CN102080578A - Compound turbo supercharging device having variable cross-section axial radial flows - Google Patents
Compound turbo supercharging device having variable cross-section axial radial flows Download PDFInfo
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- CN102080578A CN102080578A CN2011100051832A CN201110005183A CN102080578A CN 102080578 A CN102080578 A CN 102080578A CN 2011100051832 A CN2011100051832 A CN 2011100051832A CN 201110005183 A CN201110005183 A CN 201110005183A CN 102080578 A CN102080578 A CN 102080578A
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- 150000001875 compounds Chemical class 0.000 title abstract description 5
- 230000007246 mechanism Effects 0.000 claims abstract description 26
- 239000002131 composite material Substances 0.000 claims description 38
- TVEXGJYMHHTVKP-UHFFFAOYSA-N 6-oxabicyclo[3.2.1]oct-3-en-7-one Chemical compound C1C2C(=O)OC1C=CC2 TVEXGJYMHHTVKP-UHFFFAOYSA-N 0.000 claims 1
- 230000005540 biological transmission Effects 0.000 abstract description 2
- 210000000867 larynx Anatomy 0.000 abstract 3
- 239000007789 gas Substances 0.000 description 23
- 230000001276 controlling effect Effects 0.000 description 15
- 239000002912 waste gas Substances 0.000 description 11
- 238000000034 method Methods 0.000 description 7
- 238000005266 casting Methods 0.000 description 4
- 230000006872 improvement Effects 0.000 description 4
- 230000001105 regulatory effect Effects 0.000 description 4
- 239000000567 combustion gas Substances 0.000 description 3
- 230000007812 deficiency Effects 0.000 description 3
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- 230000004044 response Effects 0.000 description 2
- 230000004043 responsiveness Effects 0.000 description 2
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- 238000002485 combustion reaction Methods 0.000 description 1
- 230000006835 compression Effects 0.000 description 1
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- 230000009711 regulatory function Effects 0.000 description 1
- 238000012827 research and development Methods 0.000 description 1
- 230000000630 rising effect Effects 0.000 description 1
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Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B37/00—Engines characterised by provision of pumps driven at least for part of the time by exhaust
- F02B37/02—Gas passages between engine outlet and pump drive, e.g. reservoirs
- F02B37/025—Multiple scrolls or multiple gas passages guiding the gas to the pump drive
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D17/00—Regulating or controlling by varying flow
- F01D17/10—Final actuators
- F01D17/12—Final actuators arranged in stator parts
- F01D17/14—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits
- F01D17/141—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of shiftable members or valves obturating part of the flow path
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D9/00—Stators
- F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
- F01D9/026—Scrolls for radial machines or engines
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B37/00—Engines characterised by provision of pumps driven at least for part of the time by exhaust
- F02B37/12—Control of the pumps
- F02B37/22—Control of the pumps by varying cross-section of exhaust passages or air passages, e.g. by throttling turbine inlets or outlets or by varying effective number of guide conduits
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C6/00—Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use
- F02C6/04—Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output
- F02C6/10—Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output supplying working fluid to a user, e.g. a chemical process, which returns working fluid to a turbine of the plant
- F02C6/12—Turbochargers, i.e. plants for augmenting mechanical power output of internal-combustion piston engines by increase of charge pressure
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2220/00—Application
- F05D2220/40—Application in turbochargers
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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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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Chemical Kinetics & Catalysis (AREA)
- General Chemical & Material Sciences (AREA)
- Supercharger (AREA)
Abstract
The invention discloses a compound turbo supercharging device having variable cross-section axial radial flows, which comprises a double-flow channel volute, wherein the double-flow channel volute is provided with an axial flow channel and a radial flow channel; the axial flow channel and the radial flow channel are respectively provided with a volute nozzle connected to a volute outlet cylinder; a sliding slot is arranged on the double-flow channel volute close to the position of the volute nozzle of the radial flow channel; a slideable moveable larynx baffle is arranged in the sliding slot; and the moveable larynx baffle is in transmission connection with a moveable larynx baffle control mechanism. According to the invention, the variable cross-section function can be realized by using the compound turbo supercharging device, the problems that a blade type variable cross-section turbo supercharger has high cost, low speed and efficiency, inferior reliability, complex structure of a two-stage supercharger and high cost are solved, and the efficiency of a turbo when an engine runs in a low speed is effectively increased while the efficiency is ensured when the engine runs under the large flow working condition.
Description
Technical field
The present invention relates to a kind of turbo charging installation, relate to a kind of variable cross section diameter of axle stream composite turbocharging device specifically, can effectively take into account the high low speed supercharging requirement of motor, belong to field of internal combustion engine.
Background technique
Pressurized machine is applied to modern motor widely, and in order to satisfy performance and the emission request of motor under all operating modes, pressurized machine must have the can regulate function of boost pressure and discharge pressure.Along with the enforcement of state's four Abgasgesetzs, variable cross section pressurized machine and two-stage supercharger have been called the emphasis of the domestic and international industry research and development of industry.
Generally adopt at present at spiral case nozzle place the requirement that rotation blade satisfies variable cross section is installed, compare with traditional pressurized machine, it can effectively widen the matching range of pressurized machine and motor, realizes the regulatory function of pressurized machine to boost pressure and discharge pressure.
Rotary vane type variable-area turbocharger structural representation as shown in Figure 1, the turbine portion branch of rotary vane type variable-area turbocharger comprises spiral case 3, spiral case nozzle 5, turbine wheel 7 three parts.Driving mechanism 2 is regulated the circulation area of nozzle and the angle of outlet waste gas by the aperture that adjusting is installed in the nozzle vane 6 on the nozzle ring supporting disk 4, makes the high-temp waste gas peace blow to turbine wheel 7 according to the air-flow angle of design, promotes turbine wheel 7 high speed rotating.Compressor impeller 9 high speed rotating that rotor shaft 8 drives in the compressor casing 1 compress the air that axially enters gas compressor, and the collection that the air after the compression advanced compressor casing is sent to participation burning in the cylinder.
Rotary vane type variable cross section pressurized machine can be according to the different operating modes of motor, and the aperture of real-time regulated nozzle vane 6 changes the circulation area of spiral case nozzle, to satisfy the performance requirement of motor.The adjusting of 2 pairs of nozzle vanes 6 of driving mechanism is simple, be easy to control.But in the application of reality, find that the rotary vane type variable-area turbocharger exists some shortcomings:
When motor under big flow operating mode, nozzle vane 6 is nearer apart from the turbine blade leading edge, exhaust gas particle can cause bigger wearing and tearing to nozzle vane 6.When motor under low flow rate condition, nozzle vane 7 is far away apart from the turbine blade leading edge, at this moment the circumferential speed of high temperature gas flow is bigger, turbine becomes action turbine, aerodynamic loss is also relatively more serious in the gas flow process in addition, makes the decrease in efficiency of pressurized machine.
The waste gas of motor row temperature and has further trend of rising greatly about about 650～850 degree.The turbocharger operation environment is abominable, and strong vibration has very high requirement to the reliability of driving mechanism 2.And the relatively poor problem of the reliability of driving mechanism 2 is not well solved till now yet.
The cost of rotary vane type variable cross section pressurized machine is very high, and this makes many motors producer hang back to its expensive price.Cost and life-span have also been limited the market of the type variable cross section pressurized machine.
Two-stage supercharging adopts low pressure turbocharger and high pressure turbocharger co-operation to realize the purpose of engine booster, and describing in detail and please refer to publication number CN 101600869A denomination of invention is two-stage supercharging type exhaust turbo supercharger.Adopting two-stage supercharging in fact also is the pressurized machine co-operation that adopts two configuration different sizes and characteristic, its turbo machine is furnished with the spiral case and the turbine of two kinds of different negotiabilities, the pressurized machine that belongs to variable cross section of fluid channel and two kinds of flow characteristics turbines, it can realize higher pressure ratio, reliability is high and pressure ratio each grade turbosupercharger is lower, make single-stage compressor that the high efficiency region of broad be arranged, but major defect is that coupling, control are complicated, bulk is bigger, and cost is higher.
Summary of the invention
The problem to be solved in the present invention is, poor reliability low at rotary vane type variable-area turbocharger cost high, low speed efficient and two-stage supercharger complex structure, defect of high cost, provide a kind of simple in structure, cost is low, reliability is high, and has the variable cross section composite turbine device that greater efficiency is taken into account big flow operating mode efficient and flow characteristics simultaneously under small flow.
In order to address the above problem, the present invention by the following technical solutions:
A kind of variable cross section diameter of axle stream composite turbocharging device, comprise the double flow channel spiral case, the double flow channel spiral case is provided with axial flow runner and runoff runner, be respectively equipped with the spiral case nozzle that is communicated with the spiral case gas outlet on described axial flow runner and the runoff runner, the position of the spiral case nozzle of close runoff runner is provided with chute on the described double flow channel spiral case, be provided with slidably mobile aditus laryngis baffle plate in chute, mobile aditus laryngis baffle plate is connected with mobile aditus laryngis baffle plate control mechanism.
Below be further improvement of these options of the present invention:
Described runoff runner is positioned at the side near the spiral case gas outlet, and the axial flow runner is positioned at the side away from the spiral case gas outlet, is provided with midfeather between described runoff runner and the axial flow runner.
Further improve:
Described mobile aditus laryngis baffle plate control mechanism comprises final controlling element, outer cover at the spiral case gas outlet is connected to the shift fork ring, described mobile aditus laryngis baffle plate is fixedlyed connected with the shift fork ring, and the final controlling element push rod is installed on the described final controlling element, is connected with shift fork between final controlling element push rod and the shift fork ring.
Mobile aditus laryngis baffle plate control mechanism realizes the switch of runoff runner by controlling moving axially of described mobile aditus laryngis baffle plate, and when guaranteeing axial flow turbine work, combustion gas does not enter runoff spiral case runner, to reduce eddy current loss.
Further improve:
Be provided with the composite turbine impeller in the double flow channel spiral case, described composite turbine impeller comprises one-level turbine wheel and two-stage turbine impeller.
Described Turbine Blade and described two-stage turbine impeller blade can according to the performance requirement of pressurized machine be set to different numbers with the requirement of Engine Matching, with performance requirement and the emission request that satisfies motor.
Further improve:
Described one-level turbine wheel is made up of prismatic blade, the two-stage turbine impeller by turbine entad blade form, the one-level turbine wheel matches with the axial flow runner, the two-stage turbine impeller matches with the runoff runner.
Further improve:
Dividing plate is installed in the described runoff runner, and dividing plate is divided into two runners with the runoff runner, forms three air inlet runners with the axial flow runner.
The another kind of improvement:
In axial flow runner and runoff runner, dividing plate is installed respectively, axial flow runner and runoff runner respectively are divided into two runners.
Dividing plate is set can better utilization waste gas pulse energy, Pulse wave is propagated in less space, pulse energy reduces, improve the efficient of turbine, improve the problem of motor supercharging deficiency when low speed to a certain extent, the while has effectively been taken into account the efficient of the big flow operating mode of motor and has reduced the discharging of motor.
Further improve: the spiral case nozzle location at the axial flow runner is installed guide-ring, and guide-ring tilts to one-level turbine wheel sense of rotation, with control turbine air inlet angle, improves turbine efficiency.
The another kind of improvement:
Described one-level turbine wheel and two-stage turbine impeller are provided with at interval, has the gap between the two, the position corresponding with this gap is provided with the cavity of annular on midfeather, and all stator blades evenly are installed in the cavity of annular, and described stator blade is between one-level turbine wheel and two-stage turbine impeller.
The mobile upset that stator blade can reduce one-level turbine wheel and two-stage turbine impeller air-flow to a certain extent is set, reduces the energy loss of gas in the impeller.
The single-stage expansion of axial flow turbine is than little, and inlet loss is little, and efficient is higher, but and the single-stage expansion of radial-flow turbine is more on the low side than big efficient.
The present invention adopts the double flow channel spiral case of forming by axial flow runner and runoff runner with the composite turbine impeller sequential working of being made up of one-level turbine wheel and two-stage turbine impeller, both satisfied the performance requirement under the little load of low engine speed, and can satisfy under the big flow operating mode of motor making turbine have bigger negotiability and higher efficient again.
The range of flow of axial flow turbine is wide, and axial flow turbine has higher efficient under big flow, and the range of flow of radial-flow turbine is narrow, but higher in the efficient of small flow scope.After adopting composite turbine, just can guarantee behind the employing composite turbine that pressurized machine can both have higher efficient under small flow and big flow, satisfy the job requirement of each operating mode of motor.
Motor is under low flow rate condition, axial flow runner air intake valve is closed, runoff runner air intake valve is opened, and mobile aditus laryngis baffle plate this moment midfeather one side shifting dorsad under the drive of mobile aditus laryngis baffle plate control mechanism, makes mobile aditus laryngis baffle plate be in opening state.The waste gas that motor is discharged only does work to the two-stage turbine impeller through the runoff runner, because radial-flow turbine has higher efficient at small flow, can satisfy the supercharging requirement of the little load of low engine speed.Widen the range of flow of radial-flow turbine, just need bigger turbine diameter, after adopting diameter of axle stream composite turbine device, can reduce the diameter of turbine on the whole, make turbine structure compacter, improve the responsiveness of pressurized machine, reduce the influence of supercharging sluggishness.
Motor is under big flow operating mode, runoff runner air intake valve is closed, axial flow runner air intake valve is opened, and this moment mobile aditus laryngis baffle plate under the drive of mobile aditus laryngis baffle plate control mechanism towards midfeather one side shifting, make mobile aditus laryngis baffle plate be in closed condition, during with the work of assurance axial flow runner, combustion gas does not enter the runoff runner, reduces the flow losses of turbine.The waste gas that motor is discharged only does work to the one-level turbine wheel through the axial flow runner, the turbine inlet loss reduces, the range of flow of axial flow turbine is wide, under big flow, have higher efficient, can satisfy motor and under big flow operating mode, make the bigger negotiability of having of turbine and have higher efficient.
Double flow channel turbine volute among the present invention is simple in structure, inheritance good, qualified casting is higher; Composite turbine impeller among the present invention can obtain higher pneumatic efficiency and higher structural strength by modern CFD, FEA analysis of technology and optimization; Variable cross section composite turbine device among the present invention can adopt existing casting and process equipment to produce, the low and quick easily through engineering approaches that realizes of cost.
The present invention adopts the composite turbine device can realize the variable cross section function, solved effectively that leaf formula variable-area turbocharger cost high, low speed efficient is low, poor reliability and two-stage supercharger complex structure, problem that cost is high, the efficient of turbine when effectively improving low engine speed, the efficient when effectively having taken into account simultaneously the big flow operating mode of motor.
Below in conjunction with drawings and Examples patent of the present invention is further specified:
Description of drawings
Accompanying drawing 1 is the structural representation of the rotary vane type variable-area turbocharger in the background technique of the present invention;
Accompanying drawing 2 is structural representations of the variable cross section composite turbine device in the embodiment of the invention 1;
Accompanying drawing 3 is structural representations of air intake valve control mechanism in the embodiment of the invention 1;
Accompanying drawing 4 is structural representations of variable cross section composite turbine device under the low flow rate condition in the embodiment of the invention 1;
Accompanying drawing 5 is structural representations of variable cross section composite turbine device under the big flow operating mode in the embodiment of the invention 1;
Accompanying drawing 6 is structural representations of the embodiment of the invention 2;
Accompanying drawing 7 is structural representations of the embodiment of the invention 3;
Accompanying drawing 8 is structural representations of the embodiment of the invention 4;
Accompanying drawing 9 is structural representations of the embodiment of the invention 5;
Accompanying drawing 10 is structural representations of the embodiment of the invention 6;
Accompanying drawing 11 is structural representations of the embodiment of the invention 7.
Among the figure: the 1-compressor casing; The 2-driving mechanism; The 3-spiral case; 4-nozzle ring supporting disk; 5-spiral case nozzle; The 6-nozzle vane; The 7-turbine wheel; The 8-rotor shaft; The 9-compressor impeller; 10-double flow channel spiral case; 11-axial flow runner; 12-runoff runner; 13-composite turbine impeller; 14-one-level turbine wheel; 15-two-stage turbine impeller; The 16-midfeather; 17-moves the aditus laryngis baffle plate; The 18-final controlling element; 19-final controlling element push rod; The 20-shift fork; 21-shift fork ring; The 22-actuator bracket; The 23-fixed rotating shaft; 24-spiral case gas outlet; 25-axial flow runner air intake valve; 26-runoff runner air intake valve; 27-air intake valve control mechanism; The 28-dividing plate; The 29-guide-ring; The 30-stator blade.
Embodiment
Embodiment 1: shown in accompanying drawing 2 and accompanying drawing 3, a kind of variable cross section diameter of axle stream composite turbocharging device comprises double flow channel spiral case 10, is provided with composite turbine impeller 13 and rotor shaft 8 in the double flow channel spiral case 10; Be connected with spiral case gas outlet 24 on the described double flow channel spiral case 10; Double flow channel spiral case 10 is provided with axial flow runner 11 and runoff runner 12, is respectively equipped with the spiral case nozzle 5 that is communicated with spiral case gas outlet 24 on described axial flow runner 11 and the runoff runner 12.
Described runoff runner 12 is positioned at the side near spiral case gas outlet 24, and axial flow runner 11 is positioned at the side away from spiral case gas outlet 24, is provided with midfeather 16 between described runoff runner 12 and the axial flow runner 11.
Described runoff runner 12 is provided with runoff runner air intake valve 26, axial flow runner 11 is provided with axial flow runner air intake valve 25, described runoff runner air intake valve 26 and axial flow runner air intake valve 25 are in transmission connection with air intake valve control mechanism 27 respectively, and air intake valve control mechanism 27 is realized axial flow runner 11 and the sequential working of runoff runner 12 under motor different flow operating mode by the switching of control axial flow runner air intake valve 25 and runoff runner air intake valve 26.
Described composite turbine impeller 13 comprises one-level turbine wheel 14 and two-stage turbine impeller 15, wherein one-level turbine wheel 14 is made up of prismatic blade, two-stage turbine impeller 15 by turbine entad blade form, one-level turbine wheel 14 matches with axial flow runner 11, and two-stage turbine impeller 15 matches with runoff runner 12.
The position of the spiral case nozzle 5 of close runoff runner 12 is provided with chute on the described double flow channel spiral case 10, is provided with slidably mobile aditus laryngis baffle plate 17 in chute, and mobile aditus laryngis baffle plate 17 is connected with mobile aditus laryngis baffle plate control mechanism.
Described mobile aditus laryngis baffle plate control mechanism comprises final controlling element 18, and described final controlling element 18 is fixedly supported on the double flow channel spiral case 10 by actuator bracket 22.
Outer cover at spiral case gas outlet 24 is connected to shift fork ring 21, and described mobile aditus laryngis baffle plate 17 is fixedlyed connected with shift fork ring 21.
On the described final controlling element 18 final controlling element push rod 19 is installed, be connected with shift fork 20 between final controlling element push rod 19 and the shift fork ring 21, shift fork 20 1 ends are fixedlyed connected with shift fork ring 21, the other end and final controlling element push rod 19 are fixedlyed connected by rotating shaft, and the intermediate portion of shift fork 20 is rotationally connected by fixed rotating shaft 23 and actuator bracket 22.
Shown in accompanying drawing 3 and accompanying drawing 4, motor is under low flow rate condition, air intake valve control mechanism 27 control axial flow runner air intake valves 25 are closed, runoff runner air intake valve 26 is opened, and mobile aditus laryngis baffle plate 17 this moment midfeather 16 1 side shiftings dorsad under the drive of mobile aditus laryngis baffle plate control mechanism 18 make mobile aditus laryngis baffle plate 17 be in opening state.
The waste gas that motor is discharged only through 15 actings of 12 pairs of two-stage turbine impellers of runoff runner, because radial-flow turbine has higher efficient at small flow, can satisfy the supercharging requirement of the little load of low engine speed.And after adopting diameter of axle stream composite turbine device, can reduce the diameter of turbine on the whole, make turbine structure compacter, improve the responsiveness of pressurized machine, reduce the influence of supercharging sluggishness.
Shown in accompanying drawing 3 and accompanying drawing 5, motor is under big flow operating mode, air intake valve control mechanism 27 regulated flow runner air intake valves 26 are closed, axial flow runner air intake valve 25 is opened, and this moment, mobile aditus laryngis baffle plate 17 towards midfeather 16 1 side shiftings, made mobile aditus laryngis baffle plate 17 be in closed condition under the drive of mobile aditus laryngis baffle plate control mechanism 18, during with the work of assurance axial flow runner, combustion gas does not enter the runoff runner, reduces the flow losses of turbine.The waste gas that motor is discharged is only through 14 actings of 11 pairs of one-level turbine wheels of axial flow runner, the turbine inlet loss reduces, the range of flow of axial flow turbine is wide, under big flow, have higher efficient, can satisfy motor and under big flow operating mode, make the bigger negotiability of having of turbine and have higher efficient.
Patent of the present invention is at the demand of motor to variable-area turbocharger, finished the exploitation of variable cross section composite turbine device, adopt the compound mode of two-stage turbine, turbine efficiency when having improved low engine speed, and the low speed torque and the output power of motor have been improved, improve the booster response characteristic of motor, taken into account the boost demand under low engine speed and the high speed operating mode simultaneously.The type variable cross section composite turbine device can adopt the casting and the processing technique of existing common pressurized machine to finish.
In the foregoing description, spiral case gas outlet 24 can also be made packaged type, motor is under low flow rate condition, by regulating the axial position of spiral case gas outlet 24, satisfy the negotiability of radial-flow turbine, realize and the matched well of motor under low flow rate condition.
Embodiment 2: as shown in Figure 6, for the reasonable use pulse energy, can also in axial flow runner 11 and runoff runner 12 dividing plate 28 be installed respectively on embodiment 1 basis, axial flow runner 11 and runoff runner 12 respectively are divided into two runners.
Dividing plate 28 is cast as one with double flow channel spiral case 10.Respectively be installed into air valve in four runner imports that are divided into by dividing plate 28, the switching of controlling each air intake valve by the air intake valve control mechanism comes reasonable use waste gas pulse energy.
Adopting after this kind technological scheme can better utilization waste gas pulse energy, Pulse wave is propagated in less space, pulse energy reduces, improve the efficient of turbine, improve the problem of motor supercharging deficiency when low speed to a certain extent, can effectively take into account the negotiability of big flow operating mode turbine and the efficient of raising turbine simultaneously.
Embodiment 3, as shown in Figure 7, for the reasonable use pulse energy, can also be on embodiment 1 basis, dividing plate 28 only is installed in runoff runner 12, and dividing plate 28 is divided into two runners with runoff runner 12, forms three air inlet runners with axial flow runner 11, three air inlet runners at the double flow channel spiral case respectively are installed into air valve, the performance requirement when each operating mode of motor is satisfied in the switching of controlling each air intake valve by the air intake valve control mechanism.
Under low flow rate condition, after runoff runner 12 is installed dividing plate 28, can effectively utilize the waste gas pulse energy, improve the efficient of turbine, improve the problem of low engine speed supercharging deficiency.
Under the big flow operating mode, the range of flow broad of axial flow turbine, efficient is higher, can satisfy the turbine negotiability of motor under big flow operating mode.And compare with present embodiment 2, adopt an air intake valve control mechanism less, the composite turbine apparatus structure is become simple, operate easier realization at the axial flow runner.
Embodiment 4: as shown in Figure 8, can also be on embodiment 2 basis, guide-ring 29 is installed in spiral case nozzle 5 positions at axial flow runner 11, and guide-ring 29 tilts to one-level turbine wheel 14 sense of rotation, is blown into one-level turbine wheel 14 to guarantee air-flow direction according to the rules.Adopt and to improve motor utilization to the exhaust energy of axial flow runner 11 when high speed after this kind technological scheme, improved turbine efficiency, satisfy the requirement of the big flow operating mode of motor.
Embodiment 5: can also be on embodiment 3 basis, as shown in Figure 9, guide-ring 29 is installed in spiral case nozzle 5 positions at axial flow runner 11, and guide-ring 29 tilts to one-level turbine wheel 14 sense of rotation, is blown into one-level turbine wheel 14 to guarantee air-flow direction according to the rules.
Adopt and to improve motor utilization to the exhaust energy of axial flow runner 11 when high speed after this kind technological scheme, improved turbine efficiency, satisfy the requirement of the big flow operating mode of motor.
Embodiment 6: as shown in Figure 10, can also be on embodiment 4 basis, one-level turbine wheel 14 and two-stage turbine impeller 15 are designed to independent two-part, do not connect together, be provided with certain clearance between two impellers, the position corresponding with this gap is provided with the cavity of annular on midfeather 16, and all stator blades 30 of evenly installing in the cavity of annular are in the gap of described stator blade 30 between one-level turbine wheel 14 and two-stage turbine impeller 15.
Under the big flow operating mode of motor, minimizing flows into two-stage turbine impeller 15 to the gas of one-level turbine wheel 14 actings, under the motor low flow rate condition, minimizing flows into one-level turbine wheel 14 to the gas of two-stage turbine impeller 15 actings, reduce the mobile upset of air-flow in the impeller to a certain extent, reduce the energy loss of gas in the impeller.
Embodiment 7: as shown in Figure 11, can also be on embodiment 5 basis, one-level turbine wheel 14 and two-stage turbine impeller 15 are designed to independent two-part, do not connect together, be provided with certain clearance between two impellers, the position corresponding with this gap is provided with the cavity of annular on midfeather 16, and all stator blades 30 of evenly installing in the cavity of annular are in the gap of described stator blade 30 between one-level turbine wheel 14 and two-stage turbine impeller 15.
Under the big flow operating mode of motor, minimizing flows into two-stage turbine impeller 15 to the gas of one-level turbine wheel 14 actings, under the motor low flow rate condition, minimizing flows into one-level turbine wheel 14 to the gas of two-stage turbine impeller 15 actings, reduce the mobile upset of air-flow in the impeller to a certain extent, reduce the energy loss of gas in the impeller.
Patent of the present invention is at the demand of motor to variable-area turbocharger, finished the exploitation of variable cross section composite turbine device, adopt the compound mode of two-stage turbine, turbine efficiency when having improved low engine speed, and the low speed torque and the output power of motor have been improved, improve the booster response characteristic of motor, taken into account the boost demand under low engine speed and the high speed operating mode simultaneously.The type variable cross section composite turbine device can adopt the casting and the processing technique of existing common pressurized machine to finish.
We have been described in detail invention according to the national patent method now, can discern the improvement or the replacement of specific embodiment disclosed herein for those skilled in the art.These modifications are within the spirit and scope of the present invention.
Claims (10)
1. a variable cross section diameter of axle flows the composite turbocharging device, comprise double flow channel spiral case (10), double flow channel spiral case (10) is provided with axial flow runner (11) and runoff runner (12), be respectively equipped with the spiral case nozzle (5) that is communicated with spiral case gas outlet (24) on described axial flow runner (11) and the runoff runner (12), it is characterized in that: the position that described double flow channel spiral case (10) is gone up near the spiral case nozzle (5) of runoff runner (12) is provided with chute, be provided with slidably mobile aditus laryngis baffle plate (17) in chute, mobile aditus laryngis baffle plate (17) is connected with mobile aditus laryngis baffle plate control mechanism.
2. variable cross section diameter of axle stream composite turbocharging device according to claim 1, it is characterized in that: described runoff runner (12) is positioned at the side near spiral case gas outlet (24), axial flow runner (11) is positioned at the side away from spiral case gas outlet (24), is provided with midfeather (16) between described runoff runner (12) and the axial flow runner (11).
3. variable cross section diameter of axle stream composite turbocharging device according to claim 2, it is characterized in that: described mobile aditus laryngis baffle plate control mechanism comprises final controlling element (18), outer cover at spiral case gas outlet (24) is connected to shift fork ring (21), described mobile aditus laryngis baffle plate (17) is fixedlyed connected with shift fork ring (21), final controlling element push rod (19) is installed on the described final controlling element (18), is connected with shift fork (20) between final controlling element push rod (19) and the shift fork ring (21).
4. variable cross section diameter of axle stream composite turbocharging device according to claim 3, it is characterized in that: be provided with composite turbine impeller (13) in the double flow channel spiral case (10), described composite turbine impeller (13) comprises one-level turbine wheel (14) and two-stage turbine impeller (15).
5. variable cross section diameter of axle stream composite turbocharging device according to claim 4, it is characterized in that: described one-level turbine wheel (14) is made up of prismatic blade, two-stage turbine impeller (15) by turbine entad blade form, one-level turbine wheel (14) matches with axial flow runner (11), and two-stage turbine impeller (15) matches with runoff runner (12).
6. variable cross section diameter of axle stream composite turbocharging device according to claim 5, it is characterized in that: dividing plate (28) is installed in the described runoff runner (12), dividing plate (28) is divided into two runners with runoff runner (12), forms three air inlet runners with axial flow runner (11).
7. variable cross section diameter of axle stream composite turbocharging device according to claim 5, it is characterized in that: in axial flow runner (11) and runoff runner (12), dividing plate (28) is installed respectively, axial flow runner (11) and runoff runner (12) respectively are divided into two runners.
8. variable cross section diameter of axle stream composite turbocharging device according to claim 5, it is characterized in that: guide-ring (29) is installed in spiral case nozzle (5) position at axial flow runner (11), and guide-ring (29) tilts to one-level turbine wheel (14) sense of rotation.
9. according to claim 6 or 7 one of them described variable cross section diameter of axle stream composite turbocharging device, it is characterized in that: guide-ring (29) is installed in spiral case nozzle (5) position at axial flow runner (11), and guide-ring (29) tilts to one-level turbine wheel (14) sense of rotation.
10. variable cross section diameter of axle stream composite turbocharging device according to claim 9, it is characterized in that: described one-level turbine wheel (14) is provided with at interval with two-stage turbine impeller (15), has the gap between the two, go up the cavity that the position corresponding with this gap is provided with annular at midfeather (16), one all stator blades (30) evenly are installed in the cavity of annular, and described stator blade (30) is positioned between one-level turbine wheel (14) and the two-stage turbine impeller (15).
Priority Applications (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201110005183.2A CN102080578B (en) | 2011-01-12 | 2011-01-12 | Compound turbo supercharging device having variable cross-section axial radial flows |
| PCT/CN2011/000459 WO2012094781A1 (en) | 2011-01-12 | 2011-03-23 | Axial-radial-flow composite turbocharger with a variable section |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201110005183.2A CN102080578B (en) | 2011-01-12 | 2011-01-12 | Compound turbo supercharging device having variable cross-section axial radial flows |
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| Publication Number | Publication Date |
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| CN102080578A true CN102080578A (en) | 2011-06-01 |
| CN102080578B CN102080578B (en) | 2014-07-30 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201110005183.2A Active CN102080578B (en) | 2011-01-12 | 2011-01-12 | Compound turbo supercharging device having variable cross-section axial radial flows |
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| Country | Link |
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| CN (1) | CN102080578B (en) |
| WO (1) | WO2012094781A1 (en) |
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| CN102661180A (en) * | 2012-05-07 | 2012-09-12 | 康跃科技股份有限公司 | Dual-zone turbine for turbocharging |
| CN103266949A (en) * | 2013-05-16 | 2013-08-28 | 湖南天雁机械有限责任公司 | Turbocharger capable of changing flowing channel through lever braking |
| CN107100719A (en) * | 2017-04-27 | 2017-08-29 | 同济大学 | A kind of turbocharger in axially variable section |
| CN108894858A (en) * | 2018-06-21 | 2018-11-27 | 浙江吉利控股集团有限公司 | The ternary catalystic device structure of integrated heat-insulation window |
| CN109154229A (en) * | 2016-05-12 | 2019-01-04 | 大陆汽车有限公司 | The turbine with double volute turbine cylinder and with the valve gear for improving outflow for exhaust-driven turbo-charger exhaust-gas turbo charger |
| CN110735673A (en) * | 2019-11-18 | 2020-01-31 | 大连海事大学 | kinds of double-channel volute |
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| US10662904B2 (en) | 2018-03-30 | 2020-05-26 | Deere & Company | Exhaust manifold |
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| CN103266949A (en) * | 2013-05-16 | 2013-08-28 | 湖南天雁机械有限责任公司 | Turbocharger capable of changing flowing channel through lever braking |
| CN103266949B (en) * | 2013-05-16 | 2018-06-15 | 湖南天雁机械有限责任公司 | Turbocharger with lever braking flow-passage-changeable |
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| CN107100719A (en) * | 2017-04-27 | 2017-08-29 | 同济大学 | A kind of turbocharger in axially variable section |
| CN108894858A (en) * | 2018-06-21 | 2018-11-27 | 浙江吉利控股集团有限公司 | The ternary catalystic device structure of integrated heat-insulation window |
| CN110735673A (en) * | 2019-11-18 | 2020-01-31 | 大连海事大学 | kinds of double-channel volute |
| CN112576317A (en) * | 2020-12-08 | 2021-03-30 | 康锰 | Permanent magnet transmission low-temperature multistage turbine generator |
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|---|---|
| WO2012094781A1 (en) | 2012-07-19 |
| CN102080578B (en) | 2014-07-30 |
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Effective date of registration: 20210125 Address after: No.1 luoqian street, Gucheng street, Shouguang City, Weifang City, Shandong Province Patentee after: Kangyue Technology (Shandong) Co.,Ltd. Address before: No.01 luoqian street, Shouguang Economic Development Zone, Shandong Province 262700 Patentee before: KANGYUE TECHNOLOGY Co.,Ltd. |
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Denomination of invention: Variable cross-section axial runoff composite turbocharger Effective date of registration: 20220701 Granted publication date: 20140730 Pledgee: Shandong Shouguang Rural Commercial Bank Co.,Ltd. Pledgor: Kangyue Technology (Shandong) Co.,Ltd. Registration number: Y2022980009719 |