 is formed through Hole 225, the second rivet hole 234 that rotor end plates 23 are formed through, the first rivet hole 225 and the second rivet hole 234 are one by one Corresponding, such that it is able to the first rivet hole 225 and the second rivet hole 234 are connected using rivet 26, so that rotor end plates 23 are fixing On rotor core 22.
With reference to Fig. 2, rotor is formed with the first through hole 222 of insertion, first through hole 222 runs through rotor ferrum along the vertical direction Core 22, and be spaced apart with Magnet 221, rotor end plates 23 are formed with the second through hole 232, the second through hole 232 passes through along the vertical direction Wear rotor end plates 23, and be connected with first through hole 222, analogously, rotor bottom plate 24 could be formed with vertically side To the third through-hole 241 running through, third through-hole 241 is connected with first through hole 222, thus compression after coolant can from lower to On pass sequentially through the top that third through-hole 241, first through hole 222 and the second through hole 232 are passed to rotor, then from upper shell The exhaustor 111 at 11 tops is discharged.
Specifically, the side wall at the center of adjacent rotor end plate 23 of the second through hole 232 is provided with guide plate 231, guide plate 231 directions being used for the side wall towards housing 1 by the gas mixture in first through hole 222 are derived that is to say, that guide plate 231 are used for the gas mixture in first through hole 222 is directed away from the direction derivation at the center of rotor end plates 23.With reference to Fig. 1 And Fig. 2, rotor end plates 23 can be formed as disc, and rotor core 22 can be formed as cylindrical, the diameter of rotor end plates 23 With the equal diameters of rotor core 22, rotor end plates 23 are co-axially mounted on the upper surface of rotor core 22, first through hole 222nd, the second through hole 232 is all not passed through rotor core 22 and the central axis of rotor end plates 23, guide plate 231 and the second through hole The side wall of 232 central axis of adjacent rotor end plate 23 is connected, and guide plate 231 is bottom-up is directed away from rotor end plates 23 The direction of central axis tilts to extend, thus coolant from bottom to top can be from the second through hole 232 along leading in first through hole 222 Flow out to the surface of plate 231, the direction being directed away from rotor end plates 23 central axis because guide plate 231 is bottom-up tilts to prolong Stretch, thus coolant is bottom-up tilting to flow out along the direction away from rotor end plates 23 central axis.
Refrigerator oil can be taken due to during the bottom-up flowing of the coolant after compression out of, to be formed as mist of oil fluid-mixing, oil Mist fluid-mixing in the presence of guide plate 231, bottom-up along the direction away from rotor end plates 23 central axis from second After through hole 232 tilts to flow out, can impact on the line bag 211 of stator 21, thus playing the detached effect of mist of oil, minimizing is mixed with The coolant of refrigerator oil discharges compressor 100, reduces the oil spitting amount of compressor 100.In addition, in order to preferably reach separating of oil effect Really, the stator 21 using with the collocation of this rotor can use Distributed Winding stator 21, when mist of oil fluid-mixing gets to stator 21 line When on bag 211, preferably separating of oil effect can be reached.Certainly, the invention is not restricted to this, stator 21 can also be that concentratred winding is fixed Son 21.
Compressor 100 according to embodiments of the present invention, by guide plate 231 is arranged on rotor end plates 23, such that it is able to Carry out mist of oil effectively to separate, and then reduce the oil spitting amount of compressor 100, especially reduce when compressor 100 high frequency runs Oil spitting amount, refrigerator oil is limited in compressor 100, improves efficiency and the reliability of compressor 100.In addition, rotor end plates 23 structure is simple, is easy to process and assembles.
In one embodiment of the invention, the second through hole 232 is multiple and multiple second through holes 232 along rotor end plates 23 Circumferentially spaced distribution, guide plate 231 is multiple, and multiple guide plate 231 corresponded with multiple second through holes 232.Ginseng According to Fig. 2 and Fig. 5, rotor end plates 23 are formed with six the second through holes 232 running through, and six the second through holes 232 are in rotor-end Uniformly arranging in the ground circumferentially spaced apart from one another of plate 23, correspondingly, with reference to Fig. 3 and Fig. 4, rotor core 22 is formed with six and passes through The first through hole 222 worn, and six first through holes 222 uniformly arrange on the ground circumferentially spaced apart from one another of rotor core 22, six Individual first through hole 222 corresponds and communicates with each other with six the second through holes 232, the adjacent rotor end of each the second through hole 232 One guide plate 231 is respectively equipped with the side wall of plate 23 central axis, each guide plate 231 is all bottom-up to be directed away from rotor The direction of end plate 23 central axis tilts to extend.Thus, it is possible to improve mist of oil separating effect further, reduce compressor 100 Oil spitting amount.
Here, it should be noted that first through hole 222, the second through hole 232, the quantity of third through-hole 241, shape and Size all can be arranged according to actual requirement, preferably to meet actual requirement.
Alternatively, in the one end in the circumference of guide plate 231 (for example at the A end of the example of Fig. 5) with rotor end plates 23 The distance between center R2 is more than the other end (for example at the B end of the example of Fig. 5) and rotor end plates in the circumference of guide plate 231 The distance between 23 center R1.For example in the example of hgure 5, the geomery all same of each the second through hole 232, and equal shape Become rectangle, the geomery all same of each guide plate 231, it is all formed as homogeneous with each the second through hole 232 shape, size With rectangular slab, being connected with the second through hole 232 side wall of guide plate 231, and the two ends end points of side wall respectively terminal A and end points The distance between B, terminal A and rotor end plates 23 central axis are R2, the distance between terminal B and rotor end plates 23 central axis For R1, when rotor end plates 23 rotate counterclockwise, terminal B is located at the upstream of terminal A, now constructs R2 >=R1, works as rotor end plates 23 when turning clockwise, and terminal A is located at the upstream of terminal B, now constructs R1 >=R2, so that flow process is away from rotor end plates 23 The stress of center position increases, and lifts mist of oil separating effect.Here, it should be noted that the quantity of guide plate 231, shape with And size all can be arranged according to actual requirement, preferably to meet actual requirement.Preferably, guide plate 231 and rotor end plates 23 are integrally formed.
In one embodiment of the invention, rotor is formed with towards the unlimited cavity 223 in the side of rotor end plates 23, Cavity 223 is all connected with first through hole 222 and the second through hole 232.Specifically, reference picture 6- Fig. 9, cavity 223 is formed at rotor Rotor core 22 on, and be downwardly concaved from the upper surface of rotor core 22 and form, and the top of cavity 223 is opened wide, first leads to The top in hole 222 is connected with the bottom of cavity 223, and the bottom of the second through hole 232 is connected with the top of cavity 223, and empty Chamber 223 cross-sectional area in the horizontal plane is more than whole first through holes 222 total cross-sectional area in the horizontal plane and whole the Two through holes 232 total cross-sectional area in the horizontal plane.
Thus, behind the coolant being mixed with refrigerator oil bottom-up outflow first through hole 222, initially enter cavity 223, Cross-sectional area due to cavity 223 is more than whole first through holes 222 total cross-sectional area in the horizontal plane, thus being mixed with freezing The flows decrease of the coolant of machine oil, is collided with the side wall of cavity 223 and the diapire of rotor end plates 23 simultaneously, forms mist of oil Separating, thus reduce flowing into the coolant being mixed with refrigerator oil in the second through hole 232, reducing the oil spitting amount of compressor 100 further.
Alternatively, the height of cavity 223 is H1, the height of rotor core 22 is H2, wherein, 0.05 × H2≤H1≤0.5× H2.Specifically, with reference to Figure 10, cavity 223 can be formed as isodiametric cylinder, and with reference to Figure 12, cavity 223 can also be formed Cylinder for reducing that is to say, that along rotor core 22 central axial direction, the cross section at each height of cavity 223 Long-pending can different, shape of cross section can also be different.Thus, the coolant entering in cavity 223 can be on the side wall of cavity 223 Occur more tempestuously to collide, thus further increasing mist of oil separating effect.Here, it should be noted that the shape of cavity 223 Shape and size all can be arranged according to actual requirement, and preferably to meet actual requirement, such as cavity 223 may be formed as Polygon cylinder.In addition, for reaching more preferable mist of oil separating effect, the cross-sectional area of cavity 223 needs to do greatly as far as possible.
In some embodiments of the invention, with reference to Fig. 1, Fig. 6 and Figure 11, guide plate 231 is located at the remote of rotor end plates 23 From the side (upside for example shown in Fig. 1) of rotor, and guide plate 231 is directed away from the direction extension of rotor from inside to outside. Specifically, the lower end of guide plate 231 is connected with the side wall of the second through hole 232, and the upper end of guide plate 231 is bottom-up to be directed away from The direction of rotor end plates 23 central axis tilts to extend, and when being formed with cavity 223 on rotor core 22, guide plate 231 is located at The top of cavity 223, such that it is able to play the detached effect of mist of oil.Here, it should be noted that " interior " can be understood as direction The direction of rotor center axis, its rightabout is defined as " outward ", that is, away from the direction of rotor center axis.Wherein, guide Plate 231 can extend along straight line, curve or broken line, and guide plate 231 is less than or equal to 90 ° with the angle of horizontal plane, thus leading More preferable guide effect can be played to plate 231, to realize preferably separating of oil effect.
Certainly, the invention is not restricted to this, in other embodiments of the present invention, with reference to Figure 13, when on rotor core 22 When being formed with cavity 223, guide plate 231 can also stretch in cavity 223, and guide plate 231 is directed away from compressing from inside to outside The direction of mechanism 3 extends.Specifically, the upper end of guide plate 231 is connected with the side wall of the second through hole 232, the lower end of guide plate 231 From up to down tilt to extend towards near the direction of rotor end plates 23 central axis, and the lower end of guide plate 231 and cavity 223 Diapire is spaced apart from each other, such that it is able to play the detached effect of mist of oil.Wherein, guide plate 231 can be along straight line, curve or folding Line extends, and guide plate 231 is less than or equal to 90 ° with the angle of horizontal plane, and preferably 45 °, thus guide plate 231 can play Preferably guide effect, to realize preferably separating of oil effect.
Alternatively, the center of rotor end plates 23 is formed with the through hole 233 of insertion.With reference to Fig. 5 and Fig. 7, through hole 233 is along upper The center of rotor end plates 23, wherein a diameter of D3 of through hole 233 are run through in lower direction, and cavity 223 is located at rotor core 22 top Center, and a diameter of D1 of the cavity 223 of cylinder, rotor core 22 is also formed with the installing hole running through along the vertical direction 224, installing hole 224 is located at the center of rotor core 22 for installing bent axle, wherein first through hole 222, installing hole 224, the Two through holes 232, through hole 233 are all connected with cavity 223, and preferably, D1 >=D2, D1 >=D3.
Here, it should be noted that through hole 233 is fabrication hole, complete assembly technology for auxiliary, when by through hole 233 Diameter D3 do as far as possible little after it is ensured that the coolant major part in cavity 223 is all discharged from the second through hole 232, reduce from through hole The coolant quantities of 233 discharges, and then make more coolant being mixed with refrigerator oil get on stator 21 line bag 211, improve further and Ensure mist of oil separating effect.
Below with reference to Fig. 1-Figure 14, the compressor 100 according to the multiple embodiment of the present invention is described.
Embodiment one,
Reference picture 1- Fig. 5, the through hole 233 that rotor end plates 23 are formed through and the second through hole 232, the second through hole 232 Side wall be provided with guide plate 231, the lower end of guide plate 231 is connected with the side wall of the second through hole 232, the upper end of guide plate 231 The bottom-up direction being directed away from rotor end plates 23 central axis tilts along straight-line extension, the folder of guide plate 231 and horizontal plane Angle is 45 °, rotor rotate counterclockwise, the upstream end points of the side wall being connected with the second through hole 232 side wall of guide plate 231 and rotor The distance between end plate 23 central axis is more than or equal to the distance between downstream end points and rotor end plates 23 central axis, thus entering One step makes flow process increase away from the stress of rotor center axis direction, lifts mist of oil separating effect.
Thus, when compressor 100 operates, the fluid-mixing of coolant and refrigerator oil is discharged upwards from first through hole 222, When by the second through hole 232, fluid-mixing, because the guide effect of guide plate 231, is directed away from while flowing up turning The direction flowing of sub- rotation axiss, fluid-mixing is finally beaten on stator 21 line bag 211, leads to refrigerator oil to divide with coolant mist of oil From the refrigerator oil after separating converges, and flows down along stator 21 line bag 211, then passes through stator slot, rotor gap and determines The outer trimming of son returns to the bottom in compressor 100, reaches preferable oil return effect.Wherein stator slot and the outer trimming of stator are existing There is technology.
Embodiment two,
Reference picture 6- Figure 10, the present embodiment is roughly the same with the structure of embodiment one, and wherein identical part is using identical Reference, the difference is that only:In the present embodiment two, the top of rotor is formed with cavity 223.
As shown in fig. 6, the top of rotor core 22 is formed with the larger cavity of cross-sectional area 223, cavity 223 is from rotor ferrum The upper surface of core 22 is downwardly concaved, and when compressor 100 operates, the fluid-mixing of coolant and refrigerator oil is from first through hole 222 Discharge upwards, then flow in the larger cavity of cross-sectional area 223, the flow area of fluid-mixing increases, thus fluid-mixing Speed reduce, and fluid-mixing collided with the inwall of cavity 223 and the diapire of rotor end plates 23 simultaneously, forms first The detached effect of secondary mist of oil, now partial freeze machine oil separate formation with coolant compared with larger oil droplet, this part oil droplet is because of volume relatively Greatly, a part of oil droplet can be back to downwards compressor 100 housing 1 from the inwall of first through hole 222 and installing hole 224 Portion, another part oil droplet is easy to be attached to the housing of stator 21 line bag 211 or compressor 100 after going out rotor end plates 23 On 1 inwall, thus being also back to the bottom of housing 1.
Remaining coolant is flowed out from the second through hole 232 with the fluid-mixing of refrigerator oil, and the guiding due to guide plate 231 is made With beating on stator 21 line bag 211, serving the detached effect of secondary mist of oil.In addition, it is mixed because of coolant and refrigerator oil Interflow body is through rotor gap, thus also enabling the detached effect of mist of oil by the fluid-mixing of rotor gap portion.
Embodiment three,
With reference to Figure 11 and Figure 12, the present embodiment is roughly the same with the structure of embodiment two, and wherein identical part adopts phase Same reference, the difference is that only:The shape of cavity 223 is different.Specifically, rotor core 22 is formed as irregular shape Shape, i.e. the cylinder of variable cross-section, thus, it is possible to increase coolant and the fluid-mixing of refrigerator oil and the collision of cavity 223 inwall, Improve mist of oil separating effect.
Example IV,
With reference to Figure 13 and Figure 14, the present embodiment is roughly the same with the structure of embodiment two, and wherein identical part adopts phase Same reference, the difference is that only:The direction of guide plate 231 is different.
With reference to Figure 13, guide plate 231 is from the interior sidewall surface of the second through hole 232 downwards and towards rotor end plates 23 central axis Extend, the angle between guide plate 231 and rotor end plates 23 is 135 °.Thus, it is possible to reduce accounting for of rotor end plates 23 further Space, and because guide plate 231 is located in cavity 223, thus improve the security performance of compressor 100.
In describing the invention it is to be understood that term " " center ", " longitudinal ", " horizontal ", " on ", D score, " perpendicular Directly ", the instruction such as " level ", " top ", " bottom ", " interior ", " outward ", " clockwise ", " counterclockwise ", " axial ", " radially ", " circumferential " Orientation or position relationship are based on orientation shown in the drawings or position relationship, be for only for ease of the description present invention and simplification is retouched State, rather than instruction or the hint device of indication or element must have specific orientation, with specific azimuth configuration and operation, Therefore it is not considered as limiting the invention.
Additionally, term " first ", " second " are only used for describing purpose, and it is not intended that indicating or hint relative importance Or the implicit quantity indicating indicated technical characteristic.Thus, define " first ", the feature of " second " can express or Implicitly include one or more this feature.In describing the invention, " multiple " are meant that two or more, Unless otherwise expressly limited specifically.
In the present invention, unless otherwise clearly defined and limited, term " installation ", " being connected ", " connection ", " fixation " etc. Term should be interpreted broadly, for example, it may be being fixedly connected or being detachably connected or integral;Can be that machinery connects Connect or electrically connect;Can be to be joined directly together it is also possible to be indirectly connected to by intermediary, can be in two elements The connection in portion or the interaction relationship of two elements.For the ordinary skill in the art, can be according to concrete feelings Condition understands above-mentioned term concrete meaning in the present invention.
In the present invention, unless otherwise clearly defined and limited, fisrt feature second feature " on " or D score permissible It is the first and second feature directly contacts, or the first and second features pass through intermediary mediate contact.And, fisrt feature exists Second feature " on ", " top " and " above " but fisrt feature are directly over second feature or oblique upper, or be merely representative of Fisrt feature level height is higher than second feature.Fisrt feature second feature " under ", " lower section " and " below " can be One feature is immediately below second feature or obliquely downward, or is merely representative of fisrt feature level height and is less than second feature.
In the description of this specification, reference term " embodiment ", " some embodiments ", " example ", " specifically show The description of example " or " some examples " etc. means specific features, structure, material or the spy describing with reference to this embodiment or example Point is contained at least one embodiment or the example of the present invention.In this manual, to the schematic representation of above-mentioned term not Identical embodiment or example must be directed to.And, the specific features of description, structure, material or feature can be in office Combine in an appropriate manner in one or more embodiments or example.Additionally, in the case of not conflicting, the skill of this area The feature of the different embodiments described in this specification or example and different embodiment or example can be tied by art personnel Close and combine.

Claims (8)

1. a kind of compressor is it is characterised in that include:
Housing;
Compression mechanism, described compression mechanism is located in described housing;
Motor, described motor is located in described housing and is connected with described compression mechanism, and described motor includes stator and rotor, The first through hole of insertion is formed with described rotor;And
Rotor end plates, described rotor end plates are located at one end away from described compression mechanism of described rotor, in described rotor end plates It is formed with the second through hole connecting with described first through hole, the center of neighbouring described rotor end plates of wherein said second through hole Side wall be provided with the guide plate of tilt flat plate shape with by the gas mixture in described first through hole towards described housing side The direction of wall is derived, and described second through hole is multiple and multiple described second through holes along circumferentially spaced point of described rotor end plates Cloth, described guide plate is multiple, and multiple described guide plate is corresponded with multiple described second through holes.
2. compressor according to claim 1 it is characterised in that described guide plate be located at described rotor end plates away from institute State the side of rotor, and described guide plate is directed away from the direction extension of described rotor from inside to outside.
3. compressor according to claim 1 is it is characterised in that one end in the circumference of described guide plate and described rotor The distance between center of end plate is more than between the other end and the center of described rotor end plates in the circumference of described guide plate Distance.
4. the compressor according to claim 1 or 3 is it is characterised in that be formed with towards described rotor-end on described rotor The cavity that the side of plate is opened wide, described cavity is all connected with described first through hole and described second through hole.
5. compressor according to claim 4 is it is characterised in that described guide plate stretches in described cavity, and described leads The direction being directed away from described compression mechanism from inside to outside to plate extends.
6. compressor according to claim 5 is it is characterised in that described guide plate is spaced with the diapire of described cavity Open.
7. compressor according to claim 4 is it is characterised in that described cavity is formed at the rotor core of described rotor On, the height H1 of wherein said cavity meets:
0.05×H2≤H1≤0.5×H2
Wherein, described H2 is the height of described rotor core.
8. compressor according to claim 1 is it is characterised in that the center of described rotor end plates is formed with the logical of insertion Hole.
CN201410378180.7A 2014-08-01 2014-08-01 Compressor Active CN104165132B (en)

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CN105958681A (en) * 2016-06-08 2016-09-21 珠海凌达压缩机有限公司 Compressor rotor and compressor with same

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CN204061177U (en) * 2014-08-01 2014-12-31 广东美芝精密制造有限公司 Compressor

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CN201934313U (en) * 2011-02-16 2011-08-17 广东美芝制冷设备有限公司 Rotary compressor
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