US3687375A - Fuel injection apparatus for internal combustion engines - Google Patents
Fuel injection apparatus for internal combustion engines Download PDFInfo
- Publication number
- US3687375A US3687375A US76581A US3687375DA US3687375A US 3687375 A US3687375 A US 3687375A US 76581 A US76581 A US 76581A US 3687375D A US3687375D A US 3687375DA US 3687375 A US3687375 A US 3687375A
- Authority
- US
- United States
- Prior art keywords
- tube
- outlets
- end portion
- outlet
- fuel injection
- 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
Links
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M61/00—Fuel-injectors not provided for in groups F02M39/00 - F02M57/00 or F02M67/00
- F02M61/16—Details not provided for in, or of interest apart from, the apparatus of groups F02M61/02 - F02M61/14
- F02M61/18—Injection nozzles, e.g. having valve seats; Details of valve member seated ends, not otherwise provided for
- F02M61/1806—Injection nozzles, e.g. having valve seats; Details of valve member seated ends, not otherwise provided for characterised by the arrangement of discharge orifices, e.g. orientation or size
- F02M61/184—Discharge orifices having non circular sections
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M61/00—Fuel-injectors not provided for in groups F02M39/00 - F02M57/00 or F02M67/00
- F02M61/02—Fuel-injectors not provided for in groups F02M39/00 - F02M57/00 or F02M67/00 of valveless type
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M61/00—Fuel-injectors not provided for in groups F02M39/00 - F02M57/00 or F02M67/00
- F02M61/16—Details not provided for in, or of interest apart from, the apparatus of groups F02M61/02 - F02M61/14
- F02M61/18—Injection nozzles, e.g. having valve seats; Details of valve member seated ends, not otherwise provided for
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M61/00—Fuel-injectors not provided for in groups F02M39/00 - F02M57/00 or F02M67/00
- F02M61/16—Details not provided for in, or of interest apart from, the apparatus of groups F02M61/02 - F02M61/14
- F02M61/18—Injection nozzles, e.g. having valve seats; Details of valve member seated ends, not otherwise provided for
- F02M61/1806—Injection nozzles, e.g. having valve seats; Details of valve member seated ends, not otherwise provided for characterised by the arrangement of discharge orifices, e.g. orientation or size
- F02M61/1846—Dimensional characteristics of discharge orifices
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M69/00—Low-pressure fuel-injection apparatus ; Apparatus with both continuous and intermittent injection; Apparatus injecting different types of fuel
- F02M69/04—Injectors peculiar thereto
Definitions
- a multi-outlet fuelinjection nonle is formed from metal tube which at one end is inwardly-deformed so that portions of the wall of the tube are compressed together and divide the interior of the end of the tube into two or more passages which extend longitudinally of the tube and form tubular injection outlets of the nozzle each having a cross-section which tapers laterally of the tube.
- An object of the present invention is to provide a multi-outlet fuel injection nozzle formed from elongate metal tube an end portion of which is inwardly deformed so that portions of the wall of the tube are compressed against one another and divide the interior of the tube into two or more longitudinally extending passages which form tubular injection outlets of the nozzle each having a cross-section which tapers laterally of the tube.
- the nozzle has been designed principally for the injection of fuel supplied to the nozzle under relatively low pressures, for example of the order of 15 to 30 pounds per square inch, and it is when operating under these conditions that the best results are obtained. It is possible, however, that satisfactory results might be obtained from a nozzle in accordance with the invention to which in use fuel is supplied at a higher pressure.
- the length of the tubular outlets effects the formof the sprays in which the fuel emerges from the outlets. If the outlets are only short in length, say less than threesixteenths inch long, widely spread sprays are produced. If the outlets are fairly long, say more than one-fourth inch in length, then the resultant sprays tend to be narrow, the sprays becoming narrower and approaching stream form as the length of the outlets is increased.
- the ideal length for most applications is a compromise between these two forms, and hence it is normally desirable for the outlets to be of the order of three-sixteenths to one-fourth inches in length.
- a thin-walled tube will normally be used.
- the wall thickness is preferably in the order of 0.020 to 0.030 inches.
- the tube may be of any suitable metal. Stainless steel is particularly suitable.
- the tube may be deformed by pressing rolling or in any other appropriate way.
- outlets may be formed, as desired, the maximum number which it is possible to form depending upon the cross-sectional size of the tube used and the cross-sectional sizes of the outlets required.
- the outlets may be of similar or different cross-sec tional sizes and shapes.
- the wall of the tube may be deformed so that the tubular outlets thus formed extend parallel to one another in a row, or so that the outlets are angularly disposed about the main, longitudinal, axis of the tube.
- the end ones of the row are preferably of generally tear-drop shape in cross-section, although they may possibly be of other shapes such as, for example, substantially arrow or diamond shaped.
- the other outlet or outlets intermediate the end ones of the row may be substantially oval shape in cross-section. They may taper to sharp points at the narrower ends of their cross-sectional shape.
- the sides of the outlets may converge linearly to meet at the narrower ends of their cross-section, or they may converge in concave curves to the narrower ends, or converge in convex curves so that the narrower endsare cuspidated.
- the outlet or outlets intermediate the end ones of the row may be of generally diamond shape in cross-section, or possibly be bicuspid.
- outlets angularlydisposed about the main axis of the tube they are preferably of tear-drop shape in cross-section, the taper being towards the main axis of the tube.
- they may possibly be of other shapes such as of a row of outlets.
- a central outlet may also be formed at or near the main axis of the tube, its shape depending upon the number and form of the surrounding outlets. Where the surrounding outlets are of tear-drop shape, the central outlet will normally be of substantially star shape in cross-section with three or more points.
- FIG. 1 is a perspective view of a fuel injection nozzle in accordance with the present invention having two injection outlets;
- FIG. 2 is a fragmentary perspective view of the discharge end of a fuel injection nozzle having four injection outlets disposed side-by-side in a row;
- FIG. 3 is a fragmentary perspective view of the discharge end of another fuel injection nozzle which has four injection outlets but in which the outlets are disposed in a square, and
- FIGS. 4 and 5 are further fragmentary perspective views of the discharge ends of fuel injection nozzles having respectively three and five injection outlets.
- the fuel injection nozzles are made of thin-walled metal, preferably stainless steel, tubing.
- the end forms of the injection nozzles are exaggerated in the drawings in order that they may be clearly understood.
- the tubes are in each case designated generally be reference 10.
- the fuel injection nozzle shown in FIG. 1 has just two tubular injection outlets 11 which are disposed side-byside.
- the outlets 11 are formed by compressing tightly against one another diametrically opposite portions 12 of the tube at the end of the tube, so that passages are formed at opposite ends of a diameter of the tube 10, which passages extend longitudinally of the tube and constitute the outlets 11.
- the end of the tube 10 may be compressed by any convenient means.
- the outlets 11 thus formed are of similar size and shape. They could be of disimilar sizes if desired. In this instance the outlets are tear-drop shaped in cross-section, the narrow ends of their cross-sections being directed'inwardly towards the main, longitudinal, axis of the tube 10. i
- the fuel injection nozzle has four tubular injection outlets 11 extending parallel to one another in a row.
- the outlets 11 are produced by compressing the end of the tube 10 from opposite sides so/longitudinally extending Ithat corrugations 13 are formed.
- the valley portions 14 of the corrugations 13 of the one side of the compressed tube end meet the valley portions 14 of the corrugations of the opposite side along a diameter of the tube 10.
- the injection outlets 11 are defined by the passages left between opposed ridge portions 15 of the corrugations 13 of the two sides of the compressed tube end. Three or more than four parallel injection outlets 11 may be formed in this manner, if required. As will be seen in FIG.
- the end outlets ll of the row are of substantially tear-drop shape in cross-section with their narrower ends directed inwardly towards the main axis of the tube 10.
- the other two, intermediate, outlets 11 are of modified oval shape in cross-section, their narrower ends being cuspidated.
- the fuel injection nozzles shown respectively have three and four tubular injection outlets II which are angularly disposed about the main axis of the tube 10.
- the outlets 11 are formed by passages produced by pressing angularly spaced apart portions 16 of the wall of the tube 10 inwardly so that the portions 16 meet and are compressed together at the center of the tube.
- the outlets 11 thus formed are of tear-drop shape in cross-section with their narrower ends towards the center of the nozzle.
- the portions 16 of the wall which are pressed inwardly are spaced at equal angles apart so that the resultant outlets 11 are of similar cross-sectional size.
- the portions 16 need not necessarily be equally spaced apart.
- the tubes 10 shown in F IGS- 3 and 4 each respectively have three and four lobes 17 of tear-drop shape radiating from the main axis of the tube, each with an outlet 11 in the outer, bulbous, portion of the lobe 17.
- the axes of the outlets 11 in each of the two embodiments extend parallel to the main axis of the tube 10. More than four lobes, and hence more than four outlets could, if required, be formed in similar manner in a nozzle.
- the nozzle shown in FIG. 5, which has five outlets 11,11, is formed in a generally similar manner to the nozzle shown in FIG. 4 except that in this case equallyangularly spaced portions 18 of the wall of the tube 10 which are pressed inwardly do not meet at the center of the tube. Instead the portions 18 meet a short distance from the center so that the center of the tube is left open to provide a central outlet 11.
- This is surrounded by four outlets 11, one in the bulbous outer portion of each of four equally-angularly spaced tear-drop shaped lobes 19.
- the axes of all five outlets 11, l l are parallel to one another. Again there could be more than four lobes l9, and thus outletsll, surrounding the central outlet 11.
- the four surrounding outlets 11 each, as in the embodiments of FIG. 4, have a tear-shaped crosssection with the narrower end towards the center of the tube.
- the central outlet 11' is of a generally fourpointed star shape in cross-section.
- the tubes 10 of all the embodiments described above and illustrated by the accompanying drawings would in practice preferably have a wall thickness of 0.020 to 0.030 inches, a bore of at least one-fourth inch in diameter, and the tubular outlets ll, 11' would preferably be of the order of three-sixteenths to onefourth inch in length.
- the end of the nozzle tube 10 remote from the outlets 11, 11 is adapted, in any convenient pipe-jointing manner, to be fitted to the discharge end of a feed pipe, not shown, leading from a fuel injection pump, not shown. Fuel is fed by way of the feed pipe into the tube 10 under pressure.
- nozzles inject only fuel into the engine cylinders with which they are associated in use. Air is introduced into the cylinders independently, for example by normal air suction arrangements separate from the nozzles.
- a multi-outlet fuel injection nozzle formed from an elongate metal tube having a continuous circumferential wall, said tube comprising a plain tubular portion and an integral end portion extending from said plain portion in the longitudinal direction thereof, at which said end portion said circumferential wall has integral inwardly deformed portions which are compressed into contact one with another and divide the interior of said end portion into a plurality of parallel, elongated passages which extend longitudinally of said end portion and form tubular injection outlets of the nozzle extending from the interior of said plain tubular portion, said outlets being of substantially constant cross-section along their lengths, and the cross-section of each said outlet tapering laterally of said tube towards said inwardly deformed portions.
- each said outlet has a length of the order of three-sixteenths to one-fourth inches.
- a multi-outlet fuel injection nozzle according to claim 1 in which said tube has a bore of not less than one-fourth inch in diameter.
- a multi-outlet injection nozzle formed from an elongate metal tube having a continuous circumferential wall, said tube comprising a plain tubular portion and an integral end portion extending from said 7 plain portion in the longitudinal direction thereof, at
- said end portion said circumferential wall has integral inwardly deformed wall portions which are compressed into contact one against another and divide the interior of said end portion into a plurality of parallel, elongated passages which extend longitudinally of said end portion and are disposed side-by-side to one another in a row, said passages forming tubular injection outlets of the nozzle which extend from the interior of said plain tubular portion and are of substantially constant cross-section along their lengths, said crosssection of each said nozzle tapering laterally of said tube, and said cross-section of each of said outlets at the ends of said row being of tear-drop shape.
- a multi-outlet fuel injection nozzle in which there are at least three of said outlets, an intermediate one of said outlets disposed between said end outlets of the row being of substantially oval shape in cross-section with the ends of said oval shape tapering to shape points.
- a multi-outlet fuel injection nozzle formed from an elongate metal tube having a continuous circumferential wall, said tube comprising a plain tubular portion and an integral end portion extending from said plain portion in the longitudinal direction thereof, at which said end portion said circumferential wall has integral inwardly deformed wall portions which are compressed into contact one against another and divide the interior of said end portion into at least three parallel, elongated passages which are angularly disposed about the main, longitudinal, axis of said tube, said passages forming tubular injection outlets of the nozzle which extend from the interior of said plain tubular portion and are of substantially constant cross-section along their lengths, said cross-section of each said outlet being of tear-drop shape, tapering laterally of said tube towards said main axis of said tube.
- a multi-outlet fuel injection nozzle in which said inwardly deformed wall portions make contact one with another at a distance from said main axis and the center of said end portion is left open and forms an additional injection outlet extending from the interior of said plain tubular portion parallel to said angularly disposed outlets.
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Fuel-Injection Apparatus (AREA)
Abstract
A multi-outlet fuel injection nozzle is formed from metal tube which at one end is inwardly-deformed so that portions of the wall of the tube are compressed together and divide the interior of the end of the tube into two or more passages which extend longitudinally of the tube and form tubular injection outlets of the nozzle each having a cross-section which tapers laterally of the tube.
Description
United States Patent Griffiths [4 1 Aug. 29, 1972 [72] Inventor:
[54] FUEL INJECTION APPARATUS FOR INTERNAL COMBUSTION ENGINES Kenneth Griffiths, 100 Hall Lane, Walsall, England [22] Filed: Sept. 29, 1970 21 Appl. No.: 76,581
[30] Foreign Application Priority Data Sept. 30, 1969 Great Britain ..47,884/69 [52] US. Cl. ..239/557, 123/32 JV, 239/595,
239/601 [51] Int. Cl. ..B05b l/l4 [58] Field of Search...239/552, 556, 557, 590.5, 592, 239/595, 601; 123/32 JV [56] References Cited UNITED STATES PATENTS 2,968,150 1/1961 Goebel et al ..239/601 X 2,754,097' 7/1956 Hjulian ..239/590.5X
3,288,377 11/1966 Roer ..239/592 X 3,506,198 4/1970 Zwaal .;...239/60l X 3,499,720 3/1970 Flynn ..239/556 X 2,541,710 2/1951 Miller ,.239/552 UX FOREIGN PATENTS OR APPLICATIONS 664,542 6/ 1963 Canada ..239/601 1,309,290 10/1962 France ..239/601 Primary Examiner-M. Henson Wood, Jr. Assistant ExaminerMichael Y. Mar Attorney-Kemon, Palmer & Estabrook 57 1 ABSTRACT A multi-outlet fuelinjection nonle is formed from metal tube which at one end is inwardly-deformed so that portions of the wall of the tube are compressed together and divide the interior of the end of the tube into two or more passages which extend longitudinally of the tube and form tubular injection outlets of the nozzle each having a cross-section which tapers laterally of the tube.
8 Claims, 5 Drawing Figures FUEL INJECTION APPARATUS FOR INTERNAL COMBUSTION ENGINES This invention relates to fuel injection apparatus for internal combustion engines, and in particular to fuel injection nozzles.
Hitherto the practice has been to provide fuel injec tion nozzles with outlets of circular cross-section. Usually the outlets have simply been orifices formed by holes drilled into the end of the nozzle body. In general with the known injection nozzles fuel which is ejected under pressure from the circular outlets continues some distance from the outlets in virtually unbroken streams before breaking up and becoming diffused, the streams being of a diameter substantially similar to that of outlets from which they have emerged. If free to do so the streams could travel as far as 6 to 12 inches from the outlets before breaking up. In practice, however, they do not travel that far because of the confined space of the cylinders into which the fuel is injected from the nozzles, and the streams in fact are caused to break-up by contact with surfaces in the cylinders. This does not give good diffusion of the fuel, with the result that there is inefficient combustion.
An object of the present invention is to provide a multi-outlet fuel injection nozzle formed from elongate metal tube an end portion of which is inwardly deformed so that portions of the wall of the tube are compressed against one another and divide the interior of the tube into two or more longitudinally extending passages which form tubular injection outlets of the nozzle each having a cross-section which tapers laterally of the tube.
With the injection nozzle in accordance with the present invention it is possible to achieve break-up and diffusion of fuel supplied under pressure to the nozzle as soon as the fuel emerges from the outlets of the nozzle. This results from the fact that because of the laterally tapering cross-sectional shape of each of the outlets the pressure of the fuel passing along the outlet varies across the cross-section of the outlet. Hence at different parts of the outlets section fuel is travelling at different velocities which gives rise to the break-up of the fuel stream. A fine, well dispersed spray can be achieved and this results in improved and more complete combustion.
The nozzle has been designed principally for the injection of fuel supplied to the nozzle under relatively low pressures, for example of the order of 15 to 30 pounds per square inch, and it is when operating under these conditions that the best results are obtained. It is possible, however, that satisfactory results might be obtained from a nozzle in accordance with the invention to which in use fuel is supplied at a higher pressure.
The length of the tubular outlets effects the formof the sprays in which the fuel emerges from the outlets. If the outlets are only short in length, say less than threesixteenths inch long, widely spread sprays are produced. If the outlets are fairly long, say more than one-fourth inch in length, then the resultant sprays tend to be narrow, the sprays becoming narrower and approaching stream form as the length of the outlets is increased. The ideal length for most applications is a compromise between these two forms, and hence it is normally desirable for the outlets to be of the order of three-sixteenths to one-fourth inches in length.
. minimum bore diameter of one-fourth inch is required.
A thin-walled tube will normally be used. The wall thickness is preferably in the order of 0.020 to 0.030 inches.
The tube may be of any suitable metal. Stainless steel is particularly suitable.
The tube may be deformed by pressing rolling or in any other appropriate way.
Any number of outlets may be formed, as desired, the maximum number which it is possible to form depending upon the cross-sectional size of the tube used and the cross-sectional sizes of the outlets required. The outlets may be of similar or different cross-sec tional sizes and shapes.
The wall of the tube may be deformed so that the tubular outlets thus formed extend parallel to one another in a row, or so that the outlets are angularly disposed about the main, longitudinal, axis of the tube.
Where there are three or more outlets disposed in a row the end ones of the row are preferably of generally tear-drop shape in cross-section, although they may possibly be of other shapes such as, for example, substantially arrow or diamond shaped. The other outlet or outlets intermediate the end ones of the row may be substantially oval shape in cross-section. They may taper to sharp points at the narrower ends of their cross-sectional shape. The sides of the outlets may converge linearly to meet at the narrower ends of their cross-section, or they may converge in concave curves to the narrower ends, or converge in convex curves so that the narrower endsare cuspidated. Alternatively the outlet or outlets intermediate the end ones of the row may be of generally diamond shape in cross-section, or possibly be bicuspid.
Where there are three or more outlets angularlydisposed about the main axis of the tube they are preferably of tear-drop shape in cross-section, the taper being towards the main axis of the tube. However, they may possibly be of other shapes such as of a row of outlets.
In the case of the outlets being disposed angularly about the main axis of the tube, a central outlet may also be formed at or near the main axis of the tube, its shape depending upon the number and form of the surrounding outlets. Where the surrounding outlets are of tear-drop shape, the central outlet will normally be of substantially star shape in cross-section with three or more points.
Embodiments of the invention will now be described by way of example with reference to the accompanying drawings in which,
. FIG. 1 is a perspective view of a fuel injection nozzle in accordance with the present invention having two injection outlets;
FIG. 2 is a fragmentary perspective view of the discharge end of a fuel injection nozzle having four injection outlets disposed side-by-side in a row;
FIG. 3 is a fragmentary perspective view of the discharge end of another fuel injection nozzle which has four injection outlets but in which the outlets are disposed in a square, and
FIGS. 4 and 5 are further fragmentary perspective views of the discharge ends of fuel injection nozzles having respectively three and five injection outlets.
In all of the embodiments illustrated by the accompanying drawings the fuel injection nozzles are made of thin-walled metal, preferably stainless steel, tubing. The end forms of the injection nozzles are exaggerated in the drawings in order that they may be clearly understood. The tubes are in each case designated generally be reference 10.
The fuel injection nozzle shown in FIG. 1 has just two tubular injection outlets 11 which are disposed side-byside. The outlets 11 are formed by compressing tightly against one another diametrically opposite portions 12 of the tube at the end of the tube, so that passages are formed at opposite ends of a diameter of the tube 10, which passages extend longitudinally of the tube and constitute the outlets 11. The end of the tube 10 may be compressed by any convenient means. The outlets 11 thus formed are of similar size and shape. They could be of disimilar sizes if desired. In this instance the outlets are tear-drop shaped in cross-section, the narrow ends of their cross-sections being directed'inwardly towards the main, longitudinal, axis of the tube 10. i
In the embodiment shown in FIG. 2 the fuel injection nozzle has four tubular injection outlets 11 extending parallel to one another in a row. The outlets 11 are produced by compressing the end of the tube 10 from opposite sides so/longitudinally extending Ithat corrugations 13 are formed. The valley portions 14 of the corrugations 13 of the one side of the compressed tube end meet the valley portions 14 of the corrugations of the opposite side along a diameter of the tube 10. The injection outlets 11 are defined by the passages left between opposed ridge portions 15 of the corrugations 13 of the two sides of the compressed tube end. Three or more than four parallel injection outlets 11 may be formed in this manner, if required. As will be seen in FIG. 2 the end outlets ll of the row are of substantially tear-drop shape in cross-section with their narrower ends directed inwardly towards the main axis of the tube 10. The other two, intermediate, outlets 11 are of modified oval shape in cross-section, their narrower ends being cuspidated.
In FIGS. 3 and 4 the fuel injection nozzles shown respectively have three and four tubular injection outlets II which are angularly disposed about the main axis of the tube 10. In each case the outlets 11 are formed by passages produced by pressing angularly spaced apart portions 16 of the wall of the tube 10 inwardly so that the portions 16 meet and are compressed together at the center of the tube. The outlets 11 thus formed are of tear-drop shape in cross-section with their narrower ends towards the center of the nozzle. In these two examples the portions 16 of the wall which are pressed inwardly are spaced at equal angles apart so that the resultant outlets 11 are of similar cross-sectional size. The portions 16 need not necessarily be equally spaced apart. They could be unequally spaced apart if outlets of different cross-sectional sizes are required. As viewed from their discharge ends, the tubes 10 shown in F IGS- 3 and 4 each respectively have three and four lobes 17 of tear-drop shape radiating from the main axis of the tube, each with an outlet 11 in the outer, bulbous, portion of the lobe 17. The axes of the outlets 11 in each of the two embodiments extend parallel to the main axis of the tube 10. More than four lobes, and hence more than four outlets could, if required, be formed in similar manner in a nozzle.
The nozzle shown in FIG. 5, which has five outlets 11,11, is formed in a generally similar manner to the nozzle shown in FIG. 4 except that in this case equallyangularly spaced portions 18 of the wall of the tube 10 which are pressed inwardly do not meet at the center of the tube. Instead the portions 18 meet a short distance from the center so that the center of the tube is left open to provide a central outlet 11. This is surrounded by four outlets 11, one in the bulbous outer portion of each of four equally-angularly spaced tear-drop shaped lobes 19. The axes of all five outlets 11, l l are parallel to one another. Again there could be more than four lobes l9, and thus outletsll, surrounding the central outlet 11. The four surrounding outlets 11 each, as in the embodiments of FIG. 4, have a tear-shaped crosssection with the narrower end towards the center of the tube. The central outlet 11' is of a generally fourpointed star shape in cross-section.
The tubes 10 of all the embodiments described above and illustrated by the accompanying drawings would in practice preferably have a wall thickness of 0.020 to 0.030 inches, a bore of at least one-fourth inch in diameter, and the tubular outlets ll, 11' would preferably be of the order of three-sixteenths to onefourth inch in length.
In each case the end of the nozzle tube 10 remote from the outlets 11, 11 is adapted, in any convenient pipe-jointing manner, to be fitted to the discharge end of a feed pipe, not shown, leading from a fuel injection pump, not shown. Fuel is fed by way of the feed pipe into the tube 10 under pressure.
These nozzles inject only fuel into the engine cylinders with which they are associated in use. Air is introduced into the cylinders independently, for example by normal air suction arrangements separate from the nozzles.
With all of the examples of nozzles described and i1- lustrated, using them with fuel supplied to them at a pressure of the order of 15 to 30 p.s.i., it has been found possible to produce a fine, evenly dispersed spray immediately the fuel emerges from the outlets, and this has resulted in very good combustion and improved performance in the engines to which they have been fitted.
Particularly good results have been obtained from nozzles of the forms described and illustrated used with motor cycle one and two stroke engines.
It will be appreciated that the nozzles can be made with very little difficulty and quite cheaply.
I claim: I
1. A multi-outlet fuel injection nozzle formed from an elongate metal tube having a continuous circumferential wall, said tube comprising a plain tubular portion and an integral end portion extending from said plain portion in the longitudinal direction thereof, at which said end portion said circumferential wall has integral inwardly deformed portions which are compressed into contact one with another and divide the interior of said end portion into a plurality of parallel, elongated passages which extend longitudinally of said end portion and form tubular injection outlets of the nozzle extending from the interior of said plain tubular portion, said outlets being of substantially constant cross-section along their lengths, and the cross-section of each said outlet tapering laterally of said tube towards said inwardly deformed portions.
2. A multi-outlet fuel injection nozzle according to claim 1 in which each said outlet has a length of the order of three-sixteenths to one-fourth inches.
3. A multi-outlet fuel injection nozzle according to claim 1 in which said tube has a bore of not less than one-fourth inch in diameter.
4. A multi-outlet fuel injection nozzle according to claim 1 in which said tube has a wall thickness of the order of 0.020 to 0.030 inches.
5. A multi-outlet injection nozzle formed from an elongate metal tube having a continuous circumferential wall, said tube comprising a plain tubular portion and an integral end portion extending from said 7 plain portion in the longitudinal direction thereof, at
which said end portion said circumferential wall has integral inwardly deformed wall portions which are compressed into contact one against another and divide the interior of said end portion into a plurality of parallel, elongated passages which extend longitudinally of said end portion and are disposed side-by-side to one another in a row, said passages forming tubular injection outlets of the nozzle which extend from the interior of said plain tubular portion and are of substantially constant cross-section along their lengths, said crosssection of each said nozzle tapering laterally of said tube, and said cross-section of each of said outlets at the ends of said row being of tear-drop shape.
6. A multi-outlet fuel injection nozzle according to claim 5 in which there are at least three of said outlets, an intermediate one of said outlets disposed between said end outlets of the row being of substantially oval shape in cross-section with the ends of said oval shape tapering to shape points.
7. A multi-outlet fuel injection nozzle formed from an elongate metal tube having a continuous circumferential wall, said tube comprising a plain tubular portion and an integral end portion extending from said plain portion in the longitudinal direction thereof, at which said end portion said circumferential wall has integral inwardly deformed wall portions which are compressed into contact one against another and divide the interior of said end portion into at least three parallel, elongated passages which are angularly disposed about the main, longitudinal, axis of said tube, said passages forming tubular injection outlets of the nozzle which extend from the interior of said plain tubular portion and are of substantially constant cross-section along their lengths, said cross-section of each said outlet being of tear-drop shape, tapering laterally of said tube towards said main axis of said tube.
8. A multi-outlet fuel injection nozzle according to claim 7 in which said inwardly deformed wall portions make contact one with another at a distance from said main axis and the center of said end portion is left open and forms an additional injection outlet extending from the interior of said plain tubular portion parallel to said angularly disposed outlets.
Claims (8)
1. A multi-outlet fuel injection nozzle formed from an elongate metal tube having a continuous circumferential wall, said tube comprising a plain tubular portion and an integral end portion extending from said plain portion in the longitudinal direction thereof, at which said end portion said circumferential wall has integral inwardly deformed portions which are compressed into contact one with another and divide the interior of said end portion into a plurality of parallel, elongated passages which extend longitudinally of said end portion and form tubular injection outlets of the nozzle extending from the interior of said plain tubular portion, said outlets being of substantially constant cross-section along their lengths, and the cross-section of each said outlet tapering laterally of said tube towards said inwardly deformed portions.
2. A multi-outlet fuel injection nozzle according to claim 1 in which each said outlet has a length of the order of three-sixteenths to one-fourth inches.
3. A multi-outlet fuel injection nozzle according to claim 1 in which said tube has a bore of not less than one-fourth inch in diameter.
4. A multi-outlet fuel injection nozzle according to claim 1 in which said tube has a wall thickness of the order of 0.020 to 0.030 inches.
5. A multi-outlet injection nozzle formed from an elongate metal tube having a continuous circumferential wall, said tube comprising a plain tubular portion and an integral end portion extending from said plain portion in the longitudinal direction thereof, at which said end portion said circumferential wall has integral inwardly deformed wall portions which are compressed into contact one against another and divide the interior of said end portion into a plurality of parallel, elongated passages which extend longitudinally of said end portion and are disposed side-by-side to one another in a row, said passages forming tubular injection outlets of the nozzle which extend from the interior of said plain tubular portion and are of substantially constant croSs-section along their lengths, said cross-section of each said nozzle tapering laterally of said tube, and said cross-section of each of said outlets at the ends of said row being of tear-drop shape.
6. A multi-outlet fuel injection nozzle according to claim 5 in which there are at least three of said outlets, an intermediate one of said outlets disposed between said end outlets of the row being of substantially oval shape in cross-section with the ends of said oval shape tapering to shape points.
7. A multi-outlet fuel injection nozzle formed from an elongate metal tube having a continuous circumferential wall, said tube comprising a plain tubular portion and an integral end portion extending from said plain portion in the longitudinal direction thereof, at which said end portion said circumferential wall has integral inwardly deformed wall portions which are compressed into contact one against another and divide the interior of said end portion into at least three parallel, elongated passages which are angularly disposed about the main, longitudinal, axis of said tube, said passages forming tubular injection outlets of the nozzle which extend from the interior of said plain tubular portion and are of substantially constant cross-section along their lengths, said cross-section of each said outlet being of tear-drop shape, tapering laterally of said tube towards said main axis of said tube.
8. A multi-outlet fuel injection nozzle according to claim 7 in which said inwardly deformed wall portions make contact one with another at a distance from said main axis and the center of said end portion is left open and forms an additional injection outlet extending from the interior of said plain tubular portion parallel to said angularly disposed outlets.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB47884/69A GB1283205A (en) | 1969-09-30 | 1969-09-30 | Improvements relating to fuel injection apparatus for internal combustion engines |
Publications (1)
Publication Number | Publication Date |
---|---|
US3687375A true US3687375A (en) | 1972-08-29 |
Family
ID=10446597
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US76581A Expired - Lifetime US3687375A (en) | 1969-09-30 | 1970-09-29 | Fuel injection apparatus for internal combustion engines |
Country Status (3)
Country | Link |
---|---|
US (1) | US3687375A (en) |
DE (2) | DE7036241U (en) |
GB (1) | GB1283205A (en) |
Cited By (21)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3731517A (en) * | 1968-12-30 | 1973-05-08 | Patent And Devel Of North Caro | Method of fabricating a fluid dispersion nozzle |
US4017331A (en) * | 1976-02-12 | 1977-04-12 | Thoelen Sr Walter P | Swimming pool cleaning apparatus |
US4076082A (en) * | 1976-02-20 | 1978-02-28 | Messerschmitt-Bolkow-Blohm Gmbh | Thermal drilling device |
US4190121A (en) * | 1976-02-20 | 1980-02-26 | Messerschmitt-Bolkow-Blohm Gmbh | Thermal drilling device |
DE3125835A1 (en) * | 1981-07-01 | 1983-01-20 | Mtu Motoren- Und Turbinen-Union Friedrichshafen Gmbh, 7990 Friedrichshafen | Device for feeding cooling liquid into a piston |
US4666088A (en) * | 1984-03-28 | 1987-05-19 | Robert Bosch Gmbh | Fuel injection valve |
US5129582A (en) * | 1990-12-26 | 1992-07-14 | General Turbine Systems, Inc. | Turbine injector device and method |
US5193747A (en) * | 1989-08-19 | 1993-03-16 | Robert Bosch Gmbh | Protective cap for a fuel injection valve |
US5607109A (en) * | 1994-12-15 | 1997-03-04 | Von Berg; Richard M. | Fuel injection nozzle and method of making |
US5716006A (en) * | 1996-04-15 | 1998-02-10 | Lott; William Gerald | Jet pump having an improved nozzle and a diffuser |
US5762007A (en) * | 1996-12-23 | 1998-06-09 | Vatsky; Joel | Fuel injector for use in a furnace |
US6240918B1 (en) * | 1996-02-21 | 2001-06-05 | Schering Corporation | Powdered medication inhaler |
US20080011491A1 (en) * | 2005-08-22 | 2008-01-17 | Victaulic Company Of America | Sprinkler having non-round exit orifice |
US20120103237A1 (en) * | 2010-11-03 | 2012-05-03 | Ronny Jones | Tiltable multiple-staged coal burner in a horizontal arrangement |
WO2012078355A1 (en) * | 2010-12-06 | 2012-06-14 | Bp Corporation North America Inc. | Improved nozzle for use in fluidized catalytic cracking |
US20130048764A1 (en) * | 2011-08-31 | 2013-02-28 | Beckett Gas, Inc. | Inshot gas burner |
US20130309618A1 (en) * | 2009-03-25 | 2013-11-21 | Wallace Horn | Laminar Flow Jets |
US8622715B1 (en) * | 2011-12-21 | 2014-01-07 | Compatible Components Corporation | Twin turbine asymmetrical nozzle and jet pump incorporating such nozzle |
US20140034676A1 (en) * | 2011-03-09 | 2014-02-06 | Bravilor Holding B.V. | Beverage preparation device with a deformable outlet passage |
US20190003646A1 (en) * | 2017-06-30 | 2019-01-03 | The Boeing Company | Additively Manufactured Pressurization Diffusers |
US11098686B2 (en) * | 2017-05-12 | 2021-08-24 | Hitachi Automotive Systems, Ltd. | Fuel injection valve |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE10049517B4 (en) * | 2000-10-06 | 2005-05-12 | Robert Bosch Gmbh | Fuel injector |
Citations (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2541710A (en) * | 1948-09-21 | 1951-02-13 | Motor Wheel Corp | Sheet metal multiple gas burner |
US2754097A (en) * | 1953-02-10 | 1956-07-10 | Crane Co | Aerator device |
US2968150A (en) * | 1958-02-21 | 1961-01-17 | Rohr Aircraft Corp | Jet engine exhaust sound suppressor and thrust reverser |
FR1309290A (en) * | 1961-09-29 | 1962-11-16 | Improvements to bunsen burners for all gases | |
CA664542A (en) * | 1963-06-04 | White-Rodgers Company | Burners with cloverleaf ports | |
US3288377A (en) * | 1963-05-24 | 1966-11-29 | Roer Franciskus A Van De | Gas burner |
US3499720A (en) * | 1968-07-23 | 1970-03-10 | John H Flynn | Port-forming ribbon assembly and ribbons thereof |
US3506198A (en) * | 1968-02-19 | 1970-04-14 | Antonie M Van Der Zwaal | Bunsen burner |
-
1969
- 1969-09-30 GB GB47884/69A patent/GB1283205A/en not_active Expired
-
1970
- 1970-09-29 US US76581A patent/US3687375A/en not_active Expired - Lifetime
- 1970-09-30 DE DE7036241U patent/DE7036241U/en not_active Expired
- 1970-09-30 DE DE19702048161 patent/DE2048161A1/en active Pending
Patent Citations (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CA664542A (en) * | 1963-06-04 | White-Rodgers Company | Burners with cloverleaf ports | |
US2541710A (en) * | 1948-09-21 | 1951-02-13 | Motor Wheel Corp | Sheet metal multiple gas burner |
US2754097A (en) * | 1953-02-10 | 1956-07-10 | Crane Co | Aerator device |
US2968150A (en) * | 1958-02-21 | 1961-01-17 | Rohr Aircraft Corp | Jet engine exhaust sound suppressor and thrust reverser |
FR1309290A (en) * | 1961-09-29 | 1962-11-16 | Improvements to bunsen burners for all gases | |
US3288377A (en) * | 1963-05-24 | 1966-11-29 | Roer Franciskus A Van De | Gas burner |
US3506198A (en) * | 1968-02-19 | 1970-04-14 | Antonie M Van Der Zwaal | Bunsen burner |
US3499720A (en) * | 1968-07-23 | 1970-03-10 | John H Flynn | Port-forming ribbon assembly and ribbons thereof |
Cited By (26)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3731517A (en) * | 1968-12-30 | 1973-05-08 | Patent And Devel Of North Caro | Method of fabricating a fluid dispersion nozzle |
US4017331A (en) * | 1976-02-12 | 1977-04-12 | Thoelen Sr Walter P | Swimming pool cleaning apparatus |
US4076082A (en) * | 1976-02-20 | 1978-02-28 | Messerschmitt-Bolkow-Blohm Gmbh | Thermal drilling device |
US4190121A (en) * | 1976-02-20 | 1980-02-26 | Messerschmitt-Bolkow-Blohm Gmbh | Thermal drilling device |
DE3125835A1 (en) * | 1981-07-01 | 1983-01-20 | Mtu Motoren- Und Turbinen-Union Friedrichshafen Gmbh, 7990 Friedrichshafen | Device for feeding cooling liquid into a piston |
US4666088A (en) * | 1984-03-28 | 1987-05-19 | Robert Bosch Gmbh | Fuel injection valve |
US5193747A (en) * | 1989-08-19 | 1993-03-16 | Robert Bosch Gmbh | Protective cap for a fuel injection valve |
US5129582A (en) * | 1990-12-26 | 1992-07-14 | General Turbine Systems, Inc. | Turbine injector device and method |
US5607109A (en) * | 1994-12-15 | 1997-03-04 | Von Berg; Richard M. | Fuel injection nozzle and method of making |
US6240918B1 (en) * | 1996-02-21 | 2001-06-05 | Schering Corporation | Powdered medication inhaler |
US5716006A (en) * | 1996-04-15 | 1998-02-10 | Lott; William Gerald | Jet pump having an improved nozzle and a diffuser |
US5762007A (en) * | 1996-12-23 | 1998-06-09 | Vatsky; Joel | Fuel injector for use in a furnace |
US20080011491A1 (en) * | 2005-08-22 | 2008-01-17 | Victaulic Company Of America | Sprinkler having non-round exit orifice |
US9587823B2 (en) * | 2009-03-25 | 2017-03-07 | Wallace Horn | Laminar flow jets |
US20130309618A1 (en) * | 2009-03-25 | 2013-11-21 | Wallace Horn | Laminar Flow Jets |
US20120103237A1 (en) * | 2010-11-03 | 2012-05-03 | Ronny Jones | Tiltable multiple-staged coal burner in a horizontal arrangement |
WO2012078355A1 (en) * | 2010-12-06 | 2012-06-14 | Bp Corporation North America Inc. | Improved nozzle for use in fluidized catalytic cracking |
US8608089B2 (en) | 2010-12-06 | 2013-12-17 | Bp Corporation North America Inc. | Nozzle for use in fluidized catalytic cracking |
US20140034676A1 (en) * | 2011-03-09 | 2014-02-06 | Bravilor Holding B.V. | Beverage preparation device with a deformable outlet passage |
US9125520B2 (en) * | 2011-03-09 | 2015-09-08 | Bravilor Holding B.V. | Beverage preparation device with a deformable outlet passage |
US20130048764A1 (en) * | 2011-08-31 | 2013-02-28 | Beckett Gas, Inc. | Inshot gas burner |
US9062879B2 (en) * | 2011-08-31 | 2015-06-23 | Beckett Gas, Inc. | Inshot gas burner |
US8622715B1 (en) * | 2011-12-21 | 2014-01-07 | Compatible Components Corporation | Twin turbine asymmetrical nozzle and jet pump incorporating such nozzle |
US11098686B2 (en) * | 2017-05-12 | 2021-08-24 | Hitachi Automotive Systems, Ltd. | Fuel injection valve |
US20190003646A1 (en) * | 2017-06-30 | 2019-01-03 | The Boeing Company | Additively Manufactured Pressurization Diffusers |
US10605409B2 (en) * | 2017-06-30 | 2020-03-31 | The Boeing Company | Additively manufactured pressurization diffusers |
Also Published As
Publication number | Publication date |
---|---|
DE7036241U (en) | 1973-11-22 |
GB1283205A (en) | 1972-07-26 |
DE2048161A1 (en) | 1971-04-01 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US3687375A (en) | Fuel injection apparatus for internal combustion engines | |
US6029913A (en) | Swirl tip injector nozzle | |
EP1395739B1 (en) | Fuel injection system | |
EP1051235A1 (en) | Device for introducing a reducing agent into a section of the exhaust pipe of an internal combustion engine | |
DE19713029C2 (en) | Four-stroke internal combustion engine with spark ignition | |
US4595144A (en) | Injection device, more particularly for direct-injection diesel engines | |
KR870011367A (en) | Gasoline injectors for internal combustion engines | |
US1569448A (en) | Fuel-injection nozzle for oil engines | |
DE3005857A1 (en) | FUEL INJECTION NOZZLE | |
US5195477A (en) | Cold start fuel atomizer and process | |
US5012983A (en) | Perforated plate for a fuel injection valve | |
DE2807345A1 (en) | Turbulence producing fuel injection valve for diesel engine - has turbulence chamber with fuel feed channels entering valve seat area at tangent | |
US4231524A (en) | Large flow nozzle | |
US3958759A (en) | Directed atomized fuel jet apparatus | |
DE1526308C3 (en) | Air-compressing injection internal combustion piston engine | |
DE1083084B (en) | Air-compressing internal combustion engine with self-ignition | |
SU1740756A1 (en) | Diesel atomizer sprayer | |
CN2228137Y (en) | Fuel injector | |
RU2076234C1 (en) | Diesel engine injector spray tip | |
AT1392U1 (en) | INTERNAL COMBUSTION ENGINE | |
RU2823846C1 (en) | Atomizer | |
DE467724C (en) | Fuel spray nozzle with two diagonally directed spray channels for airless injection, especially in diesel or semi-diesel engines | |
JPH0299758A (en) | Fuel feeding device | |
SU1573230A1 (en) | Spray nozzle of injector for injection of fuel to internal combustion engine | |
SU1249185A1 (en) | Pencil-type injector |