CN201137516Y - Semi-circle shaped double flow path turbo-charger - Google Patents
Semi-circle shaped double flow path turbo-charger Download PDFInfo
- Publication number
- CN201137516Y CN201137516Y CNU2007201851590U CN200720185159U CN201137516Y CN 201137516 Y CN201137516 Y CN 201137516Y CN U2007201851590 U CNU2007201851590 U CN U2007201851590U CN 200720185159 U CN200720185159 U CN 200720185159U CN 201137516 Y CN201137516 Y CN 201137516Y
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- China
- Prior art keywords
- turbine
- wheel shaft
- engine
- runner
- blades
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- 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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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
- Y02T10/10—Internal combustion engine [ICE] based vehicles
- Y02T10/12—Improving ICE efficiencies
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- Supercharger (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
A semicircle dual channel turbocharger comprises a turbine engine, an intermediate and a compressor, wherein the turbine engine comprises a shell, a turbine, a wheel shaft and blades, the turbine is sheathed and welded at the front end of the wheel shaft integrally, the turbine shell is provided with two channels as a first channel and a second channel whose chambers are semicircle, the turbine is provided with a plurality of blades and is in radial type, the intermediate is fixedly connected with the turbine shell via bolts, the middle of the wheel shaft is provided with two floating bearings at two ends of the intermediate and embedded in the bearing base holes of the intermediate, the compressor shell is fixedly connected with the intermediate via bolts. The utility model improves the efficiency of engine, reduces the waste gas discharge of the engine, and has high practicality, simple, compact and dense structure, low material consumption, low cost, stable property, high reliability, simple maintenance and the adaptation for engine.
Description
Technical field
The utility model relates to engine supercharger, concrete is under High Temperature High Pressure and environment mal-condition still can stable operation a kind of dynamical turbosupercharger.
Background technique
Along with science and technology development, greatly promoted the development and the raising of motor industry, the pressure-increasing machine that also making accordingly matches with motor uses also constantly upgrades and is developed faster.Though the air intake pressurized of motor is a mature technique comparatively, the kind of pressurized machine also is varied, however under the condition of concrete environment and use, the work that pressurized machine can not be reliable and stable sometimes, so that can not export maximum power.Be generally and improve the way that air inflow and suction pressure have to take to increase supercharger speed, so that number of moving part reaches more than 60,000 rev/mins, add in the ambient temperature that is operated in several Baidu, this not general pressurized machine can bear.
Do not have air inflow big at present as yet, suction pressure is also big, can adapt to the pressurized machine in high temperature, the work of high-pressure working condition condition.
Summary of the invention
The purpose of this utility model should not be moved under the environment of High Temperature High Pressure for the pressurized machine that solves present use, air inflow is little, the problem that suction pressure is not high yet, and provide revolution to reach more than 70,000 rev/mins, air inflow is big, the efficient height, the semicircle double flow channel turbosupercharger of working under severe environmental conditions suits.
The technological scheme that adopts is:
Semicircle double flow channel turbosupercharger comprises turbo machine, intermediate, gas compressor.Described turbo machine comprises volute, turbine, wheel shaft, blade, turbine is sleeved on the front end of wheel shaft, be integral by being welded to connect, in the wheel shaft front portion one thermal baffle is set, thermal baffle is between turbine and intermediate, intermediate and volute are bolted to connection, intermediate is installed in the outside of wheel shaft intermediate portion, the wheel shaft intermediate portion is provided with two floating bearings, two floating bearings are positioned at the two ends of intermediate, and are embedded in the bearing saddle bore of intermediate, and a thrust bearing is installed at the wheel shaft rear portion, thrust bearing is replaced mutually with thrust ring, and thrust bearing is arranged in the thrust shaft block hole of compressor casing front end; Compressor casing and intermediate are fastenedly connected by screw, and its structure outline is:
Be provided with double flow channel in the described turbine case, i.e. 1# runner, 2# runner, the inner chamber of 1# runner, 2# runner are semicircle.
Described turbine is provided with a plurality of blades, and a plurality of blades are planely to be connected with the turbine vertical fixing, and turbine is the radial-flow type structure.
Working principle and characteristics:
There are turbo machine and gas compressor in the front and back of turbosupercharger, the suction port of turbo machine links to each other with pressurized machine engine exhaust pipe outward, the gas that has certain pressure that motor is discharged is injected on the blade of turbo machine with the form of air-flow, make turbo machine be quickened to rotate, rotate thereby drive gas compressor, the waste gas that is ejected into behind the blade is discharged from the outlet pipe of equipment outside the pressurized machine is linked in the turbo machine air outlet.The import of gas compressor links to each other with air-strainer pipeline outside the pressurized machine, the very fast rotation of gas compressor just is drawn into fresh air endlessly from air-strainer like this, blower outlet links to each other with engine air inlet tube, fresh air compresses through gas compressor, endlessly pressurized gas is sent in the motor again.When engine speed speeds, the waste gas velocity of discharge increases, secondary speed also speeds synchronously, gas compressor will compress more air and enter cylinder, the pressure of air and density increase the more fuel that can burn, and fuel combustion gets more abundant, has improved combustion efficiency, increase the rotating speed of motor, improved the delivery efficiency of motor.Both save fuel oil, reduced the pollution of tail gas again.
The HX80 turbosupercharger is installed on the KTA50 motor, and turbosupercharger adopts floating bearing, owing to have fluid to do cooling between bearing and body inwall, i.e. and " wholly floating bearing ".Its working speed can reach more than 80,000 rev/mins, can be to move in the above environment of six, 700 degree in ambient temperature, pressurized machine has improved the design of volute flow passage, adopted double flow channel volute form, the inner chamber semicircular in shape of double flow channel, and turbine is provided with a plurality of blades, a plurality of blades are planely to be connected with the turbine vertical fixing, turbine is the radial-flow type structure, reduced the resistance of waste gas in volute flow passage of motor so widely, increased the discharge value of gas, the power that is injected on the turbine bucket has been increased greatly, thereby improved efficiency of turbocharger widely.
The characteristics of this turbosupercharger are:
1 has selected enough resistant to elevated temperatures high-quality material (turbine has been selected the K418 material for use) processing and fabricatings for use, has guaranteed that pressurized machine long-time continuous under high temperature and high pressure environment runs up.
2 have adopted advanced process equipment and accurate detection means to guarantee the machining high-precision of component.
3 turbosupercharger seal points have adopted seal ring to add cushion rubber and have sealed, and sealability is superior, and leakage phenomenon had not taken place in long-time use.
4 working process advanced persons adopt computer control, and the dynamic balance accuracy of rotor assembly is reached in the 0.001mm.
5 is last by stand test, whole technical performances of complete machine check pressurized machine.
The utility model design science, reasonable, original, the suction pressure and the air inflow that have increased motor, thus make fuel combustion more abundant, improve the efficient of motor, reduced the discharging of engine exhaust, practicability is stronger, has replaced the inlet plenum device.Overall structure is simple, compact, tight, and consumptive material is few, and is with low cost, stable performance, reliable, easy to maintenance, and the utility model suits and the supporting use of motor.
Description of drawings
Fig. 1 is a structural representation of the present utility model.
Fig. 2 is a turbocharger housing structure schematic representation of the present utility model.
Fig. 3 is that the A-A of Fig. 2 is to cross-sectional schematic.
Fig. 4 is that the B-B of Fig. 2 is to cross-sectional schematic.
Fig. 5 is that the C-C of Fig. 2 is to cross-sectional schematic.
Embodiment
Embodiment
Semicircle double flow channel turbosupercharger comprises turbo machine, intermediate 4, gas compressor.Described turbo machine comprises volute 1, turbine 2, wheel shaft 11, blade 12, turbine 2 is sleeved on the front end of wheel shaft 11, is integral by being welded to connect, and is provided with double flow channel 13 and 14 in the volute 1, be 1# runner 13,2# runner 14, the inner chamber of 1# runner 13,2# runner 14 is semicircle.It is planely to be connected with turbine 2 vertical fixing that turbine 2 is provided with 12,12 blades of 12 blades 12, and turbine 2 is the radial-flow type structure.In wheel shaft 11 front portions one thermal baffle 3 is set, thermal baffle 3 is between turbine 2 and intermediate 4, intermediate 4 is bolted to connection with volute 1, intermediate 4 is installed in the outside of the intermediate portion of wheel shaft 11, the intermediate portion of wheel shaft 11 is provided with two floating bearings 6, two floating bearings 6 are positioned at the two ends of intermediate 4, and be embedded in the bearing saddle bore 5 of intermediate 4, a thrust bearing 10 is installed at the rear portion of wheel shaft 11, thrust bearing 10 is replaced mutually with thrust ring 7, and thrust bearing 10 is arranged in the thrust shaft block hole 9 of compressor casing 8 front ends; Compressor casing 8 and intermediate 4 are connected by bolton.
Claims (1)
1, semicircle double flow channel turbosupercharger comprises turbo machine, intermediate (4), gas compressor; Described turbo machine comprises volute (1), turbine (2), wheel shaft (11), blade (12), turbine (2) is sleeved on the front end of wheel shaft (11), be integral by being welded to connect, in wheel shaft (11) front portion one thermal baffle (3) is set, thermal baffle (3) is positioned between turbine (2) and the intermediate (4), intermediate (4) is bolted to connection with volute (1), intermediate (4) is installed in the outside of the intermediate portion of wheel shaft (11), the intermediate portion of wheel shaft (11) is provided with two floating bearings (6), two floating bearings (6) are positioned at the two ends of intermediate (4), and be embedded in the bearing saddle bore (5) of intermediate (4), a thrust bearing (10) is installed at the rear portion of wheel shaft (11), thrust bearing (10) is replaced mutually with thrust ring (7), and thrust bearing (10) is arranged in the thrust shaft block hole (9) of compressor casing (8) front end; Compressor casing (8) is connected by bolton with intermediate (4), it is characterized in that:
Be provided with double flow channel (13) and (14) in the described volute (1), i.e. 1# runner (13), 2# runner (14), the inner chamber of 1# runner (13), 2# runner (14) are semicircle;
Described turbine (2) is provided with a plurality of blades (12), and a plurality of blades (12) are planely to be connected with turbine (2) vertical fixing, and turbine (2) is the radial-flow type structure.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CNU2007201851590U CN201137516Y (en) | 2007-12-25 | 2007-12-25 | Semi-circle shaped double flow path turbo-charger |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CNU2007201851590U CN201137516Y (en) | 2007-12-25 | 2007-12-25 | Semi-circle shaped double flow path turbo-charger |
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CN201137516Y true CN201137516Y (en) | 2008-10-22 |
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CNU2007201851590U Expired - Fee Related CN201137516Y (en) | 2007-12-25 | 2007-12-25 | Semi-circle shaped double flow path turbo-charger |
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Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2011000182A1 (en) * | 2009-07-03 | 2011-01-06 | Wang Hang | Dual-passage variable-section turbine of turbocharger |
CN101985897A (en) * | 2010-09-14 | 2011-03-16 | 康跃科技股份有限公司 | Complex turbine device with variable section |
CN102667063A (en) * | 2010-12-07 | 2012-09-12 | 三菱重工业株式会社 | Radial turbine |
CN110735673A (en) * | 2019-11-18 | 2020-01-31 | 大连海事大学 | kinds of double-channel volute |
-
2007
- 2007-12-25 CN CNU2007201851590U patent/CN201137516Y/en not_active Expired - Fee Related
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2011000182A1 (en) * | 2009-07-03 | 2011-01-06 | Wang Hang | Dual-passage variable-section turbine of turbocharger |
CN101985897A (en) * | 2010-09-14 | 2011-03-16 | 康跃科技股份有限公司 | Complex turbine device with variable section |
WO2012034258A1 (en) * | 2010-09-14 | 2012-03-22 | Zhu Zhifu | Variable-section composite turbine apparatus |
CN102667063A (en) * | 2010-12-07 | 2012-09-12 | 三菱重工业株式会社 | Radial turbine |
CN102667063B (en) * | 2010-12-07 | 2013-05-01 | 三菱重工业株式会社 | Radial turbine |
CN110735673A (en) * | 2019-11-18 | 2020-01-31 | 大连海事大学 | kinds of double-channel volute |
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Legal Events
Date | Code | Title | Description |
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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: 20081022 Termination date: 20121225 |