CN108050152A - Spiral groove type dynamic pressure air thrust foil bearing - Google Patents

Spiral groove type dynamic pressure air thrust foil bearing Download PDF

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Publication number
CN108050152A
CN108050152A CN201711284030.XA CN201711284030A CN108050152A CN 108050152 A CN108050152 A CN 108050152A CN 201711284030 A CN201711284030 A CN 201711284030A CN 108050152 A CN108050152 A CN 108050152A
Authority
CN
China
Prior art keywords
bearing
paillon
flat paillon
flat
helicla flute
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.)
Pending
Application number
CN201711284030.XA
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Chinese (zh)
Inventor
徐方程
侯留凯
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.)
Dalian University of Technology
Original Assignee
Dalian University of Technology
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 Dalian University of Technology filed Critical Dalian University of Technology
Priority to CN201711284030.XA priority Critical patent/CN108050152A/en
Publication of CN108050152A publication Critical patent/CN108050152A/en
Pending legal-status Critical Current

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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C17/00Sliding-contact bearings for exclusively rotary movement
    • F16C17/04Sliding-contact bearings for exclusively rotary movement for axial load only
    • F16C17/08Sliding-contact bearings for exclusively rotary movement for axial load only for supporting the end face of a shaft or other member, e.g. footstep bearings
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C33/00Parts of bearings; Special methods for making bearings or parts thereof
    • F16C33/02Parts of sliding-contact bearings

Abstract

The invention belongs to air bearing fields, and in particular to a kind of spiral groove type dynamic pressure air thrust foil bearing.The bearing bearing block, bearing bottom plate, corrugated foil, flat paillon, flat paillon and screw with helicla flute;Bearing bottom plate, corrugated foil, flat paillon, the flat paillon with helicla flute welded together is fixed by screws on bearing block.Air enters from the edge of the flat paillon with helicla flute, after groove, a gases at high pressure area is formed among this special flat paillon, make this dynamic pressure air thrust foil bearing that there is higher bearing capacity, the stability of thrust bearing can be improved simultaneously, improve the overall performance of the kinetic pressure gas thrust bearing.The present invention uses air as lubricant, and air plays the role of lubrication and heat dissipation, compared to traditional oil lubrication thrust bearing, fueller is not required, mitigates the quality of thrust bearing, reliability higher, simultaneously because helicla flute is provided on flat paillon, therefore with higher bearing capacity.

Description

Spiral groove type dynamic pressure air thrust foil bearing
Technical field
The invention belongs to air bearing technology fields, and in particular to a kind of spiral groove type dynamic pressure air thrust foil bearing.
Background technology
Bearing is an extremely important part in modern machinery and equipment, and application field is very extensive, from small-sized household electricity Device has the presence of bearing to ship, aerospace.Component of the bearing as a core, but limits other technologies always Development.Gas dynamic pressure foil bearing is compared with other bearings have working speed height, friction energy loss is small, service life is long and work The features such as ambient temperature range is wide, but since working media is gas, since the compressibility of gas limits bearing capacity, Therefore the class bearing is only used on the high speed light loading rotating machinery of aerospace field at present, especially thrust foil bearing The weakness of low bearing capacity limits the further genralrlization application of the class bearing.Therefore, gas dynamic pressure thrust foil bearing is improved Bearing capacity is for improving the overall performance of bearing and being necessary in the further application of industrial circle.
The content of the invention
The present invention provides one kind to improve the bearing capacity and stability of existing dynamic pressure air thrust foil bearing Dynamic pressure air thrust foil bearing with helicla flute paillon, can be big with higher bearing capacity and better stability The earth improves the overall performance of thrust foil bearing.
Technical scheme:
A kind of spiral groove type dynamic pressure air thrust foil bearing, including bearing block 1, bearing bottom plate 2, corrugated foil 3, flat paper tinsel Piece 4, the flat paillon 5 with helicla flute and screw 6;
It is thin that bearing bottom plate 2, flat paillon 4 and the flat paillon 5 with helicla flute is that round-meshed circle is opened in centre Piece, the Circularhole diameter of three are identical with the Circularhole diameter of bearing block 1;Connecting hole is provided on the bearing block 1, passes through fixed spiral shell Nail 6 is fixedly connected with bearing bottom plate 2;The flat paillon 4 is identical with the thin rounded flakes diameter of the flat paillon 5 with helicla flute, Less than the diameter of bearing bottom plate 2;The corrugated foil 3 is made of the ripply claw type paillon of multi-group and paillon circle, is carried The claw type paillon of ripple is fixed on cambered paillon circle, multiple cambered paillon corrals into annulus, the diameter of annulus with The Circularhole diameter of bearing block 1 is identical;The outside dimension of the corrugated foil 3 is identical with the diameter of flat paillon 4;Described carries spiral shell The flat paillon 5 of spin slot is provided with multiple helicla flutes on surface;
The corrugated foil 3 is welded on bearing bottom plate 2;The flat paillon 4 is welded on corrugated foil 3;It is described The flat paillon 5 with helicla flute align and weld together with flat 4 corner of paillon, form double-deck flat paillon;Bearing bottom plate 2, ripple Line paillon 3, flat paillon 4 and the flat paillon 5 with helicla flute are fixed on by screw 6 on bearing block 1.
Beneficial effects of the present invention:
1) present invention combines corrugated foil, flat paillon, the flat paillon with helicla flute, collectively constitutes the axial direction of thrust bearing Support construction, air enters from the edge of the flat paillon with helicla flute, after groove, among this special flat paillon A gases at high pressure area is formed, makes this dynamic pressure air thrust foil bearing that there is higher bearing capacity, while thrust can be improved Antiwhip improves the overall performance of the kinetic pressure gas thrust bearing.
2) present invention is different from traditional oil lubrication thrust bearing, is to use air as lubricant, air plays lubrication With the effect of heat dissipation.Compared to traditional oil lubrication thrust bearing, fueller is not required, mitigates the quality of thrust bearing, it can By property higher, simultaneously because helicla flute is provided on flat paillon, therefore than traditional air hydrodynamic thrust paper tinsel without helicla flute Piece bearing has higher bearing capacity.
Description of the drawings
Fig. 1 is the installation diagram of the present invention.
Fig. 2 is the design sketch after present invention assembling.
Fig. 3 is the structure diagram of corrugated foil of the present invention.
Fig. 4 is the structure diagram of the flat paillon of the present invention.
Fig. 5 is the structure diagram of flat paillon of the present invention with helicla flute.
In figure:1 bearing block;2 bearing bottom plates;3 corrugated foils;4 flat paillons;
5 carry the flat paillon of helicla flute;6 screws.
Specific embodiment
Below in conjunction with attached drawing and technical solution, the specific embodiment further illustrated the present invention.
Such as Fig. 1, a kind of spiral groove type dynamic pressure air thrust foil bearing, including bearing block 1, bearing bottom plate 2, corrugated foil 3rd, flat paillon 4, the flat paillon 5 with helicla flute, screw 6;Six structures in figure, the structure as a whole of bottom bracket 1 One " frame ", corrugated foil 3, flat paillon 4, the flat paillon 5 with helicla flute are welded on successively according to order 1. 2. 3. 4. On bearing bottom plate 2, after be fixed on by screw 6 on bearing block 1, formed an assembly, as shown in Figure 2.
It is the structure diagram of the dynamic pressure air thrust foil bearing corrugated foil 3 such as Fig. 3.When the thrust foil bearing After being subject to axial thrust, corrugated foil 3 is axially deformed under the action of power, and the thrust bearing is made to have certain shock resistance Ability.It is the structure diagram of the flat paillon 4 of the dynamic pressure air thrust foil bearing such as Fig. 4, plane smoother, Ke Yiyong To form a lubrication air film.
It is the structure diagram of the flat paillon 4 with helicla flute of the dynamic pressure air thrust foil bearing such as Fig. 5.At this When thrust foil bearing works normally, rotor high-speed rotation, the arrow of extraneous air then as illustrated is from helicla flute The edge of flat paillon 5 generates vortex after entering, and then forms gases at high pressure area in the intermediate region of the paillon, makes this kinetic pressure gas Thrust foil bearing has more high bearing capacity in the axial direction, has better stability, can improve dynamic pressure air thrust The overall performance of foil bearing.

Claims (1)

1. a kind of spiral groove type dynamic pressure air thrust foil bearing, which is characterized in that including bearing block (1), bearing bottom plate (2), Corrugated foil (3), flat paillon (4), the flat paillon (5) with helicla flute and screw (6);
Bearing bottom plate (2), flat paillon (4) and the flat paillon (5) with helicla flute is that round-meshed circle is opened in centre Thin slice, the Circularhole diameter of three are identical with the Circularhole diameter of bearing block (1);Connecting hole is provided on the bearing block (1), is passed through Fixing screws (6) are fixedly connected with bearing bottom plate (2);The circle of the flat paillon (4) and the flat paillon (5) with helicla flute Wafer diameters are identical, less than the diameter of bearing bottom plate (2);The corrugated foil (3) is by the ripply claw type paillon of multi-group With paillon circle form, be fixed on ripply claw type paillon on cambered paillon circle, multiple cambered paillon corrals into Annulus, the diameter of annulus are identical with the Circularhole diameter of bearing block (1);The outside dimension of the corrugated foil (3) and flat paillon (4) Diameter it is identical;The flat paillon (5) with helicla flute is provided with multiple helicla flutes on surface;
The corrugated foil (3) is welded on bearing bottom plate (2);The flat paillon (4) is welded on corrugated foil (3); The flat paillon (5) with helicla flute aligns with flat paillon (4) corner to be welded together, and forms double-deck flat paillon;Bearing Bottom plate (2), corrugated foil (3), flat paillon (4) and the flat paillon (5) with helicla flute are fixed on bearing block by screw (6) (1) on.
CN201711284030.XA 2017-12-07 2017-12-07 Spiral groove type dynamic pressure air thrust foil bearing Pending CN108050152A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201711284030.XA CN108050152A (en) 2017-12-07 2017-12-07 Spiral groove type dynamic pressure air thrust foil bearing

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201711284030.XA CN108050152A (en) 2017-12-07 2017-12-07 Spiral groove type dynamic pressure air thrust foil bearing

Publications (1)

Publication Number Publication Date
CN108050152A true CN108050152A (en) 2018-05-18

Family

ID=62122906

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201711284030.XA Pending CN108050152A (en) 2017-12-07 2017-12-07 Spiral groove type dynamic pressure air thrust foil bearing

Country Status (1)

Country Link
CN (1) CN108050152A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
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
CN113894500A (en) * 2021-09-30 2022-01-07 西安交通大学 Manufacturing method of patch type thrust dynamic pressure gas bearing
CN114321156A (en) * 2021-12-31 2022-04-12 宙斯能源动力科技(大连)有限公司 Herringbone groove type air dynamic pressure thrust foil bearing
WO2022080807A1 (en) * 2020-10-15 2022-04-21 주식회사 티앤이코리아 Foil air bearing having herringbone pattern

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR20070108787A (en) * 2006-05-08 2007-11-13 한국기계연구원 Tilting foil bearing with the groove
CN101463868A (en) * 2009-01-14 2009-06-24 西安交通大学 Kinetic pressure gas thrust bearing with axial support
CN201373019Y (en) * 2009-01-14 2009-12-30 西安交通大学 Dynamical pressure gas thrust bearing supported in axial direction
CN202091349U (en) * 2011-06-15 2011-12-28 罗立峰 Dynamic pressure air thrust ceramic bearing
CN105202027A (en) * 2015-05-19 2015-12-30 罗立峰 Hybrid type dynamic pressure gas thrust bearing
CN206397931U (en) * 2017-01-22 2017-08-11 中国工程物理研究院机械制造工艺研究所 Dynamic pressure air thrust foil bearing

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR20070108787A (en) * 2006-05-08 2007-11-13 한국기계연구원 Tilting foil bearing with the groove
CN101463868A (en) * 2009-01-14 2009-06-24 西安交通大学 Kinetic pressure gas thrust bearing with axial support
CN201373019Y (en) * 2009-01-14 2009-12-30 西安交通大学 Dynamical pressure gas thrust bearing supported in axial direction
CN202091349U (en) * 2011-06-15 2011-12-28 罗立峰 Dynamic pressure air thrust ceramic bearing
CN105202027A (en) * 2015-05-19 2015-12-30 罗立峰 Hybrid type dynamic pressure gas thrust bearing
CN206397931U (en) * 2017-01-22 2017-08-11 中国工程物理研究院机械制造工艺研究所 Dynamic pressure air thrust foil bearing

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2022080807A1 (en) * 2020-10-15 2022-04-21 주식회사 티앤이코리아 Foil air bearing having herringbone pattern
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
CN113894500A (en) * 2021-09-30 2022-01-07 西安交通大学 Manufacturing method of patch type thrust dynamic pressure gas bearing
CN114321156A (en) * 2021-12-31 2022-04-12 宙斯能源动力科技(大连)有限公司 Herringbone groove type air dynamic pressure thrust foil bearing

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Application publication date: 20180518

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