EP0221568A2 - Flügelrad zum Homogenisieren des Gemisches einer Otto-Brennkraftmaschine - Google Patents

Flügelrad zum Homogenisieren des Gemisches einer Otto-Brennkraftmaschine Download PDF

Info

Publication number
EP0221568A2
EP0221568A2 EP86115470A EP86115470A EP0221568A2 EP 0221568 A2 EP0221568 A2 EP 0221568A2 EP 86115470 A EP86115470 A EP 86115470A EP 86115470 A EP86115470 A EP 86115470A EP 0221568 A2 EP0221568 A2 EP 0221568A2
Authority
EP
European Patent Office
Prior art keywords
turbine
blades
impeller
mixture
exhaust gas
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.)
Withdrawn
Application number
EP86115470A
Other languages
English (en)
French (fr)
Other versions
EP0221568A3 (de
Inventor
Alojzy Kowalski
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.)
Stowarzyszenie Inzynierow i Technikow Mechanikow Polskich Zespol Osrodkow Rzeczoznawstwa i Postepu Technicznego "Zorpot"
Original Assignee
Stowarzyszenie Inzynierow i Technikow Mechanikow Polskich Zespol Osrodkow Rzeczoznawstwa i Postepu Technicznego "Zorpot"
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 Stowarzyszenie Inzynierow i Technikow Mechanikow Polskich Zespol Osrodkow Rzeczoznawstwa i Postepu Technicznego "Zorpot" filed Critical Stowarzyszenie Inzynierow i Technikow Mechanikow Polskich Zespol Osrodkow Rzeczoznawstwa i Postepu Technicznego "Zorpot"
Publication of EP0221568A2 publication Critical patent/EP0221568A2/de
Publication of EP0221568A3 publication Critical patent/EP0221568A3/de
Withdrawn legal-status Critical Current

Links

Images

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
    • F02M29/02—Apparatus for re-atomising condensed fuel or homogenising fuel-air mixture having rotary parts, e.g. fan wheels

Definitions

  • the subject of this present invention is a turbine for mixing a combustion mixture used for spark--ignition, internal-combustion engines and consisting of air and fuel or air, fuel and exhaust gas.
  • the process involves intimately mixing the components and atomising and evaporating fuel drops.
  • Components and assemblies of engine feed systems are known in the form of immovable and movable inserts whose aim is to atomise fuel drops and to facilitate evaporation along the way from the carburettor to the engine cylinders. These are generally inserts with holes and kerbs, ap- prppriately shaped profiles inserted into the stream of the mixture, or whirling components in the form of appropriately shaped impellers driven by the flowing mixture.
  • a turbine known from Polish Patent Application No. P-255,444 consists of a body and an impeller running in bearings and driven with the air and exhaust gas drawn in through the engine suction manifold.
  • the essence of the turbine consisting as per this present invention of a body with exhaust gas and air jets and an impeller rotatably mounted therein is that the body has an inner section increasing towards the flow of the mixture and the-impeller is consists of blades secured to a hub and bars radially spaced relative the hub, the blades being set at an angle varying from 10 to 20° relative the plane passing through the impeller rotation axis and perpendicular to the blade generatrix.
  • the body mounts jets for delivering air and exhaust gas at an angle varying from 30 to 70° relative the longitudinal axis of the impeller and preferably tangentially to the direction of rotation of the impeller blades.
  • the turbine blades are bent at an angle varying from 10 to 90° relative their plane.
  • the advantage of the turbine as per this present invention is that its construction enables. an appropriate mixture to be obtained, which is enchanced by a purposeful combination of blades and bars.
  • the bars break fuel drops and make the mixture finer, whereas the final mixing and ho" mogenisation takes place when the mixture is passing between the impeller blades.
  • Thanks to additional air being supplied to inside the turbine through an air jet in the turbine body it is besides possible to again regulate the mixture composition and, when additionally delivering the exhaust gas, use is made of the effect of the gas-dynamic action of the exhaust jet on the mixture for further atomising it and the thermal energy of the exhaust gas for speeding up fuel evaporation in the mixture of air, fuel and exhaust gas so obtained.
  • Fig. 1 shows a cross section of the turbine
  • Fig. 2 shows a longitudinal sect- ion along line A-A
  • Fig. 3 shows a cross section along line B-B
  • Fig. 4 shows a longitudinal sect- ion through the exhaust gas delivering nozzle
  • Fig. 5 shows a side view of the blade.
  • Body 1 having an inner section increasing in the direction of the mixture flow has an impel- ler rotatably mounted therein and consisting of blades 3 and bars 4 secured to hub 2 and radially spaced relative the latter, blades 3 are set at an angle varying from 10 to 20° relative the plane passing through the impeller rotation axis and perpendicular to the generatrix of blade 3.
  • Inside body 1 there are nozzles 5 and 6 for delivering air and exhaust gas at an angle varying from 30 to 70° relative the longitudinal axis of the impeller and preferably tangentially to the direction of the rotation of impeller blades 3.
  • On the other hand on their periphery from the side of the mixture inlet blades 3 are bent at an angle varying from 10 to 90° relative their plane.
EP86115470A 1985-11-07 1986-11-07 Flügelrad zum Homogenisieren des Gemisches einer Otto-Brennkraftmaschine Withdrawn EP0221568A3 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
PL256139 1985-11-07
PL25613985A PL256139A1 (en) 1985-11-07 1985-11-07 Turbine for preparing combustive mixture for spark ignited internal combustion engines

Publications (2)

Publication Number Publication Date
EP0221568A2 true EP0221568A2 (de) 1987-05-13
EP0221568A3 EP0221568A3 (de) 1988-08-03

Family

ID=20028919

Family Applications (1)

Application Number Title Priority Date Filing Date
EP86115470A Withdrawn EP0221568A3 (de) 1985-11-07 1986-11-07 Flügelrad zum Homogenisieren des Gemisches einer Otto-Brennkraftmaschine

Country Status (2)

Country Link
EP (1) EP0221568A3 (de)
PL (1) PL256139A1 (de)

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR484128A (fr) * 1917-01-09 1917-09-07 Jean De Ferry Dispositif mélangeur de fluides, plus particulièrement applicable aux carburateurs de moteurs à explosion
US2004919A (en) * 1933-05-20 1935-06-18 William S Alvey Gasoline vapor and air mixing device
FR1171114A (fr) * 1956-04-11 1959-01-22 Pulvérisateur-mélangeur automatique relié au carburateur d'un moteur à explosionpour obtenir un mélange intime entre l'air et le carburant
FR1497807A (fr) * 1966-04-23 1967-10-13 Inpaco Trust Reg Accessoire pour les moteurs thermiques à carburateur
US3421485A (en) * 1967-06-19 1969-01-14 De Witt M Fessenden Fuel mixing device for internal combustion engines

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR484128A (fr) * 1917-01-09 1917-09-07 Jean De Ferry Dispositif mélangeur de fluides, plus particulièrement applicable aux carburateurs de moteurs à explosion
US2004919A (en) * 1933-05-20 1935-06-18 William S Alvey Gasoline vapor and air mixing device
FR1171114A (fr) * 1956-04-11 1959-01-22 Pulvérisateur-mélangeur automatique relié au carburateur d'un moteur à explosionpour obtenir un mélange intime entre l'air et le carburant
FR1497807A (fr) * 1966-04-23 1967-10-13 Inpaco Trust Reg Accessoire pour les moteurs thermiques à carburateur
US3421485A (en) * 1967-06-19 1969-01-14 De Witt M Fessenden Fuel mixing device for internal combustion engines

Also Published As

Publication number Publication date
EP0221568A3 (de) 1988-08-03
PL256139A1 (en) 1987-08-10

Similar Documents

Publication Publication Date Title
DE4137179C2 (de) Vorrichtung zum Erzeugen einer Wasser-in-Öl Emulsion und Verwendung der Vorrichtung an einem Dieselmotor
US6796296B2 (en) Fluid swirling device for an internal combustion engine
US4597524A (en) Snow making machine
GB2057051A (en) Turbulence device for engine mixture
US2812899A (en) Intake sprinkler for gas turbine engines
US6701964B1 (en) Vortex generating airfoil fuel saver
EP0221568A2 (de) Flügelrad zum Homogenisieren des Gemisches einer Otto-Brennkraftmaschine
EP1061265B1 (de) Aufladegruppe für einen Grossdieselmotor
EP0089590B1 (de) Maschine zum Erzeugen von Schnee
EP0778443B1 (de) Brennstoff-Einspritzvorrichtung und -verfahren
US4422432A (en) Variation of fuel vaporizer for internal combustion engine
US4411224A (en) Fluid injection system for a turbocharged internal combustion engine
US4399800A (en) Device for improving fuel efficiency in internal combustion engine
CN103470410B (zh) 强力旋转涡流油气混合发生器
US4671247A (en) Fuel atomizing apparatus for internal combustion engines
JPS55109724A (en) Air intake device for diesel engine
US7107962B1 (en) Carburetor hat for forced induction system
US3490883A (en) Feed of an air-fuel mixture to an internal combustion engine
CN2193929Y (zh) 用于汽车发动机的空气涡旋装置
RU2074972C1 (ru) Карбюратор двигателя внутреннего сгорания
CN2227208Y (zh) 气体旋流装置
JPS5540212A (en) Air inlet device of internal combustion engine
RU2059097C1 (ru) Система впуска карбюраторного двигателя
US4401060A (en) Fluid injection system for a supercharged internal combustion engine
CN1078308C (zh) 发动机用吸气总管

Legal Events

Date Code Title Description
PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

Free format text: ORIGINAL CODE: 0009012

AK Designated contracting states

Kind code of ref document: A2

Designated state(s): DE FR GB

PUAL Search report despatched

Free format text: ORIGINAL CODE: 0009013

AK Designated contracting states

Kind code of ref document: A3

Designated state(s): DE FR GB

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: THE APPLICATION IS DEEMED TO BE WITHDRAWN

18D Application deemed to be withdrawn

Effective date: 19890418

RIN1 Information on inventor provided before grant (corrected)

Inventor name: KOWALSKI, ALOJZY