WO2012155155A1 - Tubulure d'admission à économie de combustible pour moteur à combustion - Google Patents
Tubulure d'admission à économie de combustible pour moteur à combustion Download PDFInfo
- Publication number
- WO2012155155A1 WO2012155155A1 PCT/VN2012/000002 VN2012000002W WO2012155155A1 WO 2012155155 A1 WO2012155155 A1 WO 2012155155A1 VN 2012000002 W VN2012000002 W VN 2012000002W WO 2012155155 A1 WO2012155155 A1 WO 2012155155A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- fuel
- intake manifold
- fuel saving
- air mixture
- combustion chamber
- 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.)
- Ceased
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M29/00—Apparatus for re-atomising condensed fuel or homogenising fuel-air mixture
- F02M29/04—Apparatus for re-atomising condensed fuel or homogenising fuel-air mixture having screens, gratings, baffles or the like
- F02M29/06—Apparatus for re-atomising condensed fuel or homogenising fuel-air mixture having screens, gratings, baffles or the like generating whirling motion of mixture
Definitions
- the fuel saving intake manifold for combustion engine The fuel saving intake manifold for combustion engine.
- the purpose of invention is to reduce fuel consumption down to the lowest level without reducing the capacity, by method of smooth mixing and fine spread fuel / air mixture before entering the combustion chamber.
- the fuel saving intake manifold is made of one or “clusters" pipes between carburetor and the combustion chamber of cylinders.
- the "metal objects” has the same shapes or different shapes.
- the metal objects shaped like a wall grid shapes, piece of metal, wing screw, propeller disc .etc.. are located inside, non— stick, stick or casted into block with tube. etc..
- FIG. 1 shows in longitudinal section illustration the fuel saving intake manifold and location of metal objects(A). fuel / air mixture which not be mixed (Fl) after passing through the fuel saving intake manifold which have been mixed (F2)
- FIG. 2 is a simple drawing showing longitudinal the fuel saving intake manifold under the invention, in the case to use many propeller disks (B), they shall be fixed by the connecting wire (D) and aerodynamic movement shape of fuel / air mixture
- the fuel saving intake manifold has duty to mix smoothly and grind fuel / air mixture fine before entering to the combustion chamber of cylinder.
- Its structure includes one or (clusters) of metal tubes is connected between the carburetor and the combustion chamber of cylinder. Inside the tubes, there are the "metal objects" has the same shapes or different shapes as propeller disc shape, mesh walls, wing screw, piece of metal etc.. shape of the fuel saving intake manifold depends on the location between the carburetor and the combustion chamber of cylinder, in the condition that the length of connecting conduit is shortest, if the connecting conduit is too long, the engine acceleration is delayed. The cross-sectional area large enough in order that the amount of fuel / air mixture is enough to provide for the engine.
- Figure 2 is showing the profile of the fuel saving intake manifold in the simplest manner according to the invention.
- propeller disks B
- Each disc shall be added with wings as much as possible, between the disks are conneced with each other by a metal wire (D) to fix the propeller disc
- D metal wire
- Fuel / air mixture with are ground finely shall be burnt fully as coming to the combustion chamber.
- fuel / air mixture has numerous small spiral chaos ...
- the collision of fuel / air mixture shall be increased.
- wing screw it shall only increase the distance and velocity but the collision on the wings is less.
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Combustion Methods Of Internal-Combustion Engines (AREA)
Abstract
Lors du fonctionnement du moteur, de l'air et un combustible sont mélangés ensemble dans le carburateur puis sont aspirés dans la tubulure d'admission à économie de combustible à une vitesse considérable. A l'intérieur se trouvent des objets métalliques présentant la même forme ou des formes différentes. Grâce à ces objets, le mélange air/combustible entre en forte collision pour créer de petites spirales turbulentes et des spirales dans la même direction qui se déplacent à vitesse très élevée de manière à être mélangées de façon très homogène grâce aux impacts avant d'entrer dans la chambre de combustion. Celles-ci brûlent complètement dans le cylindre, ce qui permet d'économiser le combustible tout en atteignant la capacité requise.
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| VN201101221 | 2011-05-12 | ||
| VN1-2011-01221 | 2011-05-12 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| WO2012155155A1 true WO2012155155A1 (fr) | 2012-11-15 |
Family
ID=47139730
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| PCT/VN2012/000002 Ceased WO2012155155A1 (fr) | 2011-05-12 | 2012-05-11 | Tubulure d'admission à économie de combustible pour moteur à combustion |
Country Status (1)
| Country | Link |
|---|---|
| WO (1) | WO2012155155A1 (fr) |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| SU1262082A1 (ru) * | 1984-12-13 | 1986-10-07 | Кишиневский Политехнический Институт Им.Сергея Лазо | Устройство дл гомогенизации топливовоздушной смеси в двигателе внутреннего сгорани |
| SU1673748A1 (ru) * | 1989-01-17 | 1991-08-30 | Московский институт приборостроения | Устройство гомогенизации топливовоздушной смеси дл карбюраторного двигател внутреннего сгорани |
| SU1758267A1 (ru) * | 1990-07-09 | 1992-08-30 | Научно-исследовательский институт "Квант" | "Устройство дл гомогенизации топливовоздушной смеси двигател внутреннего сгорани "Лабиринт-К" (Лабиринт Корольковых)" |
| WO2003104624A2 (fr) * | 2002-06-05 | 2003-12-18 | Cyclone Usa, Inc. | Dispositif de tournoiement de fluide pour un moteur a combustion interne |
-
2012
- 2012-05-11 WO PCT/VN2012/000002 patent/WO2012155155A1/fr not_active Ceased
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| SU1262082A1 (ru) * | 1984-12-13 | 1986-10-07 | Кишиневский Политехнический Институт Им.Сергея Лазо | Устройство дл гомогенизации топливовоздушной смеси в двигателе внутреннего сгорани |
| SU1673748A1 (ru) * | 1989-01-17 | 1991-08-30 | Московский институт приборостроения | Устройство гомогенизации топливовоздушной смеси дл карбюраторного двигател внутреннего сгорани |
| SU1758267A1 (ru) * | 1990-07-09 | 1992-08-30 | Научно-исследовательский институт "Квант" | "Устройство дл гомогенизации топливовоздушной смеси двигател внутреннего сгорани "Лабиринт-К" (Лабиринт Корольковых)" |
| WO2003104624A2 (fr) * | 2002-06-05 | 2003-12-18 | Cyclone Usa, Inc. | Dispositif de tournoiement de fluide pour un moteur a combustion interne |
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