US937390A - Fuel-injection nozzle for oil-engines. - Google Patents
Fuel-injection nozzle for oil-engines. Download PDFInfo
- Publication number
- US937390A US937390A US48516009A US1909485160A US937390A US 937390 A US937390 A US 937390A US 48516009 A US48516009 A US 48516009A US 1909485160 A US1909485160 A US 1909485160A US 937390 A US937390 A US 937390A
- Authority
- US
- United States
- Prior art keywords
- nozzle
- fuel
- oil
- bore
- pin
- 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
- 238000002347 injection Methods 0.000 title description 10
- 239000007924 injection Substances 0.000 title description 10
- 239000000446 fuel Substances 0.000 description 15
- 239000003921 oil Substances 0.000 description 14
- 238000002485 combustion reaction Methods 0.000 description 12
- 230000003247 decreasing effect Effects 0.000 description 8
- 239000007788 liquid Substances 0.000 description 5
- 230000002459 sustained effect Effects 0.000 description 3
- 230000003405 preventing effect Effects 0.000 description 2
- 238000005507 spraying Methods 0.000 description 2
- 230000032683 aging Effects 0.000 description 1
- 229940000425 combination drug Drugs 0.000 description 1
- 238000004891 communication Methods 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 230000008878 coupling Effects 0.000 description 1
- 238000010168 coupling process Methods 0.000 description 1
- 238000005859 coupling reaction Methods 0.000 description 1
- 239000000295 fuel oil Substances 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 239000002245 particle Substances 0.000 description 1
- 230000035939 shock Effects 0.000 description 1
- 238000009834 vaporization Methods 0.000 description 1
- 230000008016 vaporization Effects 0.000 description 1
- 238000004804 winding Methods 0.000 description 1
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B05—SPRAYING OR ATOMISING IN GENERAL; APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
- B05B—SPRAYING APPARATUS; ATOMISING APPARATUS; NOZZLES
- B05B1/00—Nozzles, spray heads or other outlets, with or without auxiliary devices such as valves, heating means
- B05B1/34—Nozzles, spray heads or other outlets, with or without auxiliary devices such as valves, heating means designed to influence the nature of flow of the liquid or other fluent material, e.g. to produce swirl
- B05B1/3405—Nozzles, spray heads or other outlets, with or without auxiliary devices such as valves, heating means designed to influence the nature of flow of the liquid or other fluent material, e.g. to produce swirl to produce swirl
- B05B1/341—Nozzles, spray heads or other outlets, with or without auxiliary devices such as valves, heating means designed to influence the nature of flow of the liquid or other fluent material, e.g. to produce swirl to produce swirl before discharging the liquid or other fluent material, e.g. in a swirl chamber upstream the spray outlet
- B05B1/3421—Nozzles, spray heads or other outlets, with or without auxiliary devices such as valves, heating means designed to influence the nature of flow of the liquid or other fluent material, e.g. to produce swirl to produce swirl before discharging the liquid or other fluent material, e.g. in a swirl chamber upstream the spray outlet with channels emerging substantially tangentially in the swirl chamber
- B05B1/3431—Nozzles, spray heads or other outlets, with or without auxiliary devices such as valves, heating means designed to influence the nature of flow of the liquid or other fluent material, e.g. to produce swirl to produce swirl before discharging the liquid or other fluent material, e.g. in a swirl chamber upstream the spray outlet with channels emerging substantially tangentially in the swirl chamber the channels being formed at the interface of cooperating elements, e.g. by means of grooves
- B05B1/3447—Nozzles, spray heads or other outlets, with or without auxiliary devices such as valves, heating means designed to influence the nature of flow of the liquid or other fluent material, e.g. to produce swirl to produce swirl before discharging the liquid or other fluent material, e.g. in a swirl chamber upstream the spray outlet with channels emerging substantially tangentially in the swirl chamber the channels being formed at the interface of cooperating elements, e.g. by means of grooves the interface being a cylinder having the same axis as the outlet
Definitions
- This invention is an improvement in injection nozzles for spraying fuel into internal combustion enoines, and particularly into engines adaptedD for burning-the heavier fuel oils, the object of the invention, being particularly to improve 'the Iineness and uniformity of distribution of such fuel throughout the combustion space and to promote the rapidity of its introduction, vaporization and combustion, thereby improving the efcienoy of the engine.
- Figure l represents in longitudinal centra-l section a spraying device constructed and operating according to this invention, and includes a vportion of the water-jacketed wall in which the device is located, when in use.
- Fig. 2 is an enlarged detail view of the tip portion of the same device shown; and
- Fig. 3 is a transverse sec-' tion of Fig.
- the device comprises a tubular nozzle support or casing 1 adapted to be removably secured within an opening in the cylinder or head of the engine designated 2, for which purpose it is shoulderedI and provided with a threaded sleeve 8, revolubly fitted upon its portion of reduced diameter, so as to be screwed into the opening to confine the cas- -ing therein.
- the casing is bored with a central passage-way and its outer end car# ries a union coupling connecting it with the oil supply pipe 4 which leads from the oil pump, not shown.
- the central portion of the interior passage-way is enlarged to form a valve chamber which contains a ball-valve 5 with its seat-ing spring 6 for the purpose of prevent-ing back flow of fuel through the nozzle and casing and preventing the combustion from reaching the oil in the supply pipe.
- the inner end of the central passage-l way is further :enlarged and interiorly threaded at its extreme end, to receive the threaded .base of the nozzle proper, marked 7, which closes'the valve chamber and affords -an l abutment for the thrust of the Avalve spring.
- Thisv nozzle 7 is provided with coaxial bores of two diameters.
- the larger bore 8 communicates directly with the Valve chamber, and the smaller bore terminates in a centrally located andcomparatively fine needle-jet aperture 9 in the tip end of the nozzle, which constitutes the discharge orifice of the device, through which the oil emer es into the combustion space.
- the relatlon of the casing -tothefenginewall is lsuch that the nozzle is supported 1n' a projecting position Within the combustion space, so that it becomes heated from the combustion and thereby pre-heats and vaporizes the oil passing through it.
- 'A pin l0 occupies the smaller bore of the nozzle, fitting it sufficiently close to be sustained in axial alinement With the casing and nozzle, with its free end extending into and through the bore 8 of larger diameter and projecting through the ⁇ same into the valve-chamber and the spiral spring 6 therein.
- the end of the pin 10 in conjunction with the tip end of the smaller bore, forms a small chamber or s ace marked l1 immediately behind the ischarge orifice 9.
- the end of the pin is preferably flat for this purpose, the extreme end ofthe bore being tapered or dished toward the orifice as shown, preferably at an angle of 45 degrees with the axis of the device.
- The'en aging surfaces of the pin and bore are so ormed as to provide between them one or more spiral channels or passages 12 which lead from the space surrounding the pin in the larger bore and pass spirally aroundthe pin, with a progressively decreasing pitch toward the tip, until they reach the chamber l1, which they enter in a tangential direction.
- rlhe oil or fuel admitted under suitable pressure to the nozzle casing passes longitudinally through the valve chamber and larger bore of the nozzle and thence follows the two channels of decreasing pitch into the chamber 11, in the meantime becoming more or less vaporized by heat absorbed from the nozzle and gradually acquiring a change in its direction so that a reservoir of pre-heated fuel is thus produced in'the chamber 11 and maintained in a state of violent rotary motion while the fuel is passing.
- the discharge orifice emits a revolving jet of such fuel from the center of this whirling body and such jeton emerging into the combustion space instantly bursts into expanding particles from the centrifugal eHect, and produces a thoroughly disseminated and finely divided charge of fuel which results in immediate combustion.
- the decreasing pitch of the supply passages allows the oil to be brought to its required high rotary velocity against the frictional resistance of the passages and the inertia of the fuell in the chamber with practical instantaneity and with the least shock or wear on the controlling valves.
- the pin is held in the nozzle by its friction and by the pressure of the oil, and is readily removable for cleansing by withdrawing it, by grasping its squared free end which, as described above, projects outwardly beyond the base of the nozzle for j
- the projecting tip of the nozzle is relatively slender as compared to its base in order to facilitate the heating of thev fuel, and between the tip and thel base,
- 'it is provided with a portion 7 of squared or angular section adapted for engagement by a wrench for unscrewing thenozzle from the casing.
- An injection nozzlefor liquid fuel engines having a fuel collecting chamber at its extremity and provided with a fine, centrally located discharge orifice, opening directly from said chamber into the combus* tion space of the engine and having one or more spirally formed liquid supply passages entering said collecting chamber tangentially.
- An injection nozzle for liquid fuel engines having a collecting chamber at its extremity and ⁇ provided with a fine centrally located discharge orifice opening therefrom directly into the combustion space of the engine, the wall of said chamber being internally beveled toward the said orifice at an angle of substantially 45 degrees with the axis of the nozzle, and having one or more spiral liquid supply passages terminating in said collecting chamber and entering the same tangentially.
- An injection nozzle for oil engines comprising a nozzle tip portionhaving a central bore terminating 1n a fine discharge orifice, a flat-ended pin fitting said bore and forming an interior chamber at the end thereof, the engaging surfaces of said pin and bore being shaped to form one or more spiral channels entering said chamber tangentlally.
- An injection nozzle for oil engines formed with an internal bore of two diameters, the smaller of said bores terminating in a fuel discharge orifice, a tubular casing in which said nozzle is supported containing a chamber in communication with the larger of said bores, in combination with a pin having one end within said smaller bore and forming therewith one or more 'spiral passages leading to said orifice, the
- An injection nozzle for oil engines having a spiral liquid supply passage formed of decreasing pitch with its end of least pitch communicating with the discharge orifice.
- An injection nozzle for oil engines provided with a central bore terminating in a relatively tine discharge orifice, and a pin within said bore, the contacting surfaces of said pin and bore being formed to rovide a spiral passage of decreasing pitch -communicating with said discharge orifice at its end of least pitch.
- An. injection nozzle for oil engines formed with an internal bore of two diameters, the smaller of said bores terminatj ing in a discharge orifice, in combination with a pin held by said smaller bore and forming therewith a spiral passage of decreasing pitch communicating with said orilice at its end of least pitch, said pin being extended within said larger bore.
- a tubular nozzle casing adapted for connection in an opening in the engine wall and a nozzle carried at the terminal of said casing to project within the combustion space and formed with an internal bore terminating in a fuel collecting chamber having a relatively .Iine central discharge orifice, 1n combi nation with a pin sustained within said bore and forming therewith one or more spiral passages leading from said tubular casing and entering said chamber tangentially.
- a tubular nozzle casing adapted to be secured in the engine wall and formed wlth a longitudinal oil passage interiorly enlarged and threaded at its end, a nozzle threaded into said end and formed with an interior bore terminating in a fine discharge orifice, in combination with a pin having one end sustained within said interior bore, forming therewith a fuel passage leading to said perennial, the free end of said pin projecting orifice and having decreasing pitch as they 1o beyond the nozzle into said nozzle casing.
- a nozzle held in a projecting relation Within the combustion space of the engine and lprovided with'an interior bore terminating 1n a line central discharge orifice, in combination with a pin in said bore forming therewith a plurahty of spiral passages leading to said approach ⁇ the same.
Landscapes
- Fuel-Injection Apparatus (AREA)
Description
H. SOELDNER. IUEL INJECTION NOZZLE FOR OIL ENGINES.
APPLICATION FILED MR. 23, 1909.
Patented Oct. 19, 1909.
5 Vwc wrox UNITED sTATgits 'PATENT OFFICE.
HENRY SOELDNER, 0F EAST WILLIAMSBUR G, NEW YORK, AA SSIGrNOR TO DE LA. YEBGNE MACHINE COMPANY, OF NEW YORK, N. Y., ACORPORATION OF NEW YORK.
FUEL-INJECTION NOZZLE FOR OIL-ENGINES.
Specification of Letters Patent.
Patented oct. 19, 1909.
Application filed March 23, 1909. Serial No. 485,160.
,citizen of the Unitedl States, residing lin East Williamsburg, county of Queens, StateA of New York, have invented certain new and useful Improvements in Fuel-Injection Nozzles for Oil-Engines, of whichthe following is a full, true, and concise specification.
This invention is an improvement in injection nozzles for spraying fuel into internal combustion enoines, and particularly into engines adaptedD for burning-the heavier fuel oils, the object of the invention, being particularly to improve 'the Iineness and uniformity of distribution of such fuel throughout the combustion space and to promote the rapidity of its introduction, vaporization and combustion, thereby improving the efcienoy of the engine.
The invention also involves features of construction and operation as hereinafter eX- plained and shown in the drawings, and more particularly pointed out yin the appended claims.
In the drawings, Figure l represents in longitudinal centra-l section a spraying device constructed and operating according to this invention, and includes a vportion of the water-jacketed wall in which the device is located, when in use. Fig. 2is an enlarged detail view of the tip portion of the same device shown; and Fig. 3 is a transverse sec-' tion of Fig. 2 on line III-IIL The device comprises a tubular nozzle support or casing 1 adapted to be removably secured within an opening in the cylinder or head of the engine designated 2, for which purpose it is shoulderedI and provided with a threaded sleeve 8, revolubly fitted upon its portion of reduced diameter, so as to be screwed into the opening to confine the cas- -ing therein. The casing is bored with a central passage-way and its outer end car# ries a union coupling connecting it with the oil supply pipe 4 which leads from the oil pump, not shown. The central portion of the interior passage-way is enlarged to form a valve chamber which contains a ball-valve 5 with its seat-ing spring 6 for the purpose of prevent-ing back flow of fuel through the nozzle and casing and preventing the combustion from reaching the oil in the supply pipe.' The inner end of the central passage-l way is further :enlarged and interiorly threaded at its extreme end, to receive the threaded .base of the nozzle proper, marked 7, which closes'the valve chamber and affords -an l abutment for the thrust of the Avalve spring. Thisv nozzle 7 is provided with coaxial bores of two diameters. The larger bore 8 communicates directly with the Valve chamber, and the smaller bore terminates in a centrally located andcomparatively fine needle-jet aperture 9 in the tip end of the nozzle, which constitutes the discharge orifice of the device, through which the oil emer es into the combustion space.
The relatlon of the casing -tothefenginewall is lsuch that the nozzle is supported 1n' a projecting position Within the combustion space, so that it becomes heated from the combustion and thereby pre-heats and vaporizes the oil passing through it. 'A pin l0 occupies the smaller bore of the nozzle, fitting it sufficiently close to be sustained in axial alinement With the casing and nozzle, with its free end extending into and through the bore 8 of larger diameter and projecting through the` same into the valve-chamber and the spiral spring 6 therein. The end of the pin 10,in conjunction with the tip end of the smaller bore, forms a small chamber or s ace marked l1 immediately behind the ischarge orifice 9. The end of the pin is preferably flat for this purpose, the extreme end ofthe bore being tapered or dished toward the orifice as shown, preferably at an angle of 45 degrees with the axis of the device. The'en aging surfaces of the pin and bore are so ormed as to provide between them one or more spiral channels or passages 12 which lead from the space surrounding the pin in the larger bore and pass spirally aroundthe pin, with a progressively decreasing pitch toward the tip, until they reach the chamber l1, which they enter in a tangential direction. Two such channels are shown in the drawing and each is formed by spirally grooving the surface of the pin, beginning at a point on the pin within the larger bore where the grooves are nearly pafallel with the axis thereof, and then Winding around the pin with decreasing this purpose',
pitch until at the inner extremity they are nearly at right angles to the said aXis where they will be substantially parallel with each other and separated only by a thin iin or thread.
rlhe oil or fuel admitted under suitable pressure to the nozzle casing passes longitudinally through the valve chamber and larger bore of the nozzle and thence follows the two channels of decreasing pitch into the chamber 11, in the meantime becoming more or less vaporized by heat absorbed from the nozzle and gradually acquiring a change in its direction so that a reservoir of pre-heated fuel is thus produced in'the chamber 11 and maintained in a state of violent rotary motion while the fuel is passing. The discharge orifice emits a revolving jet of such fuel from the center of this whirling body and such jeton emerging into the combustion space instantly bursts into expanding particles from the centrifugal eHect, and produces a thoroughly disseminated and finely divided charge of fuel which results in immediate combustion. The decreasing pitch of the supply passages allows the oil to be brought to its required high rotary velocity against the frictional resistance of the passages and the inertia of the fuell in the chamber with practical instantaneity and with the least shock or wear on the controlling valves. The pin is held in the nozzle by its friction and by the pressure of the oil, and is readily removable for cleansing by withdrawing it, by grasping its squared free end which, as described above, projects outwardly beyond the base of the nozzle for j The projecting tip of the nozzle is relatively slender as compared to its base in order to facilitate the heating of thev fuel, and between the tip and thel base,
'it is provided with a portion 7 of squared or angular section adapted for engagement by a wrench for unscrewing thenozzle from the casing.
I claim the following:
1. An injection nozzlefor liquid fuel engines, having a fuel collecting chamber at its extremity and provided with a fine, centrally located discharge orifice, opening directly from said chamber into the combus* tion space of the engine and having one or more spirally formed liquid supply passages entering said collecting chamber tangentially.
2. An injection nozzle for liquid fuel engines, having a collecting chamber at its extremity and `provided with a fine centrally located discharge orifice opening therefrom directly into the combustion space of the engine, the wall of said chamber being internally beveled toward the said orifice at an angle of substantially 45 degrees with the axis of the nozzle, and having one or more spiral liquid supply passages terminating in said collecting chamber and entering the same tangentially.
3. An injection nozzle for oil engines comprising a nozzle tip portionhaving a central bore terminating 1n a fine discharge orifice, a flat-ended pin fitting said bore and forming an interior chamber at the end thereof, the engaging surfaces of said pin and bore being shaped to form one or more spiral channels entering said chamber tangentlally.
4. An injection nozzle for oil engines formed with an internal bore of two diameters, the smaller of said bores terminating in a fuel discharge orifice, a tubular casing in which said nozzle is supported containing a chamber in communication with the larger of said bores, in combination with a pin having one end within said smaller bore and forming therewith one or more 'spiral passages leading to said orifice, the
other end of said pin projecting into the said chamber in the tubular casing.
5. An injection nozzle for oil engines having a spiral liquid supply passage formed of decreasing pitch with its end of least pitch communicating with the discharge orifice.
6. An injection nozzle for oil engines provided with a central bore terminating in a relatively tine discharge orifice, and a pin within said bore, the contacting surfaces of said pin and bore being formed to rovide a spiral passage of decreasing pitch -communicating with said discharge orifice at its end of least pitch.
7. An. injection nozzle for oil engines formed with an internal bore of two diameters, the smaller of said bores terminatj ing in a discharge orifice, in combination with a pin held by said smaller bore and forming therewith a spiral passage of decreasing pitch communicating with said orilice at its end of least pitch, said pin being extended within said larger bore.
8. In a device of the kind described, a tubular nozzle casing adapted for connection in an opening in the engine wall and a nozzle carried at the terminal of said casing to project within the combustion space and formed with an internal bore terminating in a fuel collecting chamber having a relatively .Iine central discharge orifice, 1n combi nation with a pin sustained within said bore and forming therewith one or more spiral passages leading from said tubular casing and entering said chamber tangentially.
9. In a device of the kind described, a tubular nozzle casing adapted to be secured in the engine wall and formed wlth a longitudinal oil passage interiorly enlarged and threaded at its end, a nozzle threaded into said end and formed with an interior bore terminating in a fine discharge orifice, in combination with a pin having one end sustained within said interior bore, forming therewith a fuel passage leading to said orice, the free end of said pin projecting orifice and having decreasing pitch as they 1o beyond the nozzle into said nozzle casing.
10. In a device of the kind described a nozzle held in a projecting relation Within the combustion space of the engine and lprovided with'an interior bore terminating 1n a line central discharge orifice, in combination with a pin in said bore forming therewith a plurahty of spiral passages leading to said approach `the same.
In testimony whereof, I have signed my name to the specification in the presence of -two subscrlbing witnesses.
HENRY SOELDN ER. I Witnesses:
CHAS. H.- HERTER, A. *LEBRECHCR`
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US48516009A US937390A (en) | 1909-03-23 | 1909-03-23 | Fuel-injection nozzle for oil-engines. |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US48516009A US937390A (en) | 1909-03-23 | 1909-03-23 | Fuel-injection nozzle for oil-engines. |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US937390A true US937390A (en) | 1909-10-19 |
Family
ID=3005811
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US48516009A Expired - Lifetime US937390A (en) | 1909-03-23 | 1909-03-23 | Fuel-injection nozzle for oil-engines. |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US937390A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2557246A (en) * | 1948-03-11 | 1951-06-19 | Ziherl Frank | Sprayer |
| US20080179061A1 (en) * | 2006-11-13 | 2008-07-31 | Alberta Energy Partners, General Partnership | System, apparatus and method for abrasive jet fluid cutting |
-
1909
- 1909-03-23 US US48516009A patent/US937390A/en not_active Expired - Lifetime
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2557246A (en) * | 1948-03-11 | 1951-06-19 | Ziherl Frank | Sprayer |
| US20080179061A1 (en) * | 2006-11-13 | 2008-07-31 | Alberta Energy Partners, General Partnership | System, apparatus and method for abrasive jet fluid cutting |
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