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US2743961A - Needle nozzle for internal combustion engines - Google Patents

Needle nozzle for internal combustion engines Download PDF

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Publication number
US2743961A
US2743961A US253656A US25365651A US2743961A US 2743961 A US2743961 A US 2743961A US 253656 A US253656 A US 253656A US 25365651 A US25365651 A US 25365651A US 2743961 A US2743961 A US 2743961A
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Prior art keywords
needle
fuel
annular space
nozzle
seat
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US253656A
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L Orange Rudolf
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Priority to US253656A priority Critical patent/US2743961A/en
Priority to US520010A priority patent/US2769669A/en
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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
    • F02M61/00Fuel-injectors not provided for in groups F02M39/00 - F02M57/00 or F02M67/00
    • F02M61/04Fuel-injectors not provided for in groups F02M39/00 - F02M57/00 or F02M67/00 having valves, e.g. having a plurality of valves in series
    • F02M61/10Other injectors with elongated valve bodies, i.e. of needle-valve type
    • 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
    • F02M61/04Fuel-injectors not provided for in groups F02M39/00 - F02M57/00 or F02M67/00 having valves, e.g. having a plurality of valves in series
    • 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
    • F02M61/04Fuel-injectors not provided for in groups F02M39/00 - F02M57/00 or F02M67/00 having valves, e.g. having a plurality of valves in series
    • F02M61/10Other injectors with elongated valve bodies, i.e. of needle-valve type
    • F02M61/12Other injectors with elongated valve bodies, i.e. of needle-valve type characterised by the provision of guiding or centring means for valve bodies
    • 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
    • F02M2700/07Nozzles and injectors with controllable fuel supply
    • F02M2700/074Injection valve actuated by fuel pressure for pressurised fuel supply

Definitions

  • the combustion chamber of internal combustion engines especially Diesel engines having prec'ombustion or postcombustion chambers, frequently requires the injection of the fuel in a jet which widens into a relatively oblique conical surface.
  • the nozzle needles small pins which extend into the atomization bore and form, possible in cooperation with recesses, edges or the like provided in the nozzle bore, an annular gap through which the injected jet is expanded to a certain conical angle.
  • This construction affords difficulty in manufacture; especially due to the necessity of an absolutely accurate centering of the small pin with the seat.
  • annular gap which must have a width of a few hundredths of a millimeter, is exposed-to the danger of contamination, especially upon the stopping of the engine. These contaminations are mostly flushed away during the 'operation of thel'motor; but in the meantime, however, they encumber the starting of the engine by poor atomization.
  • the object of the present invention accordingly is to create a needle injection nozzle of the same manner of operation for various cone angles, which is not subject to these difficulties.
  • the solution of the problem is effected in accordance with the present invention thereby that the entrance of the fuel coming from the injection pump into the annular space which is arranged directly in front of the seat of the needle takes place over cross sections which are tangentially directed in such a manner that a rotational motion is produced in this annular space below the shoulder of the needle in front of the needle seat.
  • this rotary motion in combination with the selection of the diameter of the atomization opening, the length of the atomization opening and the stroke of the needle, there is then produced a wider or narrower atomization cone.
  • connection of this annular space to the annular space existing under the needle shoulder is then formed by the channels, the discharge of which into the annular space in front of the needle seat produces the rotation.
  • These connecting channels can be hollowed out in the form 'ice of helical grooves to the corresponding lower inlet amount.
  • the invention can therefore be applied to needle nozzles, the seat of which is developed in the customary manner as a conical valve, as well as to the known shapes of plane, fiat or annular seats in the valves; in which connection, of course, in the latter case, the influence of the passage of the fuel through the needle seat must be counted with greater weight among the factors determining the atomization shapes than in the former case.
  • the present invention is primarily intended for the injection shapes described in the preamble in a jet or cone lying in the needle axis; and therefore with an atomization bore lying in the needle axis, it is particularly applicable in special cases when the atomization bore is inclined to the needle axis; or when several atomization bores are present.
  • the influence of the measures in accordance with the present invention will, in such case, primarily act to impart to the corresponding nozzle jets a strong breaking-up and lesser penetrating force.
  • nozzle needle 3 fits tightly in the needle guide 4; and, toward the combustion chamber, seals 01f the way to the inlet opening 5 with the needle seat 6 developed as a flat seal.
  • the atomization bore 5 is arranged in the nozzle plate 7, which in its turn is pressed, together with the needle guide 4, against the nozzle holder 1 by the screw coupling 8.
  • the fuel passes through the fuel pressure path 9 out of the nozzle holder into the annular distribution space 10 of the needle guide. From the annular distribution space 10, the fuel is fed, via one or more fuel channels 11, to the upper annular space 12, which is produced by a corresponding groove in the nozzle needle 3 opposite the cylindrical wall of the needle guide 4.
  • the fuel can now only pass from the upper annular space 12 into the lower annular space 13 below the shoulder of the needle 3 through the helical grooves 14, so that it is rotated more or less forcibly, depending on the cross section and the direction of these helical grooves in the lower annular space 13. if the fuel pressure during the feed stroke of the injection pump rises so greatly below the needle shoulder in annular space 13 that the closing pressure of the coil spring 2 is overcome, needle 3 will rise and the seat 6 of the needle will open the path to the injection opening 5.
  • the atomization jet which emerges from the atomization here into the combustion chamber, has its shape decided on the one hand by the spring 2, the size of the needle shoulder above the annular space 13, the diameter of the needle 3 and the quantity delivered per unit of time by the injection pump; and also on the other hand, in accordance with the dimensions of the atomization bore 5 and the direction and velocity of the fuel rotating in the anmolar space 13. The greater the velocity and energy of the rotating components of the fuel, the Wider the fuel cone will be.
  • FIG. 2 there is shown an embodiment which differs from the one already described thereby that on the one hand instead of a flat seat needle, there is used a needle having a conical seat; and that further, the connecting paths between the upper annular space 12 and the annular space below the needle shoulder 13, which produces the rotation of the fuel, are brought about by tangential bores passing through the needle.
  • Figure 2 thus shows a needle nozzle element consisting of the needle guide 4 and the nozzle needle 3.
  • the fuel enters the upper annular space 12 through one or more atomization bores, said upper annular space being, produced in the present embodiment as a groove in the needle guide 4.
  • the connection of this annular space 12 with the lower annular space 13 below the needle shoulder is effected by two tangential bores 14 which conduct the fuel with greater or lesser rotation into the annular space 13.
  • This embodiment has the advantage that the cylindrical surface of the needle, with the exception of the small entrance places of the tangential bores 14, is not interrupted, which is of particular advantage for the bringing about of the best possible fit of the needle 3 in the needle guide 4, particularly between the upper annular space 12 and the lower annular space 13.
  • the seat 6 of needle 3 is arranged in this embodiment as a conical seat directly in the needle guide 4.
  • the atomization bore 5 is produced in the needle guide 4 itself.
  • Figure 3 is a section through the nozzle element according to Figure 2 at the height of the upper annular space 12 and of the tangential bores 14.
  • a fuel injection nozzle for internal combustion engines comprising a holder having a fuel passage therein, an elongated needle guide projecting outwardly from said holder and having a longitudinal bore extending to the outer end of said needle guide, a nozzle plate extending across the outer end of said needle guide and having a fuel atomizing port communicating with said bore and an annular seat surrounding said port, an annular groove in the inner end of said needle guide communicating with the fuel passage in said holder, circularly arranged fuel passages in said needle guide communicating with said annular groove and terminating in intake ports communicating with the bore at a point spaced axially inwardly of the bore from theouter end thereof, a needle having a sliding fit in the bore and having a portion between said intake ports and said fuel atomizing port closely fitting the bore, said needle having a reduced outer end portion provided with an end surface engageable with said annular seat to close said fuel atomizing port and forming an annular chamber around said reduced end portion at the outer end of said bore, a fuel passage in said needle extending

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

Description

y '1, 1956 R. L'ORANGE 2,743,961
NEEDLE NOZZLE FOR INTERNAL COMBUSTION ENGINES Filed Oct. 29, 195] iii E13.
I; I/I
IN VEN TOR. Aaa 04 F 4 'ORfl/VGE United States Patent NEEDLE NOZZLE FOR INTERNAL COMBUSTION ENGINES Rudolf LOrange, Glatten, near Freudenstadt in Wurttemberg, Germany This invention'relates to internal combustion engines, and refers more particularly to improvements in fuel injection means for such engines.
. The combustion chamber of internal combustion engines, especially Diesel engines having prec'ombustion or postcombustion chambers, frequently requires the injection of the fuel in a jet which widens into a relatively oblique conical surface. For this purpose there have been provided on the nozzle needles small pins which extend into the atomization bore and form, possible in cooperation with recesses, edges or the like provided in the nozzle bore, an annular gap through which the injected jet is expanded to a certain conical angle. This construction, however, affords difficulty in manufacture; especially due to the necessity of an absolutely accurate centering of the small pin with the seat. Furthermore the annular gap, which must have a width of a few hundredths of a millimeter, is exposed-to the danger of contamination, especially upon the stopping of the engine. These contaminations are mostly flushed away during the 'operation of thel'motor; but in the meantime, however, they encumber the starting of the engine by poor atomization.
The object of the present invention accordingly is to create a needle injection nozzle of the same manner of operation for various cone angles, which is not subject to these difficulties. The solution of the problem is effected in accordance with the present invention thereby that the entrance of the fuel coming from the injection pump into the annular space which is arranged directly in front of the seat of the needle takes place over cross sections which are tangentially directed in such a manner that a rotational motion is produced in this annular space below the shoulder of the needle in front of the needle seat. Depending on the intensity of this rotary motion, in combination with the selection of the diameter of the atomization opening, the length of the atomization opening and the stroke of the needle, there is then produced a wider or narrower atomization cone. In this connection there can also be produced nozzles of the same size atomization cone angle, in connection with which however the penetrating power varies, depending on the influence of the said factor. The admission cross sections which bring out the rotation in the annular space below the needle shoulder can be arranged in the needle guide itself, penetrating inwards to the needle guide bore from the outside. Such constructions can be realized in a particularly good manner in connection with needle seats which are separated from the cylindrical needle guides. From the point of manufacture, particularly practicable solutions result if these admission cross sections are hollowed out ofthe needle. In this case the annular space, which is ordinarily arranged around the needle, must be removed somewhat from the needle seat. The connection of this annular space to the annular space existing under the needle shoulder is then formed by the channels, the discharge of which into the annular space in front of the needle seat produces the rotation. These connecting channels can be hollowed out in the form 'ice of helical grooves to the corresponding lower inlet amount. A particularly advantageous solution, both for manufacture and operation, results if these connections consist of bores which lead, outside of the axis of the needle and at an inclination to same, from the annular space in the needle guide to the space below the needle shoulder. The invention can therefore be applied to needle nozzles, the seat of which is developed in the customary manner as a conical valve, as well as to the known shapes of plane, fiat or annular seats in the valves; in which connection, of course, in the latter case, the influence of the passage of the fuel through the needle seat must be counted with greater weight among the factors determining the atomization shapes than in the former case.
Although the present invention is primarily intended for the injection shapes described in the preamble in a jet or cone lying in the needle axis; and therefore with an atomization bore lying in the needle axis, it is particularly applicable in special cases when the atomization bore is inclined to the needle axis; or when several atomization bores are present. The influence of the measures in accordance with the present invention will, in such case, primarily act to impart to the corresponding nozzle jets a strong breaking-up and lesser penetrating force. In addition to this one improvement which the present invention can impart to all such-nozzle needle valves, is an improved protection of the needle seat from dirt particles, inasmuch as such particles are flushed away in a somewhat better manner; as well as, in those designs in which tangential cross sections are recessed out of the needle, an improvement of the life of the needleseat due to a continuous rotation of the needle seat.
The attached drawings show a number of embodiments by way of example, without it being intendedby this to exhaust the posssibility of the variants.
Referring to Fig. 1, there can be noted the lower end of the nozzle holder 1, the coil spring 2 of which acts against the nozzle needle 3. The nozzle needle 3 fits tightly in the needle guide 4; and, toward the combustion chamber, seals 01f the way to the inlet opening 5 with the needle seat 6 developed as a flat seal. The atomization bore 5 is arranged in the nozzle plate 7, which in its turn is pressed, together with the needle guide 4, against the nozzle holder 1 by the screw coupling 8. During the feed stroke of the injection pump, the fuel passes through the fuel pressure path 9 out of the nozzle holder into the annular distribution space 10 of the needle guide. From the annular distribution space 10, the fuel is fed, via one or more fuel channels 11, to the upper annular space 12, which is produced by a corresponding groove in the nozzle needle 3 opposite the cylindrical wall of the needle guide 4.
The fuel can now only pass from the upper annular space 12 into the lower annular space 13 below the shoulder of the needle 3 through the helical grooves 14, so that it is rotated more or less forcibly, depending on the cross section and the direction of these helical grooves in the lower annular space 13. if the fuel pressure during the feed stroke of the injection pump rises so greatly below the needle shoulder in annular space 13 that the closing pressure of the coil spring 2 is overcome, needle 3 will rise and the seat 6 of the needle will open the path to the injection opening 5. The atomization jet, which emerges from the atomization here into the combustion chamber, has its shape decided on the one hand by the spring 2, the size of the needle shoulder above the annular space 13, the diameter of the needle 3 and the quantity delivered per unit of time by the injection pump; and also on the other hand, in accordance with the dimensions of the atomization bore 5 and the direction and velocity of the fuel rotating in the anmolar space 13. The greater the velocity and energy of the rotating components of the fuel, the Wider the fuel cone will be.
In Figure 2 there is shown an embodiment which differs from the one already described thereby that on the one hand instead of a flat seat needle, there is used a needle having a conical seat; and that further, the connecting paths between the upper annular space 12 and the annular space below the needle shoulder 13, which produces the rotation of the fuel, are brought about by tangential bores passing through the needle.
Figure 2 thus shows a needle nozzle element consisting of the needle guide 4 and the nozzle needle 3. Also in this case the fuel enters the upper annular space 12 through one or more atomization bores, said upper annular space being, produced in the present embodiment as a groove in the needle guide 4. The connection of this annular space 12 with the lower annular space 13 below the needle shoulder is effected by two tangential bores 14 which conduct the fuel with greater or lesser rotation into the annular space 13. This embodiment has the advantage that the cylindrical surface of the needle, with the exception of the small entrance places of the tangential bores 14, is not interrupted, which is of particular advantage for the bringing about of the best possible fit of the needle 3 in the needle guide 4, particularly between the upper annular space 12 and the lower annular space 13. The seat 6 of needle 3 is arranged in this embodiment as a conical seat directly in the needle guide 4. Similarly, the atomization bore 5 is produced in the needle guide 4 itself.
Figure 3 is a section through the nozzle element according to Figure 2 at the height of the upper annular space 12 and of the tangential bores 14.
What I claim as my invention is:
A fuel injection nozzle for internal combustion engines, comprising a holder having a fuel passage therein, an elongated needle guide projecting outwardly from said holder and having a longitudinal bore extending to the outer end of said needle guide, a nozzle plate extending across the outer end of said needle guide and having a fuel atomizing port communicating with said bore and an annular seat surrounding said port, an annular groove in the inner end of said needle guide communicating with the fuel passage in said holder, circularly arranged fuel passages in said needle guide communicating with said annular groove and terminating in intake ports communicating with the bore at a point spaced axially inwardly of the bore from theouter end thereof, a needle having a sliding fit in the bore and having a portion between said intake ports and said fuel atomizing port closely fitting the bore, said needle having a reduced outer end portion provided with an end surface engageable with said annular seat to close said fuel atomizing port and forming an annular chamber around said reduced end portion at the outer end of said bore, a fuel passage in said needle extending from said intake port to said annular chamber andbeing in the form of a groove in the outer surface of said needle extending helically with respect to the axis thereof, and means for clamping together said needle guide, nozzle plate and holder comprising a coupling sleeve surrounding said needle guide and having an outer end turned radially inwardly to overlie and abut the outer end of said nozzle plate, and a releasable connection between the outer end of said holder and the inner end of said sleeve.
References Cited in the file of this patent UNITED STATES PATENTS 1,964,218 Schargorodsky June 26, 1934 2,110,365 Infeld Mar. 8, 1938 FOREIGN PATENTS 258,431 Great Britain Sept. 23, 1926 273,251 Great Britain of 1928 371,572 Germany Mar. 16, 1923 551,912 Great Britain Mar. 15, 1943
US253656A 1951-10-29 1951-10-29 Needle nozzle for internal combustion engines Expired - Lifetime US2743961A (en)

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US253656A US2743961A (en) 1951-10-29 1951-10-29 Needle nozzle for internal combustion engines
US520010A US2769669A (en) 1951-10-29 1955-07-05 Needle nozzle for internal combustion engines

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5012981A (en) * 1986-07-19 1991-05-07 Robert Bosch Gmbh Injection valve

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE371572C (en) * 1923-03-16 Heinrich Kaemper Injection valve with cleaning needle for direct injection of fuel into the compression chamber or the ignition chamber or the glow head of an internal combustion engine
GB258431A (en) * 1925-09-29 1926-09-23 Herbert Vincent Senior Improvements in or relating to spraying nozzles for liquids
GB273251A (en) * 1926-06-28 1928-03-29 Hatz Motoren Improvements in injection valves for internal combustion engines
US1964218A (en) * 1931-03-17 1934-06-26 Firm Hannoversche Maschb Actie Means for filtering the fuel supplied to the injector nozzles of internal combustion engines
US2110365A (en) * 1936-02-22 1938-03-08 Saurer Ag Adolph Injection nozzle for internal combustion engines
GB551912A (en) * 1941-03-12 1943-03-15 Scintilla Ltd Fuel injector for internal combustion engines

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE371572C (en) * 1923-03-16 Heinrich Kaemper Injection valve with cleaning needle for direct injection of fuel into the compression chamber or the ignition chamber or the glow head of an internal combustion engine
GB258431A (en) * 1925-09-29 1926-09-23 Herbert Vincent Senior Improvements in or relating to spraying nozzles for liquids
GB273251A (en) * 1926-06-28 1928-03-29 Hatz Motoren Improvements in injection valves for internal combustion engines
US1964218A (en) * 1931-03-17 1934-06-26 Firm Hannoversche Maschb Actie Means for filtering the fuel supplied to the injector nozzles of internal combustion engines
US2110365A (en) * 1936-02-22 1938-03-08 Saurer Ag Adolph Injection nozzle for internal combustion engines
GB551912A (en) * 1941-03-12 1943-03-15 Scintilla Ltd Fuel injector for internal combustion engines

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5012981A (en) * 1986-07-19 1991-05-07 Robert Bosch Gmbh Injection valve

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