CN1955472A - Friction reducing structure of blade rotary compressor - Google Patents

Friction reducing structure of blade rotary compressor Download PDF

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Publication number
CN1955472A
CN1955472A CN 200510015673 CN200510015673A CN1955472A CN 1955472 A CN1955472 A CN 1955472A CN 200510015673 CN200510015673 CN 200510015673 CN 200510015673 A CN200510015673 A CN 200510015673A CN 1955472 A CN1955472 A CN 1955472A
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CN
China
Prior art keywords
cylinder
blade
ring
rotary compressor
friction reducing
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Pending
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CN 200510015673
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Chinese (zh)
Inventor
李允熙
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LG Electronics Tianjin Appliances Co Ltd
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LG Electronics Tianjin Appliances Co Ltd
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Publication date
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Priority to CN 200510015673 priority Critical patent/CN1955472A/en
Publication of CN1955472A publication Critical patent/CN1955472A/en
Pending legal-status Critical Current

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Abstract

A friction decreasing mechanism arranged between rolling ring and cylinder of the blade rotation type compressor is composed of high-pressure sealed container, cylinder in said sealed container, rolling ring in the internal space of cylinder, a rotary shaft linked with drive motor and inserted in cylinder, the primary and secondary bearings at both ends of cylinder for sealing its internal space, the blade insertion slots on rotary shaft, blades dividing the internal space of cylinder into suction-in space and compression space, and a rotation structure between said rolling ring and cylinder and rotating with rolling ring.

Description

The friction reducing structure of blade rotary compressor
Technical field
What the present invention related to is blade rotary compressor, particularly be to reduce the friction reducing structure that rolls the blade rotary compressor that rubs between ring and the cylinder.
Background technique
Usually, compressor is to convert electrical energy into kinetic energy refrigerant is compressed.Compressor constitutes refrigerating circulation system with agglomerator, capillary tube, rapid steamer, and this refrigerating circulation system is installed in the devices such as refrigerator, air-conditioning.
In constituting the device of above-mentioned refrigerating circulation system, compressor is the parts of core the most, and its research-and-development activity is very many, and content is very abundant.
Fig. 1 and Fig. 2 are existing blade rotary compressor longitudinal sectional drawing and transverse cross-sectional view.As shown in the figure, blade rotary compressor comprises: seal container 10; Be installed on seal container 10 inside and be used to produce the drive motor 20 of rotating force; Form circular inner space P in inside, keep at a certain distance away with drive motor 20 and be combined in cylinder 30 in the seal container 10 with certain internal diameter; Form and to have the concentric eccentric part 41 of concentric mutually with rotating center and combine, make concentric eccentric part 41 be positioned at the running shaft 40 of the inner space P of cylinder simultaneously with drive motor 20; Cover upside and the downside and the combination of cylinder 30 respectively, main bearing 50 and auxilliary bearing 60 that the inner space P of cylinder 30 is sealed; Be inserted into the blade slot 42 in the concentric eccentric part 41 that is formed at running shaft, the blade 70 that the inner space P of cylinder 30 is separated; Be inserted into blade slot 42, be used for blade 70 is carried out the spring 80 of elastic support; Be used for the tap hole 51 that is formed at main bearing 50 is carried out the valve assembly body 90 of switch.
In above-mentioned seal container 10, connect the discharge tube 12 that is used to suck the suction pipe 11 of gas and is used to discharge gas respectively.
The different position, running shaft 40 centers that are centered close to of the inner space P of above-mentioned cylinder, and roll the inner space P that ring 100 will be inserted into cylinder 30, wherein roll ring 100 for to have the drum shape of certain-length and external diameter, roll the corresponding formation of internal diameter of external diameter with the inner space P of cylinder 30 of ring 100.Blade 70 carries out linearity with the inner side surface that rolls ring 100 and contacts, and blade 70 is supported by spring 80.Above-mentioned rolling encircled 100 frictions that can reduce between blade 70 and the cylinder interior space P inner peripheral surface.
Above-mentioned running shaft 40 with certain length comprises: the axial region 43 that combines with drive motor 20; The concentric eccentric part 41 that forms with external diameter and certain length in a side of axial region 43 greater than axial region 43; At the blade slot 42 of concentric eccentric part 41 with certain width and degree of depth formation.Wherein the center of eccentric part 41 is consistent with the center of axial region 43 with one heart, and blade slot 42 forms to the central direction of concentric eccentric part 41 at the outer circumferential face of concentric eccentric part 41.
The inside of above-mentioned main bearing 50 and auxilliary bearing 60 is inserted with running shaft 40, and main bearing 50 and auxilliary bearing 60 will support running shaft 40.Has the inlet hole 61 that is used for sucking gas in the auxilliary bearing 60 to the inner space of cylinder P.
The symbol that does not describe in the accompanying drawings is respectively: 11 are suction pipe, and 21 is stator, and 22 is rotor.
Below, the work of aforesaid blade rotary compressor is described.
At first, when compressor connection power supply, drive motor 20 is started working and is produced rotating force, and the rotating force of drive motor 20 is passed to running shaft 40 and makes running shaft 40 begin rotation.Along with the rotation of running shaft 40, the concentric eccentric part 41 of running shaft will be rotated at the inner space of cylinder P.
Gas is inhaled into the inner space P of cylinder by suction pipe 11 and inlet hole 61, will be discharged to the inside of seal container 10 by tap hole 51 along with the work of valve assembly body 90 at the compressed high temperature and high pressure gas of the inner space of cylinder P.Be discharged to the pressurized gas of seal container 10 inside, then will be discharged to the outside of seal container 10 by discharge tube 12.
In said process, the blade 70 of blade slot 42 that is inserted into the concentric eccentric part 41 of running shaft is along with the rotation of running shaft 40, with roll ring 100 state of contact and in blade slot 42, carry out the straight line back and forth movement.At this moment, will form airtight state between blade 70 and all bearings 50 and the auxilliary bearing 60, and the space that is positioned at above-mentioned blade 70 both sides will be configured for respectively sucks the suction space P1 of gas and be used for the compression volume P2 of pressurized gas.
Along with the concentric eccentric part 41 of above-mentioned running shaft rotates in the P of the inner space of cylinder, with one heart a side of eccentric part 41 peripheries and contacts side surfaces of rolling week in the ring 100, be inserted in the concentric eccentric part 41 blade 70 will with the inner peripheral surface state of contact of rolling ring 100 under be rotated.Thus, at the inner space P that is divided into two regional cylinders by concentric eccentric part 41 and blade 70, its volume separately changes and gas is sucked, compresses and action such as discharge.
At this moment, to slide with respect to the inner peripheral surface that rolls ring 100 with above-mentioned the ring 100 concentric eccentric parts 41 that contacts and be rotated and the blade 70 of rolling, and the outer circumferential face that rolls ring 100 will encircle 100 rotation and slide with respect to the inner peripheral surface of cylinder interior space P along with rolling.But roll between the inner peripheral surface of ring 100 outer circumferential face and cylinder 30 as shown in Figure 3, produce compressive force because of speed difference each other and cause friction to take place.Especially because roll ring 100 and cylinder 30 use metallic material making usually, therefore can produce problems such as noise and wearing and tearing because of the friction between the metal.
Summary of the invention
The objective of the invention is to overcome the deficiency of above-mentioned technology, provide a kind of when running shaft is rotated, be inserted in the running shaft blade with the process of rolling loop contacts and being rotated that is inserted into cylinder interior in, make the friction reducing structure that rolls the blade rotary compressor that the friction that forms reduces between ring and the cylinder.
The technological scheme that solves the problems of the technologies described above is:
A kind of friction reducing structure of blade rotary compressor, the friction reducing structure of this blade rotary compressor comprises: the seal container that keeps high pressure conditions; Be incorporated into the cylinder of sealed container interior; Be inserted into the inner space of cylinder and be rotated roll ring; With produce the running shaft that the rotating force drive motor combined and be inserted into the cylinder interior space; Main bearing and auxilliary bearing that covering is combined in the cylinder both sides and the inner space of cylinder is sealed; Be inserted into the blade slot that is formed in the running shaft,, also comprise being installed in and roll between ring and the cylinder with rolling the rotational structure that ring rotates along with the rotation of running shaft is divided into the blade that sucks space and compression volume with the inner space of cylinder.
Described rotational structure is installed in the inner peripheral surface of cylinder, make its with roll the ring contact.
Described rotational structure is installed in the outer circumferential face that rolls ring, and it is contacted with cylinder.
Described rotational structure is spherical bearing and the inner peripheral surface that is installed in cylinder, make its with roll the ring contact.
Described rotational structure is the needle-type bearing of cylindrical shape.
The invention has the beneficial effects as follows: the present invention by reduction roll the ring and cylinder between friction reducing structure, make and roll ring and can be rotated more glibly, simultaneously can also reduce blade and roll frictional force between the ring, thereby reduce noise and the wearing and tearing that produce because of friction, and improve the quality of compressor.
Description of drawings
Fig. 1 and Fig. 2 are existing blade rotary compressor longitudinal sectional drawing and transverse cross-sectional view;
Fig. 3 is existing blade rotary compressor working state floor map;
Fig. 4 is a blade rotary compressor blade support structure embodiment's of the present invention longitudinal sectional drawing;
Fig. 5 is a blade rotary compressor major component three-dimensional exploded view of the present invention.
The symbol description material * * * of * * accompanying drawing major component
10: seal container 20: drive motor
30: cylinder 40: running shaft
41: concentric eccentric part 42: blade slot
50: main bearing 51: tap hole
60: auxilliary bearing 70: blade
80: spring 90: the valve assembly body
100: roll ring 200: rotational structure
P: inner space P1: suck the space
P2: compression volume
Embodiment
Below, in conjunction with the accompanying drawings embodiments of the invention are elaborated.
Fig. 4 is a blade rotary compressor blade support structure embodiment's of the present invention longitudinal sectional drawing; Fig. 5 is a blade rotary compressor major component three-dimensional exploded view of the present invention.Part same as the prior art has been used identical symbol.
As shown above, the reduction friction structure of leaf type compressor of the present invention comprises: the seal container 10 that keeps high pressure conditions; Be incorporated into the cylinder 30 of seal container 10 inside; Be inserted into the inner space of cylinder 30 and be rotated roll the ring 100; Combine and be inserted into the running shaft of the inner space P of cylinder 30 with the drive motor 20 that is used to produce rotating force; Cover cylinder 30 both sides and combination, main bearing 50 and auxilliary bearing 60 that the inner space P of cylinder 30 is sealed; Be inserted into the blade slot 42 that is formed in the running shaft 40, the inner space P of cylinder 30 be divided into the blade 70 of suction space and compression volume along with the rotation of running shaft 40.Also comprise: rolling install between ring 100 and the cylinder 30 a kind of with the rotational structure 200 that rolls ring 100 rotations.
In above-mentioned seal container 10, connect the discharge tube 12 that is used to suck the suction pipe 11 of gas and is used to discharge gas respectively.
The above-mentioned ring 100 that rolls rolls the corresponding formation of internal diameter of external diameter with the cylinder 30 inner space P of ring 100 for to have the drum shape of certain-length and external diameter.Blade 70 contacts with the inner side surface that rolls ring 100 is linear, and blade 70 is supported by spring 80.Roll ring 100 frictions that can reduce between blade 70 and the cylinder interior space P inner peripheral surface.
Above-mentioned running shaft 40 has certain length, comprises the axial region 43 that combines with drive motor 20; In a side of axial region 43, with the concentric eccentric part 41 that forms greater than the external diameter of axial region 43 and certain length; Eccentric part 41 is with the blade slot 42 of certain width and degree of depth formation with one heart.Wherein the center of eccentric part 41 is consistent with the center of axial region 43 with one heart, and blade slot 42 forms to the central direction of concentric eccentric part 41 at the outer circumferential face of concentric eccentric part 41.
Be formed for inserting through hole 53,63 (not shown) of running shaft 40 in the inside of main bearing 50 and auxilliary bearing 60, and main bearing 50 and auxilliary bearing 60 will support to running shaft 40.
In above-mentioned main bearing 50, form and prolong the extending portion 54 that forms, so that can more stably support running shaft 40 along Vertical direction.And in auxilliary bearing 60, be formed for sucking the inlet hole 61 of gas to the inner space of cylinder P.
Above-mentioned rotational structure 200 uses the needle-type bearing of cylindrical shape, makes it can carry out the linearity contact.
Above-mentioned rotational structure 200 is installed in the inner peripheral surface of cylinder 30, makes it and rolls ring 100 and contact and be advisable.
In addition, rotational structure 200 also can be installed in the outer circumferential face that rolls ring 100, and it is contacted with cylinder 30.
In addition, rotational structure 200 can also use spherical bearing and be installed in the inner peripheral surface of cylinder, makes it and rolls ring 100 and carry out contacting.
The symbol that does not describe in the accompanying drawings is respectively: 11 are suction pipe, and 21 is stator, and 22 is rotor.
Below, the aforesaid process that is suitable for the friction reducing structure of blade rotary compressor of the present invention is described.
At first, rotating force will be started working and produce to drive motor 20 when connecting power supply, and the rotating force of drive motor 20 will be passed to running shaft 40, and running shaft 40 begins rotation.Along with the rotation of running shaft 40, the concentric eccentric part 41 of running shaft will be rotated in the inner space of cylinder 30.
Along with the concentric eccentric part 41 of running shaft is rotated in the P of the inner space of cylinder, a concentric side contacts of a side of the outer circumferential face of eccentric part 41 and the inner peripheral surface that rolls ring 100, and be inserted in the concentric eccentric part 41 blade 70 will with the inner peripheral surface state of contact of rolling ring 100 under be rotated.When with one heart eccentric part 41 and blade 70 are divided into two zones with the inner space P of cylinder, its volume separately will change and gas is sucked, compresses and discharges.
Along with the rotation that is inserted into rotational structure 200 in cylinder 30 surface of contact, will carry out the friction that sliding contact reduces generation with it thereby roll ring 100.Promptly roll between the ring 100 and the inner peripheral surface of cylinder 30 because of the face contact produces friction original, because the present invention can make its rotational structure that carries out linear contact and even face contact by inserting, thus the generation that reduction rubs.In addition,, can also reduce blade 70 and roll the relative velocity difference of encircling between 100, also reduce the generation of friction, can also reduce the noise and the wearing and tearing of generation because rub along with the smoothness of rolling ring 100 is rotated.The present invention has not only improved the quality of compressor, can also reduce the loss that produces because of friction, effectively improves the efficient of compressor.

Claims (5)

1. the friction reducing structure of a blade rotary compressor, the friction reducing structure of this blade rotary compressor comprises: the seal container that keeps high pressure conditions; Be incorporated into the cylinder of sealed container interior; Be inserted into the inner space of cylinder and be rotated roll ring; With produce the running shaft that the rotating force drive motor combined and be inserted into the cylinder interior space; Main bearing and auxilliary bearing that covering is combined in the cylinder both sides and the inner space of cylinder is sealed; Be inserted into the blade slot that is formed in the running shaft,, it is characterized in that, also comprise being installed in and roll between ring and the cylinder with rolling the rotational structure that ring rotates along with the rotation of running shaft is divided into the blade that sucks space and compression volume with the inner space of cylinder.
2. the friction reducing structure of blade rotary compressor according to claim 1 is characterized in that, described rotational structure is installed in the inner peripheral surface of cylinder, make its with roll the ring contact.
3. the friction reducing structure of blade rotary compressor according to claim 1 is characterized in that, described rotational structure is installed in the outer circumferential face that rolls ring, and it is contacted with cylinder.
4. the friction reducing structure of blade rotary compressor according to claim 1 is characterized in that, described rotational structure is spherical bearing and the inner peripheral surface that is installed in cylinder, make its with roll the ring contact.
5. the friction reducing structure of blade rotary compressor according to claim 1 is characterized in that, described rotational structure is the needle-type bearing of cylindrical shape.
CN 200510015673 2005-10-27 2005-10-27 Friction reducing structure of blade rotary compressor Pending CN1955472A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN 200510015673 CN1955472A (en) 2005-10-27 2005-10-27 Friction reducing structure of blade rotary compressor

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN 200510015673 CN1955472A (en) 2005-10-27 2005-10-27 Friction reducing structure of blade rotary compressor

Publications (1)

Publication Number Publication Date
CN1955472A true CN1955472A (en) 2007-05-02

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ID=38062973

Family Applications (1)

Application Number Title Priority Date Filing Date
CN 200510015673 Pending CN1955472A (en) 2005-10-27 2005-10-27 Friction reducing structure of blade rotary compressor

Country Status (1)

Country Link
CN (1) CN1955472A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106401969A (en) * 2016-10-17 2017-02-15 珠海格力节能环保制冷技术研究中心有限公司 Rotary compressor

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106401969A (en) * 2016-10-17 2017-02-15 珠海格力节能环保制冷技术研究中心有限公司 Rotary compressor

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Open date: 20070502