CN213298580U - Bidirectional elastic foil gas dynamic pressure thrust bearing - Google Patents
Bidirectional elastic foil gas dynamic pressure thrust bearing Download PDFInfo
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- CN213298580U CN213298580U CN202022301634.4U CN202022301634U CN213298580U CN 213298580 U CN213298580 U CN 213298580U CN 202022301634 U CN202022301634 U CN 202022301634U CN 213298580 U CN213298580 U CN 213298580U
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Abstract
The utility model discloses a bidirectional elastic foil gas dynamic pressure thrust bearing; belonging to the field of electric air compressors of new energy automobiles; the technical key points are as follows: the method comprises the following steps: the first top foil, the second fixed-distance top foil and the thrust disc; the first top foil and the second fixed-distance top foil are respectively arranged on two sides of the thrust disc; a second distance top foil provided with a raised elastic member on a side thereof facing the first top foil; the elastic pieces are uniformly arranged on the surface of the second distance top foil; in the initial state the resilient member of the second distance top foil is in a compressed state, i.e. the second distance top foil, the first top foil are in a compressed state in the initial state. The utility model aims at providing a two-way elasticity foil gas dynamic pressure footstep bearing improves footstep bearing's working property.
Description
Technical Field
The utility model relates to a new energy automobile electric air compressor machine field, more specifically say, especially relate to a gaseous dynamic pressure footstep bearing of two-way elasticity foil.
Background
F16C17/04 is a sliding contact bearing for axial loads only; F16C17/08 is an end face for supporting a shaft or other member, such as a thrust bearing.
Compared with the traditional rolling bearing or an oil-lubricated sliding bearing, the gas dynamic pressure thrust bearing has the advantages of small mass, difficult abrasion, long maintenance period, low operation cost, high working rotating speed, wide working temperature range and the like, and is a core part of an oil-free turbomachine; is a core component of the electric air compressor of the new energy automobile. Therefore, it has been the focus of research and development.
Relevant studies are as follows:
linshaoning, et al, research on the dynamic pressure gas thrust bearing of new elastic foil, J, proceedings of the university of Western Ann traffic, 2005(07):45-49.
The study on the theory of the novel elastic foil dynamic pressure gas thrust bearing [ J ] school of Sigan traffic university, 2006,040(009): 1032-.
Houanping, Lingfeng, Wangrui, et al, performances of gas dynamic thrust bearing and experiment [ J ] aeronautical dynamics report, 2018, 33(6): 1510-.
The above studies were made on theoretical calculations of the aerodynamic thrust bearing, and the above studies did not describe how the elastic foils are arranged.
As for the mounting arrangement of the elastic foil, there are two representative ways:
first, NTN corporation of japan proposed an elastic foil mounting method in CN108350933 a: the plurality of foils are arranged on the end surface of the foil retainer in parallel along the circumferential direction; that is, a plurality of bump foils are welded (electrical discharge machining) to the foil holder on the back.
Second, professor von kaki university at hunen, CN106763151A, proposed: the first layer of wave foil 3, the second layer of wave foil 4, the third layer of wave foil 5 and the top foil 6 are all formed by die punch; and then connected to each other through the respective outer rings to form a whole.
For the first mode, it is difficult to operate in actual operation because: the thickness of the foil is relatively thin (100-150 microns), when the foil is welded with a foil holder (actually a plate), only a spot welding mode can be adopted, and the welding firmness degree cannot be ensured. Particularly, when the rotor runs at a high speed, the thrust end plate can generate large aerodynamic pressure on the foil, the strength (attention is to the fatigue strength) of a welding point is difficult to guarantee, and the thrust bearing can be easily failed.
On the other hand, the shape of the bump foil cannot meet the design requirements during welding; for example, the height of the welding is low, and the welding height of the adjacent part is high (in the spot welding of 100-150 micrometers, the welding precision is difficult to keep consistent); that is, the actual shape of the bump foil does not conform to the designed shape, and the thrust bearing manufactured thereby does not achieve the intended effect.
For the second mode, the whole body is punched and formed, welding is not needed, and all parts can be connected into a whole; and, its shape can be secured. Therefore, it is a more excellent concept.
However, as shown in fig. 3, when the utility model team tries to form the integrated body (i.e. the second mode), it is found that: there is a new problem with this approach: the wave foil has a warping problem, that is, the end of the wave foil has a serious warping problem, so that the shape of the wave foil cannot meet the design requirement.
To the above problem, the utility model team has carried out the following research:
first, the molding sequence is changed. Firstly, designing an integrated die and forming at one time; the problem of warping cannot be eliminated. Secondly, the single-lobe sequential molding of the bump foil has no particular advantage, and the problem of warpage cannot be eliminated.
And secondly, heat treatment. The molded part is subjected to heat treatment, and warpage is restrained by the heat treatment. This proposal does partially improve the warpage, but cannot truly eliminate the warpage problem.
However, a design similar to CN106763151A cannot be practically applied if the warpage problem cannot be truly eliminated.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide a two-way elasticity foil gas dynamic pressure footstep bearing to above-mentioned prior art not enough.
The technical scheme of the utility model is that:
a bidirectional flex foil aerodynamic thrust bearing comprising: the first top foil, the second fixed-distance top foil and the thrust disc; the first top foil and the second fixed-distance top foil are respectively arranged on two sides of the thrust disc;
a second distance top foil provided with a raised elastic member on a side thereof facing the first top foil; the elastic pieces are uniformly arranged on the surface of the second distance top foil;
in the initial state the resilient member of the second distance top foil is in a compressed state, i.e. the second distance top foil, the first top foil are in a compressed state in the initial state.
Further, the elastic member is provided at an outer peripheral portion of the pitch roof foil.
Further, the elastic part and the distance adjusting top foil are integrally formed, and the elastic part is a raised lath and/or a spring.
Further, still include: the device comprises a first bearing seat, a second bearing seat, a first positioning pin, a second positioning pin, a first corrugated foil assembly, a second corrugated foil assembly, a first leveling plate and a second leveling plate;
one side of the thrust disc is sequentially as follows: the device comprises a first top foil, a first leveling plate, a first bump foil assembly and a first bearing seat;
the other side of the thrust disc is sequentially as follows: the second fixed-distance top foil, the second calibrating plate, the second corrugated foil assembly and the second bearing seat;
the first bearing seat is provided with a positioning hole, and the positioning pin is embedded into the positioning hole; the first bump foil assembly, the first leveling plate and the first top foil are provided with pin holes and are sequentially stacked on the first bearing seat.
A positioning hole is formed in the second bearing seat, and the positioning pin is embedded into the positioning hole; the second corrugated foil assembly, the second correcting plate and the second fixed-distance top foil are provided with pin holes and are sequentially stacked on the bearing seat;
the first bump foil of the first bump foil assembly closest to the first top foil is integrally formed in a punching mode;
the second wave foil of the second wave foil assembly closest to the second distance top foil is integrally formed in a punching mode;
the first leveling plate and the second leveling plate have the same structure;
a first leveling plate comprising: the leveling mechanism comprises a second plate and a plurality of leveling action pressure strip groups, wherein holes are formed in the second plate; the leveling action pressing strip group corresponds to a foil of the first bump foil; the leveling action pressure strip group is arranged in the second plate along the circumferential direction; a plurality of leveling action pressure strip groups are formed with middle hollow holes around the pressure strip groups so as to facilitate the passing of the rotating shaft;
the leveling action presser bar group of the second leveling plate corresponds to the foil of the second bump foil.
Further, the leveling action bar set includes: a plurality of leveling action pressing strips, wherein gaps are arranged between every two adjacent leveling action pressing strips; the leveling action pressing bar is in a corrugated shape or a straight strip shape; one side of the leveling action pressing strip facing the bump foil is in contact with the bump of the bump foil; and the direction of the leveling action pressing strip is consistent with the direction of the convex part of the bump foil.
Furthermore, leveling action pressing strips are arranged in a snake shape, namely, a leveling action pressing strip group comprises 1 continuous pressing strip; the 1 progression of the serpentine bead is perpendicular to the progression of the bump.
Furthermore, the leveling action batten group adopts a flat batten plate.
The beneficial effect of this application lies in:
1) the first utility model of this application lies in: the problem of the wavy foil warping when integrally molded was found. In order to solve the problems, two technical routes are proposed: the molding process is improved, and the problem of material warping is solved; however, the above-described technique cannot effectively improve warpage, so that: the integrally formed bump foil can only be formed on a drawing and cannot be practically applied to production. To this end, a third technical route has been proposed, which proposes the concept of "levelling plates", which limit the buckling of the wave foils by means of levelling plates with supporting stiffness.
2) The second utility model of this application lies in: a new technical problem was found: there may be tilting of the top foil (i.e. the top foil is not parallel to the thrust disc 5) and the thrust disc collides with the top foil after take-off rotation of the axis of rotation (10 tens of thousands of revolutions). In order to solve the problems, the top foil of the bidirectional thrust bearing is in an asymmetric design, an elastic part (such as a convex plate and a spring) is fixedly arranged on the top foil on one side, and the top foils on two sides are stressed, so that the top foil is ensured to be in a vertical state.
3) The utility model discloses a first utility model point, second utility model point of this application are interrelated, and its meaning lies in: the top foil of the bidirectional thrust bearing is designed asymmetrically, an elastic piece (such as a convex plate and a spring) is fixedly arranged on the top foil on one side, when the bidirectional thrust bearing is installed, the top foils on two sides are in a compressed state in advance, the top foil-bump foil-bearing seats on two sides are all under the same pressure, the top foil can be ensured to be in a vertical state (parallel to a thrust disc), and the leveling plate can be ensured to treat the bump foil warpage (the leveling plate can only play a role when being in contact with the bump foil).
4) The design of the application is not only suitable for a one-way thrust bearing, but also can be used for a two-way thrust bearing; whereas prior art CN106763151A is only applicable to one-way thrust bearings.
Drawings
The present invention will be described in further detail with reference to the following examples, which are not intended to limit the invention.
Fig. 1 is prior art: design schematic of a bump foil of CN 108350933A.
Fig. 2 is prior art: the overall structure of the thrust bearing of CN106763151A is shown schematically.
Fig. 3 is a schematic view of the entire structure of the thrust bearing of embodiment 1.
Fig. 4 is a schematic three-dimensional design of the bump foil 1 of example 1.
Fig. 5 is a schematic three-dimensional design of the leveling plate 2 of example 1.
Fig. 6 is a schematic three-dimensional design of the top foil 3 of example 1.
Fig. 7 is a schematic three-dimensional design of the leveling plate 2 of example 2.
Fig. 8 is a schematic three-dimensional design of the leveling plate 2 of example 3.
Fig. 9 is a schematic three-dimensional design of the leveling plate 2 of example 4.
FIG. 10 is a schematic view showing the overall structure of the thrust bearing of embodiment 5.
Figure 11 is a design diagram of the second distance top foil of example 5.
Detailed Description
In embodiment 1, a thrust bearing, which belongs to an elastic foil gas dynamic pressure thrust bearing, comprises a bearing seat, a positioning pin, a corrugated foil assembly, a leveling plate 2, a top foil 3 and a thrust disc 5;
wherein the wave foil assembly comprises at least 1 layer of wave foil 1;
a positioning hole is formed in a bearing seat (not shown in the figure) and is embedded into the bearing seat; the corrugated foil assembly, the leveling plate 2 and the top foil 3 are all provided with pin holes and are sequentially stacked on the bearing block;
the bump foil 1 of the bump foil assembly closest to the top foil 3 is integrally punched and formed;
the corrugated foil 1 adopts a specific structure formed by integral punching:
the bump foil 1 includes: a first plate 1-1, a plurality of foils 1-2; a circular hole is formed in the first plate 1-1; the plurality of foils 1-2 are arranged in parallel in the circumferential direction in the inner part of the first plate (i.e. the plurality of foils 1-2 are arranged in the inner circular hole of the first plate);
a plurality of foils 1-2 are formed with intermediate holes around them so that the rotation shaft passes through them;
each foil is connected with at least 1 adjacent foil through a first connecting sheet 1-3;
each foil 1-2 is connected with the first plate 1-1 through a second connecting sheet 1-4;
the first plate 1-1, the plurality of foils 1-2, the first connecting piece and the second connecting piece are integrally formed in a punching mode.
To address the problems mentioned in the background:
for the second mode, the whole body is punched and formed, welding is not needed, and all parts can be connected into a whole; and, its shape can be secured. Therefore, it is a more excellent concept.
However, as shown, when the utility model team attempts to form the integrated body (i.e. the second mode), it is found that: there is a new problem with this approach: the wave foil has a warping problem, that is, the end of the wave foil has a serious warping problem, so that the shape of the wave foil cannot meet the design requirement.
The present application addresses the above-mentioned problems and inventively proposes the concept of a "leveling plate".
The method is provided on the basis of failure of two technical routes of 'forming process' and 'heat treatment process', and the original technical prejudice is abandoned.
It should be noted that the leveling plate is different from the top foil and has a thickness of at least 0.25mm or more (up to 0.25mm or more, maintaining rigidity) regardless of the material used, and preferably, 0.35mm, 0.36mm, 0.37mm, 0.38mm, 0.39mm, 0.40mm, 0.41mm, 0.42mm, 0.43mm, 0.44mm, 0.45mm, 0.46mm, 0.47mm, 0.48mm, 0.49mm, 0.5mm, 0.51mm, 0.52mm, 0.53mm, 0.54mm, 0.55mm, 0.56mm, 0.57mm, 0.58mm, 0.59mm, 0.60mm, 0.61mm, 0.62mm, 0.63mm, 0.64mm, 0.65mm, 0.66mm, 0.67mm, 0.68mm, 0.69mm, 0.70mm, 0.61mm, 0.62mm, 0.63mm, 0.64mm, 0.65mm, 0.66mm, 0.73mm, or less preferably, 0.73mm, although the thickness thereof is not limited to the above
Leveling plate 2, comprising: the leveling device comprises a second plate 2-1 and a plurality of leveling action pressure strip groups, wherein a circular hole is formed in the second plate 2-1; the leveling action pressing strip group corresponds to the foils 1-2 of the bump foil 1 (the number and the position correspond to each other);
the leveling action bead groups are circumferentially arranged inside the second plate (i.e. a plurality of leveling action bead groups are arranged in the inner circular hole of the second plate);
leveling action bead set includes: the leveling action pressing strips 2-2 are arranged, and gaps are arranged between the adjacent leveling action pressing strips 2-2.
A plurality of leveling action pressure strip groups are formed with middle hollow holes around the pressure strip groups so as to facilitate the passing of the rotating shaft;
a plurality of wavy bulges are arranged on the foil pieces 1-2 of the bump foil 1;
the number of leveling action battens 2-2 of the leveling plate 2 is the same as that of all the wavy bulges of the bump foil 1; and the direction of the leveling action batten 2-2 is consistent with the direction of the convex direction of the bump foil 1.
In particular, as shown in FIG. 5, leveling action beads 2-2 are of a bellows-like design.
In particular, the pin holes are provided in the first plate and the second plate.
Example 2: as shown in fig. 7, the leveling action bead set of the leveling plate 2 is replaced with a flat bead plate (i.e., the gap of the leveling action bead in embodiment 1 is removed).
Example 3: as shown in fig. 8, the corrugated leveling action bead 2-2 of the leveling plate 2 is replaced with a flat leveling action bead 2-2.
Example 4: as shown in fig. 9, the corrugated leveling action bead 2-2 of the leveling plate 2 is replaced by a serpentine bead, and 1 of the serpentine beads runs perpendicular to the convex run of the bump foil 1.
Example 5: the design of embodiment 1 can be used for both one-way and two-way thrust bearings. Example 1 still presents 1 technical problem:
for CN106763151A, the bump foil was welded to the top foil. Whereas several of the components of example 1 are not welded but merely put together.
With the solution of embodiment 1, a new technical problem is found: there may be tilting of the top foil (i.e. the top foil is not parallel to the thrust disc 5) and the thrust disc collides with the top foil after take-off rotation of the axis of rotation (10 tens of thousands of revolutions).
In order to solve the above problems, embodiment 5 proposes the following design:
the thrust bearing belongs to an elastic foil gas dynamic pressure thrust bearing and is a bidirectional thrust bearing; the device comprises a first bearing seat, a second bearing seat, a first positioning pin, a second positioning pin, a first corrugated foil assembly, a second corrugated foil assembly, a first leveling plate, a second leveling plate, a first top foil, a second fixed-distance top foil and a thrust disc 5;
one side of the thrust disc 5 is in turn: the device comprises a first top foil 3, a first leveling plate 2, a first bump foil assembly and a first bearing seat;
the other side of the thrust disc 5 is sequentially: a second fixed-distance top foil 4, a second calibrating plate 6, a second corrugated foil component and a second bearing seat;
a positioning hole is formed in the first bearing seat (not shown) and the positioning pin is embedded therein; the first bump foil assembly, the first leveling plate 2 and the first top foil 3 are all provided with pin holes and are sequentially stacked on the first bearing seat.
A positioning hole is formed in the second bearing seat (not shown) and the positioning pin is embedded therein; the second corrugated foil assembly, the second correcting plate 6 and the second fixed-distance top foil 4 are provided with pin holes and are sequentially stacked on the bearing seat;
the first bump foil 1 of the first bump foil component closest to the first top foil 3 is integrally formed in a punching mode;
the second bump foil 7 (which is the same design as the first bump foil 1) of the second bump foil assembly closest to the second distance top foil 4 is integrally punched and formed;
the corrugated foil 1 adopts a specific structure formed by integral punching:
the bump foil 1 includes: a first plate 1-1, a plurality of foils 1-2; a circular hole is formed in the first plate 1-1; the plurality of foils 1-2 are arranged in parallel in the circumferential direction in the inner part of the first plate (i.e. the plurality of foils 1-2 are arranged in the inner circular hole of the first plate);
a plurality of foils 1-2 are formed with intermediate holes around them so that the rotation shaft passes through them;
each foil is connected with at least 1 adjacent foil through a first connecting sheet 1-3;
each foil 1-2 is connected with the first plate 1-1 through a second connecting sheet 1-4;
the first plate 1-1, the plurality of foils 1-2, the first connecting piece and the second connecting piece are integrally formed in a punching mode.
The first leveling plate and the second leveling plate are designed according to any one of embodiments 1 to 4.
A second distance top foil 4 provided with a raised elastic member 4-1 on its side facing the first top foil; the elastic members 4-1 are evenly arranged on the surface of the second distance top foil.
In the initial state the resilient member 4-1 of the second distance top foil 4 is in a compressed state, i.e. the second distance top foil 4, the first top foil, is in a compressed state in the initial state, thereby ensuring that: the second distance top foil 4 and the first top foil are in a vertical state.
The above embodiment is the preferred embodiment of the present invention, which is only used to facilitate the explanation of the present invention, it is not right to the present invention, which makes the restriction on any form, and any person who knows commonly in the technical field can use the present invention to make the equivalent embodiment of local change or modification without departing from the technical features of the present invention.
Claims (7)
1. A bidirectional elastic foil aerodynamic thrust bearing comprising: the first top foil, the second fixed-distance top foil and the thrust disc; the first top foil and the second fixed-distance top foil are respectively arranged on two sides of the thrust disc;
a second distance top foil provided with a raised elastic member on a side thereof facing the first top foil; the elastic pieces are uniformly arranged on the surface of the second distance top foil;
in the initial state the resilient member of the second distance top foil is in a compressed state, i.e. the second distance top foil, the first top foil are in a compressed state in the initial state.
2. The bidirectional elastic foil aerodynamic thrust bearing of claim 1, wherein said elastic member is provided on an outer peripheral portion of the adjustable top foil.
3. A bidirectional resilient foil aerodynamic thrust bearing as claimed in claim 1 wherein said resilient member is integrally formed with the spacer foil, said resilient member being a raised strip and/or a spring.
4. The bidirectional flex foil aerodynamic thrust bearing of claim 1 further comprising: the device comprises a first bearing seat, a second bearing seat, a first positioning pin, a second positioning pin, a first corrugated foil assembly, a second corrugated foil assembly, a first leveling plate and a second leveling plate;
one side of the thrust disc is sequentially as follows: the device comprises a first top foil, a first leveling plate, a first bump foil assembly and a first bearing seat;
the other side of the thrust disc is sequentially as follows: the second fixed-distance top foil, the second calibrating plate, the second corrugated foil assembly and the second bearing seat;
the first bearing seat is provided with a positioning hole, and the positioning pin is embedded into the positioning hole; the first bump foil assembly, the first leveling plate and the first top foil are provided with pin holes and are sequentially stacked on the first bearing block;
a positioning hole is formed in the second bearing seat, and the positioning pin is embedded into the positioning hole; the second corrugated foil assembly, the second correcting plate and the second fixed-distance top foil are provided with pin holes and are sequentially stacked on the bearing seat;
the first bump foil of the first bump foil assembly closest to the first top foil is integrally formed in a punching mode;
the second wave foil of the second wave foil assembly closest to the second distance top foil is integrally formed in a punching mode;
the first leveling plate and the second leveling plate have the same structure;
a first leveling plate comprising: the leveling mechanism comprises a second plate and a plurality of leveling action pressure strip groups, wherein holes are formed in the second plate; the leveling action pressing strip group corresponds to a foil of the first bump foil; the leveling action pressure strip group is arranged in the second plate along the circumferential direction; a plurality of leveling action pressure strip groups are formed with middle hollow holes around the pressure strip groups so as to facilitate the passing of the rotating shaft;
the leveling action presser bar group of the second leveling plate corresponds to the foil of the second bump foil.
5. The bidirectional flex foil aerodynamic thrust bearing of claim 4 wherein said leveling action bar set comprises: a plurality of leveling action pressing strips, wherein gaps are arranged between every two adjacent leveling action pressing strips; the leveling action pressing bar is in a corrugated shape or a straight strip shape; one side of the leveling action pressing strip facing the bump foil is in contact with the bump of the bump foil; and the direction of the leveling action pressing strip is consistent with the direction of the convex part of the bump foil.
6. The bidirectional flex foil aerodynamic thrust bearing of claim 4, wherein the leveling lands are arranged in a serpentine pattern, i.e., the leveling land set is 1 continuous land; the 1 progression of the serpentine bead is perpendicular to the progression of the bump.
7. The bidirectional flex foil aerodynamic thrust bearing of claim 4, wherein the leveling action bead set comprises a flat bead plate.
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| CN202022301634.4U CN213298580U (en) | 2020-10-15 | 2020-10-15 | Bidirectional elastic foil gas dynamic pressure thrust bearing |
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| CN202022301634.4U CN213298580U (en) | 2020-10-15 | 2020-10-15 | Bidirectional elastic foil gas dynamic pressure thrust bearing |
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| CN213298580U true CN213298580U (en) | 2021-05-28 |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113482965A (en) * | 2021-07-07 | 2021-10-08 | 鑫磊压缩机股份有限公司 | Air suspension axial bearing and hydrogen energy compressor |
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2020
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Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113482965A (en) * | 2021-07-07 | 2021-10-08 | 鑫磊压缩机股份有限公司 | Air suspension axial bearing and hydrogen energy compressor |
| WO2023279586A1 (en) * | 2021-07-07 | 2023-01-12 | 鑫磊压缩机股份有限公司 | Air suspension axial bearing and hydrogen energy compressor |
| CN113482965B (en) * | 2021-07-07 | 2024-05-03 | 鑫磊压缩机股份有限公司 | Air suspension axial bearing and hydrogen energy compressor |
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