US2733960A - Barfod - Google Patents

Barfod Download PDF

Info

Publication number
US2733960A
US2733960A US2733960DA US2733960A US 2733960 A US2733960 A US 2733960A US 2733960D A US2733960D A US 2733960DA US 2733960 A US2733960 A US 2733960A
Authority
US
United States
Prior art keywords
nozzle
valve
insert
passage
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.)
Expired - Lifetime
Application number
Publication date
Application granted granted Critical
Publication of US2733960A publication Critical patent/US2733960A/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
    • F02M61/00Fuel-injectors not provided for in groups F02M39/00 - F02M57/00 or F02M67/00
    • F02M61/16Details not provided for in, or of interest apart from, the apparatus of groups F02M61/02 - F02M61/14
    • F02M61/18Injection nozzles, e.g. having valve seats; Details of valve member seated ends, not otherwise provided for
    • F02M61/188Spherical or partly spherical shaped valve member ends
    • 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
    • F02M61/00Fuel-injectors not provided for in groups F02M39/00 - F02M57/00 or F02M67/00
    • F02M61/16Details not provided for in, or of interest apart from, the apparatus of groups F02M61/02 - F02M61/14
    • F02M61/162Means to impart a whirling motion to fuel upstream or near discharging orifices
    • 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
    • F02M61/00Fuel-injectors not provided for in groups F02M39/00 - F02M57/00 or F02M67/00
    • F02M61/16Details not provided for in, or of interest apart from, the apparatus of groups F02M61/02 - F02M61/14
    • F02M61/18Injection nozzles, e.g. having valve seats; Details of valve member seated ends, not otherwise provided for
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23DBURNERS
    • F23D11/00Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space
    • F23D11/36Details, e.g. burner cooling means, noise reduction means
    • F23D11/38Nozzles; Cleaning devices therefor
    • F23D11/383Nozzles; Cleaning devices therefor with swirl means

Definitions

  • An object of the invention is to provide a fuel injection nozzle which is efficient in operation and at the same time is usually simple in design and embodies a minimum number of parts.
  • Another object is to provide a fuel injection nozzle embodying an inlet passage controlled by a simple springpressed check valve and having a coacting nozzle insert so constructed and arranged as to avoid disturbance of the spray cone due to fluctuation or instability of the check valve while the latter is unseated and held open due to a build-up in fuel pressure in the inlet passage.
  • Figure 1 illustrates in substantially central longitudinal section a nozzle constructed in accordance with the invention
  • Figure 2 is a section taken substantially on the line 22, Figure 1, and
  • Figure 3 is a substantially central longitudinal section of a modification, only the discharge extremity of the nozzle being shown.
  • a hollow nozzle body is indicated at 10, and in the particular form shown, it is adapted to be inserted in the combustion chamber or cylinder of a reciprocating internal combustion engine, where injection is usually timed to occur at the end of the compression stroke.
  • a central elongated chamber 11 is defined by the body 10, which at one end is enlarged and internally threaded as at 12, to receive an externally-threaded fuel conduit and valve seat member 13 formed with a central passage 14, terminating in a valve seat 15.
  • the entrance end of the passage is shown enlarged and formed with a wrench socket 16, to facilitate tightening of the member 13 in its socket.
  • the external threads of the member 13 and the coacting threads 12 of the body are preferably of a reduced or relatively steep helical angle, so that if a reasonable amount of torque is used in installation of said member, it will be held securely in place by friction.
  • the entrance end of the passage 14 is adapted to receive one of the fuel lines from an injection pump.
  • a check valve 17 is adapted to engage a seat 15 and close the discharge end of the passage 14 until sufiicient pressure is built up to unseat said valve.
  • the check valve 17 is in the form of a substantially flat disc, such type of valve being preferred since it has been found "ice to effectively serve the desired function while tending toward economy in manufacture.
  • a nozzle insert is indicated at 18; it is provided with a reduced inwardly projecting portion 19, terminating in a valve stop 19.
  • a spring 20 encircles the portion 19 and seats at one end on a shoulder 21, the opposite free end of the spring engaging the check valve.
  • the nozzle insert At its discharge end the nozzle insert is formed with a series of passages 22, which are formed at a tangent to a central swirl chamber or discharge opening 23, from which the fuel is discharged in the form of a substantially cone-shaped spray.
  • a series of passages 22 which are formed at a tangent to a central swirl chamber or discharge opening 23, from which the fuel is discharged in the form of a substantially cone-shaped spray.
  • annular shoulder 24 in the tip end of the valve body 10, against which a similar shoulder 25 formed on the insert engages, the end, of the body 10 being peened over the latter shoulder.
  • the check valve 17 Due to the fact that the check valve 17 is limited in its opening movement and then brought up against the stop 19', the said valve remains fixed during the discharge of fuel and does not flutter or fluctuate and thus affect the nozzle spray, as would be the case were the valve supported by the spring only.
  • the simplicity of the nozzle assembly is obvious.
  • the member 13 may be readily removed when it is desired to inspect and clean the nozzle.
  • the valve seat member 13 may be readily fabricated to obtain the most effective length and area of passage 14 and seating surface for valve 17.
  • Figure 3 illustrates a modified construction in the nozzle insert and associated check valve of Figures 1 and 2.
  • parts which correspond to related parts in Figures 1 and 2 are designated by similar reference numerals except that a prime has been added.
  • An orifice plate 27 is removably secured over the discharge opening 23, and this together with the nozzle insort and associated check valve assembly are removable from the discharge end of the nozzle.
  • the orifice plate may have an orifice 28 therein contoured to obtain a discharge spray having the desired characteristics as to shape, spray angle, etc.
  • a ball type is used as indicated at 29.
  • the operation in Figure 3 is essentially the same as above described, the check valve 29 being limited in its opening movement as it is brought up against the stop 19".
  • a fluid spray nozzle comprising a hollow body having an inlet and an outlet; an internal annular recess in said body adjacent the outlet, a nozzle insert formed with an annular projection for engagement with said recess, an inwardly extending annular shoulder on said insert spaced from said body; an inwardly projecting portion on said insert spaced farther from said body than said shoulder; a helical spring of smaller diameter than said shoulder encircling said portion; a seat mern ber secured in said body adjacent the inlet; a longitudinal passage through said member; a chamber defined by said insert, scat member and body; a valve in sai chamber formed to seat on said member and to T4353.- ulate communication between said passage and chamber; said valve urged in a seating direction by said spring and limited in movement in the opposite direction by said projecting portion; a cylindrical discharge orifice centrally located in said insert unrestrictedly in communication with said outlet; a plurality of passages in said shoulder tangentially intersecting said orifice and opening directly
  • a fluid spray nozzle comprising a hollow body having an'inlet and an outlet; a nozzle insert secured insaid body adjaceutthe outlet thereof; an inwardly extending annular shoulder on said insert spaced from said body; an imperforate stepped down portion on said insert projecting inwardly from said shoulder; a seat member secured in said body adjacent the inlet; a longitudinal passage through said member; a chamber in said body defined by said seat member and insert; a valve in said chamber adapted to seat on one of said members to control communication between said passage and [i chamber; a spring encircling said portion formed at one end to abut said shoulder; said valve urged in a seat ing direction by said spring, and limited in movement in the opposite direction by said projecting portion; a discharge orifice in said insert; and a plurality of passages in said shoulder tangentially intersecting said orifice and terminating in said chamber.

Description

Feb. 7, 1956 F. BARFOD 2,733,960
FUEL INJECTION NOZZLES Filed June 11, 1952 IN VEN TOR.
J 1 z FPfDER/K BAP/'00 ATTOF/Vf) United States Patent FUEL INJECTION NOZZLES Frederik Barfod, South Bend, Ind., assignor to Bendix Aviation Corporation, South Bend, Ind., a corporation of Delaware Application June 11, 1952, Serial No. 292,879
2 Claims. (Ci. 299-1016) The type of nozzle to which the present invention relates is particularly adapted for spraying fuel either directly into the combustion chambers or into the fuel manifolds of reciprocating internal combustion engines and gas turbine engines. One of the problems which gave rise to the instant invention was to provide a nozzle for installations where mass production and low retail costs demand simplicity in design and economy in manufacture.
An object of the invention, therefore, is to provide a fuel injection nozzle which is efficient in operation and at the same time is usually simple in design and embodies a minimum number of parts.
Another object is to provide a fuel injection nozzle embodying an inlet passage controlled by a simple springpressed check valve and having a coacting nozzle insert so constructed and arranged as to avoid disturbance of the spray cone due to fluctuation or instability of the check valve while the latter is unseated and held open due to a build-up in fuel pressure in the inlet passage.
The foregoing and other objects and advantages will become apparent in view of the following descriptions taken in conjunction with the drawing, wherein:
Figure 1 illustrates in substantially central longitudinal section a nozzle constructed in accordance with the invention,
Figure 2 is a section taken substantially on the line 22, Figure 1, and
Figure 3 is a substantially central longitudinal section of a modification, only the discharge extremity of the nozzle being shown.
Referring to Figures 1 and 2 of the drawing, a hollow nozzle body is indicated at 10, and in the particular form shown, it is adapted to be inserted in the combustion chamber or cylinder of a reciprocating internal combustion engine, where injection is usually timed to occur at the end of the compression stroke. A central elongated chamber 11 is defined by the body 10, which at one end is enlarged and internally threaded as at 12, to receive an externally-threaded fuel conduit and valve seat member 13 formed with a central passage 14, terminating in a valve seat 15. The entrance end of the passage is shown enlarged and formed with a wrench socket 16, to facilitate tightening of the member 13 in its socket. It is preferred to have the external threads of the member 13 and the coacting threads 12 of the body of a reduced or relatively steep helical angle, so that if a reasonable amount of torque is used in installation of said member, it will be held securely in place by friction. As will be obvious, the entrance end of the passage 14 is adapted to receive one of the fuel lines from an injection pump.
A check valve 17 is adapted to engage a seat 15 and close the discharge end of the passage 14 until sufiicient pressure is built up to unseat said valve. As shown, the check valve 17 is in the form of a substantially flat disc, such type of valve being preferred since it has been found "ice to effectively serve the desired function while tending toward economy in manufacture. A nozzle insert is indicated at 18; it is provided with a reduced inwardly projecting portion 19, terminating in a valve stop 19. A spring 20 encircles the portion 19 and seats at one end on a shoulder 21, the opposite free end of the spring engaging the check valve. At its discharge end the nozzle insert is formed with a series of passages 22, which are formed at a tangent to a central swirl chamber or discharge opening 23, from which the fuel is discharged in the form of a substantially cone-shaped spray. To retain the insert 18 in position, it is preferred to form an annular shoulder 24 in the tip end of the valve body 10, against which a similar shoulder 25 formed on the insert engages, the end, of the body 10 being peened over the latter shoulder.
Operation When the pressure of fuel in the passage 14 attains a predetermined value as determined by the strength of the Spring 20, it unseats the valve 17 and moves the latter against the stop 19', whereupon the fuel is free to pass through passage 26 and thence to the tangential passages 22, into the swirl chamber 23, from which it is discharged in a substantially cone-shaped spray. The characteristics of the spray, such as atomization, penetration and spray angle are determined by the proper size of the tangential holes 22 and their location in relation to the swirl chamber 23.
Due to the fact that the check valve 17 is limited in its opening movement and then brought up against the stop 19', the said valve remains fixed during the discharge of fuel and does not flutter or fluctuate and thus affect the nozzle spray, as would be the case were the valve supported by the spring only.
The simplicity of the nozzle assembly is obvious. The member 13 may be readily removed when it is desired to inspect and clean the nozzle. The valve seat member 13 may be readily fabricated to obtain the most effective length and area of passage 14 and seating surface for valve 17.
Figure 3 illustrates a modified construction in the nozzle insert and associated check valve of Figures 1 and 2. In the modification of Figure 3, parts which correspond to related parts in Figures 1 and 2 are designated by similar reference numerals except that a prime has been added.
An orifice plate 27 is removably secured over the discharge opening 23, and this together with the nozzle insort and associated check valve assembly are removable from the discharge end of the nozzle. The orifice plate may have an orifice 28 therein contoured to obtain a discharge spray having the desired characteristics as to shape, spray angle, etc. Also, instead of the fiat check valve of Figures 1 and 2 a ball type is used as indicated at 29. The operation in Figure 3 is essentially the same as above described, the check valve 29 being limited in its opening movement as it is brought up against the stop 19".
Although only two forms of the improved nozzle are shown, certain limited changes in design to suit difierent installations will be obvious to those having a knowledge of the art.
I claim:
1. A fluid spray nozzle comprising a hollow body having an inlet and an outlet; an internal annular recess in said body adjacent the outlet, a nozzle insert formed with an annular projection for engagement with said recess, an inwardly extending annular shoulder on said insert spaced from said body; an inwardly projecting portion on said insert spaced farther from said body than said shoulder; a helical spring of smaller diameter than said shoulder encircling said portion; a seat mern ber secured in said body adjacent the inlet; a longitudinal passage through said member; a chamber defined by said insert, scat member and body; a valve in sai chamber formed to seat on said member and to T4353.- ulate communication between said passage and chamber; said valve urged in a seating direction by said spring and limited in movement in the opposite direction by said projecting portion; a cylindrical discharge orifice centrally located in said insert unrestrictedly in communication with said outlet; a plurality of passages in said shoulder tangentially intersecting said orifice and opening directly into said chamber.
2. A fluid spray nozzle comprising a hollow body having an'inlet and an outlet; a nozzle insert secured insaid body adjaceutthe outlet thereof; an inwardly extending annular shoulder on said insert spaced from said body; an imperforate stepped down portion on said insert projecting inwardly from said shoulder; a seat member secured in said body adjacent the inlet; a longitudinal passage through said member; a chamber in said body defined by said seat member and insert; a valve in said chamber adapted to seat on one of said members to control communication between said passage and [i chamber; a spring encircling said portion formed at one end to abut said shoulder; said valve urged in a seat ing direction by said spring, and limited in movement in the opposite direction by said projecting portion; a discharge orifice in said insert; and a plurality of passages in said shoulder tangentially intersecting said orifice and terminating in said chamber.
References Cited in the file of this patent UNITED STATES PATENTS 1,011,036 Dahl Dec. 5, 19 11 1,505,331 Gold Aug. 19, 1924 2,247,520 Paxton July 1, 1941 2,568,240 Mart Sept. 18, 1951 2,571,501 Truxell Oct. 16, 1951 2,590,772 Joyce Mar. 25, 1952 2,636,778 Michelsen Apr. 28, 1953 2,665,167 High Jan. 5, 1954 FOREIGN PATENTS 208,219 Great Britain Dec. 13, 1923 374,570 Italy Aug. 31, 1939 804,852 France Aug. 10, 1 936
US2733960D Barfod Expired - Lifetime US2733960A (en)

Publications (1)

Publication Number Publication Date
US2733960A true US2733960A (en) 1956-02-07

Family

ID=3443505

Family Applications (1)

Application Number Title Priority Date Filing Date
US2733960D Expired - Lifetime US2733960A (en) Barfod

Country Status (1)

Country Link
US (1) US2733960A (en)

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2805891A (en) * 1954-04-05 1957-09-10 Mcculloch Motors Corp Fluid spray nozzle
US2961741A (en) * 1956-05-09 1960-11-29 American Steel Foundries Hydraulic descaler
US3097752A (en) * 1960-10-12 1963-07-16 Miehle Goss Dexter Inc Cutting knife-stack support
US3223331A (en) * 1962-08-21 1965-12-14 Clarence P Baker Oil burner nozzles
DE1275828B (en) * 1963-02-04 1968-08-22 Martin J Berlyn Hole nozzle for fuel injection in internal combustion engines
US3406912A (en) * 1966-05-09 1968-10-22 Bosch Arma Corp Capsulated fuel injection nozzle
US3406910A (en) * 1966-05-20 1968-10-22 Parker Hannifin Corp Fuel injection nozzle
US4394973A (en) * 1980-04-03 1983-07-26 Robert Bosch Gmbh Injection valve
US4981266A (en) * 1981-05-30 1991-01-01 Robert Bosch Gmbh Injection valve
WO2017112842A1 (en) 2015-12-22 2017-06-29 Nostrum Energy Pte. Ltd. Liquid atomizing nozzle insert with colliding jets

Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1011036A (en) * 1911-08-02 1911-12-05 Union Iron Works Co Liquid-atomizer.
GB208219A (en) * 1922-09-13 1923-12-13 White & Co Ltd Samuel Improvements in or relating to fuel injection devices for semi-diesel engines
US1505331A (en) * 1921-03-28 1924-08-19 Weber Engine Company Spraying nozzle for oil engines
FR804852A (en) * 1935-04-13 1936-11-04 Injector nozzle for combustion engines
US2247520A (en) * 1939-06-13 1941-07-01 Curtis Anti Vapor Pumps Inc Check valve
US2568240A (en) * 1947-05-26 1951-09-18 Marley Company Inc Spray nozzle
US2571501A (en) * 1945-08-17 1951-10-16 Gen Motors Corp Fuel injection pump
US2590772A (en) * 1943-06-11 1952-03-25 Power Jets Res & Dev Ltd Liquid fuel burner and the like
US2636778A (en) * 1948-08-27 1953-04-28 Michelsen Karl Apparatus for atomizing liquids
US2665167A (en) * 1951-07-06 1954-01-05 Carl F High Fuel injection nozzle

Patent Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1011036A (en) * 1911-08-02 1911-12-05 Union Iron Works Co Liquid-atomizer.
US1505331A (en) * 1921-03-28 1924-08-19 Weber Engine Company Spraying nozzle for oil engines
GB208219A (en) * 1922-09-13 1923-12-13 White & Co Ltd Samuel Improvements in or relating to fuel injection devices for semi-diesel engines
FR804852A (en) * 1935-04-13 1936-11-04 Injector nozzle for combustion engines
US2247520A (en) * 1939-06-13 1941-07-01 Curtis Anti Vapor Pumps Inc Check valve
US2590772A (en) * 1943-06-11 1952-03-25 Power Jets Res & Dev Ltd Liquid fuel burner and the like
US2571501A (en) * 1945-08-17 1951-10-16 Gen Motors Corp Fuel injection pump
US2568240A (en) * 1947-05-26 1951-09-18 Marley Company Inc Spray nozzle
US2636778A (en) * 1948-08-27 1953-04-28 Michelsen Karl Apparatus for atomizing liquids
US2665167A (en) * 1951-07-06 1954-01-05 Carl F High Fuel injection nozzle

Cited By (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2805891A (en) * 1954-04-05 1957-09-10 Mcculloch Motors Corp Fluid spray nozzle
US2961741A (en) * 1956-05-09 1960-11-29 American Steel Foundries Hydraulic descaler
US3097752A (en) * 1960-10-12 1963-07-16 Miehle Goss Dexter Inc Cutting knife-stack support
US3223331A (en) * 1962-08-21 1965-12-14 Clarence P Baker Oil burner nozzles
DE1275828B (en) * 1963-02-04 1968-08-22 Martin J Berlyn Hole nozzle for fuel injection in internal combustion engines
US3406912A (en) * 1966-05-09 1968-10-22 Bosch Arma Corp Capsulated fuel injection nozzle
US3406910A (en) * 1966-05-20 1968-10-22 Parker Hannifin Corp Fuel injection nozzle
US4394973A (en) * 1980-04-03 1983-07-26 Robert Bosch Gmbh Injection valve
US4981266A (en) * 1981-05-30 1991-01-01 Robert Bosch Gmbh Injection valve
WO2017112842A1 (en) 2015-12-22 2017-06-29 Nostrum Energy Pte. Ltd. Liquid atomizing nozzle insert with colliding jets
CN109477450A (en) * 2015-12-22 2019-03-15 秘方能源私人有限公司 Liquid atomizing nozzle insertion piece with impacting jet
EP3394421A4 (en) * 2015-12-22 2019-10-16 Nostrum Energy Pte. Ltd. Liquid atomizing nozzle insert with colliding jets
CN109477450B (en) * 2015-12-22 2021-06-15 秘方能源私人有限公司 Liquid atomizing nozzle insert with impinging jet

Similar Documents

Publication Publication Date Title
US1952816A (en) Fuel injector
US2733960A (en) Barfod
US1834061A (en) Fuel nozzle
US4467965A (en) Fuel injection nozzles
US2898051A (en) Fluid injection device
US2382151A (en) Fuel injector
US2172556A (en) Fuel injector
US2096581A (en) Fuel injection valve
US3095153A (en) Variable area spray nozzle
US3029029A (en) Dual-orifice return flow nozzle
ES382122A1 (en) Fuel injection nozzles
US2351965A (en) Nozzle
US1755192A (en) Atomizing valve
US2753217A (en) Fuel injection nozzle for internal combustion engine
US3531052A (en) Fuel injector for internal combustion engines
GB2108579A (en) Fuel injector for internal combustion engines
US2901185A (en) Dampened pintle nozzle
US2556369A (en) Accumulator type injection nozzle
US4413780A (en) Fuel injection nozzles
US3528613A (en) Fuel injector for internal combustion engines
US2572606A (en) Burner nozzle
US3032279A (en) Nozzle construction
US2827922A (en) Stream-lined check-valve
US2986342A (en) Fuel injection nozzle
US2569033A (en) Burner nozzle