CN204827541U - Full floating bearing turbo charger rotor system - Google Patents
Full floating bearing turbo charger rotor system Download PDFInfo
- Publication number
- CN204827541U CN204827541U CN201520502196.4U CN201520502196U CN204827541U CN 204827541 U CN204827541 U CN 204827541U CN 201520502196 U CN201520502196 U CN 201520502196U CN 204827541 U CN204827541 U CN 204827541U
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- CN
- China
- Prior art keywords
- floating bearing
- full floating
- turbine
- bearing
- booster
- 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
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Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C17/00—Sliding-contact bearings for exclusively rotary movement
- F16C17/12—Sliding-contact bearings for exclusively rotary movement characterised by features not related to the direction of the load
- F16C17/18—Sliding-contact bearings for exclusively rotary movement characterised by features not related to the direction of the load with floating brasses or brushing, rotatable at a reduced speed
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C17/00—Sliding-contact bearings for exclusively rotary movement
- F16C17/10—Sliding-contact bearings for exclusively rotary movement for both radial and axial load
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C2360/00—Engines or pumps
- F16C2360/23—Gas turbine engines
- F16C2360/24—Turbochargers
Abstract
The utility model provides a full floating bearing turbo charger rotor system, the full floating bearing of turbine end is installed in the full floating bearing mounting hole of turbine end on the bearing body, the first thrust terminal surface of the full floating bearing of turbine end and the end end face contaction of the full floating bearing mounting hole of turbine end, the full floating bearing of the end of calming the anger is installed in the full floating bearing mounting hole of end of calming the anger on the bearing body, the second thrust terminal surface of the full floating bearing of end and the end end face contaction of the full floating bearing mounting hole of end of calming the anger calm the anger, the turbine rotor axle is installed at the dead eye of the full floating bearing of turbine end and is calmed the anger in the dead eye of the full floating bearing of end, the other end at turbine rotor axle axostylus axostyle is installed in proper order to end seal cover and the impeller of calming the anger, and fix on the axostylus axostyle of turbine rotor axle through the nut, the ring packing inslot on turbine rotor axle axostylus axostyle is installed to the sealing ring, turbine end to the bearing body seals up. Axostylus axostyle and the first axostylus axostyle hole and the downthehole wall of second axostylus axostyle of turbine rotor axle form first oil extraction chamber A and second oil extraction chamber B respectively.
Description
Technical field
The utility model relates to turbosupercharger of car engine rotor-support-foundation system, particularly a kind of turbocharger rotor system adopting full floating bearing structure.
Background technique
Turbosupercharging is a kind of technology residual amount of energy in engine exhaust being converted into raising effective engine power, this technology not only can significantly improve the power character of motor, reduce the fuel oil consumption of motor, also effectively can reduce the harmful components in motor discharging waste gas, there is effect that is efficient, energy-saving and environmental protection.This technology is also the important means that plateau section engine power is recovered simultaneously, makes the service condition of starting functional adaptation different altitude height.So technology for Turbocharger Manufacturing has become the development trend of motor.
Rotor-support-foundation system is one of important composition parts of turbosupercharger, is respectively equipped with thrust bearing and floating bearing under normal circumstances in rotor-support-foundation system.Along with Modern Engine reinforcing degree constantly strengthens and light-weight design, special various countries require more and more stricter to environmental legislation, promote constantly advancing of technology for Turbocharger Manufacturing, novel automobile turbosupercharger by towards increasing pressure ratio, the aspect development of increase work efficiency, widen range of flow, constantly miniaturization, turbocharger arrangement is further compact, its working speed improves constantly, operating mode is further severe and lubricating condition is more severe, and this design to rotor-support-foundation system, manufacture and processing are had higher requirement.
Existing turbocharger rotor system architecture as shown in Figure 1, comprises impeller 1, stuffing box gland 2, thrust housing 3, thrust bearing 4, bearing support 5, seal ring 6, turbine rotor shaft 7, opening floating bearing back-up ring 8 and the first floating bearing 9 and the second floating bearing 10.
Bearing support 5 is provided with oil inlet hole 5-3 and spill port 5-7, the bottom of oil inlet hole 5-3 is provided with horizontal oilhole 5-4, the two ends of horizontal oilhole 5-4 are respectively equipped with oilhole 5-5,5-6, oilhole 5-5,5-6 communicate with bearing hole 5-1 and 5-2 in bearing support 5 respectively, for the first floating bearing 9 and the second floating bearing 10 provide lubricant oil.
The center of the first floating bearing 9 is provided with shaft lever hole 9-1, and the outer garden of the first floating bearing 9 is provided with annular oil groove 9-2, is provided with four equally distributed oilhole 9-3 in annular oil groove 9-2.Second floating bearing 10 is identical with the structure of the first floating bearing 9.
First floating bearing 9 and the second floating bearing 10 are arranged on respectively by opening floating bearing back-up ring 8 in bearing hole 5-1 and 5-2 in bearing support 5, and opening floating bearing back-up ring 8 is arranged in the annular retaining ring groove on bearing hole 5-1 and 5-2 hole wall respectively.
The axostylus axostyle of turbine rotor shaft 7 is arranged in the shaft lever hole of the first floating bearing 9 and the second floating bearing 10, thrust housing 3, stuffing box gland 2, impeller 1 are arranged on the other end of turbine rotor shaft 7 axostylus axostyle successively, and being fixed on the axostylus axostyle of turbine rotor shaft 7 by nut, thrust bearing 4 is arranged on thrust housing 3.Seal ring 6 is arranged in the annular seal groove on turbine rotor shaft 7 axostylus axostyle, seals the turbine end of bearing support 5.
The Main Function of existing turbocharger rotor System Halt thrust bearing 4 is balance supercharger rotor system alternate loads that turbine end and air end of booster produce in rotary course, first floating bearing 9 and the second floating bearing 10 Main Function rely on its internal surface and outer surface to form oil film to do high speed rotary motion to support turbocharger rotor assembly, and effectively cushion the vibration and reduction fretting wear that produce in turbosupercharger rotary course.In addition, the axial and radial alternate load of pressurized machine is balanced by the cooperation of thrust housing 3, stuffing box gland 2 and opening floating bearing back-up ring 8.Because existing turbocharger rotor system parts is too much, bearing arrangement is comparatively complicated and cost is higher, and this limits the reliability of turbosupercharger and the problem of physical dimension to a certain extent.
Summary of the invention
The purpose of this utility model be overcome prior art above-mentioned deficiency and a kind of turbocharger rotor system adopting full floating bearing structure is provided.
The technical solution of the utility model is: a kind of full floating bearing turbocharger rotor-support-foundation system, comprises impeller, seal ring, bearing support, turbine end full floating bearing, air end of booster full floating bearing, air end of booster stuffing box gland and turbine rotor shaft.
The first shaft lever hole and the second shaft lever hole is provided with in described bearing support, one end of first shaft lever hole is provided with turbine end full floating bearing mounting hole, the port of turbine end full floating bearing mounting hole is provided with the first oil extraction chamfering, one end of second shaft lever hole is provided with air end of booster full floating bearing mounting hole, and the port of air end of booster full floating bearing mounting hole is provided with the second oil extraction chamfering.
The end face of bearing support air end of booster is provided with the tapped hole installing back of the body dish.
Oil inlet hole and spill port is provided with in bearing support, the bottom of oil inlet hole is respectively equipped with the first oilhole and the second oilhole, first oilhole communicates with the clutch shaft bearing hole in bearing support, second oilhole communicates with the second bearing hole in bearing support, and the first oilhole and the second oilhole are respectively turbine end full floating bearing and air end of booster full floating bearing provides lubricant oil.
The center of described air end of booster full floating bearing is provided with bearing hole, its cylindrical is provided with annular oil groove, four equally distributed oilholes are provided with in annular oil groove, the two ends of air end of booster full floating bearing are respectively the first Thrust Faces and the second Thrust Faces, first Thrust Faces is provided with two ~ eight equally distributed wedge shape oil grooves, wedge shape oil groove is fan-shaped, it is contrary with the sense of rotation of turbine rotor shaft that the section depth of wedge shape oil groove reduces direction gradually, second Thrust Faces of air end of booster full floating bearing is provided with two ~ eight equally distributed wedge shape oil grooves, wedge shape oil groove is fan-shaped, it is identical with the sense of rotation of turbine rotor shaft that the section depth of wedge shape oil groove reduces direction gradually.
The center of described turbine end full floating bearing is provided with bearing hole, its cylindrical is provided with annular oil groove, four equally distributed oilholes are provided with in annular oil groove, the two ends of turbine end full floating bearing are respectively the first Thrust Faces and the second Thrust Faces, first Thrust Faces is provided with two ~ eight equally distributed wedge shape oil grooves, wedge shape oil groove is fan-shaped, it is identical with the sense of rotation of turbine rotor shaft that the section depth of wedge shape oil groove reduces direction gradually, second Thrust Faces of turbine end full floating bearing is provided with two ~ eight equally distributed wedge shape oil grooves, wedge shape oil groove is fan-shaped, it is contrary with the sense of rotation of turbine rotor shaft that the section depth of wedge shape oil groove reduces direction gradually.
The axostylus axostyle of described turbine rotor shaft is provided with successively annular seal groove, turbine end axostylus axostyle and air end of booster axostylus axostyle, one end of turbine end axostylus axostyle is processed with first shaft shoulder, and the diameter of first shaft shoulder is more than or equal to the external diameter of turbine end full floating bearing.
Described air end of booster stuffing box gland is provided with the oil baffle mounting groove of annular seal groove and annular, the external diameter that stuffing box gland closes on floating bearing end face slightly larger than or equal the external diameter of floating bearing.
During installation, turbine end full floating bearing is arranged in the turbine end full floating bearing mounting hole on bearing support, first Thrust Faces of turbine end full floating bearing contacts with the bottom end of turbine end full floating bearing mounting hole, air end of booster full floating bearing is arranged in the air end of booster full floating bearing mounting hole on bearing support, second Thrust Faces of air end of booster full floating bearing contacts with the bottom end of air end of booster full floating bearing mounting hole, turbine rotor shaft is arranged in the bearing hole of turbine end full floating bearing and the bearing hole of air end of booster full floating bearing, the turbine end axostylus axostyle of turbine rotor shaft is corresponding with the bearing hole of turbine end full floating bearing, the air end of booster axostylus axostyle of turbine rotor shaft is corresponding with the bearing hole of air end of booster full floating bearing, air end of booster stuffing box gland and impeller are arranged on the other end of turbine rotor shaft axostylus axostyle successively, and be fixed on the axostylus axostyle of turbine rotor shaft by nut, seal ring is arranged in the annular seal groove on turbine rotor shaft axostylus axostyle, the turbine end of bearing support is sealed.
The axostylus axostyle of turbine rotor shaft and the first shaft lever hole and the second shaft lever hole inwall form first row oil pocket A and second row oil pocket B respectively.
When turbocharger rotor system high-speed rotates, lubricant oil enters from the oil inlet hole bearing support, provides lubricant oil by the first oilhole and the second oilhole to turbine end full floating bearing and air end of booster full floating bearing.
Now, turbine end full floating bearing and its internal surface of air end of booster full floating bearing and outer surface form oil film and support turbocharger rotor system and do high speed rotary motion.
First Thrust Faces of turbine end full floating bearing and the bottom end of turbine end full floating bearing mounting hole form oil film and form the supporting surface a pair with thrust load bearing capacity, and first shaft shoulder on the second Thrust Faces of turbine end full floating bearing and turbine rotor shaft forms oil film and forms the stayed surface a pair with thrust load bearing capacity.
First Thrust Faces of air end of booster full floating bearing and the end face of air end of booster stuffing box gland form oil film and form the supporting surface a pair with thrust load bearing capacity, and the second Thrust Faces of air end of booster full floating bearing and the bottom end of air end of booster full floating bearing mounting hole form oil film and form the supporting surface a pair with thrust load bearing capacity.
First oil extraction chamfering is used for draining the high temperature grease at turbine end full floating bearing second Thrust Faces place, and first row oil pocket A is used for draining the high temperature grease at turbine end full floating bearing first Thrust Faces place.Second oil extraction chamfering is used for draining the high temperature grease at air end of booster full floating bearing first Thrust Faces place, and second row oil pocket B is used for the high temperature grease at the second Thrust Faces place of draining air end of booster full floating bearing.The temperature of bearing is effectively reduced by above oil extraction mode.
The utility model compared with prior art has following features:
The turbocharger rotor system that the utility model provides adopts full floating bearing, by to bearing support, turbine end full floating bearing, air end of booster full floating bearing, the redesign of air end of booster stuffing box gland and turbine rotor shaft, make turbine end full floating bearing and air end of booster full floating bearing not only can bear radial load, but also the axial force pointing to air end of booster from turbine end and the axial alternate load produced when air end of booster points to the axial force of turbine end can be born, and the thrust bearing eliminated in existing turbocharger rotor system, thrust housing, the parts such as back-up ring, simplify bearing support mechanical processing technique, optimize turbocharger rotor system unit, also can simplify turbosupercharger assembly technology further, effectively reduce costs, make turbocharger arrangement more compact, improve the competitive advantage of product.
Below in conjunction with the drawings and specific embodiments, detailed construction of the present utility model is further described.
Accompanying drawing explanation
Accompanying drawing 1 is existing turbocharger rotor system architecture schematic diagram;
Accompanying drawing 2 is existing floating bearing structural representation;
Accompanying drawing 3 is the left view in accompanying drawing 2;
The full floating bearing turbocharger rotor-support-foundation system structural representation that accompanying drawing 4 provides for the utility model;
Accompanying drawing 5 is the I portion enlarged view in accompanying drawing 4;
Accompanying drawing 6 is the II portion enlarged view in accompanying drawing 4;
Accompanying drawing 7 is bearing body structure schematic diagram;
Accompanying drawing 8 is turbine end full floating bearing structure schematic diagram;
Accompanying drawing 9 is turbine end full floating bearing first Thrust Faces structural representation;
Accompanying drawing 10 is the wedge shape oil groove cross-sectional structure schematic diagram in turbine end full floating bearing first Thrust Faces, and in figure, arrow is rotor shaft sense of rotation;
Accompanying drawing 11 is turbine end full floating bearing second Thrust Faces structural representation;
Accompanying drawing 12 is the wedge shape oil groove cross-sectional structure schematic diagram in turbine end full floating bearing second Thrust Faces, and in figure, arrow is rotor shaft sense of rotation;
Accompanying drawing 13 is air end of booster full floating bearing structure schematic diagram;
Accompanying drawing 14 is air end of booster full floating bearing first Thrust Faces structural representation;
Accompanying drawing 15 is the wedge shape oil groove cross-sectional structure schematic diagram in air end of booster full floating bearing first Thrust Faces, and in figure, arrow is rotor shaft sense of rotation;
Accompanying drawing 16 is air end of booster full floating bearing second Thrust Faces structural representation;
Accompanying drawing 17 is the wedge shape oil groove cross-sectional structure schematic diagram in air end of booster full floating bearing second Thrust Faces, and in figure, arrow is rotor shaft sense of rotation;
Accompanying drawing 18 is turbine rotor shaft structural representation;
Accompanying drawing 19 is air end of booster stuffing box gland structural representation.
Embodiment
A kind of full floating bearing turbocharger rotor-support-foundation system, comprises impeller 1, seal ring 6, bearing support 11, turbine end full floating bearing 12, air end of booster full floating bearing 13, air end of booster stuffing box gland 14 and turbine rotor shaft 15.
The first shaft lever hole 11-1 and the second shaft lever hole 11-2 is provided with in described bearing support 11, one end of first shaft lever hole 11-1 is provided with turbine end full floating bearing mounting hole 11-1-1, the port of turbine end full floating bearing mounting hole 11-1-1 is provided with the first oil extraction chamfering 11-1-2, and one end of the second shaft lever hole 11-2 is provided with
Air end of booster full floating bearing mounting hole 11-2-1, the port of air end of booster full floating bearing mounting hole 11-2-1 is provided with the second oil extraction chamfering 11-2-2.
The end face of bearing support 11 air end of booster is provided with the tapped hole 11-6 installing back of the body dish.
Oil inlet hole 11-3 and spill port 11-7 is provided with in bearing support 11, the bottom of oil inlet hole 11-3 is respectively equipped with the first oilhole 11-4 and the second oilhole 11-5, first oilhole 11-4 communicates with the clutch shaft bearing hole 11-1-1 in bearing support 11, second oilhole 11-5 communicates with the second bearing hole 11-2-1 in bearing support 11, and the first oilhole 11-4 and the second oilhole 11-5 is respectively turbine end full floating bearing 12 and air end of booster full floating bearing 13 provides lubricant oil.
The center of described air end of booster full floating bearing 13 is provided with bearing hole 13-1, its outer garden is provided with annular oil groove 13-2, four equally distributed oilhole 13-3 are provided with in annular oil groove 13-2, the two ends of air end of booster full floating bearing 13 are respectively the first Thrust Faces 13-4 and the second Thrust Faces 13-5, first Thrust Faces 13-4 is provided with four equally distributed wedge shape oil groove 13-4-1, wedge shape oil groove 13-4-1 is fan-shaped, it is contrary with the sense of rotation of turbine rotor shaft 15 that the section depth of wedge shape oil groove 13-4-1 reduces direction gradually, second Thrust Faces 13-5 of air end of booster full floating bearing 13 is provided with four equally distributed wedge shape oil groove 13-5-1, wedge shape oil groove 13-5-1 is fan-shaped, it is identical with the sense of rotation of turbine rotor shaft 15 that the section depth of wedge shape oil groove 13-5-1 reduces direction gradually.
The center of described turbine end full floating bearing 12 is provided with bearing hole 12-1, its outer garden is provided with annular oil groove 12-2, four equally distributed oilhole 12-3 are provided with in annular oil groove 12-2, the two ends of turbine end full floating bearing 12 are respectively the first Thrust Faces 12-4 and the second Thrust Faces 12-5, first Thrust Faces 12-4 is provided with four equally distributed wedge shape oil groove 12-4-1, wedge shape oil groove 12-4-1 is fan-shaped, it is identical with the sense of rotation of turbine rotor shaft 15 that the section depth of wedge shape oil groove 12-4-1 reduces direction gradually, second Thrust Faces 12-5 of turbine end full floating bearing 12 is provided with four equally distributed wedge shape oil groove 12-5-1, wedge shape oil groove 12-5-1 is fan-shaped, it is contrary with the sense of rotation of turbine rotor shaft 15 that the section depth of wedge shape oil groove 12-5-1 reduces direction gradually.
The axostylus axostyle of described turbine rotor shaft 15 is provided with successively annular seal groove 15-3, turbine end axostylus axostyle 15-1 and air end of booster axostylus axostyle 15-2, one end of turbine end axostylus axostyle 15-1 is processed with the first shaft shoulder 15-1-1, the diameter of the first shaft shoulder 15-1-1 slightly larger than or equal the external diameter of turbine end full floating bearing 12.
Described air end of booster stuffing box gland 14 is provided with the oil baffle mounting groove 14-2 of annular seal groove 14-1 and annular, the external diameter of air end of booster stuffing box gland 14-3 slightly larger than or equal the external diameter of floating bearing 13.
During installation, turbine end full floating bearing 12 is arranged in the turbine end full floating bearing mounting hole 11-1-1 on bearing support 11, first Thrust Faces 12-4 of turbine end full floating bearing 12 contacts with the bottom end of turbine end full floating bearing mounting hole 11-1-1, air end of booster full floating bearing 13 is arranged in the air end of booster full floating bearing mounting hole 11-2-1 on bearing support 11, second Thrust Faces 13-5 of air end of booster full floating bearing 13 contacts with the bottom end of air end of booster full floating bearing mounting hole 11-2-1, turbine rotor shaft 15 is arranged in the bearing hole 12-1 of turbine end full floating the bearing 12 and bearing hole 13-1 of air end of booster full floating bearing 13, the turbine end axostylus axostyle 15-1 of turbine rotor shaft 15 is corresponding with the bearing hole 12-1 of turbine end full floating bearing 12, the air end of booster axostylus axostyle 15-2 of turbine rotor shaft 15 is corresponding with the bearing hole 13-1 of air end of booster full floating bearing 13, air end of booster stuffing box gland 14 and impeller 1 are arranged on the other end of turbine rotor shaft 15 axostylus axostyle successively, and be fixed on the axostylus axostyle of turbine rotor shaft 15 by nut, seal ring 6 is arranged in the annular seal groove 15-3 on turbine rotor shaft 15 axostylus axostyle, the turbine end of bearing support 15 is sealed.
The axostylus axostyle of turbine rotor shaft 15 and the first shaft lever hole 11-1 and the second shaft lever hole 11-2 inwall form first row oil pocket A and second row oil pocket B respectively.
Claims (3)
1. a full floating bearing turbocharger rotor-support-foundation system, is characterized in that: comprise impeller, seal ring, bearing support, turbine end full floating bearing, air end of booster full floating bearing, air end of booster stuffing box gland and turbine rotor shaft;
During installation, turbine end full floating bearing is arranged in the turbine end full floating bearing mounting hole on bearing support, first Thrust Faces of turbine end full floating bearing contacts with the bottom end of turbine end full floating bearing mounting hole, air end of booster full floating bearing is arranged in the air end of booster full floating bearing mounting hole on bearing support, second Thrust Faces of air end of booster full floating bearing contacts with the bottom end of air end of booster full floating bearing mounting hole, turbine rotor shaft is arranged in the bearing hole of turbine end full floating bearing and the bearing hole of air end of booster full floating bearing, the turbine end axostylus axostyle of turbine rotor shaft is corresponding with the bearing hole of turbine end full floating bearing, the air end of booster axostylus axostyle of turbine rotor shaft is corresponding with the bearing hole of air end of booster full floating bearing, air end of booster stuffing box gland and impeller are arranged on the other end of turbine rotor shaft axostylus axostyle successively, and be fixed on the axostylus axostyle of turbine rotor shaft by nut, seal ring is arranged in the annular seal groove on turbine rotor shaft axostylus axostyle, the turbine end of bearing support is sealed,
The axostylus axostyle of turbine rotor shaft and the first shaft lever hole and the second shaft lever hole inwall form first row oil pocket A and second row oil pocket B respectively.
2. a kind of full floating bearing turbocharger rotor-support-foundation system as claimed in claim 1, it is characterized in that: in described bearing support, be provided with the first shaft lever hole and the second shaft lever hole, one end of first shaft lever hole is provided with turbine end full floating bearing mounting hole, the port of turbine end full floating bearing mounting hole is provided with the first oil extraction chamfering, one end of second shaft lever hole is provided with air end of booster full floating bearing mounting hole, and the port of air end of booster full floating bearing mounting hole is provided with the second oil extraction chamfering;
The end face of bearing support air end of booster is provided with the tapped hole installing back of the body dish;
Oil inlet hole and spill port is provided with in bearing support, the bottom of oil inlet hole is respectively equipped with the first oilhole and the second oilhole, first oilhole communicates with the clutch shaft bearing hole in bearing support, second oilhole communicates with the second bearing hole in bearing support, and the first oilhole and the second oilhole are respectively turbine end full floating bearing and air end of booster full floating bearing provides lubricant oil;
The axostylus axostyle of described turbine rotor shaft is provided with successively annular seal groove, turbine end axostylus axostyle and air end of booster axostylus axostyle, one end of turbine end axostylus axostyle is processed with first shaft shoulder, and the diameter of first shaft shoulder is more than or equal to the external diameter of turbine end full floating bearing;
Described air end of booster stuffing box gland is provided with the oil baffle mounting groove of annular seal groove and annular, the external diameter that stuffing box gland closes on floating bearing end face slightly larger than or equal the external diameter of floating bearing.
3. a kind of full floating bearing turbocharger rotor-support-foundation system as claimed in claim 1 or 2, it is characterized in that: the center of described air end of booster full floating bearing is provided with bearing hole, its outer garden is provided with annular oil groove, four equally distributed oilholes are provided with in annular oil groove, the two ends of air end of booster full floating bearing are respectively the first Thrust Faces and the second Thrust Faces, first Thrust Faces is provided with two ~ eight equally distributed wedge shape oil grooves, wedge shape oil groove is fan-shaped, it is contrary with the sense of rotation of turbine rotor shaft that the section depth of wedge shape oil groove reduces direction gradually, second Thrust Faces of air end of booster full floating bearing is provided with two ~ eight equally distributed wedge shape oil grooves, wedge shape oil groove is fan-shaped, it is identical with the sense of rotation of turbine rotor shaft that the section depth of wedge shape oil groove reduces direction gradually,
The center of described turbine end full floating bearing is provided with bearing hole, its outer garden is provided with annular oil groove, four equally distributed oilholes are provided with in annular oil groove, the two ends of turbine end full floating bearing are respectively the first Thrust Faces and the second Thrust Faces, first Thrust Faces is provided with two ~ eight equally distributed wedge shape oil grooves, wedge shape oil groove is fan-shaped, it is identical with the sense of rotation of turbine rotor shaft that the section depth of wedge shape oil groove reduces direction gradually, second Thrust Faces of turbine end full floating bearing is provided with two ~ eight equally distributed wedge shape oil grooves, wedge shape oil groove is fan-shaped, it is contrary with the sense of rotation of turbine rotor shaft that the section depth of wedge shape oil groove reduces direction gradually.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520502196.4U CN204827541U (en) | 2015-07-13 | 2015-07-13 | Full floating bearing turbo charger rotor system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520502196.4U CN204827541U (en) | 2015-07-13 | 2015-07-13 | Full floating bearing turbo charger rotor system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204827541U true CN204827541U (en) | 2015-12-02 |
Family
ID=54685152
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520502196.4U Expired - Fee Related CN204827541U (en) | 2015-07-13 | 2015-07-13 | Full floating bearing turbo charger rotor system |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN204827541U (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104989461A (en) * | 2015-07-13 | 2015-10-21 | 湖南天雁机械有限责任公司 | Full-floating bearing turbocharger rotor system |
| CN107060910A (en) * | 2017-03-24 | 2017-08-18 | 中国北方发动机研究所(天津) | A kind of arrangement of turbo-charger shaft module |
| EP3875737A1 (en) * | 2020-03-03 | 2021-09-08 | Borgwarner Inc. | Bearing assembly for a charging apparatus |
| US11598372B2 (en) | 2020-03-03 | 2023-03-07 | Borgwarner Inc. | Bearing assembly for a charging apparatus |
-
2015
- 2015-07-13 CN CN201520502196.4U patent/CN204827541U/en not_active Expired - Fee Related
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104989461A (en) * | 2015-07-13 | 2015-10-21 | 湖南天雁机械有限责任公司 | Full-floating bearing turbocharger rotor system |
| CN107060910A (en) * | 2017-03-24 | 2017-08-18 | 中国北方发动机研究所(天津) | A kind of arrangement of turbo-charger shaft module |
| CN107060910B (en) * | 2017-03-24 | 2019-04-05 | 中国北方发动机研究所(天津) | A kind of arragement construction of turbo-charger shaft module |
| EP3875737A1 (en) * | 2020-03-03 | 2021-09-08 | Borgwarner Inc. | Bearing assembly for a charging apparatus |
| US11560924B2 (en) | 2020-03-03 | 2023-01-24 | Borgwarner Inc. | Bearing assembly for a charging apparatus |
| US11598372B2 (en) | 2020-03-03 | 2023-03-07 | Borgwarner Inc. | Bearing assembly for a charging apparatus |
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