CN211398020U - Axial air suspension bearing, compressor and air conditioner - Google Patents
Axial air suspension bearing, compressor and air conditioner Download PDFInfo
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- CN211398020U CN211398020U CN202020041861.5U CN202020041861U CN211398020U CN 211398020 U CN211398020 U CN 211398020U CN 202020041861 U CN202020041861 U CN 202020041861U CN 211398020 U CN211398020 U CN 211398020U
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Abstract
The utility model relates to an axial gas suspension bearing, compressor and air conditioner, axial gas suspension bearing includes: a first foil (51); a second foil (52) spaced from the first foil (51); a third foil (53) having a wave shape and disposed between the first foil (51) and the second foil (52); at least one vent (54) in communication with the cavity between the third foil (53) and the second foil (52); and at least one orifice (55) extending in the thickness direction of the axial aerostatic bearing for conveying gas between the second foil (52) and the rotating part carried by the axial aerostatic bearing. Use the technical scheme of the utility model, the air vent carries gas to the cavity between second foil and the third foil in, can change the anti deformability of second foil to be favorable to improving the rigidity of axial gas suspension bearing.
Description
Technical Field
The utility model relates to a refrigeration plant field particularly, relates to an axial gas suspension bearing, compressor and air conditioner.
Background
The gas bearing is adopted by the gas suspension centrifugal compressor as a supporting element of the compressor rotor, the compressor realizes oil-free and friction-free operation, and the gas bearing has small friction, small temperature rise and low loss during high-speed operation, and is suitable for high-speed operation of the centrifugal compressor. The high-speed development of the centrifugal compressor can promote the miniaturization of the centrifugal compressor, so that the gas bearing can promote the miniaturization development of the centrifugal compressor and expand the cooling capacity range of the centrifugal compressor.
The air suspension centrifugal compressor is mainly divided into a dynamic pressure air suspension compressor and a static pressure air suspension compressor, and a dynamic pressure air bearing and a static pressure air bearing are respectively adopted, wherein the dynamic pressure air bearing generates a supporting force by utilizing the high-speed rotation motion of the bearing, and the static pressure air bearing generates a supporting force by utilizing the introduction of external high-pressure air into the bearing. The dynamic pressure gas bearing has good adaptability during high-speed operation, but when the dynamic pressure gas bearing operates at low speed, the bearing and the rotor have friction, and the static pressure bearing does not have friction at low speed, but easily generates an air hammer phenomenon during high-speed operation, thereby causing instability.
After the design of the conventional dynamic pressure bearing and the hydrostatic bearing is finished, the bearing characteristics are not changed any more, and the change of external load is large in the operation process of the compressor, so that the bearing is difficult to adapt to the external change load at many times, and the abnormality of the compressor is easily caused.
SUMMERY OF THE UTILITY MODEL
The utility model aims at providing an axial gas suspension bearing, compressor and air conditioner to there is the gas suspension bearing among the improvement prior art and accomplishes the problem that the back bearing characteristic can not change in the design.
According to the utility model discloses an aspect provides an axial gas suspension bearing, and axial gas suspension bearing includes:
a first foil;
a second foil spaced apart from the first foil;
the third foil is wave-shaped and is arranged between the first foil and the second foil;
at least one vent in communication with the cavity between the third foil and the second foil; and
at least one orifice extending in the thickness direction of the axial aerostatic bearing for conveying gas between the second foil and the rotating component carried by the axial aerostatic bearing.
Alternatively, the axial air bearing includes a shaft hole for allowing the rotating shaft to pass therethrough and a plurality of rows of orifices arranged in a circumferential direction of the shaft hole, each row of orifices including a plurality of orifices arranged in a radial direction of the shaft hole.
Optionally, the second foil comprises a plurality of fan-shaped foils arranged along a circumference of the shaft hole.
Optionally, at least one row of orifices is arranged between two adjacent fan foils.
Alternatively, the first foil may be provided with a plurality of protrusions arranged in a circumferential direction of the shaft hole, the protrusions being bar-shaped extending in a radial direction of the shaft hole, and the orifice being provided on the protrusions.
Optionally, a fan foil is located between two adjacent bumps.
Optionally, the wave trough portion of the third foil abuts the first foil and the wave crest portion of the third foil abuts the second foil.
Optionally, the ventilation holes are provided on the wave trough portions of the third foil.
According to the utility model discloses an on the other hand still provides a compressor, and the compressor includes:
a housing;
the rotating shaft is arranged in the shell;
the thrust disc is connected with the rotating shaft; and
the axial air suspension bearing is arranged opposite to the thrust disc.
Optionally, the compressor further comprises:
a first air source in communication with both the vent hole and the orifice hole; or
And one of the first air source and the second air source is communicated with the vent hole, and the other one of the first air source and the second air source is communicated with the throttling hole.
Optionally, at least one of the first and second air sources is an air pump.
Optionally, the compressor further comprises a control valve,
the control valve is used for controlling the pressure and/or flow of the gas output by the vent hole and the throttling hole; or
The control valve includes a first control valve for controlling the pressure and/or flow rate of the gas output from the vent hole and a second control valve for controlling the pressure and/or flow rate of the gas output from the orifice.
According to another aspect of the utility model, still provide an air conditioner, the air conditioner includes foretell compressor.
Use the technical scheme of the utility model, the air vent carries gas to the cavity between second foil and the third foil in, can change the anti deformability of second foil to be favorable to improving the rigidity of axial gas suspension bearing.
Other features of the present invention and advantages thereof will become apparent from the following detailed description of exemplary embodiments of the invention, which proceeds with reference to the accompanying drawings.
Drawings
In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the drawings needed to be used in the description of the embodiments or the prior art will be briefly described below, it is obvious that the drawings in the following description are only some embodiments of the present invention, and for those skilled in the art, other drawings can be obtained according to these drawings without inventive exercise.
Fig. 1 shows a schematic structural view of a compressor according to an embodiment of the present invention;
FIG. 2 shows a partial enlarged view of FIG. 1;
fig. 3 shows a schematic partial cross-sectional structure view of a first face of an axial air bearing of an embodiment of the present invention;
FIG. 4 shows a partial enlarged view of FIG. 3;
fig. 5 shows a schematic partial cross-sectional structure view of a second face of an axial air bearing according to an embodiment of the present invention.
In the figure:
1. a housing; 2. a rotating shaft; 3. a thrust plate; 4. a carrier member; 41. a gas distribution chamber; 42. a duct; 5. an axial air bearing; 51. a first foil; 52. a second foil; 53. a third foil; 54. a vent hole; 55. an orifice; 6. a diffuser; 7. a bearing seat; 71. a gas flow channel; 8. an impeller; 9. and (4) controlling the valve.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. The following description of at least one exemplary embodiment is merely illustrative in nature and is in no way intended to limit the invention, its application, or uses. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative efforts belong to the protection scope of the present invention.
Fig. 1 shows a partial sectional view of the compressor of the present embodiment. As shown in fig. 1, the compressor of the present embodiment includes a housing 1, a rotating shaft 2 disposed in the housing 1, an impeller 8 mounted on the rotating shaft 2, a diffuser 6, a thrust disk 3 fixedly mounted on the rotating shaft 2, an axial air-suspension bearing 5 disposed opposite to the thrust disk 3, a radial bearing sleeved on the rotating shaft 2, and a bearing seat 7. The diffuser 6 is provided with a diffuser flow passage, and the refrigerant accelerated by the impeller 8 is compressed in the diffuser flow passage.
The bearing housing 7 is provided with a gas flow passage 71 for supplying gas to the axial air bearing 5. The bearing seat 7 is also provided with a bearing hole matched with the radial bearing. The axial air bearing 5 is located at one end of the bearing hole. Both sides of the thrust disk 3 are provided with an axial air suspension bearing 5. The thrust disc 3 and the axial air suspension bearing 5 are both positioned between the diffuser 6 and the bearing seat 7. The diffuser 6 is also provided with a flow passage for conveying gas to the gas suspension bearing.
As shown in fig. 1 and 2, the compressor further comprises a carrier 4 for carrying an axial air bearing 5, the axial air bearing 5 being mounted on the carrier 4.
As shown in fig. 3 to 5, the axial air bearing 5 of the present embodiment includes a first foil 51 connected to the carrier 4, a second foil 52 spaced apart from the first foil 51, and a third foil 53 disposed between the first foil 51 and the second foil 52. The second foil 52 is located on the side of the first foil 51 adjacent to the rotating part carried by the aerostatic bearing 5. In this embodiment, the rotating member is supported by the air bearing 5 as the thrust plate 3.
The third foil 53 is wave-shaped. In some embodiments, the valley portions 53a of the third foil 53 abut the first foil 51 and the peak portions 53b of the third foil 53 abut the second foil 52.
The axial air bearing 5 is further provided with at least one vent hole 54, and the vent hole 54 penetrates through the first foil 51 and the third foil 53 and is communicated with the cavity between the third foil 53 and the second foil 52. The vent holes 54 deliver gas to the cavity between the third foil 53 and the second foil 52 to support the second foil 52, thereby improving the supporting ability and the deformation resistance of the second foil 52 and improving the rigidity of the axial air bearing 5.
The vent hole 54 penetrates through the first foil 51 and the third foil 53 into the cavity between the second foil 52 and the third foil 53, the vent hole does not penetrate through the second foil 52, and the gas entering the axial air bearing 5 from the vent hole cannot enter the gap between the second foil 52 and the thrust plate 3.
As shown in fig. 3 and 4, the vent holes 54 are provided on the valley portions 53a of the third foil 53.
The bearing housing 7 is provided with a gas flow passage 71 for supplying gas to the vent hole 54. The carrier 4 is provided with a gas distribution chamber 41 on the side thereof adjacent the bearing seat 7. The bearing part 4 is further provided with a gas duct 42 extending from the gas distribution chamber 41 to the axial gas suspension bearing 5, and the gas duct 42 is used for communicating the gas distribution chamber 41 and the vent 54. Optionally, the gas distribution chamber 41 is annular.
The axial aerostatic bearing is further provided with at least one orifice 55, the orifice 55 extending in the thickness direction of the axial aerostatic bearing for transporting gas between the second foil 52 and the rotating part carried by the axial aerostatic bearing 5, so that the axial aerostatic bearing 5 has both the dynamic and the hydrostatic bearing characteristics.
In the present embodiment, the orifice 55 and the vent hole 54 are both communicated with the gas flow passage 71, and the orifice 55 and the vent hole 54 are supplied with gas from the same gas source.
In other alternative embodiments, orifice 55 and vent 54 are each supplied by different gas sources. The compressor includes a first source and a second source, one of which is in communication with the vent 54 and the other of which is in communication with the orifice 55. One of the first air source and the second air source is an air pump.
The compressor in this embodiment also comprises a control valve 9 communicating with the gas flow channel 71. Optionally, the control valve 9 comprises a regulating valve for regulating the pressure and/or flow of the gas output by the orifice 55 and/or the vent 54. By adjusting the pressure and/or flow of the gas output by the vent 54, the stiffness of the axial aero-suspension bearing 5 may be adjusted.
In some embodiments, the compressor includes a first control valve for regulating the pressure and/or flow of gas output by the orifice 55 and a second control valve for regulating the pressure and/or flow of gas output by the vent 54.
As shown in fig. 3, the axial air bearing includes a shaft hole through which the rotating shaft is allowed to pass and a plurality of rows of orifices 55 arranged in the circumferential direction of the shaft hole, each row of orifices including a plurality of orifices 55 arranged in the radial direction of the shaft hole.
The second foil 52 includes a plurality of fan-shaped foils arranged along the circumferential direction of the shaft hole. Two adjacent fan-shaped foils are arranged at intervals, and a row of throttling holes 55 are arranged between the two adjacent fan-shaped foils.
The first foil 51 is provided with a plurality of protrusions arranged in the circumferential direction of the shaft hole, the protrusions being in the form of strips extending in the radial direction of the shaft hole, and the throttle holes 55 are provided on the protrusions. A fan-shaped foil is arranged between every two adjacent bulges.
Axial air suspension bearings 5 are arranged on two sides of the thrust disc 3. Two axial air suspension bearings 5 are respectively positioned at two sides of the thrust disc 3 and can bear loads in the front direction and the rear direction, the rigidity of the bearings is adjustable, so that the rotating shaft 2 is more suitable for the working condition of variable axial loads, and the axial stability of a motor shaft is ensured.
Two axial air suspension bearings 5 are respectively positioned on two sides of the thrust disk 3 and respectively fixed on the two bearing parts 4. The two carrier parts 4 are of substantially the same construction but with different mounting directions, and the two carrier parts 4 are provided with gas distribution chambers 41 and ducts 42. The hole passages 42 correspond to air holes (including the vent holes 54 and the throttle holes 55) on the bearing one by one, so that external high-pressure air can be introduced into the axial air suspension bearing 5 through the air holes.
As shown in fig. 3 to 5, the first foil 51 is opened with a plurality of air holes, and external air can enter the cavity between the second foil 52 and the third foil 53 through the air holes of the first foil 51. The pores of the first foil 51 are arranged in a local pattern according to the number of the second foils 52 and are uniformly distributed in the circumferential direction.
As shown in figures 3 and 4, the axial air suspension bearing 5 comprises 4-8 groups of fan-shaped foils which are uniformly distributed in the circumferential direction. The bearing is provided with two air hole structures of a vent hole 54 and a throttle hole 55, the vent hole 54 is mainly used for adjusting the rigidity of the bearing, the vent hole 54 only passes through the first foil 51 and the third foil 53, and the vent hole does not penetrate through the second foil 52. Therefore, the gas output from the vent hole 54 cannot enter the gap between the bearing and the thrust disk 3 through the second foil 52.
The vent holes are located on the concave structure between the two protrusions of the third foil 53 and are arranged on the concave structure in order, and may be arranged at equal intervals or at unequal intervals as required. The throttling hole 55 mainly leads external high-pressure gas into the space between the bearing and the thrust disc 3 to increase the bearing supporting force, so that the bearing realizes high bearing capacity at low speed, the reliability of the bearing is improved, and the gas injection holes penetrate through all foil structures.
The source of the air from the vent 54 and the orifice 55 is usually the high pressure side air of the air conditioning unit itself, which is fed to the compressor and the bearing through the control valve 9, so that the rigidity of the bearing can be adjusted and the static pressure function can be realized only when the air conditioning unit has a pressure difference. When the unit is just started, the system does not establish differential pressure, so that the rigidity of the bearing is not adjustable in the starting process, and the static pressure function cannot be realized. Therefore, a booster pump structure can be added outside, and when the unit is just started and differential pressure is not established, the booster pump is used for pressurizing gas, so that the functions of adjusting the performance of the bearing and increasing static pressure are realized when the compressor is started.
The vent hole for adjusting the bearing rigidity and the orifice for realizing the static pressure function may use a unified air supply source or separate air supply sources.
According to another aspect of the present invention, the present embodiment further provides an air conditioner, which includes the above-mentioned compressor.
The above description is only exemplary embodiments of the present invention, and should not be construed as limiting the present invention, and any modifications, equivalent replacements, improvements, etc. made within the spirit and principle of the present invention should be included in the protection scope of the present invention.
Claims (13)
1. An axial air bearing comprising:
a first foil (51);
a second foil (52) spaced from the first foil (51);
a third foil (53) having an undulated shape and being arranged between the first foil (51) and the second foil (52);
at least one vent (54) in communication with the cavity between the third foil (53) and the second foil (52); and
at least one orifice (55) extending in the thickness direction of the axial aerostatic bearing for conveying gas between the second foil (52) and a rotating part carried by the axial aerostatic bearing.
2. The axial air suspension bearing according to claim 1, comprising a shaft hole for allowing a rotating shaft (2) to pass through and a plurality of rows of orifices (55) arranged in a circumferential direction of the shaft hole, each row of orifices comprising a plurality of orifices (55) arranged in a radial direction of the shaft hole.
3. The axial air suspension bearing of claim 2, wherein the second foil (52) comprises a plurality of fan-shaped foils arranged along a circumference of the shaft bore.
4. The axial air suspension bearing according to claim 3, characterized in that at least one row of said orifices (55) is provided between two adjacent fan foils.
5. The axial air suspension bearing according to claim 3, wherein the first foil (51) is provided with a plurality of protrusions arranged in a circumferential direction of a shaft hole, the protrusions having a bar shape extending in a radial direction of the shaft hole, and the orifice (55) is provided on the protrusions.
6. The axial air suspension bearing of claim 5, wherein the fan-shaped foils are located between two adjacent protrusions.
7. Axial aerostatic bearing according to claim 1, characterized in that the wave troughs (53a) of the third foil (53) abut the first foil (51) and the wave crests (53b) of the third foil (53) abut the second foil (52).
8. Axial aerostatic bearing according to claim 7, characterized in that the vent holes (54) are provided on the wave troughs (53a) of the third foil (53).
9. A compressor, comprising:
a housing (1);
a rotating shaft (2) arranged in the shell (1);
the thrust disc (3) is connected with the rotating shaft; and
the axial air suspension bearing of any one of claims 1 to 8, arranged opposite the thrust disk (3).
10. The compressor of claim 9, further comprising:
a first gas source in communication with both the vent hole (54) and the orifice (55); or
A first gas source and a second gas source, one in communication with the vent (54) and the other in communication with the orifice (55).
11. The compressor of claim 10, wherein at least one of the first and second gas sources is an air pump.
12. Compressor according to claim 9, characterized in that it further comprises a control valve (9),
the control valve (9) is used for controlling the pressure and/or flow of the gas output by the vent hole (54) and the throttling hole (55); or
The control valve (9) includes a first control valve for controlling the pressure and/or flow rate of the gas outputted from the vent hole (54) and a second control valve for controlling the pressure and/or flow rate of the gas outputted from the orifice (55).
13. An air conditioner characterized by comprising the compressor of any one of claims 9 to 12.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202020041861.5U CN211398020U (en) | 2020-01-09 | 2020-01-09 | Axial air suspension bearing, compressor and air conditioner |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202020041861.5U CN211398020U (en) | 2020-01-09 | 2020-01-09 | Axial air suspension bearing, compressor and air conditioner |
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| Publication Number | Publication Date |
|---|---|
| CN211398020U true CN211398020U (en) | 2020-09-01 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN202020041861.5U Active CN211398020U (en) | 2020-01-09 | 2020-01-09 | Axial air suspension bearing, compressor and air conditioner |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113007211A (en) * | 2021-02-07 | 2021-06-22 | 北京伯肯当代氢燃料电池实验室有限公司 | High-heat-dissipation-rate foil type axial thrust bearing, combined bearing and heat management method |
-
2020
- 2020-01-09 CN CN202020041861.5U patent/CN211398020U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113007211A (en) * | 2021-02-07 | 2021-06-22 | 北京伯肯当代氢燃料电池实验室有限公司 | High-heat-dissipation-rate foil type axial thrust bearing, combined bearing and heat management method |
| CN113007211B (en) * | 2021-02-07 | 2021-11-26 | 北京伯肯当代氢燃料电池实验室有限公司 | High-heat-dissipation-rate foil type axial thrust bearing, combined bearing and heat management method |
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