US2332716A - Carburetor - Google Patents

Carburetor Download PDF

Info

Publication number
US2332716A
US2332716A US424021A US42402141A US2332716A US 2332716 A US2332716 A US 2332716A US 424021 A US424021 A US 424021A US 42402141 A US42402141 A US 42402141A US 2332716 A US2332716 A US 2332716A
Authority
US
United States
Prior art keywords
air
venturi
pressure
carburetor
mixture
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
US424021A
Inventor
Arleigh J Hess
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
Application filed by Individual filed Critical Individual
Priority to US424021A priority Critical patent/US2332716A/en
Application granted granted Critical
Publication of US2332716A publication Critical patent/US2332716A/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
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M17/00Carburettors having pertinent characteristics not provided for in, or of interest apart from, the apparatus of preceding main groups F02M1/00 - F02M15/00
    • F02M17/02Floatless carburettors
    • F02M17/04Floatless carburettors having fuel inlet valve controlled by diaphragm
    • 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
    • F02M7/00Carburettors with means for influencing, e.g. enriching or keeping constant, fuel/air ratio of charge under varying conditions
    • F02M7/12Other installations, with moving parts, for influencing fuel/air ratio, e.g. having valves
    • F02M7/18Other installations, with moving parts, for influencing fuel/air ratio, e.g. having valves with means for controlling cross-sectional area of fuel-metering orifice
    • 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
    • F02M9/00Carburettors having air or fuel-air mixture passage throttling valves other than of butterfly type; Carburettors having fuel-air mixing chambers of variable shape or position
    • F02M9/10Carburettors having air or fuel-air mixture passage throttling valves other than of butterfly type; Carburettors having fuel-air mixing chambers of variable shape or position having valves, or like controls, of elastic-wall type for controlling the passage, or for varying cross-sectional area, of fuel-air mixing chambers or of the entry passage
    • F02M9/103Mechanical control
    • 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
    • F02M2700/4361Mixing chambers
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10STECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S261/00Gas and liquid contact apparatus
    • Y10S261/02Airplane

Definitions

  • the object of this invention is to obtain improved load and altitude compensation with a variable venturi aircraft carburetor in which the variable Venturi forms the throttle.
  • a variable venturi carburetor in which the needle is moved with the throttle
  • This invention utilizes the carburetor drop in pressure, that is the suction below the throttle, to correct for this inherent defect in all variable venturi carburetors, which defect shows up at the extreme air velocities, to secure which is one of the reasons for carburetor.
  • FIG. 1 shows diagrammatically the general arrangement of my invention.
  • Fig. 2 shows diagrammatically a modification using a variable venturi of myA invention.
  • a passage 26 connects these holes 42 with the air chambers 21, 28, which determine the pressure in the fuel chamber 36 which is bounded on the left by the diaphragm 32 and on the right by the 4diaphragm 33.
  • These diaphragms control the inlet valve mechanism in a well known v manner.
  • a pressure control valve 29 is provided with the leaner the mixture and when the valve 29 is thrown into the position C, We have a zero open,-
  • a temperature responsive capsule 34 is housed under a cover 35 and is connected by a bell crank charge into the throat of .thevariable ⁇ venturiy formed between the throttles I3, I4.
  • Adjacent to the downstream side ofl a'fuel restriction 20 is an air vent or passage ZI which communicates with a. chamber 22 which is in and thus records the average pressure in the air entrance I0 immediately before the air flows bythe partition I9 and beforethe air enters the variable venturi.
  • a venturi 24 connects the chamber 22 with the mixture -outlet 40.
  • the ilow ⁇ from the chamber 22 tothe mixture outlet at 40 is due to the pressure drop across the carburetor.v
  • the flow through the venturi 24 is accelerated by the lever 3l with the needle valve 38 which controls the entrance to .a passage 39, which ⁇ admits air from the chamber 22 to the restriction 30, BI in the valve 29.
  • the air in thejchamber 22 is at the same pressure as the pressure of the air in the ⁇ piezoxneter ring 23, namely, the pressure ofthe air in theair. entrance.,v
  • the capsules 34 are made-to respond primarily to temperature, but may respond also' tothe atimosphericV pressure or'altitude. However, I have discovered that with this. arrangement very little correction for altitude is needed. It appears that the venturi 24 with air of low density maintains its efliciency and creates a relatively larger suction in the chambers 21, 28, than does the venturi A the relative neiclency of the throttle I3, I4 be ⁇ -.
  • emciency is meant the recovery of pressure in an air venturi after the air has been through the throat of the venturi, in which throat its velocity has been raised and its pressure lowered. If air at, 30" Hg falls to 29", then there is a 97% recovery and the venturi is 97% eilicient.
  • venturi 24 becomes relatively more eiective to hold fuel back than the variable venturi I3, I4, I9 are to cause fuel to flow.
  • variable venturi I3-I4 the airflow through the venutri 24 also increases and thus the tendency for the mixture to become rich is checked by the depression in the throat of the fixed venturi 24 which depression is communicated to the chamber 21-28 through 26.
  • Altitude control Discussing rst, Fig. 2 means are shown for adding atmospheric pressure to modify the depression in the chambers 21 and 28 at low altitude.
  • the barometric element 34, Fig. 1) is compressed, bell crank lever 21 moves counterclockwise, altitude valve 38 moves to the right and air at substantially atmospheric pressure flows from chamber ⁇ 22 through passage 44 and modifies the eiect of the suction in the venturi'42 so that an increase in air density increases the airflow down passage 44 and therefore the desired altitude compensation results from the increased pressure in 21 and 28.
  • mixture is corrected for temperature.
  • variable Venturi carburetor of the type i which the variable venturi is formed by a movable throttle, a fuel nozzle discharging into the throat of said variable venturi, a fuel chamber associated therewith, pressure regulating means for maintaining the fuel in said chamber at a sub-atmospheric pressure, said pressure being higher than that in the throat of the variable venturi, means for creating said sub-atmospheric pressure comprising a fixed venturi 'having an air entrance in communication with the air entrance to the carburetor and having an exit in the mixture outlet from the carburetor, a passage connecting the throat of the xed venturi to the pressure regulating means in said fuel supply chamber, a device responsive to the pressure and to the temperature of the air in the air entrance leading to the carburetor, a, valve controlled thereby, a restricted air vent controlled by said valve and a passage communicating with the throat of the fixed venturi and adapted to supply air from said vent, to reduce the suction created by said ixed

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Control Of The Air-Fuel Ratio Of Carburetors (AREA)

Description

A. J. HESS @et 26, R43..
CARBURETOR Filed Deo. 22 1941 INVENTOR ATTORNEY Patented Oct. 26, 1943 CARBURETOR Arleigh J. Hess, Detroit, Mich., assignor to George M. Holley and Earl Holley Application December 22, 1941, Serial No. 424,021
1 Claim.
The object of this invention is to obtain improved load and altitude compensation with a variable venturi aircraft carburetor in which the variable Venturi forms the throttle. With such a variable venturi carburetor (in which the needle is moved with the throttle) if, when the engine is rotating at a high rate, the load on the engine is increased when the throttle is held in the partly closed position, the revolutions per minute will be reduced and the air flow will decrease and the mixture will then have a tendency to become lean.
On the other hand, if the air flow increases greatly, because of a decrease in load with a fixed throttle, the revolutions per minute will increase and the mixture will have a tendency to become rich because of an excessive drop in the throat I of the variable venturi.
This invention utilizes the carburetor drop in pressure, that is the suction below the throttle, to correct for this inherent defect in all variable venturi carburetors, which defect shows up at the extreme air velocities, to secure which is one of the reasons for carburetor.
In the drawing: Fig. 1 shows diagrammatically the general arrangement of my invention.
Fig. 2 shows diagrammatically a modification using a variable venturi of myA invention.
4mixture outlets I I` andl. VThese outlets disfact that the air converges in a 25 funnel into the throat of a venturi having a .120" diameter (.0112 sq. in.). This throat suddenly enlarges to a diameter .147" (.0177 sq. inch=60% increase) and at the point of enlargement there enter: tangentially 6 openings #56 dri11=.0465" diam-- eter (.0101 sq. in. total), one of them having the reference character 42. The air stream then enlarges in a funnel 4I having a 6 included angle. A passage 26 connects these holes 42 with the air chambers 21, 28, which determine the pressure in the fuel chamber 36 which is bounded on the left by the diaphragm 32 and on the right by the 4diaphragm 33. These diaphragms control the inlet valve mechanism in a well known v manner.
A pressure control valve 29 is provided with the leaner the mixture and when the valve 29 is thrown into the position C, We have a zero open,-
. ing and hence we have an idle cut off position asv the vacuum in the venturi 24 is transferred to the chambers 21 and 28. The suction is thus controlled by the valve 29.
A temperature responsive capsule 34 is housed under a cover 35 and is connected by a bell crank charge into the throat of .thevariable` venturiy formed between the throttles I3, I4.
Adjacent to the downstream side ofl a'fuel restriction 20 is an air vent or passage ZI which communicates with a. chamber 22 which is in and thus records the average pressure in the air entrance I0 immediately before the air flows bythe partition I9 and beforethe air enters the variable venturi.
A venturi 24 connects the chamber 22 with the mixture -outlet 40. Thus, the ilow` from the chamber 22 tothe mixture outlet at 40 is due to the pressure drop across the carburetor.v The flow through the venturi 24 is accelerated by the lever 3l with the needle valve 38 which controls the entrance to .a passage 39, which` admits air from the chamber 22 to the restriction 30, BI in the valve 29. The air in thejchamber 22 is at the same pressure as the pressure of the air in the `piezoxneter ring 23, namely, the pressure ofthe air in theair. entrance.,v
The capsules 34 are made-to respond primarily to temperature, but may respond also' tothe atimosphericV pressure or'altitude. However, I have discovered that with this. arrangement very little correction for altitude is needed. It appears that the venturi 24 with air of low density maintains its efliciency and creates a relatively larger suction in the chambers 21, 28, than does the venturi A the relative neiclency of the throttle I3, I4 be`-.
comes more pronounced as the air becomes less dense and the more ineiiicient the throttle I3, I4 becomes the bigger the drop causing flow through venturi 24. By emciency is meant the recovery of pressure in an air venturi after the air has been through the throat of the venturi, in which throat its velocity has been raised and its pressure lowered. If air at, 30" Hg falls to 29", then there is a 97% recovery and the venturi is 97% eilicient.
Hence as the air becomes less dense the venturi 24 becomes relatively more eiective to hold fuel back than the variable venturi I3, I4, I9 are to cause fuel to flow.
In the modication shown in Fig. 2, the needle valve 38 controls an orice 43 which communicates through the pipe 44 with the air chambers 21, 28. Hence the opening 43 admits air in parallel with either the air admitted through 30 or 3|. Hence the areas of 30 and 3I are correspondingly decreased. The reason for the modification is to avoid having two restrictions in series which complicates the control.
Operation In the operation of the carburetor, the throttles I3 and I4 are opened at the same time that the needle I2 moves to the right and the bell crank lever I rotates clockwise. There imr'nediately follows an increased iiow of air and fuel. In the event that a light load is imposed on the engine as is possible with a variable pitch propeller, the engine tends to rotate rapidly at a wide open throttle and with this type of carburetor, there is a tendency for the mixture to become rich assuming that the mixture ratio is correct at wide open throttle low engine speed. In order that the mixture should remain constant regardless of load, the air pressure in chambers 21 and 28 is made to respond to these variations of load as follows:
The pressure in the chambers 21 and 28 is controlled by the pressure in the passage 26 which communicates through the opening 42 with the downstream side of the throat of the small fixed venturi 24.
Obviously, when the airflow increases through the variable venturi I3-I4 the airflow through the venutri 24 also increases and thus the tendency for the mixture to become rich is checked by the depression in the throat of the fixed venturi 24 which depression is communicated to the chamber 21-28 through 26.
Altitude control Discussing rst, Fig. 2, means are shown for adding atmospheric pressure to modify the depression in the chambers 21 and 28 at low altitude. Under such circumstances, the barometric element 34, Fig. 1) is compressed, bell crank lever 21 moves counterclockwise, altitude valve 38 moves to the right and air at substantially atmospheric pressure flows from chamber` 22 through passage 44 and modifies the eiect of the suction in the venturi'42 so that an increase in air density increases the airflow down passage 44 and therefore the desired altitude compensation results from the increased pressure in 21 and 28. For the same reason, mixture is corrected for temperature.
In Fig. 1, the altitude compensation valve 33 is put in series with the mixture control valve 29 whereas in Fig. 2, the altitude control valve 38 is placed in parallel with mixture control valve 29 so that in Fig. 1, the effect of the altitude control valve 38 is influenced by the valve 2,9. In any event, the rotation of mixture control valve 29 provides for three mixture ratios, positions A, B, and C. In position A, the mixture is controlled by virtue of the restriction 30, in position B by virtue of the restriction 3I and in position C, there is no opening whatsoever through the valve 29. The larger the opening through the valve 29, the less influence has the venturi 24 on the pressure in the chamber 21-28.
What I claim is: In a variable Venturi carburetor of the type i which the variable venturi is formed by a movable throttle, a fuel nozzle discharging into the throat of said variable venturi, a fuel chamber associated therewith, pressure regulating means for maintaining the fuel in said chamber at a sub-atmospheric pressure, said pressure being higher than that in the throat of the variable venturi, means for creating said sub-atmospheric pressure comprising a fixed venturi 'having an air entrance in communication with the air entrance to the carburetor and having an exit in the mixture outlet from the carburetor, a passage connecting the throat of the xed venturi to the pressure regulating means in said fuel supply chamber, a device responsive to the pressure and to the temperature of the air in the air entrance leading to the carburetor, a, valve controlled thereby, a restricted air vent controlled by said valve and a passage communicating with the throat of the fixed venturi and adapted to supply air from said vent, to reduce the suction created by said ixed venturi.
ARLEIGH J. HESS.
US424021A 1941-12-22 1941-12-22 Carburetor Expired - Lifetime US2332716A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US424021A US2332716A (en) 1941-12-22 1941-12-22 Carburetor

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US424021A US2332716A (en) 1941-12-22 1941-12-22 Carburetor

Publications (1)

Publication Number Publication Date
US2332716A true US2332716A (en) 1943-10-26

Family

ID=23681127

Family Applications (1)

Application Number Title Priority Date Filing Date
US424021A Expired - Lifetime US2332716A (en) 1941-12-22 1941-12-22 Carburetor

Country Status (1)

Country Link
US (1) US2332716A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2502602A (en) * 1944-07-20 1950-04-04 Niles Bement Pond Co Flow restricting device
US2631024A (en) * 1948-02-13 1953-03-10 United Aircraft Corp Carburetor having a density responsive fuel control

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2502602A (en) * 1944-07-20 1950-04-04 Niles Bement Pond Co Flow restricting device
US2631024A (en) * 1948-02-13 1953-03-10 United Aircraft Corp Carburetor having a density responsive fuel control

Similar Documents

Publication Publication Date Title
US2224472A (en) Pressure fed carburetor
US3243167A (en) Constant vacuum type carburetor
US2367606A (en) Governor
GB523895A (en) Improvements in or relating to the feeding of fuel to internal combustion engines
US2836957A (en) Fuel control for a gas turbine power plant
US3477699A (en) Metering means
US2283021A (en) Pressure carburetor
US2447261A (en) Charge forming device
US2332716A (en) Carburetor
US2430693A (en) Hot-spot manifold
US2215683A (en) Carburetor
US2741089A (en) Controlling fuel supply for an aircraft gas turbine engine during acceleration at different altitudes
US2880579A (en) Automatic buzz control
US2438662A (en) Fuel injection system for internalcombustion engines
US2447263A (en) Charge forming device
US2447791A (en) Carburetor
US2389219A (en) Mixture control
US2443527A (en) Fuel supply system
US2705866A (en) De-icing for gas turbines
US2399077A (en) Power limiting carburetor
US2460528A (en) Carburetor
US2566012A (en) Carburetor
US2187885A (en) Carburetor
US2228000A (en) Airplane carburetor
US1945189A (en) Carburetor