US1336144A - Aerating device for primers for internal-combustion engines - Google Patents

Aerating device for primers for internal-combustion engines Download PDF

Info

Publication number
US1336144A
US1336144A US249766A US24976618A US1336144A US 1336144 A US1336144 A US 1336144A US 249766 A US249766 A US 249766A US 24976618 A US24976618 A US 24976618A US 1336144 A US1336144 A US 1336144A
Authority
US
United States
Prior art keywords
way
valve
manifold
spring
fitting
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 - Lifetime
Application number
US249766A
Inventor
Kocourek Henry
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
Priority claimed from US21843118A external-priority patent/US1293804A/en
Application filed by Individual filed Critical Individual
Priority to US249766A priority Critical patent/US1336144A/en
Application granted granted Critical
Publication of US1336144A publication Critical patent/US1336144A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02NSTARTING OF COMBUSTION ENGINES; STARTING AIDS FOR SUCH ENGINES, NOT OTHERWISE PROVIDED FOR
    • F02N99/00Subject matter not provided for in the other groups of this subclass
    • F02N99/002Starting combustion engines by ignition means
    • F02N99/008Providing a combustible mixture outside the cylinder

Definitions

  • Figure l' is a diagrammatic view showin in side elevation a priming device equipped with the specific feature constituting this invention, the priming device illustrated being that shown in my application No. 218,431.
  • Fig. 2 is a section at the line, 22, on Fig. 1, through the fittingwhich constitutes the connection with the manifold and embodies the aerating device of the invention of this application, the same being shown on a full sized scale.
  • This fitting, 6, is a three-way fitting, having its three ways meeting at a common junction point, the first way, 6 being the stem of the T, said stem being adapted for connection with the pipe, 8, the second way, 6, being in one end of the cross of the T and open to the atmosphere, and being in line with the third way, 6 which is in the other end of the cross of the T, and adapted for connection with the manifold.
  • the stem of the T comprises two parts, for convenience offorming in the outer part, 6", a seat at 6 for a valve, 9, opening inwardly and seating outwardly, and provided with a spring, 10, coiled around its stem for seating it.
  • the second way, 6, has a seat at 6, for a ball valve, 11, seating outwardly and opening inwardly, and provided with a coil spring, 12, which operates to seat it.
  • This spring, 12, extends'in the second way, 6, and in the alined way, 6", past the junction of the three ways, and is stopped at its end remote from the valve b a plug 6 which is screwed into the end 0 the third way, 6", and which besides serving the function of stopping said spring, 12, constitutes a restricted discharge from said third way, 6", into the manifold, the plug having a very small a rture, 6 for such discharge.
  • this end of the cross of the T-fitting is provided with a spun cap, 18, which is expanded at the top and apertured as seen at 19, in the shoulder formed by the expansion and the end of the fitting is provided with notches, 20, "20, so that when the cap is pressed on against the end, free entrance of air is provided through the concealed apertures of the shoulder of the cap and through the'notches.
  • I having three ways purpose for which it is rovided consists 'in that the sprin 12, whic seats the air inlet valve, 11, is adapted to yield to less pressure than the spring, 10, which seats the valve, 9, at the liquid inlet.
  • the operation of the device in view of this difference in the resistance of the two springs is as follows: When the engine is to beprimed, the operator presses the pump, handle, producing pressure upon the priming liquid in the re- 4, causing the priming liquid to be three-way valve fitting past the valve, 9, and out through the third way, through. the 'reduced discharge aperture, 6, and injects a fine needle-like jet into the manifold.
  • I claim 2- A fitting for the purpose indicated with a common junction oint independentof each other up to that junction; a valve in the first way opening toward the junction point and a spring to seat it; a valve in the second way opening towardthe' junction and a spring to seat it which yields to less pressure than the'first spring, the third way being adapted for connection to the chamber in which the discharge is to be made.
  • said third way having its discharge mouth restricted relatively to the size of the valved ports of the other two ways.
  • the second and thirdways being alined with each other, and the third way having at its discharge mouth a plug provided with a restricted discharge aperture, the spring which seats the second men-& tioned valve being stopped by said lug 4:.
  • the second and third ways being alined and the spring which seats thevalve .in the second way being positioned extending into the third way, and an apertured plug in the discharge end of said third way which serves as a stop for said spring.
  • the first way having intake provided with a screening chamber anterior to v the seat of the valve in said way, said screen chamber comprisingtwo woven-wire screen disks and, a fibrous filling occupying the space between them.
  • a three-way fitting having one way connected with a source of primin liquid; a second way leading to the atmosp ere and a third way opening into the manifold, said third wa having a restricted discharge aperture or discharge into the manifold; a check valve in the first way openin inward, a spring to seat it in the opposite irection; a check valve in the second way opening inward, and a sprin to seat it in the opposite direction which yields to less pressure than the first mentioned spring.
  • I 7 In combination with the engine manifold, a receptacle for priming liquid, a device for producing pressure on the liquid in said receptacle; a duct leading from the lower part of the receptacle for connection with the engine manifold; a fitting for making said connection, having three ways meeting at a common junction point; an independent of each other up to that junction point; a valve in the first way opening toward the junction point and a spring to seat it; avalve in the second way opening toward the junction and a spring to seat itwhich yields to less pressure than the first mentioned spring, the third way being con- 125 August, 1918.

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Fuel-Injection Apparatus (AREA)

Description

r H. KOCOUREK.
AERATING DEVICE FOR PRIMERS FOR INTERNAL COMBUSTION ENGINES.
APPLICATION FILED AUG. 141 i918- ma ma. Patented Apr. 6,1920.
HENRY KOGOUBEK, OF CHICAGO, ILLINOIS.
AERATING DEVICE FOR PBIIERS FOK'INTEB NAL-COMBUSTION ENGINES.
Specification of Letters Iatent.
Patented Apr. 6, 1920.
Original application filed February 21, 1918, Serial No. 218,431. Divided and 'this application filed August 14, 1918. Serial No. 249,766.
To all whom it may concern:
Be it known that I, HENRY KOCOUREK, a citizen of the United States, residing at Chicago, in the county of Cook and the State of Illinois, have invented certain new and useful Improvements in Aerating Devices for Primers for Internal-Combustion Engines, of which the following is a specification, reference being had to the accompan ing drawings, forming a part thereof.
T is application is a division of my application No. 218,431, filed February 21, 1918.
The purpose of .the specific invention shown herein is -to aerate a liquid fuel charge furnished by a priming device to the manifold or other intake connection of an internal combustion engine. It consists in the elements and features of constructionshown .and described as indicated in the claims.
In the drawings:
Figure l'is a diagrammatic view showin in side elevation a priming device equipped with the specific feature constituting this invention, the priming device illustrated being that shown in my application No. 218,431.
Fig. 2 is a section at the line, 22, on Fig. 1, through the fittingwhich constitutes the connection with the manifold and embodies the aerating device of the invention of this application, the same being shown on a full sized scale.
Preferring the diagrammatic view to locate in its roper connection the specific features to which the application relates,1 is the intake manifold of. the engine to be served; 2 is the carbureter comprising the intake pipe and the float chamber in familiar form; 3 represents the vacuum fuel feed tank of common construction for supplying the carbureter; 4 is a priming reservoir from which the liquid fuel is to be drawn for priming;- 5 is. an air pump for producing pressure on the fuel in the reservoir, 4, to feed it to the mixing device shown at 6, which constitutes the specific invention of this application, and which is full shown in axial section in Fig. 2. The wings show various operating parts and pipe connections which will be understood as to their general purpose without further description.
From the foregoing, however, it will be understood that the liquid fuel isto be forced by pressure operating in the receptacle, 4,
through the fitting, 7, the pipe, 8, leading to the mixing device, 6, into the manifold.
.This fitting, 6, is a three-way fitting, having its three ways meeting at a common junction point, the first way, 6 being the stem of the T, said stem being adapted for connection with the pipe, 8, the second way, 6, being in one end of the cross of the T and open to the atmosphere, and being in line with the third way, 6 which is in the other end of the cross of the T, and adapted for connection with the manifold. The stem of the T comprises two parts, for convenience offorming in the outer part, 6", a seat at 6 for a valve, 9, opening inwardly and seating outwardly, and provided with a spring, 10, coiled around its stem for seating it. The second way, 6, has a seat at 6, for a ball valve, 11, seating outwardly and opening inwardly, and provided with a coil spring, 12, which operates to seat it. This spring, 12, extends'in the second way, 6, and in the alined way, 6", past the junction of the three ways, and is stopped at its end remote from the valve b a plug 6 which is screwed into the end 0 the third way, 6", and which besides serving the function of stopping said spring, 12, constitutes a restricted discharge from said third way, 6", into the manifold, the plug having a very small a rture, 6 for such discharge. In
the inta e mouth of the first way, 6*, in the stem of the T, there is provided a screen chamber for the liquid anterior to the valve seat in said way, said screen chamber being formed by two fine wovenwire disks, 16, 16, between which the space is filled with fibrous material, '17. "Similarly in the intake mouth of the second way, 6, anterior to the valve seat, 6, in said second way, there is a screen chamber at m, in which there is secured a screen, M, through which the air entering said way must pass, thereby preventing the drawing in of dust which might block the valve. As a further expedient for prevent,
in foreign matter passing into this way, this end of the cross of the T-fitting is provided with a spun cap, 18, which is expanded at the top and apertured as seen at 19, in the shoulder formed by the expansion and the end of the fitting is provided with notches, 20, "20, so that when the cap is pressed on against the end, free entrance of air is provided through the concealed apertures of the shoulder of the cap and through the'notches. An important feature of this fitting for the ceptacle,
discharged in through the first way of'the and second ways respectively,
' space in the fitting,
I having three ways purpose for which it is rovided consists 'in that the sprin 12, whic seats the air inlet valve, 11, is adapted to yield to less pressure than the spring, 10, which seats the valve, 9, at the liquid inlet. The operation of the device in view of this difference in the resistance of the two springs is as follows: When the engine is to beprimed, the operator presses the pump, handle, producing pressure upon the priming liquid in the re- 4, causing the priming liquid to be three-way valve fitting past the valve, 9, and out through the third way, through. the 'reduced discharge aperture, 6, and injects a fine needle-like jet into the manifold. The pressure which forces this discharge, seats the ball valve, 11, preventing the possibility of discharging through the air inlet-afiorded by the way, 6, of the fitting. In the operation of the engine producing a partial vacuum in the manifold, tending to suck the liquid fuel in through the fitting, 6, the fact that the spring, 12, controlling the air valve, 11, yields more readily than the spring, 10, which controls the fuel inlet valve, 9, causes the suction to produce inflow and jets of air only coming in past the valve, 11, to the second way, and discharging through the reduced aperture, 6, at the .end of the third Way. Upon the starting of the engine without the manual operation of the primer, the partial vacuum rising in the manifold, producing suction as described, will draw in and cause to be discharged -in a jet through the reduced aperture, 6, at the end of the third way, the small amount of liquid fuel that will be occupying the space in the third way, and extending back to the two valves in the first this liquid being followed by air drawn in past the valve, 11, through the second way, to cause this small quantity of liquid fuel to be forcibly aspirated and dispersed intermixed with air at its emergence from-the manifold. The usual situation when the engine is stopped after having been running, will be that the 6, beyond the valve and tothe discharge mouth in the manifold will be occupied by air only, and an effective mode of operating the device for priming will usually be for the operator to depress the pum plunger sufficiently only to force enough uel through the pipe, 8, to fill said space in thefitting; and then when the en gine starts, the partial vacuum resulting in the manifold will draw in the as irated charge of liquid fuel as above descri ed.
I claim 2- 1. A fitting for the purpose indicated with a common junction oint independentof each other up to that junction; a valve in the first way opening toward the junction point and a spring to seat it; a valve in the second way opening towardthe' junction and a spring to seat it which yields to less pressure than the'first spring, the third way being adapted for connection to the chamber in which the discharge is to be made. i
2. In a fitting such as indicated in claim 1 foregoing, said third way having its discharge mouth restricted relatively to the size of the valved ports of the other two ways.
3. In a construction such as defined by claim 1, the second and thirdways being alined with each other, and the third way having at its discharge mouth a plug provided with a restricted discharge aperture, the spring which seats the second men-& tioned valve being stopped by said lug 4:. In a construction such as defihed by claim 1, the second and third ways being alined and the spring which seats thevalve .in the second way being positioned extending into the third way, and an apertured plug in the discharge end of said third way which serves as a stop for said spring.
5. In a structure such as defined in claim 1, foregoing the first way having intake provided with a screening chamber anterior to v the seat of the valve in said way, said screen chamber comprisingtwo woven-wire screen disks and, a fibrous filling occupying the space between them.
6. In combination with the engine manifold a three-way fitting having one way connected with a source of primin liquid; a second way leading to the atmosp ere and a third way opening into the manifold, said third wa having a restricted discharge aperture or discharge into the manifold; a check valve in the first way openin inward, a spring to seat it in the opposite irection; a check valve in the second way opening inward, and a sprin to seat it in the opposite direction which yields to less pressure than the first mentioned spring.
I 7. In combination with the engine manifold, a receptacle for priming liquid, a device for producing pressure on the liquid in said receptacle; a duct leading from the lower part of the receptacle for connection with the engine manifold; a fitting for making said connection, having three ways meeting at a common junction point; an independent of each other up to that junction point; a valve in the first way opening toward the junction point and a spring to seat it; avalve in the second way opening toward the junction and a spring to seat itwhich yields to less pressure than the first mentioned spring, the third way being con- 125 August, 1918.
. HENRY KOCOUREK.
US249766A 1918-02-21 1918-08-14 Aerating device for primers for internal-combustion engines Expired - Lifetime US1336144A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US249766A US1336144A (en) 1918-02-21 1918-08-14 Aerating device for primers for internal-combustion engines

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US21843118A US1293804A (en) 1918-02-21 1918-02-21 Priming device for internal-combustion engines.
US249766A US1336144A (en) 1918-02-21 1918-08-14 Aerating device for primers for internal-combustion engines

Publications (1)

Publication Number Publication Date
US1336144A true US1336144A (en) 1920-04-06

Family

ID=26912902

Family Applications (1)

Application Number Title Priority Date Filing Date
US249766A Expired - Lifetime US1336144A (en) 1918-02-21 1918-08-14 Aerating device for primers for internal-combustion engines

Country Status (1)

Country Link
US (1) US1336144A (en)

Similar Documents

Publication Publication Date Title
US1336144A (en) Aerating device for primers for internal-combustion engines
US1262013A (en) Automatic cut-off valve for gasolene-engines.
US1092079A (en) Carbureter.
US1349751A (en) Dust-fuel carbureter
US1722791A (en) Fuel-feeding device for internal-combustion engines
US2619333A (en) Carburetor
US1373550A (en) Carbureter
US2146397A (en) Fuel feeding and filtering
US2187998A (en) Upper cylinder lubricator
US1264464A (en) Auxiliary carbureter.
US1105134A (en) Carbureter.
US1063866A (en) Fuel-feed regulator for explosive-engines.
US1881559A (en) Accelerator pump
US1181356A (en) Carbureter.
US1293804A (en) Priming device for internal-combustion engines.
US1132942A (en) Consolidated carbureter and vacuum-feed fuel-receptacle.
US1861694A (en) Carburetor
US1328235A (en) Air-valve attachment for carbureters
US1153089A (en) Fuel-feeding device for internal-combustion engines.
US1414035A (en) Carburetor
US1961775A (en) Carburetor
US1177040A (en) Engine-primer.
US1269177A (en) Carbureter.
US1000518A (en) Carbureter.
US1898672A (en) Carburetor