CN201874832U - Exhaust structure of rotary compressor - Google Patents

Exhaust structure of rotary compressor Download PDF

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Publication number
CN201874832U
CN201874832U CN 201020620729 CN201020620729U CN201874832U CN 201874832 U CN201874832 U CN 201874832U CN 201020620729 CN201020620729 CN 201020620729 CN 201020620729 U CN201020620729 U CN 201020620729U CN 201874832 U CN201874832 U CN 201874832U
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CN
China
Prior art keywords
baffler
bearing
exhaust
rotary compressor
silencer
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
CN 201020620729
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Chinese (zh)
Inventor
孟亮
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Guangdong Meizhi Compressor Co Ltd
Original Assignee
Guangdong Meizhi Compressor Co Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Guangdong Meizhi Compressor Co Ltd filed Critical Guangdong Meizhi Compressor Co Ltd
Priority to CN 201020620729 priority Critical patent/CN201874832U/en
Application granted granted Critical
Publication of CN201874832U publication Critical patent/CN201874832U/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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Abstract

An exhaust structure of a rotary compressor comprises a compression mechanism and a motor component, wherein the compression mechanism and the motor component are disposed in a casing, the compression mechanism includes a bearing, a silencer with an exhaust hole is disposed on the bearing, the motor component includes a motor stator with a stator coil and a motor rotor with a balance block, a fan mechanism facing the silencer is disposed on the end face of the motor rotor, the exhaust hole of the silencer is arranged at a position on a hub close to the bearing, the fan mechanism is positioned with a region enclosed by the stator coil, the exhaust hole of the silencer consists of a gap between a central hole of the silencer and the hub of the bearing, the fan mechanism is disposed on the motor rotor, the silencer or the bearing through an auxiliary support part, and the fan mechanism includes a guide part disposed at the central hole of the silencer. The exhaust structure has the advantages of simple and reasonable structure, low manufacturing cost, low exhaust resistance, low energy loss and high operating efficiency of the compressor.

Description

The exhaust structure of rotary compressor
Technical field
The utility model relates to the exhaust structure of a kind of rotary compressor, particularly a kind of rotary compressor.
Background technique
Common rotary compressor is seen accompanying drawing 1-accompanying drawing 2, and the exhaust structure of this rotary compressor has housing 1, is installed in the housing and has the compression member 2 of bearing 5, is installed on the bearing 5 and has the baffler 6 of exhaust port; Rotating component in the drive compression member 2 rotates and has the rotor 4 of equilibrium block 7; Be installed on the housing and supporting and have a motor stator 3 of stator line bag 8 with rotor.
When above-mentioned exhaust structure during in exhaust, pressurized gas are discharged from the exhaust port on the bearing 5, through baffler 6 and form high velocity air by the exhaust port on the baffler 6 and discharge.This high velocity air directly impacts the equilibrium block 7 on the rotor 4, thereby produces bigger energy loss and disorderly eddy current, has caused exhaust resistance increase and noise to increase.
In addition, after impacting equilibrium block 7 from the high velocity air of the exhaust port of baffler 6 ejection, to around disperse mobile, this air-flow directly flows away through the lower space of stator line bag 8, fully do not contact with stator line bag 8, be unfavorable for separating of lubricated oil droplet that gas and its are carried secretly, the oil content that causes at last discharging in the gas is higher, compressor to tell oil mass bigger.
The exhaust structure that Chinese patent literature CN1916425A disclosed a kind of main bearing in revolve type compressor on 18th in 08 month in 2005, this exhaust structure prevents exhaust frontal impact balancing rotor piece by by changing exhaust position, to reduce pneumatic noise.Though this exhaust structure can reduce gas shock, can not initiatively change airflow direction, still be unfavorable for compressor is told the control of oil mass.
The model utility content
The purpose of this utility model aim to provide a kind of simple and reasonable, fabricating cost is low, exhaust resistance is little and energy loss is few, the exhaust structure of the rotary compressor of the high working efficiency of compressor, to overcome deficiency of the prior art.
Press the exhaust structure of a kind of rotary compressor of this purpose design, comprise the compressing mechanism and the electric machine assembly that are arranged in the housing, compressing mechanism comprises bearing, the baffler that has exhaust port is arranged on the bearing, electric machine assembly comprises motor stator that has stator line bag and the rotor that has equilibrium block, its structure characteristic is that the end face of rotor is provided with the fan towards baffler, and the exhaust port of baffler is arranged on the position near the wheel hub of bearing.
Described fan is positioned at the zone that the stator line is surrounded as.
The exhaust port of described baffler is formed by the space between the wheel hub of the center hole of baffler and bearing.
Described fan is arranged on rotor, baffler or the bearing by auxiliary supports.
Described fan comprises the import conducting element, and this import conducting element is arranged on the central hole of baffler.
One end and the baffler of described import conducting element join, and the other end of import conducting element is outstanding to be established, and this other end is arranged on towards the direction that deviates from fan.
The end face of the utility model by rotor is provided with the fan towards baffler, can be under the effect of fan, change the flow direction of exhaust, avoided original energy loss that causes from the direct column air-flow high speed impact balancing rotor piece of discharging of baffler and caused bigger operation noise; And under the effect of fan, the pressure of outside near zone of the exhaust port of baffler is reduced, make the easier discharge of air-flow in the baffler to have reduced exhaust resistance and energy loss, improve the working efficiency of compressor, also reduced pneumatic noise simultaneously.
The air-flow after change direction after the fan effect in the utility model, stator line bag with the flow direction motor stator, when this air-flow streams stator line bag, increased the separation effect of the gas lubricated oil droplet entrained with it, take and enter low gas the lubricants capacity of air-conditioning system out of in the compressor, improved the working efficiency of air-conditioning system.
The utlity model has simple and reasonable, fabricating cost is low, exhaust resistance is little and energy loss is few, the characteristics of the high working efficiency of compressor.
Description of drawings
Fig. 1 is the broken section structural representation of common rotary compressor.
Fig. 2 is the plan structure schematic representation of existing baffler.
Fig. 3 is the utility model one embodiment's a broken section structural representation.
Fig. 4 removes the broken section structural representation behind housing, motor stator and the liquid-storage container.
Fig. 5 for the A-A among Fig. 4 to analysing and observe the structure for amplifying schematic representation.
Fig. 6 is first embodiment's of the baffler in the utility model a plan structure schematic representation.
Fig. 7 is second embodiment's of the baffler in the utility model a plan structure schematic representation.
Among the figure: 1 is housing, and 2 is compressing mechanism, and 3 is motor stator, and 4 is rotor, and 5 is bearing, and 6 is baffler, and 7 is equilibrium block, and 8 is stator line bag, and 9 is fan, and 10 are the import conducting element, and 11 is auxiliary supports.
Embodiment
Below in conjunction with drawings and Examples the utility model is further described.
Referring to Fig. 3-Fig. 7, the exhaust structure of this rotary compressor, comprise the compressing mechanism 2 and the electric machine assembly that are arranged in the housing 1, compressing mechanism 2 comprises bearing 5, the baffler 6 that has exhaust port is arranged on the bearing 5, electric machine assembly comprises motor stator 3 that has stator line bag 8 and the rotor 4 that has equilibrium block 7, and the end face of rotor 4 is provided with the fan 9 towards baffler 6, and the exhaust port of baffler 6 is arranged on the position near the wheel hub of bearing 5.
Fan 9 is positioned at the zone that stator line bag 8 surrounds.The exhaust port of baffler 6 is formed by the space between the wheel hub of the center hole of baffler 6 and bearing 5.
Fan 9 is arranged on rotor 4, baffler 6 or the bearing 5 by auxiliary supports 11.When fan 9 is arranged on the rotor 4, because the existence of equilibrium block 7, so auxiliary supports 11 should be avoided the position of equilibrium block 7, as shown in Figure 5.It is tabular that this auxiliary supports 11 can be circular arc.
The center hole of baffler 6 can be circular hole or elliptical aperture.
In order to improve the effect of water conservancy diversion, fan 9 can also comprise import conducting element 10, and this import conducting element 10 is arranged on the central hole of baffler 6, sees Fig. 4 and Fig. 7; One end and the baffler 6 of import conducting element 10 join, and the other end of import conducting element 10 is outstanding to be established, and this other end is arranged on towards the direction that deviates from fan 9.Perhaps, directly enlarge the center hole of baffler, the internal diameter R1 of the center hole of the radius R 2 of the center hole of the baffler of this moment>existing baffler.

Claims (6)

1. the exhaust structure of a rotary compressor, comprise the compressing mechanism (2) and the electric machine assembly that are arranged in the housing (1), compressing mechanism (2) comprises bearing (5), the baffler (6) that has exhaust port is arranged on the bearing (5), electric machine assembly comprises motor stator (3) that has stator line bag (8) and the rotor (4) that has equilibrium block (7), the end face that it is characterized in that rotor (4) is provided with the fan (9) towards baffler (6), and the exhaust port of baffler (6) is arranged on the position near the wheel hub of bearing (5).
2. the exhaust structure of rotary compressor according to claim 1 is characterized in that described fan (9) is positioned at the zone that stator line bag (8) surrounds.
3. the exhaust structure of rotary compressor according to claim 2, the exhaust port that it is characterized in that described baffler (6) is formed by the space between the wheel hub of the center hole of baffler (6) and bearing (5).
4. the exhaust structure of rotary compressor according to claim 3 is characterized in that described fan (9) is arranged on rotor (4), baffler (6) or the bearing (5) by auxiliary supports (11).
5. according to the exhaust structure of the arbitrary described rotary compressor of claim 1 to 4, it is characterized in that described fan (9) comprises import conducting element (10), this import conducting element (10) is arranged on the central hole of baffler (6).
6. the exhaust structure of rotary compressor according to claim 5, the end and the baffler (6) that it is characterized in that described import conducting element (10) join, the other end of import conducting element (10) is outstanding to be established, and this other end is arranged on towards the direction that deviates from fan (9).
CN 201020620729 2010-11-17 2010-11-17 Exhaust structure of rotary compressor Expired - Lifetime CN201874832U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN 201020620729 CN201874832U (en) 2010-11-17 2010-11-17 Exhaust structure of rotary compressor

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN 201020620729 CN201874832U (en) 2010-11-17 2010-11-17 Exhaust structure of rotary compressor

Publications (1)

Publication Number Publication Date
CN201874832U true CN201874832U (en) 2011-06-22

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Family Applications (1)

Application Number Title Priority Date Filing Date
CN 201020620729 Expired - Lifetime CN201874832U (en) 2010-11-17 2010-11-17 Exhaust structure of rotary compressor

Country Status (1)

Country Link
CN (1) CN201874832U (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111550409A (en) * 2019-02-12 2020-08-18 纳博特斯克有限公司 Air compressor and method for manufacturing air compressor
CN114483584A (en) * 2020-10-23 2022-05-13 广东美芝制冷设备有限公司 Rotor subassembly, motor and compressor

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111550409A (en) * 2019-02-12 2020-08-18 纳博特斯克有限公司 Air compressor and method for manufacturing air compressor
CN114483584A (en) * 2020-10-23 2022-05-13 广东美芝制冷设备有限公司 Rotor subassembly, motor and compressor
CN114483584B (en) * 2020-10-23 2023-10-24 广东美芝制冷设备有限公司 Rotor assembly, motor and compressor

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GR01 Patent grant
CX01 Expiry of patent term
CX01 Expiry of patent term

Granted publication date: 20110622