CN202732101U - Axial-flow type aerodynamic internal-combustion engine air inflow supercharger with arbitrarily combined air compression stage number - Google Patents

Axial-flow type aerodynamic internal-combustion engine air inflow supercharger with arbitrarily combined air compression stage number Download PDF

Info

Publication number
CN202732101U
CN202732101U CN201220312607XU CN201220312607U CN202732101U CN 202732101 U CN202732101 U CN 202732101U CN 201220312607X U CN201220312607X U CN 201220312607XU CN 201220312607 U CN201220312607 U CN 201220312607U CN 202732101 U CN202732101 U CN 202732101U
Authority
CN
China
Prior art keywords
combustion engine
internal
supercharger
axial
arbitrarily combined
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Fee Related
Application number
CN201220312607XU
Other languages
Chinese (zh)
Inventor
许俊成
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Priority to CN201220312607XU priority Critical patent/CN202732101U/en
Application granted granted Critical
Publication of CN202732101U publication Critical patent/CN202732101U/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Images

Classifications

    • 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

Landscapes

  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Supercharger (AREA)

Abstract

The utility model discloses an axial-flow type aerodynamic internal-combustion engine air inflow supercharger with an arbitrarily combined air compression stage number, comprising a diffuser barrel (1), a connecting shaft impeller (2), a bearing (3), an M6 lead screw (4), a retaining washer (5) and a silicon gel sealing ring (6). The axial-flow type aerodynamic internal-combustion engine air inflow supercharger with the arbitrarily combined air compression stage number is simple in structure and composed of only 8 parts; during working, each stage is capable of feeding spiral air energy to the previous stage; a plurality of stages connected in series are capable of effectively forming a high-speed, high-pressure spiral air flow, thereby generating strong stirring action; as a result, the combustible mixed gas is thoroughly mixed, the flame wavefront range is increased, the combustion speed is increased, the thermal efficiency is improved, and the effects of promoting power, saving energy and reducing emission can be achieved; more specifically, the actually measured fuel saving ratio according to different vehicle models can be 5%-15%. The axial-flow type aerodynamic internal-combustion engine air inflow supercharger with the arbitrarily combined air compression stage number is suitable for various combustible oil, gas internal-combustion engines, especially for old internal-combustion engines low in efficiency, and is one of the optimal settlement methods for developing the originally designed rated maximal power of the engines, and simultaneously, solves the popularization and application of the internal-combustion engine air inflow supercharger too.

Description

The calm the anger air-intake of combustion engine pressurized machine of progression of axial flow aerodynamic force combination in any
Technical field
The utility model belongs to the pressurized machine technical field, especially relates to the calm the anger air-intake of combustion engine pressurized machine of progression of a kind of axial flow aerodynamic force combination in any.
Background technique
Along with the development of technology, the requirement of people's combustion motor is also more and more harsher, not only will have powerful power, also must have high efficient and the discharging of clean enough.This just requires internal-combustion engine can both reach its most efficient working state under various operating modes, therefore just must satisfy internal-combustion engine demand for air inflow under each working state.This just requires each parts of internal-combustion engine to satisfy condition under different operating modes by " variable ".Such as Variable Valve Timing that we were familiar with, variable cross section turbocharging technology, variable intake manifold technology etc.
Existing internal-combustion engine generally adopts traditional natural aspiration mode, deficiency of air, fuel atomization and incomplete combustion, the tail gas severe contamination of discharge environment.How improving the efficient of internal-combustion engine and the discharging of minimizing tail gas is that pendulum is in the problem of auto industry field.
Summary of the invention
The utility model namely is for the problems referred to above, provide a kind of structure simple especially, the calm the anger pressurized machine of progression of the axial flow aerodynamic force combination in any of only having 8 Component to form, thereby its Component material is common to have preferably durability and reliability and has eliminated defective in the above-mentioned background technology, has solved the popularization and application problem of supercharger arrangement.
The calm the anger air-intake of combustion engine pressurized machine of progression of axial flow aerodynamic force combination in any, comprise diffusion barrel (1), connecting shaft impeller (2), bearing (3), M6 screw mandrel (4), floor clip (5), silica gel sealing ring (6), at diffusion barrel one end internal thread silk mouth is set, at the diffusion barrel the other end body external thread wire mouth and seal groove are set, on the connecting shaft impeller, impeller and axle are arranged to one, and each blade structure of axial flow turbine leaf is comprised of blade radial part and blade axial component.
When internal combustion engine operation, enter the air push first order blade radial part of suction port, when making blade rotary, again along sharf to the radial component that forms rotation forced air promotion second level blade, can make the rotating forced air thrust that superposeed again remove subordinate's turbine blade of promoting to intend combining, so analogize, make the device outlet end be input to air in the induction system of internal combustion engine, be not only greater than atmospheric pressure and be again the air-flow of High Rotation Speed. effectively improved the combustion performance of internal-combustion engine.When internal-combustion engine rotational speed strengthened or reduces, the variation of air pressure value can make the rotating speed of Multistage Axial Flow Turbines flabellum also will or reduce along with increase.
Electric turbine is the lifting power of dynamics greatly, exactly because but like this, the infringement of combustion motor is very large, a large amount of kinetic energy of its generation need to consume combustion engine powered, if the discharge capacity of internal-combustion engine own is low, can't consume the kinetic energy of its generation, this combustion motor is to have increased load, can produce potential impact.Secondly the cost long-life of electric turbocharger is short.
Exhaust gas turbine can be extraordinary lifting power, but the design accuracy of turbine height, complex manufacturing technology, bulky heaviness, price is high.The problem that exhaust gas turbine exists is that the power of driving turbine rotation is the high-temp waste gas (about 700 ℃) that internal-combustion engine is discharged, turbine and floating axle must use the high duty alloy material for this reason, the floating axle very easily axis of at high temperature working, this axis fault remains unsurmountable fault so far.
Because the internal-combustion engine natural inflow is subjected to the constraint of factors, general air inflow can only reach 65~90% of designing institute needs, and therefore internal-combustion engine also can only send 65~90% of former design power under the natural inflow state.Use the burning that has improved mixed gas behind this device, improve fuel economy and reduced the discharge amount of exhaust pollutant, therefore internal-combustion engine can send the peak output that former designing institute is demarcated.Simultaneously, it has the unexistent uniqueness of other turbosupercharger " high-speed screw air inlet function " to reach the special effect of " art is good for strength ".
Modern Internal-Combustion Engine is in order to improve natural inflow efficient, adopted many new technologies. such as " improving compression ratio; many valves; variable air inlet length suction tude; spiral hole suction tude, high flow capacity air filtering core, secondary air-in device " etc., but under present technical specifications, the utility model is unique device that can make internal-combustion engine increase output power in the constant situation of machinery, circuit, discharge capacity and operating mode.And to dispatch from the factory with in the old internal-combustion engine of inefficiency, the utility model may be to allow internal-combustion engine send one of best solution that former design demarcates peak output.
Compare with other turbosupercharger and the utlity model has that (only being made of 8 Component) simple in structure, easy to manufacture, cost lowly are convenient to popularize, long service life, advantage that cost performance is high.Be applicable to use various types of internal-combustion engines such as gasoline, diesel oil, ethanol petrol, rock gas.Every one-level can both be to prime conveying screw wind energy during work, and the plural serial stage combination just can be satisfied the demand of various internal-combustion engines, has solved the popularization and application problem of supercharger arrangement.
Specifically, the calm the anger air-intake of combustion engine pressurized machine of progression of axial flow aerodynamic force combination in any described in the utility model, it is characterized in that: described pressurized machine comprises diffusion barrel, connecting shaft impeller, bearing, floor clip, M6 screw mandrel, silica gel sealing ring, and structure and the position relationship of each several part are as described below:
1, the cylinder type diffusion barrel is tubular structure, and the mouth of an end has designed internal thread silk mouth in the cylinder type diffusion barrel, and the other end body has designed external thread wire mouth and seal groove outside the cylinder type diffusion barrel.Designed the bearing support of the one that links to each other with barrel at the middle part of diffusion barrel;
2, the connecting shaft impeller is positioned at diffusion barrel inside, and the axle head of connecting shaft impeller inserts the bearing in the bearing support, and the shaft end of connecting shaft impeller has axial mesopore, is provided with the M6 internal thread in the hole;
3, the axle head of two connecting shaft impellers inserts the bearing in the bearing support in the diffusion barrel in opposite directions, adds floor clip with the M6 screw mandrel and is rotatably connected fixingly, makes the table top of connecting shaft impeller underpart compress bearing inner race.
4, silica gel sealing ring is embedded in when being connected in the seal groove of diffusion barrel.
The calm the anger air-intake of combustion engine pressurized machine of progression of axial flow aerodynamic force combination in any described in the utility model,
Have following advantage:
1., simple in structure, easy for installation:
2., floor clip is the axle head of two connecting shaft impellers location, avoided impeller contingent phenomenon that gets loose in the process of High Rotation Speed;
3., the designed interior external sealing plug in diffusion barrel two ends is convenient to combination in any.
4., on the connecting shaft impeller, impeller and axle are designed to one, the working state in the time of making rotation is more stable.
Description of drawings
Fig. 1 is the utility model embodiment's diffusion barrel, connecting shaft impeller, bearing, floor clip, M6 screw mandrel, the dual impeller structural profile schematic representation of silica gel sealing ring;
Fig. 2 is the utility model embodiment's diffusion barrel, connecting shaft impeller, bearing, floor clip, M6 screw mandrel, the single impeller type structural profile schematic representation of silica gel sealing ring;
Fig. 3 is the utility model embodiment's bilobed wheel composite structure generalized section;
Fig. 4 is the utility model embodiment's single, double impeller combination structural profile schematic representation;
Wherein, 1 is that diffusion barrel, 2 is that connecting shaft impeller, 3 is that bearing, 4 is that M6 screw mandrel, 5 is that floor clip, 6 is silica gel sealing ring.
Embodiment
Below in conjunction with accompanying drawing; the calm the anger air-intake of combustion engine pressurized machine of progression of axial flow aerodynamic force combination in any described in the utility model is described; purpose is better to understand technology contents described in the utility model for the public; rather than to the restriction of described technology contents; in fact; in invention Spirit Essence of the present utility model, to structure, the element of described pressurized machine, comprise that the combination that realizes various patterns is all within the utility model technological scheme required for protection.
The air-intake of combustion engine pressurized machine of the variable progression of calming the anger of combination in any described in the utility model, comprise diffusion barrel, connecting shaft impeller, bearing, floor clip, M6 screw mandrel, silica gel sealing ring, wherein, as shown in Figure 1, connecting shaft impeller 2 is positioned at diffusion barrel 1 inside, be screwed into M6 screw mandrel 4 from the axle head screw of connecting shaft impeller 2, and put floor clip 5, insert the inner ring of the bearing 3 the bearing support of the one that links to each other with the diffusion barrel from an end of diffusion barrel.The axle head of another connecting shaft impeller 2, insert the inner ring of another bearing 3 the bearing support of the one that links to each other with the diffusion barrel from the other end of diffusion barrel, and aim at M6 screw mandrel 4 with the M6 screw of axle head, two connecting shaft impellers of rotation flatten floor clip 5 relatively, the table top of connecting shaft impeller shaft end compresses bearing 3 inner rings simultaneously, when needs are used in combination silica gel sealing ring 6 is enclosed within the seal groove of diffusion barrel 1.
Preferably, at first describedly designed internal thread silk mouth at diffusion barrel one end, external thread wire mouth and seal groove have been designed at diffusion barrel the other end body, but his odevity impeller combination in any secondly, have because particular design and this device of mounting type inlets and putlets of ventilation of axial-flow blower are positive and negative mutually general, this has brought greatest convenience to the user again.
The calm the anger air-intake of combustion engine pressurized machine of progression of axial flow aerodynamic force combination in any described in the utility model, it is easy to have processing and fabricating, the reliable advantage of function-stable, the spiral air flow that can effectively form high speed and high pressure produces powerful agitaion, make that mixed gas is easier and mix (well-known, the wind-force of typhoon and tornado is all very large, but the collapsing force of tornado is far longer than typhoon, its main difference is exactly that tornado rotates), increase the scope of flame wavefront, accelerate velocity of combustion, improve the thermal efficiency, reach lifting power, the effect of energy-saving and emission-reduction, application prospect are very wide.

Claims (1)

1. the axial flow aerodynamic force combination in any air-intake of combustion engine pressurized machine of progression of calming the anger, it is characterized in that: comprise diffusion barrel (1), connecting shaft impeller (2), bearing (3), M6 screw mandrel (4), floor clip (5), silica gel sealing ring (6), at diffusion barrel one end internal thread silk mouth is set, at the diffusion barrel the other end body external thread wire mouth and seal groove are set, on the connecting shaft impeller, impeller and axle are arranged to one, and each blade structure of axial flow turbine leaf is comprised of blade radial part and blade axial component.
CN201220312607XU 2012-07-02 2012-07-02 Axial-flow type aerodynamic internal-combustion engine air inflow supercharger with arbitrarily combined air compression stage number Expired - Fee Related CN202732101U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201220312607XU CN202732101U (en) 2012-07-02 2012-07-02 Axial-flow type aerodynamic internal-combustion engine air inflow supercharger with arbitrarily combined air compression stage number

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201220312607XU CN202732101U (en) 2012-07-02 2012-07-02 Axial-flow type aerodynamic internal-combustion engine air inflow supercharger with arbitrarily combined air compression stage number

Publications (1)

Publication Number Publication Date
CN202732101U true CN202732101U (en) 2013-02-13

Family

ID=47657811

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201220312607XU Expired - Fee Related CN202732101U (en) 2012-07-02 2012-07-02 Axial-flow type aerodynamic internal-combustion engine air inflow supercharger with arbitrarily combined air compression stage number

Country Status (1)

Country Link
CN (1) CN202732101U (en)

Similar Documents

Publication Publication Date Title
CN102900479B (en) Variable nozzle turbocharger regulating mechanism integrated on turbine shell
CN204692191U (en) The compressor housings of the exhaust-gas turbocharger peculiar to vessel with gas compensation function
CN201650444U (en) Turbocharger
CN105298633A (en) Adjustable type exhaust gas turbocharger
CN102828813B (en) A kind of self-priming whirlpool drum boosting energy-saving device
CN202001100U (en) Structure capable of improving engine power and reducing exhaust emission
CN202732101U (en) Axial-flow type aerodynamic internal-combustion engine air inflow supercharger with arbitrarily combined air compression stage number
CN205445778U (en) Vane type car exhaust turbine supercharging device
CN209908612U (en) Miniature gas turbine system based on turbo charger technology development
CN206299407U (en) Ventilation device in a kind of turbine box
CN102155287B (en) Structure capable of exhaust emission
CN102242645B (en) Integral variable nozzle ring of turbocharger
CN206386307U (en) Using the compressor volute of lemniscate air inlet
CN201381893Y (en) Air inlet negative pressure turbocharger of internal combustion engine
CN205936820U (en) High -efficient low emission turbo charger
CN212454961U (en) Compressor casing of exhaust gas turbocharger
CN204402644U (en) Electric turbocharger
CN103161766A (en) Air compressor of supercharged engine
CN202417694U (en) Turbocharger middle body
CN2916154Y (en) Rotary-vane type variable-cross-section turbocharger
CN2505601Y (en) Spindle shaft of core rotor of gas-turbine engine
CN213116875U (en) Turbocharger compressor brake structure with high surge margin
CN201351635Y (en) Turbocharger compressor impeller
CN101139947A (en) Vortex air supercharger
CN2603223Y (en) Cyclone natural pressure booster

Legal Events

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

Granted publication date: 20130213

Termination date: 20140702

EXPY Termination of patent right or utility model