CN1707109A - Air leakage preventing device for closed compressor - Google Patents
Air leakage preventing device for closed compressor Download PDFInfo
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- CN1707109A CN1707109A CN 200410019510 CN200410019510A CN1707109A CN 1707109 A CN1707109 A CN 1707109A CN 200410019510 CN200410019510 CN 200410019510 CN 200410019510 A CN200410019510 A CN 200410019510A CN 1707109 A CN1707109 A CN 1707109A
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- bearing
- demarcation strip
- space
- running shaft
- type compressor
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Abstract
The present invention provides one kind of gas leak preventer for closed compressor. The compressor consists of cylinder, bearings, rotation shaft and several guide boards. Sealing parts are set between the bearing thrust surface and the rotation shaft bearing and between the bearing thrust surface and the partition board to avoid the leakage of refrigerant from the compression space to the suction space while reducing the friction loss between the bearing and the rotation shaft to prevent performance degradation of the compressor.
Description
Technical field
The present invention relates to the hermetic type compressor that a kind of inner space cylinder is divided into several confined spaces, relate in particular to the hermetic type compressor that prevents from the leakage of demarcation strip flex point cold media air.
Background technique
General hermetic type compressor is blade (vane) to be installed make the inner space of cylinder be divided into suction space and compression volume on solid of rotation, and along with being rotated in of running shaft sucks space and compression volume suction, compression and the discharge of conversion to finish fluid back and forth.
Fig. 1 is the partial cutaway schematic of hermetic type compressor in the past, and Fig. 2 is the partial cutaway schematic of compression mechanical part in the hermetic type compressor in the past, and Fig. 3 is the generalized section of running shaft demarcation strip in the hermetic type compressor in the past.As shown in the figure, hermetic type compressor includes mechanism portion and compression mechanical part in the past.Described mechanism portion is arranged on the inside upper part of shell 1, is used for providing power to system; Compression mechanical part is connected mechanism portion and finishes the suction of fluid, compression and discharge.Compression mechanical part has and can absorb and the inner space of compression refrigerant gas and be made up of cylinder 2, upper bearing (bearing plate) 3A, lower bearing 3B, running shaft 4, the first guide plate 5A, the second guide plate 5B and guide plate spring 6.Cylinder 2 is installed in the Lower Half of shell 1; Upper bearing 3A and lower bearing 3B are enclosed within on the above and below of cylinder, form cylinder block dress body jointly; Running shaft 4 has the demarcation strip 4C that the inner space V of cylinder assembly body is divided into several confined spaces S1, S2, and the transmission of power of mechanism portion to compression mechanical part; The first guide plate 5A and the second guide plate 5B are installed in the both sides of running shaft 4 demarcation strip 4C, and when running shaft is worked, make each confined space S1, S2 suck conversion back and forth between space and compression volume; Leaf spring 6 is used for supporting above-mentioned guide plate 5A, 5B.In order to cover the upper and lower surface of cylinder 2, bearing 3A, 3B make disc-shape and are made up of 3a of thrust bearing portion and the 3b of radial bearing portion.The 3a of thrust bearing portion is used for the 4B of bearing portion of supporting rotating shaft 4 to prevent its skidding on axial direction; The central authorities of the 3b of radial bearing portion are formed with axis hole, and the axial region 4A of running shaft 4 is rotated on its radial direction.
Running shaft 4 is made of axial region 4A, the 4B of bearing portion and demarcation strip (blade).Axial region 4A portion within it forms oil circuit 4a, is combined on the rotor of mechanism portion connecting upper bearing 3A and lower bearing 3B, and transmits the power of mechanism portion; The 4B of bearing portion along radial direction be installed in axial region 4A below, support upper bearing 3A and lower bearing 3B; Demarcation strip 4C is formed on the outer circumferential face of the 4B of bearing portion, and the inner space V of cylinder assembly body is divided into the first airtight space S 1 and second space S 2.The flex point of demarcation strip 4C bi-side contacts with upper bearing 3A and lower bearing 3B respectively, and demonstrates bellows-shaped when projecting on the plane.In order to make each bearing 3A, 3B reach the face contact, process sealing surface 4b at the flex point place usually.The first guide plate 5A and the second guide plate 5B make rod shape, but the connection curved surface surface of contact of each guide plate 5A, 5B is corresponding the both sides of demarcation strip, makes curve form.Unaccounted symbol SP is a gas inlet pipe in the accompanying drawing.
The working procedure of hermetic type compressor was described as follows in the past.After connecting power supply on the mechanism portion, rotor is along with rotation, and running shaft 4 begins rotation, makes the first guide plate 5A that is installed in the upper and lower bi-side of demarcation strip 4C and the second guide plate 5B along with demarcation strip 4C moves in the opposite direction.The mutual conversion of volume of first space S 1 of cylinder and second space S 2 in this process makes cold media air enter first space S 1 and second space S 2 continuously along gas inlet pipe SP.The refrigerant that enters the cylinder assembly body is along with the rotation of demarcation strip 4C is compressed gradually, and the both sides flex point of demarcation strip 4C excretes from the exhaust port of discharging starting point and going to the process of exhaust port by separately by the time.
But as shown in Figure 2, each confined space S1, S2 are to be that boundary is divided into and forms low voltage section that sucks Space L and the high-voltage section of forming compression volume H with each sealing surface 4b of demarcation strip 4C and guide plate 5A, 5B in the above-mentioned hermetic type compressor.When the approaching discharge of above-mentioned demarcation strip 4c starting point, the cold media air in the compressor might flow to the relatively low suction Space L of pressure along the sealing surface 4b of demarcation strip 4c and the slit between bearing 3A.Moreover, when sucking refrigerant, the demarcation strip 4c of running shaft 4 is excessively tight with contacting of bearing 3A, 3B, therefore increases frictional loss, reduces the performance of compressor.
Summary of the invention
In order to solve the problems of the technologies described above, the anti-locking apparatus of the gas leakage of the hermetic type compressor of the frictional loss when the purpose of this invention is to provide the secondary refrigerant leakage that can prevent demarcation strip flex point place between minimizing and bearing.
The technical solution adopted for the present invention to solve the technical problems is:
Locking apparatus is prevented in a kind of gas leakage of hermetic type compressor, and the compressor among the present invention is made of cylinder, several bearings, running shaft, several guide plates.Above-mentioned cylinder has the inner space of oneself; Above-mentioned Bearing Installation is at the opening of cylinder; Above-mentioned running shaft comprises bearing portion and demarcation strip, and its middle (center) bearing portion connects and spring bearing, and demarcation strip is divided into several confined spaces to the cylinder interior space; Guide plate and along with the curvature of demarcation strip is done upper and lower to-and-fro motion, makes each confined space suck conversion back and forth between space and compression volume on the upper and lower bi-side that axially are installed in above-mentioned running shaft of bearing.It is characterized in that between the bearing portion, demarcation strip of the running shaft of the bearing thrust face of bearing and contact bearing thrust surface sealed department being set sucks the space to prevent that refrigerant is leaked to from compression volume.
On the bearing portion of the running shaft that is cut in bearing and demarcation strip, form sealed department according to the anti-locking apparatus of the gas leakage of hermetic type compressor of the present invention and suck the space, reduce frictional loss between bearing and the running shaft simultaneously to prevent the decreased performance of compressor to prevent that cold media air is leaked to from compression volume.
Description of drawings
Fig. 1 is the partial cutaway schematic of hermetic type compressor in the past;
Fig. 2 is the partial cutaway schematic of compression mechanical part in the hermetic type compressor in the past;
Fig. 3 is the generalized section of running shaft demarcation strip in the hermetic type compressor in the past;
Fig. 4 is the section schematic perspective view according to compression mechanical part in the hermetic type compressor of the present invention;
Fig. 5 is the generalized section according to running shaft demarcation strip in the hermetic type compressor of the present invention;
Fig. 6 is the generalized section that prevents the gas leakage process according to expression in the hermetic type compressor of the present invention;
Fig. 7 is the generalized section according to the variation of the anti-locking apparatus of gas leakage of hermetic type compressor of the present invention;
Fig. 8 is the schematic perspective view according to other embodiment of the anti-locking apparatus of gas leakage of hermetic type compressor of the present invention.
The critical piece description of reference numerals
12. cylinder 13A, 13B. bearing (bearing plate)
13a. thrust bearing (thrust bearing) 13b. radial bearing (radial bearing)
14. running shaft 14A. axial region
14B. the 14C. of bearing portion demarcation strip
14b. sealing surface 15A, 15B. guide plate (vane)
17. sealed department
17a. socket (tip seal) 17b. sealed member
17c. groove Bt. bearing thrust face
L. suck Space H. compression volume
Embodiment
Below, describe the preferred embodiment that is used for the anti-locking apparatus of gas leakage of hermetic type compressor according to of the present invention in detail with reference to accompanying drawing.
Fig. 4 is the schematic perspective view according to compression mechanical part in the hermetic type compressor of the present invention; Fig. 5 is the generalized section according to running shaft demarcation strip in the hermetic type compressor of the present invention; Fig. 6 is the generalized section that prevents the gas leakage process according to expression in the hermetic type compressor of the present invention; Fig. 7 is the generalized section that is used to reduce the hermetic type compressor variation of gas leakage according to of the present invention.
As shown in the figure, the anti-locking apparatus of gas leakage that is used for hermetic type compressor according to the present invention is made of cylinder (cylinder) 12, upper bearing 13A and lower bearing 13B, running shaft 14, the first guide plate 15A and the second guide plate 15B, guide plate spring and sealed member.Above-mentioned cylinder 12 is installed in shell Lower Half as shown in Figure 4, and has the inner space V of absorption and compression refrigerant gas; Upper bearing 13A and lower bearing 13B are connected on the above and below of cylinder 12, with the cylinder 12 common cylinder block dress bodies of forming; Above-mentioned running shaft 14 has the demarcation strip 14 that the inner space V of cylinder assembly body is divided into several confined spaces S1, S2, and the transmission of power of mechanism portion is arrived compression mechanical part; The above-mentioned first guide plate 15A contacts the both sides of running shaft 14 demarcation strip 14C respectively with the second guide plate 15B, and when running shaft 14 rotations, makes each confined space S1, S2 suck space and compression volume conversion back and forth; Above-mentioned guide plate spring is used for supporting above-mentioned guide plate 15A, 15B; Above-mentioned sealed member is arranged on the 14B of bearing portion and demarcation strip 14C of running shaft 14, is used to prevent that cold media air is leaked to the suction space from the compression volume of each confined space S1, S2.
In order to cover the upper and lower surface of cylinder 12, bearing 13A, 13B make disc-shape and are made up of thrust bearing 13a and radial bearing 13b.Thrust bearing 13a is used for the 14B of bearing portion of supporting rotating shaft 14 to prevent its skidding on axial direction; The central authorities of radial bearing 13b are formed with axis hole, and the axial region 14A of running shaft 14 is rotated on its radial direction.Running shaft 14 is by axial region 14A, and 14B of bearing portion and demarcation strip 14C constitute.Described axial region 14A portion within it forms oil circuit, and is combined on the rotor of mechanism portion to connect upper bearing 3A and lower bearing 13B, is used to transmit the power of mechanism portion; The described bearing 14B of portion along radial direction be installed in axial region 14A below, support upper bearing 13A and lower bearing 13B; Demarcation strip 14C is formed on the outer circumferential face of the 14B of bearing portion, and the inner space V of cylinder assembly body is divided into the first airtight space S 1 and second space S 2.The flex point of demarcation strip 14C bi-side contacts with upper bearing 13A and lower bearing 13B respectively, and demonstrates bellows-shaped when projecting on the plane.In order to make each bearing 13A, 13B reach the face contact, process sealing surface 14b at the flex point place usually.
Sealed member 17 is made of socket 17a and sealed member 17b.Described socket 17a is along the sealing surface 14b of demarcation strip 14C, is recessed to form to demarcation strip 14C from the 14B of bearing portion of running shaft 14; Described sealed member 17b inserts to be installed in the socket 17a, and rises along with the pressure difference between compression volume H in each space S 1 and suction Space L and contact to prevent the leakage of cold media air with the bearing thrust face Bt of bearing 13A, 13B.Socket 17 and sealed member 17b on projecting to the plane time its shape be rectangular.And can enlarge its size from rotating center along radial direction as required.In addition as shown in Figure 6, sealed member 17b can form with single part, also can according to circumstances make with a plurality of sheet materials as shown in Figure 7.In order to make sealed member 17b along with the bearing thrust face Bt of the flexible rising of pressure difference between compression volume H and suction Space L with bearing 13A, 13B keeps lubricating, sealed member 17b preferably makes less than the material of running shaft with lubriation material or friction factor.
The working procedure of above-mentioned hermetic type compressor in the past is as follows.Rotor (not illustrating among the figure) rotated after mechanism portion was connected power supply, and running shaft 14 beginnings rotation thereupon, the feasible first guide plate 15A that contacts in the upper and lower bi-side of demarcation strip 14C and the second guide plate 15B are along with demarcation strip 14C moves in the opposite direction.The mutual conversion of volume of first space S 1 of cylinder and second space S 2 in this process makes cold media air enter first space S 1 and second space S 2 continuously along gas inlet pipe SP.The refrigerant that enters the cylinder assembly body is along with the rotation of demarcation strip 14C is compressed gradually, and the both sides convex curved surface of demarcation strip 4C excretes from the exhaust port of discharging starting point and going to the process of exhaust port by separately by the time.When demarcation strip 14C near the process of discharging starting point in cold media air in the compression volume will be by demarcation strip 14C sealing surface 14b and the suction space that flows to low-pressure, the slit between the bearing thrust face Bt of bearing 13A, 13B, but the refrigerant among the compression volume H flows to socket 17a earlier, be brought to sealed member 17b then, make the sealing parts closely contact, prevent the leakage of cold media air and the decreased performance of compressor with the bearing thrust face Bt of bearing 13A, 13B.In contrast, when demarcation strip 14C when carrying out inhalation process, sealed member 17b descends some slightly to reduce the density that contacts between demarcation strip and bearing 13A, 13B.Significantly reduce the demarcation strip 14C of turning axle 14 and the friction between bearing 13A, 13B like this, effectively prevented the decreased performance of compressor.
Besides it is bright according to another embodiment who is used for the anti-locking apparatus of gas leakage of hermetic type compressor of the present invention.Be between the 14B of bearing portion of running shaft 14 and demarcation strip 14C, to insert sealed member among the aforesaid embodiment, and between the bearing portion of above-mentioned running shaft 14 and demarcation strip 14C, a plurality of groove 17c be set in the present embodiment along radial direction.At this moment, when the approaching discharge of demarcation strip 14C initial point, rising along with pressure among the compression volume H, the slit of cold media air between the bearing thrust face Bt of the sealing surface 14b of demarcation strip 14C and bearing 13A, 13B will be flowed out outside the compression volume H, but by above-mentioned groove 17c, prevent the leakage of cold media air to a certain extent, thereby prevented the decline of compressor performance in advance.When demarcation strip 14C carries out inhalation process in addition, and the area of contact between bearing 13A, 13B is reduced to the area that is equivalent to groove 17c, prevented the decreased performance of the compressor that causes because of frictional loss thus.
Claims (5)
1, the anti-locking apparatus of a kind of gas leakage of hermetic type compressor, its compressor is made of cylinder, several bearings, running shaft, several guide plates; Above-mentioned cylinder has the inner space; Above-mentioned Bearing Installation is at the opening of cylinder; Above-mentioned running shaft comprises bearing portion and demarcation strip, and its middle (center) bearing portion connects and spring bearing, and demarcation strip is divided into several confined spaces to the cylinder interior space; Guide plate and along with the curvature of demarcation strip is done upper and lower to-and-fro motion, makes each confined space suck space and compression volume conversion back and forth on the upper and lower bi-side that axially are installed in above-mentioned running shaft of bearing; It is characterized in that: sealed department is set between the bearing portion of the bearing thrust face of bearing and the running shaft of contact bearing thrust surface, the demarcation strip sucks the space to prevent that refrigerant is leaked to from compression volume.
2, the anti-locking apparatus of the gas leakage of hermetic type compressor according to claim 1 is characterized in that:
Sealed department is made of socket and sealed member, and described socket forms along radial direction to demarcation strip in the bearing portion of running shaft; Described sealed member is installed in socket, and along with compression volume with suck on the bearing thrust face of pressure difference between space contact bearing when rising along axle direction.
3, the anti-locking apparatus of the gas leakage of hermetic type compressor according to claim 2 is characterized in that:
Above-mentioned sealed member is made with single part.
4, the anti-locking apparatus of the gas leakage of hermetic type compressor according to claim 2 is characterized in that:
Above-mentioned sealed member is made with a plurality of sheet materials.
5, the anti-locking apparatus of the gas leakage of hermetic type compressor according to claim 1 is characterized in that:
Above-mentioned sealed department to demarcation strip, forms more than one mazy type groove along radial direction in the bearing portion of running shaft.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNB200410019510XA CN100455801C (en) | 2004-06-09 | 2004-06-09 | Air leakage preventing device for closed compressor |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNB200410019510XA CN100455801C (en) | 2004-06-09 | 2004-06-09 | Air leakage preventing device for closed compressor |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN1707109A true CN1707109A (en) | 2005-12-14 |
| CN100455801C CN100455801C (en) | 2009-01-28 |
Family
ID=35581179
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CNB200410019510XA Expired - Fee Related CN100455801C (en) | 2004-06-09 | 2004-06-09 | Air leakage preventing device for closed compressor |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN100455801C (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104594953A (en) * | 2014-01-03 | 2015-05-06 | 摩尔动力(北京)技术股份有限公司 | Circular cylinder axial isolation fluid mechanism and device comprising same |
| CN104632287A (en) * | 2014-01-03 | 2015-05-20 | 摩尔动力(北京)技术股份有限公司 | Circular cylinder axial fluid isolation mechanism and device comprising same |
| CN104632288A (en) * | 2014-01-09 | 2015-05-20 | 摩尔动力(北京)技术股份有限公司 | Round cylinder axial-isolation same-wheel control fluid mechanism and device comprising same |
Family Cites Families (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4093408A (en) * | 1976-12-03 | 1978-06-06 | Yoshichika Yamaguchi | Positive cam type compressor |
| JPH0763175A (en) * | 1993-08-25 | 1995-03-07 | Kobe Steel Ltd | Scroll compressor |
| JPH11166493A (en) * | 1997-12-03 | 1999-06-22 | Mitsubishi Electric Corp | Rotary compressor |
| JP2002021752A (en) * | 2000-07-05 | 2002-01-23 | Fujitsu General Ltd | Scroll compressor |
| KR100417584B1 (en) * | 2001-06-04 | 2004-02-05 | 주식회사 엘지이아이 | Cylinder assembly of compressor |
| CN1451867A (en) * | 2002-04-15 | 2003-10-29 | 乐金电子(天津)电器有限公司 | Sealed compressor partition plate structure |
-
2004
- 2004-06-09 CN CNB200410019510XA patent/CN100455801C/en not_active Expired - Fee Related
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104594953A (en) * | 2014-01-03 | 2015-05-06 | 摩尔动力(北京)技术股份有限公司 | Circular cylinder axial isolation fluid mechanism and device comprising same |
| CN104632287A (en) * | 2014-01-03 | 2015-05-20 | 摩尔动力(北京)技术股份有限公司 | Circular cylinder axial fluid isolation mechanism and device comprising same |
| CN104632288A (en) * | 2014-01-09 | 2015-05-20 | 摩尔动力(北京)技术股份有限公司 | Round cylinder axial-isolation same-wheel control fluid mechanism and device comprising same |
Also Published As
| Publication number | Publication date |
|---|---|
| CN100455801C (en) | 2009-01-28 |
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Granted publication date: 20090128 |