US1821468A - Mixing device - Google Patents

Mixing device Download PDF

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Publication number
US1821468A
US1821468A US270225A US27022528A US1821468A US 1821468 A US1821468 A US 1821468A US 270225 A US270225 A US 270225A US 27022528 A US27022528 A US 27022528A US 1821468 A US1821468 A US 1821468A
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slits
flange
conical
area
mixing device
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US270225A
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Hanley John
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M1/00Carburettors with means for facilitating engine's starting or its idling below operational temperatures
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M2700/00Supplying, feeding or preparing air, fuel, fuel air mixtures or auxiliary fluids for a combustion engine; Use of exhaust gas; Compressors for piston engines
    • F02M2700/43Arrangements for supplying air, fuel or auxiliary fluids to a combustion space of mixture compressing engines working with liquid fuel
    • F02M2700/4302Arrangements for supplying air, fuel or auxiliary fluids to a combustion space of mixture compressing engines working with liquid fuel whereby air and fuel are sucked into the mixture conduit
    • F02M2700/4373Mixture improving devices
    • F02M2700/4376Mechanical devices

Definitions

  • My invention relates to a new and useful improvement in a mixing device adapted for use on internal combustion engines and intended to effect a thorough mixing of the air and fuel delivered to the combustion chamber.
  • Another object of the invention is the provision of a device of this class which may be easily and quickly installed and which, when in operation, will serve to setup a Vor-v tex or whirling of the air and fuel being delivered to the engine and serve to remove from the walls of the intake manifoldsuch.
  • Fig. 1 is a side elevational View of the invention showing it applied.
  • Fig.2 is asectional view of the invention taken on line 22 of Fig. 1.
  • the invention is formed preferably from a single piece of metal and'comprises the flange 8 which is preferably formed circular or of a contourto correspond to the contour of the intake manifold with which used.
  • a conical-shaped portion 10 slitted as at 9 Projecting outwardly from one face of the flange 8 is a conical-shaped portion 10 slitted as at 9 to provide a plurality of veins or blades 10,,these veins'or'blades being inclined to the axis of the device, as shown in Fig. 2.
  • the slits 9 may be termed elemental slits since each of the slits defines a position of the generatrix of the cone and since thegeneratrix in any position is called an element of the conical surface.
  • the provision of the flange on the conical-shaped portion affords a means for easily and quickly assembling the device,-and" the formation of the slits so that their coinbined area bears a relation to the cross section area of the mam fold .12, in addition to permitting a free flow of the gas, sets up a maximum vortex or whirling of the aira-nd the fuel
  • the closed cone cap 11 deflects the central portion of the gas stream from the carburetor so that it is driven downwardly and outwardly. This deflection causes a vacuum above the cone into which a section of the gas rushes, thus adding to the thoroughness of the mixing.
  • a flange adapted for insertion in an intake conduit, comprising: a flange; and a hollow conical body having an open large end and a closed small end and projecting outwardly from one face of said flange, the sides of said body being provided with slits formed therein, the combined area of said slits being equal to the area of the open end of said cone.
  • a mixing device of the class described adapted for insertion in an intake conduit, comprising: a flange; and a hollow conical body having an open large end and a closed small end and projecting outwardly from one face of said flange, the sides of said body being provided with slits formed therein, the combined area of said slits being equal to the area of the open end of saidcone, the
  • a device of the class described comprising: a flange; a conical-shaped hollow body having an open large end and a closed small end and projecting outwardly from one face of said flange and provided with elemental slits; the combined area of said slits being equal to the area of the open end of said cone.

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  • 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)

Description

Sept. 1, 1931. HANLEY 1,821,468
. I MIXING DEVICE Filed April 16, 1928 INVENTOR. 1/060 W027): 3/.
W ATTORNEY. S
Patented Sept. 1, -1931 UNITED STATES JOHN HARLEY, OF DETROIT, MICHIGAN MIXING DEVICE Application filed April 1c, 1928. Serial mfzvoaas.
My invention relates to a new and useful improvement in a mixing device adapted for use on internal combustion engines and intended to effect a thorough mixing of the air and fuel delivered to the combustion chamber.
It is an object of the present invention to provide a device of this class which will be simple in structure, economical of manufacture and highly efficient in use.
Another object of the invention is the provision of a device of this class which may be easily and quickly installed and which, when in operation, will serve to setup a Vor-v tex or whirling of the air and fuel being delivered to the engine and serve to remove from the walls of the intake manifoldsuch.
fuel as would otherwise accumulatelthereon.
It is another object of theinvention to provide a device of this class which will assure nate engine knock, aiford an easy and quick starting of the motor and efiect an economy in operation of the engine. v Other objects will appear hereinafter.
- Theinvention consists in the combination and arrangement of parts hereinafter described and claimed. i
The invention will be best understood by a reference tothe accompanying. drawings which form a part of this specification and in which,
Fig. 1 is a side elevational View of the invention showing it applied. Fig.2 is asectional view of the invention taken on line 22 of Fig. 1.
The invention is formed preferably from a single piece of metal and'comprises the flange 8 which is preferably formed circular or of a contourto correspond to the contour of the intake manifold with which used.
Projecting outwardly from one face of the flange 8 is a conical-shaped portion 10 slitted as at 9 to provide a plurality of veins or blades 10,,these veins'or'blades being inclined to the axis of the device, as shown in Fig. 2. The slits 9 may be termed elemental slits since each of the slits defines a position of the generatrix of the cone and since thegeneratrix in any position is called an element of the conical surface.
The end 11 of the conical-shaped member is closed. i 1 In a device of this kind it is desirable that a free flowing of the fuel to the engine be permitted and to this end I have provided slits in the conical-shaped portion of such width that their combined area is equal to the cross section area of the manifold with which used, so that there is no retarding of the gases. In the form illustrated in the drawings this area is, of course, the same as lllhe area of the open end of the' conical mem- In Fig. 1 I have shown the invention applied inwhich the flange is inserted and clamped between the sections 10 and 13 of the manifold. 1 Bolts 14 which project through the flanges 15 and 16 also project through the spacer ring 17 positioned therebetween. j
In operation as the air and gas is. drawn through the conical-shaped member a whirling motion is set up and the fuel which ordinarily would accumulate on the surface of the manifold 12 is removed therefrom by the vortex or whirling motion of the fuel and air passing into the engine. I am aware that various devices for attempting a vortex have been developed but in the 'present invention, whichhas proven most efiicient in use, the advantages sought for are obtained which it is not believed are possibleili known devices. The provision of the flange on the conical-shaped portion affords a means for easily and quickly assembling the device,-and" the formation of the slits so that their coinbined area bears a relation to the cross section area of the mam fold .12, in addition to permitting a free flow of the gas, sets up a maximum vortex or whirling of the aira-nd the fuel The closed cone cap 11 deflects the central portion of the gas stream from the carburetor so that it is driven downwardly and outwardly. This deflection causes a vacuum above the cone into which a section of the gas rushes, thus adding to the thoroughness of the mixing.
While I have illustrated and described the wish to limit myself to the precise details of structure shown, but desire tooavaitmyself of such variations and modifications as come within the scope of the appended claims. Having thus described my invention what I claim as new and desire to secure by Letters Patent is:
1. A mixing device of the class described,
adapted for insertion in an intake conduit, comprising: a flange; and a hollow conical body having an open large end and a closed small end and projecting outwardly from one face of said flange, the sides of said body being provided with slits formed therein, the combined area of said slits being equal to the area of the open end of said cone.
2. A mixing device of the class described adapted for insertion in an intake conduit, comprising: a flange; and a hollow conical body having an open large end and a closed small end and projecting outwardly from one face of said flange, the sides of said body being provided with slits formed therein, the combined area of said slits being equal to the area of the open end of saidcone, the
open end of said cone being of the same I diameter as said conduit,
3, A device of the class described, comprising: a flange; a conical-shaped hollow body having an open large end and a closed small end and projecting outwardly from one face of said flange and provided with elemental slits; the combined area of said slits being equal to the area of the open end of said cone.
In testimony whereof I have signed the foregoing specification.
' JOHN HANLEY.
US270225A 1928-04-16 1928-04-16 Mixing device Expired - Lifetime US1821468A (en)

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Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2560069A (en) * 1946-02-21 1951-07-10 Lummus Co Mixer
US3546854A (en) * 1967-11-30 1970-12-15 Oke W Muller Centrifugal separator
EP0077060A1 (en) * 1981-10-10 1983-04-20 Günter Schallenberg Intermediate flange for positioning between the carburettor and the intake manifold of a combustion engine
WO2018026523A1 (en) * 2016-08-05 2018-02-08 Jetoptera, Inc. Internal combustion engine intake power booster system
US10207812B2 (en) 2015-09-02 2019-02-19 Jetoptera, Inc. Fluidic propulsive system and thrust and lift generator for aerial vehicles
US10464668B2 (en) 2015-09-02 2019-11-05 Jetoptera, Inc. Configuration for vertical take-off and landing system for aerial vehicles
USD868627S1 (en) 2018-04-27 2019-12-03 Jetoptera, Inc. Flying car

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2560069A (en) * 1946-02-21 1951-07-10 Lummus Co Mixer
US3546854A (en) * 1967-11-30 1970-12-15 Oke W Muller Centrifugal separator
EP0077060A1 (en) * 1981-10-10 1983-04-20 Günter Schallenberg Intermediate flange for positioning between the carburettor and the intake manifold of a combustion engine
US10207812B2 (en) 2015-09-02 2019-02-19 Jetoptera, Inc. Fluidic propulsive system and thrust and lift generator for aerial vehicles
US10464668B2 (en) 2015-09-02 2019-11-05 Jetoptera, Inc. Configuration for vertical take-off and landing system for aerial vehicles
WO2018026523A1 (en) * 2016-08-05 2018-02-08 Jetoptera, Inc. Internal combustion engine intake power booster system
CN109844296A (en) * 2016-08-05 2019-06-04 杰托普特拉股份有限公司 Internal combustion engine introduces dynamic supercharging system
USD868627S1 (en) 2018-04-27 2019-12-03 Jetoptera, Inc. Flying car

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