CN203867702U - Turbine air intake supercharger of axial-flow type aerodynamic internal combustion engine - Google Patents

Turbine air intake supercharger of axial-flow type aerodynamic internal combustion engine Download PDF

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Publication number
CN203867702U
CN203867702U CN201420028517.7U CN201420028517U CN203867702U CN 203867702 U CN203867702 U CN 203867702U CN 201420028517 U CN201420028517 U CN 201420028517U CN 203867702 U CN203867702 U CN 203867702U
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China
Prior art keywords
turbine air
air intake
combustion engine
rotating shaft
axial
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Expired - Fee Related
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CN201420028517.7U
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Chinese (zh)
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许俊成
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Individual
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Individual
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    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00Road transport of goods or passengers
    • Y02T10/10Internal combustion engine [ICE] based vehicles
    • Y02T10/12Improving ICE efficiencies

Abstract

The utility model discloses a turbine air intake supercharger of an axial-flow type aerodynamic internal combustion engine. The turbine air intake supercharger of the axial-flow type aerodynamic internal combustion engine comprises a diffusion cylinder, impellers, a rotating shaft and two bearings. A bearing seat is arranged in the middle of the diffusion cylinder. The rotating shaft penetrates through the bearing seat. The two bearings are installed on the two sides of the bearing seat respectively and are fixed through clamp springs. Impellers are installed at the two ends of the rotating shaft. The impellers are left-handed impellers or right-handed impellers. According to the turbine air intake supercharger, the structure is simple, the number of assemblies is small, turbine air intake supercharging can be conducted on an automobile engine without the help of external power, the turbine air intake supercharger can be directly and additionally arranged in an air intake pipe connected between a throttle valve of the automobile engine and an air filter, parts are made of ordinary materials, the durability and the safety reliability are high, and the problem that existing turbine air intake superchargers cannot be applied to old automobiles or be popularized among the old automobiles can be solved.

Description

Axial flow aerodynamic force internal-combustion engine turbine air-admission pressure-booster
Technical field
The utility model belongs to internal combustion engine turbocharging technical field, relate in particular to a kind of without by external impetus, the structure that do not change automobile just can combustion motor realizes the pressurized machine of turbine air intake pressurized.
Background technique
At present, the turbosupercharger that motor car engine is used is both at home and abroad divided into two kinds substantially, comprises and need to consume external energy and not need to consume two kinds of external energies.The pressurized machine that need to consume external energy has mechanical type and electrodynamic type: mechanical turbine pressurized machine obtains power from engine output shaft, complex structure, and volume is larger, and price is high; Electric turbocharger is with the electric drive pressurized machine motor work of automobile itself, and working life is partially short.Do not need the pressurized machine that consumes external energy taking exhaust-gas turbocharger as main representative.Exhaust-gas turbocharger is taking the waste gas of motor discharge as power, and distinct disadvantage is response lag, and the floating axle that connects exhaust driven gas turbine and the air inlet turbine easy axis of at high temperature working; In addition, the design accuracy of exhaust gas turbine requires high, complex manufacturing technology, volume larger.In order to make up the defect of exhaust gas turbocharge, composite turbocharging system had both adopted exhaust-gas turbocharger, and while application machine drive-type turbosupercharger overcomes the retardation phenomenon of exhaust-gas turbocharger again, but manufacture cost and maintenance expenses are higher.
Above-mentioned turbosupercharger also has a common problem, while using above-mentioned turbosupercharger to reequip the old motor car engine of having dispatched from the factory, need to carry out some transformations to automobile local location structure or circuit etc., therefore these turbosupercharger, except new car prepackage, are promoted not by most of car owners are accepted by repacking.
How not change under the condition of vehicle structure, can make some old vehicle motors obtain a kind of axial flow aerodynamic turbine of turbo charged effect pressurized machine to have solved preferably the deficiency of above-mentioned turbosupercharger.Aerodynamic turbine pressurized machine does not need to consume external energy, only just can realize the high-speed rotary of turbine blade by the air-breathing power of internal-combustion engine then reach the object of supercharging, turbo charged effect just can play a role in the time that engine speed 1200 turns, to meet the demand of urban district low speed driving, and apparatus structure is simple, install additional conveniently, cost is low.
Summary of the invention
The utility model provides a kind of bilobed wheel axial flow aerodynamic turbine air-admission pressure-booster in order to solve deficiency of the prior art, simple in structure, assembly is few, without just realizing turbine air intake pressurized to motor car engine by external impetus, can directly be installed in the suction tude that motor car engine closure is connected with air filter, its Component material is common, there is good durability and safety reliability, not only can overcome the defect in above-mentioned background technology, and can solve turbine air intake pressurized apparatus and on old automobile, carry out popularization and application problem.
For achieving the above object, the technical solution adopted in the utility model is:
Axial flow aerodynamic force internal-combustion engine turbine air-admission pressure-booster, comprises diffusion barrel, impeller, rotating shaft, bearing, and described diffusion barrel middle part arranges bearing support; Described rotating shaft through bearing support and in bearing support both sides each bearing of installing, and fix with jump ring; Impeller is installed at rotating shaft two ends, and described impeller is all levoform or right-spiral, and single pressurized machine adopts bilobed wheel structural design, can ensure that impeller is in the lower maintenance balance that works long hours, and bilobed wheel can also ensure good continous blowing.The blade of turbine adopts not combination in the same way.In the time that motor car engine is moved, air-flow in suction tude promotes the first order blade radial part of turbine, when making blade rotary, again along sharf to the radial component that forms rotation forced air promotion second level blade, also can multiple pressurized machine series connection use, the forced air that can make the to rotate thrust that superposeed is again removed the first order blade of the pressurized machine that promotes next series connection, so analogizes.
As a kind of preferred version of axial flow aerodynamic force internal-combustion engine turbine air-admission pressure-booster described in the utility model, described rotating shaft end adopts interference fit to be connected with impeller, roller end is provided with the groove of wedge structure, thus the problem that gets loose of screw rod and screw while having solved turbine High Rotation Speed.Screw rod screw structural can produce screw and gets loose and fall in the cylinder of motor car engine in the time of High Rotation Speed, causes the damage of motor car engine, thereby causes traffic accident and human casualty accident.
As a kind of preferred version of axial flow aerodynamic force internal-combustion engine turbine air-admission pressure-booster described in the utility model, described impeller adopts axial flow structural design, axial dimension and radial dimension 1: 2-3, the angle of inclination of blade axial component and radial component design, can be consistent in the time installing in opposite directions, it has ensured that blade reduces radially windage energy loss in the time of High Rotation Speed, and obtains better pressurized effect, and pressurized machine turnover airflow direction can be mutually general.
As a kind of preferred version of axial flow aerodynamic force internal-combustion engine turbine air-admission pressure-booster described in the utility model, described bearing support is connected by the uniform some supports of angle intervals with diffusion barrel inwall, preferably be made up of three supports that are mutually 120 °, support is connected bearing support with diffusion barrel inwall.
As a kind of preferred version of axial flow aerodynamic force internal-combustion engine turbine air-admission pressure-booster described in the utility model, described support is provided with is convenient to the breach that swirling eddy passes through, reduce bearing support fixed support stopping and decaying rotation forced air, rotation forced air can be linked up and pass through smoothly, finally improve the delivery efficiency of pressurized machine.
Pressurized machine is arranged in the pipeline between air filter of automobile and closure, and shell sizes and the caliber of pressurized machine match.In order further to improve pressurized effect, under the condition allowing in pipe diameter length, can be installed in series two and above pressurized machine, plural serial stage is installed and not limited by pressurized machine direction.Generally, plural serial stage pressurized effect is better than single pressurized machine,
Beneficial effect:
Axial flow aerodynamic force internal-combustion engine turbine air-admission pressure-booster described in the utility model, there is processing and fabricating easy, stable and reliable for performance, the advantage that effect is high, be applicable to the installation of all motor car engines in suction tude, and the spiral air flow that can effectively form high speed and high pressure enters cylinder oil, gas is produced to powerful agitaion.Make the mixed gas of oil, gas more easily mix abundant atomization (refinement fuel molecule), start with from the mechanism of combustion of fuel oil, make fuel oil in cylinder, accelerate velocity of combustion, improve the thermal efficiency, fuel oil is fully and completely burnt totally, reduce the discharge of tail gas harmful substance, reduce carbon distribution increasing service life of engine, allow same fuel oil break into larger strength, promote engine performance, reach the effect of energy-saving and emission-reduction.The utility model can allow the under equal conditions fuel-economizing 5%~20% of automobile in normal use, power-lift 10%~30%, and toxic emission reduces by 30%, and cost is but 1% of exhaust gas turbine, and application prospect is very wide.
Brief description of the drawings
Fig. 1 is axial flow aerodynamic force internal-combustion engine turbine air-admission pressure-booster STRUCTURE DECOMPOSITION schematic diagram described in the utility model (not containing diffusion barrel).
Fig. 2 is axial flow aerodynamic force internal-combustion engine turbine air-admission pressure-booster assembled state generalized section described in the utility model.
Fig. 3 is axial flow aerodynamic force internal-combustion engine turbine air-admission pressure-booster diffusion barrel structural representation described in the utility model.
Wherein: 1, diffusion barrel 2, impeller 3, rotating shaft 4, bearing 5, jump ring 6, support
Embodiment
Below in conjunction with the drawings and specific embodiments, the utility model is described in further detail.
Embodiment 1
As shown in the figure, axial flow aerodynamic force internal-combustion engine turbine air-admission pressure-booster, comprises diffusion barrel 1, impeller 2, rotating shaft 3, bearing 4, and diffusion barrel 1 middle part arranges bearing support, and bearing support is connected with diffusion barrel by three supports 6 that are mutually 120 °.A bearing 4 is respectively installed in rotating shaft 3 through bearing support and in bearing support both sides, corresponding two draw-in grooves that distribute in rotating shaft 3, and jump ring 5 is arranged in draw-in groove, fixes with the relative position of rotating shaft 3 for limiting bearing 4.Rotating shaft two ends are provided with wedge groove structure, impeller 2 is compressed into rotating shaft and allow them become one, and the working state while making to rotate is more stable, can avoid impeller 2 contingent phenomenon that gets loose in High Rotation Speed process.Described impeller is levoform or right-spiral, and impeller adopts axial flow structural design, axial dimension and radial dimension 1: 2-3.Support 6 is provided with is convenient to the breach that swirling eddy passes through, and has reduced bearing support fixed support to rotating stopping and decaying of forced air, rotation forced air can be linked up and pass through smoothly, finally improves the delivery efficiency of pressurized machine.
Although mode of execution of the present utility model is illustrated in specification, these mode of executions just, as prompting, should not limit protection domain of the present utility model.In the scope that does not depart from the utility model aim, carrying out various omissions, displacement and change all should be included in protection domain of the present utility model.

Claims (5)

1. axial flow aerodynamic force internal-combustion engine turbine air-admission pressure-booster, comprise diffusion barrel (1), impeller (2), rotating shaft (3), bearing (4), it is characterized in that: described diffusion barrel (1) middle part arranges bearing support; A bearing (4) is respectively installed in described rotating shaft through bearing support and in bearing support both sides, and fixing with jump ring (5); Impeller is installed at rotating shaft (3) two ends, and described impeller is levoform or right-spiral.
2. axial flow aerodynamic force internal-combustion engine turbine air-admission pressure-booster according to claim 1, is characterized in that: described rotating shaft (3) end adopts interference fit to be connected with impeller (2).
3. axial flow aerodynamic force internal-combustion engine turbine air-admission pressure-booster according to claim 1, is characterized in that: described impeller (2) axial dimension and radial dimension 1: 2-3.
4. axial flow aerodynamic force internal-combustion engine turbine air-admission pressure-booster according to claim 1, is characterized in that: described bearing support is connected by the uniform some supports of angle intervals (6) with diffusion barrel (1) inwall.
5. axial flow aerodynamic force internal-combustion engine turbine air-admission pressure-booster according to claim 4, is characterized in that: described support (6) is provided with is convenient to the breach that swirling eddy passes through.
CN201420028517.7U 2014-01-17 2014-01-17 Turbine air intake supercharger of axial-flow type aerodynamic internal combustion engine Expired - Fee Related CN203867702U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201420028517.7U CN203867702U (en) 2014-01-17 2014-01-17 Turbine air intake supercharger of axial-flow type aerodynamic internal combustion engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201420028517.7U CN203867702U (en) 2014-01-17 2014-01-17 Turbine air intake supercharger of axial-flow type aerodynamic internal combustion engine

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CN203867702U true CN203867702U (en) 2014-10-08

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Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105986882A (en) * 2015-02-13 2016-10-05 陈瑞峰 Eddy turbocharging power system
CN109915262A (en) * 2017-12-12 2019-06-21 中电科特种飞机系统工程有限公司 A kind of aero-engine and its wind power boosting device
CN110030035A (en) * 2018-01-11 2019-07-19 长兴永能动力科技有限公司 The centripetal turbine that a kind of bilobed wheel is vented back to arrangement and respectively
CN115370466A (en) * 2021-05-20 2022-11-22 许俊成 Ozone generator and turbocharger combined oil saving device

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105986882A (en) * 2015-02-13 2016-10-05 陈瑞峰 Eddy turbocharging power system
CN109915262A (en) * 2017-12-12 2019-06-21 中电科特种飞机系统工程有限公司 A kind of aero-engine and its wind power boosting device
CN110030035A (en) * 2018-01-11 2019-07-19 长兴永能动力科技有限公司 The centripetal turbine that a kind of bilobed wheel is vented back to arrangement and respectively
CN115370466A (en) * 2021-05-20 2022-11-22 许俊成 Ozone generator and turbocharger combined oil saving device

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GR01 Patent grant
CF01 Termination of patent right due to non-payment of annual fee
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20141008

Termination date: 20190117