CN203404085U - Rotary compressor, as well as rotor component and rotor balancing block thereof - Google Patents
Rotary compressor, as well as rotor component and rotor balancing block thereof Download PDFInfo
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- CN203404085U CN203404085U CN201320423804.3U CN201320423804U CN203404085U CN 203404085 U CN203404085 U CN 203404085U CN 201320423804 U CN201320423804 U CN 201320423804U CN 203404085 U CN203404085 U CN 203404085U
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Abstract
The utility model discloses a rotary compressor, as well as a rotor component and a rotor balancing block thereof. The rotor balancing block comprises a first balancing piece, the first balancing piece is cylindrical, the cross section of the first balancing piece is formed by intersection of an inner curve and an outer curve, an acute angle is formed at the intersection, the contour lines of the inner curve and the outer curve, which are in the vicinity of the acute angle, respectively form arc lines, an included angle alpha is formed between the tangent lines of the two arc lines, and the included angle alpha is not less than 0 degrees and not more than 90 degrees. The rotor balancing block according to the embodiment of the utility model enables a gas flow to be divided at the acute end by forming the acute angle at the intersection of the inner curve and the outer curve, enables the gas flow to smoothly flow along the inner cylindrical surface and the outer cylindrical surface, reduces the vertical action force of the gas flow on the peripheral surface of the balancing block, further reduces the loss of wind resistance, relieves the gas turbulent flow situations, reduces the loss of gas energy, further improves the energy efficiency of the compressor and reduces the noise of the compressor.
Description
Technical field
The utility model relates to rotary compressor field, relates in particular to a kind of balancing rotor piece for rotary compressor, for the rotor assembly of rotary compressor with have the rotary compressor of described rotor assembly.
Background technique
In the compression structure of existing rotary compressor, the imbalance for crankshaft eccentric portion and piston in the balance pump housing produce when rotating with compressor, is generally provided with semiorbicular equilibrium block at the two ends of rotor, plays the object that reduces vibration of compressor and noise.
The balancing rotor piece of traditional form is as shown in Figure 15-16, equilibrium block 1 ' windward side has windward side 11 ', leeward end has lee face 12 ', when rotor 3 ' is pressed solid arrow rotation, and the 1 ' rotation of rotor driven equilibrium block, balancing rotor piece 1 ' both ends of the surface are subject to fluid impact, produce windage loss, affect the efficiency of compressor, also will cause balancing rotor piece 1 ' surrounding fluid turbulent flow simultaneously, cause fluid capacity loss, and produce noise.
Model utility content
The utility model is intended at least solve one of technical problem existing in prior art.For this reason, an object of the present utility model is to propose a kind of balancing rotor piece that reduces windage loss, alleviation fluid turbulent, lifting compressor efficiency, improves noise.
Another object of the present utility model is to propose a kind of rotor assembly with described balancing rotor piece.
Another object of the present utility model is to propose a kind of rotary compressor with described rotor assembly.
According to a kind of balancing rotor piece for rotary compressor of the utility model first aspect embodiment, comprise: the first counterbalance, described the first counterbalance forms cylindricality and its cross section is intersected and formed by inner curve and external curve, and at intersection formation wedge angle, on described inner curve and external curve, the profile line of contiguous described sharp corner forms respectively camber line, angle between described two camber line tangent lines is α, wherein 0 °≤α≤90 °.
According to the utility model embodiment's balancing rotor piece, by forming wedge angle at inner curve and external curve intersection, make air-flow at tip punishment stream, air-flow is smooth mobile along inner cylinder and outer cylinder, has reduced the vertical of air-flow to equilibrium block side face, has reduced thus windage loss, alleviated gas turbulence situation, reduce gas energy loss, and then improved compressor efficiency, reduced compressor noise.
In addition, according to balancing rotor piece of the present utility model, also there is following additional technical feature:
According to an embodiment of the present utility model, described inner curve and external curve all form arcuate line segment, and the radius of arc R2 of inner curve and the radius of arc R1 of external curve unequal.
According to an embodiment of the present utility model, described inner curve forms arcuate line segment, and described external curve forms multi-section-line.
According to an embodiment of the present utility model, described external curve forms arcuate line segment, and described inner curve forms multi-section-line.
According to an embodiment of the present utility model, described inner curve and external curve all form multi-section-line.
According to an embodiment of the present utility model, on described the first counterbalance, along it, be axially provided at least one first mounting hole of connection.
According to an embodiment of the present utility model, described balancing rotor piece also comprises the second counterbalance, and the second end face of the second counterbalance and first counterbalance the first end face fit.
According to an embodiment of the present utility model, described the second counterbalance forms cylindricality, and its cross section forms crescent shape or ring.Thus, easily manufactured and be easily mounted on rotor.
According to an embodiment of the present utility model, on described the second counterbalance, be provided at least one second mounting hole of connection.
According to an embodiment of the present utility model, described the first counterbalance and described the second counterbalance are one-body molded.
According to an embodiment of the present utility model, between the first counterbalance and the second counterbalance, by welding or screw, be connected.
Compared with prior art, according to the utility model embodiment's balancing rotor piece, by adopting said structure can effectively improve compressor efficiency, improve compressor noise, simple and reasonable, applied widely.
A kind of rotor assembly for rotary compressor according to the utility model second aspect embodiment, comprising: rotor; And according to the utility model first aspect embodiment's balancing rotor piece, described balancing rotor piece is located at least one end of described rotor.
According to the utility model third aspect embodiment's rotary compressor, comprise according to the utility model second aspect embodiment's the rotor assembly for rotary compressor.
Additional aspect of the present utility model and advantage in the following description part provide, and part will become obviously from the following description, or recognize by practice of the present utility model.
Accompanying drawing explanation
Above-mentioned and/or additional aspect of the present utility model and advantage accompanying drawing below combination obviously and is easily understood becoming embodiment's description, wherein:
Fig. 1 is according to the schematic diagram of an embodiment's of the utility model balancing rotor piece;
The schematic diagram of Fig. 2 when to be that the balancing rotor shown in Fig. 1 is packaged be assigned on rotor;
Fig. 3 is the schematic diagram while being assigned on rotor according to second embodiment's of the utility model balancing rotor is packaged;
Fig. 4 is the schematic diagram while being assigned on rotor according to the 3rd embodiment's of the utility model balancing rotor is packaged;
Fig. 5 is according to the schematic diagram of the 4th embodiment's of the utility model balancing rotor piece;
The schematic diagram of Fig. 6 when to be that the balancing rotor shown in Fig. 5 is packaged be assigned on rotor;
Fig. 7 is according to the schematic diagram of the 5th embodiment's of the utility model balancing rotor piece;
The schematic diagram of Fig. 8 when to be that the balancing rotor shown in Fig. 7 is packaged be assigned on rotor;
Fig. 9 is according to the schematic diagram of the 6th embodiment's of the utility model balancing rotor piece;
The schematic diagram of Figure 10 when to be that the balancing rotor shown in Fig. 9 is packaged be assigned on rotor;
Figure 11 is according to the schematic diagram of the 7th embodiment's of the utility model balancing rotor piece;
Figure 12 is the sectional view of the balancing rotor piece shown in Figure 11;
The schematic diagram of Figure 13 when to be that the balancing rotor shown in Figure 11 is packaged be assigned on rotor;
Figure 14 is according to the schematic diagram of the 8th embodiment's of the utility model balancing rotor piece;
The schematic diagram of Figure 15 when to be that traditional balancing rotor is packaged be assigned on rotor;
Figure 16 is the phantom shown in Figure 15.
Reference character:
The first counterbalance 1; External curve 11; Inner curve 12; Wedge angle 13; The first mounting hole 14;
The second counterbalance 2; The second mounting hole 21;
Embodiment
Describe embodiment of the present utility model below in detail, described embodiment's example is shown in the drawings, and wherein same or similar label represents same or similar element or has the element of identical or similar functions from start to finish.Below by the embodiment who is described with reference to the drawings, be exemplary, only for explaining the utility model, and can not be interpreted as restriction of the present utility model.
In description of the present utility model, it will be appreciated that, term " on ", orientation or the position relationship of the indication such as D score, 'fornt', 'back', " left side ", " right side ", " vertically ", " level ", " top ", " end ", " interior ", " outward " be based on orientation shown in the drawings or position relationship, only the utility model and simplified characterization for convenience of description, rather than indicate or imply that the device of indication or element must have specific orientation, with specific orientation, construct and operation, therefore can not be interpreted as restriction of the present utility model.In addition, term " first ", " second " be only for describing object, and can not be interpreted as indication or hint relative importance or the implicit quantity that indicates indicated technical characteristics.Thus, one or more these features can be expressed or impliedly be comprised to the feature that is limited with " first ", " second ".In description of the present utility model, except as otherwise noted, the implication of " a plurality of " is two or more.
In description of the present utility model, it should be noted that, unless otherwise clearly defined and limited, term " installation ", " being connected ", " connection " should be interpreted broadly, and for example, can be to be fixedly connected with, and can be also to removably connect, or connect integratedly; Can be mechanical connection, can be to be also electrically connected to; Can be to be directly connected, also can indirectly be connected by intermediary, can be the connection of two element internals.For the ordinary skill in the art, can concrete condition understand the concrete meaning of above-mentioned term in the utility model.
Below with reference to Fig. 1-Figure 14, describe in detail according to the balancing rotor piece of a kind of rotary compressor of the utility model first aspect embodiment, this balancing rotor piece is used in rotary compressor, be arranged on upper end and/or the lower end of rotor 3, windage loss and turbulent flow situation while rotating to reduce rotor.
Balancing rotor piece according to the utility model embodiment, comprising: the first counterbalance 1.The first counterbalance 1 forms cylindricality and its cross section and is intersected and formed by inner curve 12 and external curve 11, and forms wedge angle 13 in intersection, because inner curve 12 and external curve 11 have two crosspoints, therefore wedge angle 13 has two.Wherein, inner curve 12 is identical with the protrusion direction of external curve 11.Particularly, as shown in Figure 1, the first counterbalance 1 comprises: outer cylinder 101, inner cylinder 102,103He lower end surface, upper-end surface (scheming not shown), inner cylinder 102 intersects with outer cylinder 101 and be identical with the protrusion direction of outer cylinder 101.Upper-end surface 103 is located at the top of outer cylinder 101 and inner cylinder 102, and lower end surface is located at the bottom of outer cylinder 101 and inner cylinder 102.
On inner curve 12 and external curve 11, the profile line at contiguous wedge angle 13 places forms respectively camber line, and wherein two radius of curvature are unequal.Article two, the angle between camber line tangent line is α, wherein 0 °≤α≤90 °.As shown in Fig. 2-Fig. 4, the angle between two camber line tangent lines at two wedge angle 13 places at the two ends of the first counterbalance 1 is respectively α 1 and α 2.
In one of them example of the present utility model, as shown in Figure 2, the first counterbalance 1 is configured to the central point o1 of its external curve 11 and the central point o3 of rotor 3 overlaps, and the central point o2 of inner curve 12 and the central point o3 of rotor 3 depart from certain distance L 1, and wherein L1 is determined by specific design.Certainly, the utility model is not limited to this, in another example of the present utility model, as shown in Figure 3, the first counterbalance 1 be configured to the central point o1 of its external curve 11, the central point o2 of inner curve 12 respectively with central point o3 deviation distance L2 and the L1 of rotor 3, wherein L1 and L2 determine by specific design.And in another example of the present utility model, as shown in Figure 4, the first counterbalance 1 is configured to the central point o2 of its inner curve 12 and the central point o3 of rotor 3 overlaps, and the central point o1 of external curve 11 and the central point o3 of rotor 3 depart from.
Preferably, the first counterbalance 1 is symmetrical with respect to the central point o1 of external curve 11 and inner curve 12 and the line of o2, as shown in Fig. 2-Fig. 4.
According to the utility model embodiment's balancing rotor piece, by forming wedge angle 13 at inner curve 12 and external curve 11 intersections, make air-flow at tip punishment stream, air-flow is smooth mobile along inner cylinder and outer cylinder, has reduced the vertical of air-flow to equilibrium block side face, has reduced thus windage loss, alleviated gas turbulence situation, reduce gas energy loss, and then improved compressor efficiency, reduced compressor noise.
According to an embodiment of the present utility model, inner curve 12 and external curve 11 all form arcuate line segment, and the radius of arc R2 of inner curve 12 and the radius of arc R1 of external curve 11 unequal.That is to say, outer cylinder 101 and inner cylinder 102 all form cylndrical surface.So-called cylinder wherein, those skilled in the art are appreciated that cylinder is defined as straight line and determines the formed curved surface of curve parallel along one, wherein determine the directrix that curve is called cylinder, when this directrix is bowlder, gained cylinder is called cylndrical surface.Thus, in balancing rotor piece of the present utility model, outer cylinder 101 and outer cylinder 102 are that straight line is formed around external curve 11 and inner curve 12 parallels respectively, as Figure 1-Figure 4.
According to another embodiment of the present utility model, inner curve 12 forms arcuate line segment, and external curve 11 forms multi-section-line.Preferably, external curve 11 at least comprises straight line line segment.In example as shown in Figure 6, external curve 11 comprises straight line line segment.That is to say on outer cylinder 101, to there is an outerplanar 1011, as shown in Figure 5.
According to another embodiment of the present utility model, external curve 11 forms arcuate line segment, and inner curve 12 forms multi-section-line.Preferably, inner curve 12 at least comprises straight line line segment.In as the embodiment of Fig. 8, inner curve 12 comprises straight line line segment.That is to say in inner cylinder 102, to there is an inner plane 1021, as shown in Figure 7.
As shown in Figure 9 and Figure 10, according to another embodiment of the present utility model, inner curve 12 all forms multi-section-line with external curve 11.Preferably, on inner curve 12 and external curve 11, has respectively straight line line segment at least.That is to say in inner cylinder 102, to have an inner plane 1021 at least, on outer cylinder 101, have an outerplanar 1011 at least.
In embodiments more of the present utility model, as shown in Fig. 1-Figure 10, on the first counterbalance 1, along it, be axially provided with at least one first mounting hole 14, for example, according to balancing rotor piece of the present utility model, can be connected with described rotor by the screw through the first mounting hole 14.
As shown in Figure 11-Figure 14, according to embodiments more of the present utility model, balancing rotor piece also comprises the second counterbalance 2, the first end face of the second end face of the second counterbalance 2 and the first counterbalance 1 fits, wherein the first end face is the end face towards one end of rotor, and the second end face is the end face away from one end of rotor.The second counterbalance 2 is arranged at least one end of rotor.Particularly, when balancing rotor piece is located on the upper-end surface of rotor, the laminating of the lower end surface of the upper-end surface of the second counterbalance 2 and the first counterbalance.And when balancing rotor piece is located on the lower end surface of rotor, the laminating of the upper-end surface of the lower end surface of the second counterbalance 2 and the first counterbalance.
In examples more of the present utility model, the second counterbalance 2 forms cylindricality, and its cross section forms crescent shape, for example, can be the semicircle annular as shown in Figure 11-Figure 12.Preferably, the center of circle of the center of circle of the second counterbalance and the outer cylinder 101 of the first counterbalance 1 is concentric and outer surface is concordant with the outer surface of the first counterbalance.Thus, easily manufactured and be easily mounted on rotor.Certainly, the utility model is not limited to this, in other examples of the present utility model, the second counterbalance 2 forms ring, as shown in figure 14, preferably, the center of circle of the center of circle of the second counterbalance and the outer cylinder 101 of the first counterbalance 1 is concentric and outer surface is concordant with the outer surface of the first counterbalance, equally also easily manufactured and be easily mounted on rotor.
Alternatively, as shown in Figure 11-14, on the second counterbalance 2, be provided at least one second mounting hole 21 of connection, now according to balancing rotor piece of the present utility model, can be connected with described rotor by the screw through the second mounting hole 15, that is to say, after the second mounting hole 21 is set on the second counterbalance 2, balancing rotor piece can be installed, and not need at the first counterbalance 1, to offer the first mounting hole 14 again.
Alternatively, the first counterbalance 1 and the second counterbalance 2 are one-body molded.Or between the first counterbalance 1 and the second counterbalance 2, by welding or screw, be connected alternatively.
Below with reference to Fig. 1-Figure 14, specifically describe according to a plurality of embodiments' of the utility model balancing rotor piece, wherein balancing rotor piece is located on rotor 3.
Embodiment one,
In the present embodiment, as depicted in figs. 1 and 2, balancing rotor piece comprises the first counterbalance 1.The first counterbalance 1 forms cylindricality and its cross section is intersected and formed by inner curve 12 and external curve 11, and form respectively two wedge angles 13 two intersections, angle between two camber line tangent lines at two wedge angle 13 places at the two ends of the first counterbalance 1 is respectively α 1 and α 2,1≤90 ° of 0≤α, 2≤90 ° of 0≤α.
Particularly, as shown in Figure 1, the first counterbalance 1 comprises: outer cylinder 101, inner cylinder 102,103He lower end surface, upper-end surface (scheming not shown), inner cylinder 102 intersects with outer cylinder 103 and be identical with the protrusion direction of outer cylinder 101.Upper-end surface 103 is located at the top of outer cylinder 101 and inner cylinder 102, and lower end surface is located at the bottom of outer cylinder 101 and inner cylinder 102.
In the present embodiment, inner curve 12 and external curve 11 all form arcuate line segment, and the radius of arc R2 of inner curve 12 and the radius of arc R1 of external curve 11 are unequal, and the central point o1 of external curve 11 overlaps with the central point o3 of rotor 3, and the central point o2 of inner curve 12 and the central point o3 of rotor 3 depart from certain distance L 1, wherein L1 is determined by specific design.
In addition, by the first mounting hole 14 being located on the first counterbalance 1, be connected with rotor, the first end face and the rotor of the first counterbalance 1 are fitted.
In actual processing process, corresponding relevant manufacturing technology and method, permission is carried out the processing of technique circular arc chamfering to wedge angle 13 places of the first counterbalance 1, wherein the radius of circular arc chamfering is R0, R0≤3mm, allow outer cylinder 101, inner cylinder 102 to have certain pattern draft, pattern draft≤5 ° simultaneously.
Embodiment two,
As shown in Figure 3, the balancing rotor piece of the present embodiment and embodiment one difference are only, the first counterbalance 1 be configured to the central point o1 of its external curve 11, the central point o2 of inner curve 12 respectively with central point o3 deviation distance L2 and the L1 of rotor 3, wherein L1 and L2 determine by specific design.Other structures and principle are described in embodiment one, do not repeat them here.
Embodiment three,
As shown in Figure 4, the balancing rotor piece of the present embodiment and embodiment one difference be only, the first counterbalance 1 is configured to the central point o2 of its inner curve 12 and the central point o3 of rotor 3 overlaps, and the central point o1 of external curve 11 and the central point o3 of rotor 3 depart from.
Other structures and principle are described in embodiment one, do not repeat them here.
Embodiment four,
As shown in Figure 5 and Figure 6, the balancing rotor piece of the present embodiment and embodiment one difference be only, inner curve 12 forms arcuate line segment, and external curve 11 forms multi-section-line, and external curve 11 comprises straight line line segment.That is to say on outer cylinder 101, to there is an outerplanar 1011, as shown in Figure 5.
Other structures and principle are described in embodiment one, do not repeat them here.
Embodiment five,
As shown in Figure 7 and Figure 8, the balancing rotor piece of the present embodiment and embodiment one difference be only, external curve 11 forms arcuate line segment, and inner curve 12 forms multi-section-line, and inner curve 12 comprises straight line line segment.That is to say in inner cylinder 102, to there is an inner plane 1021, as shown in Figure 7.
Other structures and principle are described in embodiment one, do not repeat them here.
Embodiment six,
As shown in Figure 9 and Figure 10, the balancing rotor piece of the present embodiment and embodiment one difference be only, inner curve 12 all forms multi-section-line with external curve 11, and has respectively straight line line segment on inner curve 12 and external curve 11.That is to say in inner cylinder 102, to have an inner plane 1021 at least, on outer cylinder 101, have an outerplanar 1011 at least.
Other structures and principle are described in embodiment one, do not repeat them here.
Embodiment seven,
As shown in Figure 11-13, the balancing rotor piece of the present embodiment comprises any described in the first counterbalance 1 and the second counterbalance 2, the first counterbalances 1 as embodiment one to six above, at this, no longer describes.The second counterbalance 2 forms cylindricality, and its cross section forms semicircle annular.Wherein the center of circle of the center of circle of the second counterbalance and the outer cylinder 101 of the first counterbalance 1 is concentric and outer surface is concordant with the outer surface of the first counterbalance.
The first end face of the second end face of the second counterbalance 2 and the first counterbalance 1 fits, and wherein the first end face is the end face towards one end of rotor, and the second end face is the end face away from one end of rotor.The second counterbalance 2 is arranged at least one end of rotor.Particularly, when balancing rotor piece is located on the upper-end surface of rotor, the laminating of the lower end surface of the upper-end surface of the second counterbalance 2 and the first counterbalance.And when balancing rotor piece is located on the lower end surface of rotor, the laminating of the upper-end surface of the lower end surface of the second counterbalance 2 and the first counterbalance.
According to balancing rotor piece of the present utility model, can be connected with described rotor by the screw through the second mounting hole 15, the first end face and the rotor of the second counterbalance 2 are fitted, and the second end face laminating of the first end face of the first counterbalance 1 and the second counterbalance 2.
Alternatively, the first counterbalance 1 and the second counterbalance 2 are one-body molded.Or between the first counterbalance 1 and the second counterbalance 2, by welding or screw, be connected alternatively.
Embodiment eight,
As shown in figure 14, the balancing rotor piece of the present embodiment and embodiment seven difference be only, the second counterbalance 2 forms ring.
Other structures and principle are described in embodiment seven, do not repeat them here.
Compared with prior art, according to the utility model embodiment's balancing rotor piece, by adopting said structure can effectively improve compressor efficiency, improve compressor noise, simple and reasonable, applied widely.
A kind of rotor assembly for rotary compressor according to the utility model second aspect embodiment, comprising: rotor; And according to the utility model first aspect embodiment balancing rotor piece, balancing rotor piece is located at least one end of rotor.Alternatively, balancing rotor piece is located at the two ends of rotor.
According to a kind of rotary compressor of the utility model third aspect embodiment, comprise according to the utility model second aspect embodiment's the rotor assembly for compressor.According to other formations of the utility model embodiment's rotary compressor, waiting and operate is all known for those of ordinary skills, is not described in detail here.
In the description of this specification, the description of reference term " embodiment ", " some embodiments ", " illustrative examples ", " example ", " concrete example " or " some examples " etc. means to be contained at least one embodiment of the present utility model or example in conjunction with specific features, structure, material or the feature of this embodiment or example description.In this manual, the schematic statement of above-mentioned term is not necessarily referred to identical embodiment or example.And the specific features of description, structure, material or feature can be with suitable mode combinations in any one or more embodiments or example.
Although illustrated and described embodiment of the present utility model, those having ordinary skill in the art will appreciate that: in the situation that not departing from principle of the present utility model and aim, can carry out multiple variation, modification, replacement and modification to these embodiments, scope of the present utility model is limited by claim and equivalent thereof.
Claims (13)
1. for a balancing rotor piece for rotary compressor, it is characterized in that, comprising:
The first counterbalance, described the first counterbalance forms cylindricality and its cross section is intersected and formed by inner curve and external curve, and at intersection formation wedge angle, on described inner curve and external curve, the profile line of contiguous described sharp corner forms respectively camber line, article two, the angle between described camber line tangent line is α, wherein 0 °≤α≤90 °.
2. the balancing rotor piece for rotary compressor according to claim 1, is characterized in that, described inner curve and external curve all form arcuate line segment, and the radius of arc R2 of inner curve and the radius of arc R1 of external curve unequal.
3. the balancing rotor piece for rotary compressor according to claim 1, is characterized in that, described inner curve forms arcuate line segment, and described external curve forms multi-section-line.
4. the balancing rotor piece for rotary compressor according to claim 1, is characterized in that, described external curve forms arcuate line segment, and described inner curve forms multi-section-line.
5. the balancing rotor piece for rotary compressor according to claim 1, is characterized in that, described inner curve and external curve all form multi-section-line.
6. according to the balancing rotor piece for rotary compressor described in any one in claim 2-5, it is characterized in that, on described the first counterbalance, along it, be axially provided at least one first mounting hole of connection.
7. the balancing rotor piece for rotary compressor according to claim 1, is characterized in that, also comprises the second counterbalance, and the second end face of the second counterbalance and first counterbalance the first end face fit.
8. the balancing rotor piece for rotary compressor according to claim 7, is characterized in that, described the second counterbalance forms cylindricality, and its cross section forms crescent shape or ring.
9. the balancing rotor piece for rotary compressor according to claim 8, is characterized in that, is provided at least one second mounting hole of connection on described the second counterbalance.
10. the balancing rotor piece for rotary compressor according to claim 7, is characterized in that, described the first counterbalance and described the second counterbalance are one-body molded.
The 11. balancing rotor pieces for rotary compressor according to claim 7, is characterized in that, between the first counterbalance and the second counterbalance, by welding or screw, are connected.
12. 1 kinds of rotor assembly for rotary compressor, is characterized in that, comprising:
Rotor; And
According to the balancing rotor piece for rotary compressor described in any one in claim 1-11, described balancing rotor piece is located at least one end of described rotor.
13. 1 kinds of rotary compressors, is characterized in that, comprise the rotor assembly for compressor according to claim 12.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201320423804.3U CN203404085U (en) | 2013-07-16 | 2013-07-16 | Rotary compressor, as well as rotor component and rotor balancing block thereof |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201320423804.3U CN203404085U (en) | 2013-07-16 | 2013-07-16 | Rotary compressor, as well as rotor component and rotor balancing block thereof |
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| Publication Number | Publication Date |
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| CN203404085U true CN203404085U (en) | 2014-01-22 |
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| CN201320423804.3U Expired - Lifetime CN203404085U (en) | 2013-07-16 | 2013-07-16 | Rotary compressor, as well as rotor component and rotor balancing block thereof |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103511276A (en) * | 2013-07-16 | 2014-01-15 | 广东美芝制冷设备有限公司 | Rotary compressor and rotor assembly and rotor balancing block of the rotary compressor |
-
2013
- 2013-07-16 CN CN201320423804.3U patent/CN203404085U/en not_active Expired - Lifetime
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103511276A (en) * | 2013-07-16 | 2014-01-15 | 广东美芝制冷设备有限公司 | Rotary compressor and rotor assembly and rotor balancing block of the rotary compressor |
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| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CX01 | Expiry of patent term | ||
| CX01 | Expiry of patent term |
Granted publication date: 20140122 |