CN201180738Y - Thrust bearing of turbosupercharger - Google Patents

Thrust bearing of turbosupercharger Download PDF

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Publication number
CN201180738Y
CN201180738Y CNU2008200527147U CN200820052714U CN201180738Y CN 201180738 Y CN201180738 Y CN 201180738Y CN U2008200527147 U CNU2008200527147 U CN U2008200527147U CN 200820052714 U CN200820052714 U CN 200820052714U CN 201180738 Y CN201180738 Y CN 201180738Y
Authority
CN
China
Prior art keywords
oil
bearing
tank deck
turbocharger
thrust bearing
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 - Fee Related
Application number
CNU2008200527147U
Other languages
Chinese (zh)
Inventor
廖云
曾国卫
胡辽平
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.)
Hunan Tianyan Machinery Co Ltd
Original Assignee
Hunan Tianyan Machinery 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 Hunan Tianyan Machinery Co Ltd filed Critical Hunan Tianyan Machinery Co Ltd
Priority to CNU2008200527147U priority Critical patent/CN201180738Y/en
Application granted granted Critical
Publication of CN201180738Y publication Critical patent/CN201180738Y/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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    • 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
    • F16C17/047Sliding-contact bearings for exclusively rotary movement for axial load only with fixed wedges to generate hydrodynamic pressure
    • 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
    • F16C33/04Brasses; Bushes; Linings
    • F16C33/06Sliding surface mainly made of metal
    • F16C33/10Construction relative to lubrication
    • F16C33/1025Construction relative to lubrication with liquid, e.g. oil, as lubricant
    • F16C33/106Details of distribution or circulation inside the bearings, e.g. details of the bearing surfaces to affect flow or pressure of the liquid
    • F16C33/1075Wedges, e.g. ramps or lobes, for generating pressure
    • 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
    • F16C2360/00Engines or pumps
    • F16C2360/23Gas turbine engines
    • F16C2360/24Turbochargers

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  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Oil, Petroleum & Natural Gas (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Supercharger (AREA)

Abstract

The utility model provides a thrust bearing of a turbocharger. A plurality of bearing bushes are uniformly distributed along the circumferences of the front and the back surfaces of the thrust bearing; each bearing bush includes an oil wedge surface, an oil baffling step, an oil storing surface and an oil retaining step; the oil wedge surface is arranged between the oil baffling step and the oil storing surface; the oil baffling step is a platform bulging outwards; the oil storing surface is recessed inwards; the oil retaining step is arranged on the outside of the oil wedge surface; one end of the oil retaining step is connected with the oil baffling step, and the other end thereof id connected with the oil baffling step of the adjacent bearing bush; the whole of the oil retaining steps and the oil baffling steps of the bearing bushes forms an annular convex platform higher than the oil storing surface outside the oil storing surface and the oil wedge surface. Therefore, the lubricating oil flowing through the oil wedge surface of one bearing bush of the thrust bearing of the turbocharger can be prevented from flowing into the next bearing bush of the thrust bearing of the turbocharger, the decompression of the lubricating oil outside the bearing bushes of the thrust bearing of the turbocharger can be prevented, and the bearing capacity of the thrust bearing of the turbocharger can be further improved.

Description

Thrust bearing of turbocharger
Technical field
The utility model relates to a kind of parts of engine turbine pressurized machine, particularly a kind of thrust bearing of turbocharger.
Background technique
Along with the more and more stricter propelling of vehicular discharge rules, make the supercharging technology widespread usage on vehicle.Turbosupercharger is that the turbine that the high-temp waste gas that utilizes motor to discharge blows pressurized machine runs up, run up thereby drive with the coaxial compressor impeller of turbine, the pressurized air that compressor impeller produces offers motor again, makes the air inlet of motor become pressure air by natural aspiration.Because the air quantity that provides increases, the motor more fuel that can burn makes burning also more simultaneously, and the turbosupercharger power of consumption of engine not, so turbosupercharger also is exhaust-gas turbocharger.After motor uses turbosupercharger, can improve the power per liter of motor greatly, reduce fuel consumption rate, improve the discharging of motor, turbosupercharger is the new high-tech product of energy-saving and environmental protection.Thrust bearing of turbocharger is a vitals of turbosupercharger, at present, the vehicle turbocharger thrust bearing adopts accompanying drawing 4 to the structure shown in the accompanying drawing 5 usually, (front is an accompanying drawing 4 on its two sides, front and back, the back is an accompanying drawing 5) be equipped with the polylith bearing liner that is uniformly distributed along the circumference, bearing liner comprises oil film wedge face 1, retaining tank deck rank 2 and store oil face 3; Oil film wedge face 1 is between retaining tank deck rank 2 and store oil face 3, and oil film wedge face 1 is provided with low side 11 and high-end 12, and low side 11 caves inward, and high-end 12 to outer lug, oil film wedge face 1 be from low side 11 to high-end 12 progressively to the inclined-plane of outer lug; Retaining tank deck rank 2 are the platform to outer lug, and it is high-end 12 identical to the height of outer process to the height of outer process and oil film wedge face 1; Store oil face 3 caves inward.The thrust bearing of turbocharger working principle of this structure is: thrust bearing is fixed on the turbo-charger bearing body by other parts of turbosupercharger, rely on self lubricating oil path and engine oil gallery to be connected as a single entity, the lubricant oil that flows into forms the pressure-bearing oil film between thrust bearing oil film wedge face and other core part of pressurized machine, the pressure-bearing oil film mainly bears the summation of turbocharger air compressor end and turbine end axial force, gap between control turbocharger air compressor and turbine wheel and the housing is to guarantee booster performance and reliable operation.Though the lubricated cooling performance of the thrust bearing of turbocharger of this structure is better, but raising along with HP, hp/litre, under the situation of exhaust brake and high supercharging pressure level, the axial force of turbine rotor also increases, require thrust bearing that higher bearing capacity is arranged, and can make the outside Zhou Liudong of lubricant oil between the retaining tank deck rank 2 of this thrust bearing of turbocharger bearing liner (shown in accompanying drawing 4 to 5), can not will lubricate oil catch in oil film wedge face 1 well, because lubricant oil can outwards flow, the pressure of the oil film on the oil film wedge face 1 can reduce like this, the bearing capacity of thrust bearing of turbocharger is descended, influence turbocharger performance and functional reliability.
Chinese patent CN2900796 discloses another thrust bearing of turbocharger, thrust bearing is made up of 8 bearing tiles that are uniformly distributed along the circumference, bearing tile is by the oil film wedge inclined-plane, bearing tile plane and oil groove are formed, though the oil film wedge inclined-plane is in the middle of oil groove and bearing tile plane. this thrust bearing of turbocharger has the bearing capacity of certain bearing, but it is can make the outside Zhou Liudong of lubricant oil on the oil film wedge inclined-plane and the oil groove outside equally, can not will lubricate oil catch in oil film wedge face and oil groove well, because lubricant oil can outwards flow, the pressure of the oil film on oil film wedge face and the oil groove can reduce like this, the bearing capacity of thrust bearing is descended, influence turbocharger performance and functional reliability.
Summary of the invention
The purpose of this utility model is to overcome the above-mentioned deficiency of prior art and a kind of thrust bearing of turbocharger is provided, it can prevent to flow into through the lubricant oil of the oil film wedge face of thrust bearing of turbocharger bearing liner the next bearing liner of thrust bearing of turbocharger, it can also prevent the pressure release of lubricant oil in the bearing liner outside of thrust bearing of turbocharger, further improves the bearing capacity of thrust bearing of turbocharger.
The technical solution of the utility model is: a kind of thrust bearing of turbocharger, and two sides is equipped with the polylith bearing liner that is uniformly distributed along the circumference before and after it, and bearing liner comprises oil film wedge face, retaining tank deck rank, store oil face and protects the tank deck rank; The oil film wedge face is between retaining tank deck rank and store oil face, and the oil film wedge face is provided with low side and high-end, and low side caves inward, and is high-end to outer lug, the oil film wedge face be from low side to high-end progressively to the inclined-plane of outer lug; Retaining tank deck rank are the platform to outer lug, and its height to outer process is identical with the high-end height to outer process of oil film wedge face; Store oil is towards sunken inside; Protect the outside that the tank deck rank are located at the oil film wedge face, an end that protects the tank deck rank joins with retaining tank deck rank, its the other end joins with the retaining tank deck rank of the bearing liner of vicinity, protect the tank deck rank and be platform to outer lug, its height to outer process is identical to the height of outer process with the retaining tank deck rank that its two ends are right after, and the tank deck rank of protecting of whole polylith bearing liner form the annular protrusion platform that is higher than store oil face with retaining tank deck rank at the store oil face and the oil film wedge face outside.
The further technological scheme of the utility model is: equal four of the bearing liner that the two sides, front and back of described thrust bearing of turbocharger is provided with.
The utility model further technological scheme is: the degree of depth that the store oil of described bearing liner caves inward towards the low side of the depth ratio oil film wedge face of sunken inside wants dark.
The utility model compared with prior art has following advantage:
1, other part of turbosupercharger need not to do any change, all can use with the utility model assembling.
2, the retaining tank deck rank that are provided with of bearing liner of the present utility model can prevent to flow into next bearing liner through the lubricant oil of the oil film wedge face of the bearing liner of thrust bearing of turbocharger, it can also prevent the pressure release of lubricant oil in the bearing liner outside of thrust bearing of turbocharger, the bearing capacity of the pressure-bearing oil film that forms on thrust bearing of turbocharger like this is enhanced, further improve the bearing capacity of thrust bearing of turbocharger, guaranteed the turbosupercharger reliability of operation.
Below in conjunction with the drawings and specific embodiments detailed structure of the present utility model is further described.
Description of drawings
Accompanying drawing 1 is a structural representation of the present utility model;
Accompanying drawing 2 is the rear view of accompanying drawing 1;
Accompanying drawing 3 is the cutaway view Amplified image along A-A semicircle loop wire of accompanying drawing 1;
Accompanying drawing 4 is the structural representation of the thrust bearing of turbocharger of prior art;
Accompanying drawing 5 is the rear view of accompanying drawing 4.
Embodiment
Embodiment
Shown in accompanying drawing 1 to 3: a kind of thrust bearing of turbocharger, two sides (front is an accompanying drawing 1, and the back is an accompanying drawing 2) is equipped with four bearing liners that are uniformly distributed along the circumference before and after it, and bearing liner comprises oil film wedge face 1, retaining tank deck rank 2, store oil face 3 and protects tank deck rank 4; Oil film wedge face 1 is between retaining tank deck rank 2 and store oil face 3, and oil film wedge face 1 is provided with low side 11 and high-end 12, and low side 11 caves inward, and high-end 12 to outer lug, oil film wedge face 1 be from low side 11 to high-end 12 progressively to the inclined-plane of outer lug; Retaining tank deck rank 2 are the platform to outer lug, and it is high-end 12 identical to the height of outer process to the height of outer process and oil film wedge face 1; Store oil face 3 caves inward, and it is darker than the degree of depth that the low side 11 of oil film wedge face 1 caves inward; Protect the outside that tank deck rank 4 are located at oil film wedge face 1, an end that protects tank deck rank 4 joins with retaining tank deck rank 2, its the other end joins with the retaining tank deck rank of the bearing liner of vicinity, protect tank deck rank 4 and be platform to outer lug, its height to outer process is identical to the height of outer process with the retaining tank deck rank 2 that its two ends are right after, and the tank deck rank 4 of protecting of whole four bearing liners form the annular protrusion platform that is higher than store oil face 3 with retaining tank deck rank 2 at the store oil face 3 and oil film wedge face 1 outside.
The utility model working principle: owing to produce dynamic pressure on the oil film wedge face 1, lubricating oil temperature behind the thrust bearing of turbocharger of flowing through is raise, the rising of oil temperature will make oil body descend, and then bearing capacity is reduced, and the store oil face 3 of the bearing liner of thrust bearing of turbocharger with oil film wedge face 1 outside design by protecting the annular protrusion platform that is higher than store oil face 1 that tank deck rank 4 and retaining tank deck rank 5 constitute, it can prevent to flow into through the lubricant oil of the oil film wedge face 1 of the bearing liner of thrust bearing of turbocharger the next bearing liner of thrust bearing of turbocharger, it can also prevent the pressure release of lubricant oil in the bearing liner outside of thrust bearing of turbocharger, further improves the bearing capacity of thrust bearing of turbocharger.
The utility model is not limited to above-mentioned concrete structure, so long as the thrust bearing of turbocharger that is provided with the annular protrusion platform that is higher than store oil face 3 outside with oil film wedge face 1 at the store oil face 3 of thrust bearing of turbocharger bearing liner just drops within the protection domain of the present utility model.

Claims (3)

1, a kind of thrust bearing of turbocharger, two sides is equipped with the polylith bearing liner that is uniformly distributed along the circumference before and after it, and bearing liner comprises oil film wedge face, retaining tank deck rank and store oil face; The oil film wedge face is between retaining tank deck rank and store oil face, and the oil film wedge face is provided with low side and high-end, and low side caves inward, and is high-end to outer lug, the oil film wedge face be from low side to high-end progressively to the inclined-plane of outer lug; Retaining tank deck rank are the platform to outer lug, and its height to outer process is identical with the high-end height to outer process of oil film wedge face; Store oil is towards sunken inside; It is characterized in that: bearing liner also comprises and protects the tank deck rank, protect the outside that the tank deck rank are located at the oil film wedge face, an end that protects the tank deck rank joins with retaining tank deck rank, its the other end joins with the retaining tank deck rank of the bearing liner of vicinity, protect the tank deck rank and be platform to outer lug, its height to outer process is identical to the height of outer process with the retaining tank deck rank that its two ends are right after, and the tank deck rank of protecting of whole polylith bearing liner form the annular protrusion platform that is higher than store oil face with retaining tank deck rank at the store oil face and the oil film wedge face outside.
2, thrust bearing of turbocharger according to claim 1 is characterized in that: equal four of the bearing liner that the two sides, front and back of described thrust bearing of turbocharger is provided with.
3, thrust bearing of turbocharger according to claim 1 and 2 is characterized in that: the degree of depth that the store oil of described bearing liner caves inward towards the low side of the depth ratio oil film wedge face of sunken inside wants dark.
CNU2008200527147U 2008-03-28 2008-03-28 Thrust bearing of turbosupercharger Expired - Fee Related CN201180738Y (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CNU2008200527147U CN201180738Y (en) 2008-03-28 2008-03-28 Thrust bearing of turbosupercharger

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CNU2008200527147U CN201180738Y (en) 2008-03-28 2008-03-28 Thrust bearing of turbosupercharger

Publications (1)

Publication Number Publication Date
CN201180738Y true CN201180738Y (en) 2009-01-14

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Application Number Title Priority Date Filing Date
CNU2008200527147U Expired - Fee Related CN201180738Y (en) 2008-03-28 2008-03-28 Thrust bearing of turbosupercharger

Country Status (1)

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104389905A (en) * 2014-11-04 2015-03-04 湖南崇德工业科技有限公司 Vertical sliding bearing thrust block

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104389905A (en) * 2014-11-04 2015-03-04 湖南崇德工业科技有限公司 Vertical sliding bearing thrust block

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Date Code Title Description
C14 Grant of patent or utility model
GR01 Patent grant
C17 Cessation of patent right
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20090114

Termination date: 20130328