CN2597686Y - Pressurizing device for round case pneumatic turbine - Google Patents
Pressurizing device for round case pneumatic turbine Download PDFInfo
- Publication number
- CN2597686Y CN2597686Y CNU032036787U CN03203678U CN2597686Y CN 2597686 Y CN2597686 Y CN 2597686Y CN U032036787 U CNU032036787 U CN U032036787U CN 03203678 U CN03203678 U CN 03203678U CN 2597686 Y CN2597686 Y CN 2597686Y
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- air
- turbine
- housing
- garden
- air inlet
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Abstract
The utility model relates to an air-drive turbine pressure intensifier device with round casing, which takes the air for drive. The cavity of the round casing is provided with eleven air inlets, one special air inlet and twelve air inlet guide plates inside. The turbine of the device is a radial-inward turbine with a plurality of vanes, and each vane has a radial part and an axial part. The air after filtrating by starting the engine can synchronously drive the radial part of each vane. A bundle of high speed airflow is collected to directly enter the special air inlet when the car runs, which makes the turbine during rotating repeatedly add a drive. So the outlet of the device outputs the air with the atmospheric pressure value larger than one and the rotating airflow in high speed to the air inlet system of the engine.
Description
The utility model relates to the motor car engine supercharger arrangement that a kind of air is a power, especially to the garden housing aerodynamic turbosupercharging devic 3 of engine aspirating system input greater than the high speed rotating air-flow of 1 atmospheric pressure value.
The engine booster apparatus has several, and at home and abroad Ding Xing product mainly is the exhaust-gas turbocharger device.The motor of every installation exhaust-gas turbocharger device can both increase the mean effective pressure (Pe) of motor, has improved the engine combustion performance preferably, and function is clear and definite.But the problem of existence is that the power that promotes the turbine rotation is high-temp waste gas.For this reason, the average operating temperature of hydrostatic bearing in the device and floating axle all is not less than 450 ℃, makes the easy gum deposit matter of oil channel hole of floating axle stop up oil channel hole, causes floating axle not float and axis.The durable reliability of device is poor, and the relatively advanced country of this problem world car industry so far also is the problem that is difficult to resolve.What turbine adopted is high-quality refractory steel, and blade shape complexity, technology difficulty are big, for this reason the price of import exhaust-gas turbocharger device: 3000 yuan /~6000 yuan/, and costliness.And for example: " automobile powerful economizer " of " the whirlwind economizer " of Korea S, China, and " space wheel ", the said goods is claimed and is the pressurized machine working principle of walking back and forth.Device can both increase the charging efficiency of motor in automobile is used, and can effectively improve the engine combustion performance.The problem that exists is the limiting value of effect, still can not satisfy more best performance value of motor.During supporting installation, need matching and debugging hell to pay one by one, unstable properties.The patent No.; 991155625 " aerodynamic turbosupercharging devic 3 " and the patent No.s: 022024301 " four suction port wind turbine supercharger arrangements ", the effect of device all is clear and definite.But, the problem of existence: the structural design reason, the performance of turbine acceleration, revolution preferred values is had any problem in the device; Big and the inevitable big bad solution of contradiction of housing of device air inlet; Supporting connection is complicated.
The utility model purpose provides the garden housing aerodynamic turbosupercharging devic 3 that a kind of air is a power, in housing footpath, garden portion chamber 11 suction ports is set, 1 special suction port and 12 air inlet guide plates.Turbine is the multiple-blade centripetal turbine in the device, each blade all has warp-wise in the multiple-blade, when axial component starts when motor car engine one, air after the filtration is by air guide cover before the device, back air guide cover air just enters into 11 suction ports in the device case footpath portion chamber, 1 special suction port, effect at 11 air inlet guide plates, air after the filtration can drive the radial part of each blade in the multiple-blade simultaneously, so, the turbine acceleration is big, the rotation that revolution is high, make the air after the filtration form swirling eddy in the axial flow motion device outlet plenum of each blade in the multiple-blade again, when automobile running, gather a branch of high velocity air again at Che Nei through particular filter, special suction port in the straight inletting device, make the turbine that is the rotating driving force that superposes again, so, the turbine acceleration is bigger, revolution is higher, forming high speed rotating in the device outlet plenum this moment just enters in the automotive engine air intake system for the air greater than 1 atmospheric pressure value, effectively raise the mean effective pressure value (Pe) of motor, improved the engine combustion performance, supporting connection is simple.
The utility model purpose be achieved in that since device case be designed to the garden housing, so, in housing footpath, the garden portion chamber, be easy to, be provided with uniformly 11 suction ports, 1 special suction port and 12 air inlet guide plates.The radial part that has realized each blade in the multiple-blade turbine can receive driving force simultaneously, so turbine ability acceleration is big, revolution is high in rotation.Automobile driving speed is 60 kilometers/hour, the about strong breeze speed of wind speed on the vehicle body, 100 kilometers/hour of speeds of operation, the vehicle body wind speed reaches storm speed approximately after tested, so a branch of air of gathering on the car is a high velocity air, so the turbine acceleration is bigger in the device, revolution is higher.Because device is provided with back air guide cover, supporting connection is simple especially.
Owing to adopted such scheme, not only acceleration is bigger, revolution is higher for the multiple-blade centripetal turbine in the device; The device air inflow is big, volume is little, and convenient supporting connection, so the structure of device is simple especially.
Below in conjunction with drawings and Examples the utility model is further specified.
Fig. 1 is the utility model device plan view
Fig. 2 is Figure 1A-A sectional view
In the air 5.6.7.8.9.10.11.12.13.14.15. housing footpath section chamber among the figure after 3. rear air guide cover 4. filterings of 1. front air guide cover 2. device cases in the air inlet 16.17.18.19.20.21.22.23.24.25.26.27. housing footpath section chamber in the connected chamber 30.31. multiple-blade turbine in the air inlet guide plate 28.29. housing footpath section chamber in radial part 32. " " the housing footpath section chamber of two blades the air ecto-entad drive axial component 44. that air in reference symbol 33. " ⊙ " the housing footpath section chamber drives 2 blades in the reference symbol 34. multiple-blade centripetal turbines 35. bearing outsides 36. bearing inner sleeves 37. spring pads 38. screws 39. nuts 40. back shrouds 41. air combined guide housing 42.43. multiple-blades from inside to outside and install outlet plenum 45.46.47. plus screw 48. housing rearward end 49. housing leading sections 50. and install 1 special air inlet.
1. preceding air guide cover is fixed on 49. housing front ends, 1. preceding air guide cover is connected with 3. back air guide cover interference, 3. back air guide cover is connected with the air-strainer outlet, 34. turbine is connected with 35. bearing outside interference fit, 36. bearing inner sleeve and 38. screws are slidingly matched, 37. spring pad 38. screws 39. nuts are fixed tightly in 35. bearing inner sleeves on 40. back shrouds, 40. back shroud is fixed tightly in 48. housing rearward end with the 45.46.47. plus screw, 44. housing outlet plenums are connected with engine aspirating system.
When motor one starts, 4. filtering the back air enters 5.6.7.8.9.10.11.12.13.14.15. suction port 17.18.19.20.21.22.23.24.25.26.27. in the housing footpath portion chamber by guide housing before and after the device and leads into communicated cavity in the portion of 28.29. housing footpath by the air of air inlet guide plate after with 4. filtrations, the radial part of each blade all is subjected to 4. simultaneously and filters the back air driven in moments 34. turbines, so 34 turbine acceleration are big, in the time of the high rapid rotation of revolution 4. filter the back air again in the multiple-blade each axial part enter into and form the high speed rotating air-flow in the 44 housing outlet plenums.When vehicle driving, gather a branch of air again and directly advance 50. special suction ports through particular filter, just make 34. multiple-blade centripetal turbines at the high speed rotating driving force that superposes again, so, the rotation that 34. the turbine acceleration is bigger, revolution is higher, just enter in the automotive engine air intake system greater than 1 atmospheric pressure value air high speed rotating air-flow 44. just form in the device outlet plenum, improved motor mean effective pressure value (Pe), improved the engine combustion performance.
Claims (5)
1. a garden housing aerodynamic turbosupercharging devic 3 is provided with 11 suction ports, 1 special suction port and 12 air inlet guide plates in housing footpath, garden portion chamber, and it is characterized in that: turbine is the multiple-blade centripetal turbine in the device.
2. according to the described garden of claim 1. housing aerodynamic turbosupercharging devic 3, it is characterized in that: device case is the garden housing.
3. according to the described garden of claim 1. housing aerodynamic turbosupercharging devic 3, it is characterized in that: each blade all has radial part, axial part in the multiple-blade centripetal turbine.
4. according to the described garden of claim 1. housing aerodynamic turbosupercharging devic 3, it is characterized in that: multiple-blade centripetal turbine airintake direction is consistent with the turbine sense of rotation.
5. according to the described garden of claim 1. housing aerodynamic turbosupercharging devic 3, it is characterized in that: bearing inner sleeve is fixed on the housing back shroud with bolt, spring pad, nut; Bearing outside is connected with the turbine interference fit.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CNU032036787U CN2597686Y (en) | 2003-02-10 | 2003-02-10 | Pressurizing device for round case pneumatic turbine |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CNU032036787U CN2597686Y (en) | 2003-02-10 | 2003-02-10 | Pressurizing device for round case pneumatic turbine |
Publications (1)
Publication Number | Publication Date |
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CN2597686Y true CN2597686Y (en) | 2004-01-07 |
Family
ID=34158217
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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CNU032036787U Expired - Fee Related CN2597686Y (en) | 2003-02-10 | 2003-02-10 | Pressurizing device for round case pneumatic turbine |
Country Status (1)
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CN (1) | CN2597686Y (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN102203429B (en) * | 2008-11-18 | 2015-05-20 | 博格华纳公司 | Compressor of an exhaust-gas turbocharger |
-
2003
- 2003-02-10 CN CNU032036787U patent/CN2597686Y/en not_active Expired - Fee Related
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN102203429B (en) * | 2008-11-18 | 2015-05-20 | 博格华纳公司 | Compressor of an exhaust-gas turbocharger |
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Legal Events
Date | Code | Title | Description |
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C14 | Grant of patent or utility model | ||
GR01 | Patent grant | ||
C19 | Lapse of patent right due to non-payment of the annual fee | ||
CF01 | Termination of patent right due to non-payment of annual fee |