The present disclosure relates to a structure for creating a directed fluid spray plume from colliding jets. More particularly, the present disclosure relates to a mechanism used for internal combustion engines for implementing satisfactory collision of a plurality of fluid jets.
Directing a spray of fuel into an internal combustion engine is an important aspect of the design and operation of spark-ignition or compression ignition engines. In operation, the plume of fuel can be directed into a combustion chamber, the intake tract of an engine or the individual cylinder intake runners, to minimize surface impingement, improve vaporization and mixture formation to maximize the volume of the liquid participating in the intended purpose (such as combustion) of a volatile and/or a non-volatile liquid (such as, fuels and/or water). The directing of fuel sprays is of particular importance in internal combustion (spark or compression ignition) engines with direct fuel injection or with port fuel injection.
Achieving effective spray targeting, whether in a direct injection, port fuel injection or multi-cylinder port injection, is an important aspect of the design and operation of an internal combustion engine and provides significant advantages thereto.
Both liquid fuels and water are typically injected into engines. Fuels can be diesel-type fuels, gasoline (petrol), alcohols, and mixtures thereof. Alcohols include ethanol and methanol, which are commonly blended with gasoline. Water is also often injected into engines to provide an internal cooling effect and knock or NOx reduction; and because of the large coefficient of expansion provided by water, it is converted to steam during combustion.
Modern engines typically use fuel injection to introduce fuel into engines. Such fuel injection may be by port injection or direct injection. In port injection engines, fuel injectors are located at some point in the intake train before the cylinder, and the fuel is introduced into the air stream, which is generally close to atmospheric pressures for normally aspirated operation and up to 2-3 atm for forced induction applications. Atomization of fuels and other liquids injected into engines is important, as only fuel vapor can participate in combustion. Optimally, any injected liquid is atomized prior to contact of a stream of injected liquid with any interior surface of the engine. If liquid contacts surfaces, it can wash away lubricants, and pool, which results in sub-optimal combustion. Pooled fuel, during combustion, causes carbon deposits, increased emissions, and reduced engine power.
The spray configuration in conventional fuel injectors or atomizers typically consists of one or more jets or streams aimed outwards from the injector. However, this configuration results in impaction of liquids on the intake manifold and intake port walls, which causes a film to be formed. The film needs to be accounted for in transient fuelling calculations.
In an internal combustion engine with a stratified direct injection fuel system, fuel is injected directly into the combustion chamber in the form of a spray plume that is most often targeted down the combustion chamber toward the piston, which is also referenced as a wall guided injection system. The most common injector location is at an acute angle, between 60 and 90 degrees to the central longitudinal axis of the combustion chamber cylinder and at the top of the combustion chamber, usually at the top dome edge or ceiling edge of the combustion chamber, on the intake side of the combustion chamber, as illustrated in
In an internal combustion engine with homogenous port injection fuel system, where fuel is injected into the intake air stream prior to entering the combustion chamber, either through a single injector located before an air metering device or through multiple injectors immediately before entering the combustion chamber and downstream of an air metering device, it is not uncommon to direct the spray plume to minimize surface impingement on interior walls of the intake tract, the intake valves or the walls of the intake track in the cylinder head, as illustrated in
Therefore, there is a need for improved spray targeting and plume shaping methodology, which is capable of colliding jets to generate a fine spray plume of atomized liquid.
According to an exemplary aspect of the present disclosure, an injector nozzle used with an internal combustion engine for guiding and shaping a fluid flow is provided. The injector nozzle includes a nozzle body, which includes an inlet for admitting the fluid flow and an outlet. The injector nozzle further includes a fluid flow guide in fluid communication with the outlet of the nozzle body. The fluid flow guide includes a plurality of fluid passageways for creating a plurality of stream jets. Each passageway has an orifice through which a respective stream jet is discharged from a respective passageway. Imaginary extensions of the plurality of passageways converge to create at least one focal point, such that the plurality of stream jets impinge on each other to form a spray plume. The plurality of orifices of the fluid passageways are arranged on an imaginary circle on an exterior surface of the fluid flow guide. The plurality of orifices are radially asymmetrically distributed on the imaginary circle with respect to the central axis of the imaginary circle.
According to another exemplary aspect of the present disclosure, an injector nozzle used with an internal combustion engine for guiding and shaping a fluid flow is provided. The injector nozzle includes a nozzle body, which includes an inlet for admitting the fluid flow and an outlet. The injector nozzle further includes a fluid flow guide in fluid communication with the outlet of the nozzle body. The fluid flow guide includes a plurality of fluid passageways for creating a plurality of stream jets. Each passageway has an orifice through which a respective stream jet is discharged from a respective passageway. The plurality of fluid passageways includes: a first group of fluid passageways and a first group of orifices corresponding to the first group of fluid passageways, respectively; and a second group of fluid passageways and a second group of orifices corresponding to the second group of fluid passageways, respectively. Imaginary extensions of the first group of passageways converge to create at least one first focal point, such that the plurality of stream jets passing through the first group of passageways impinge on each other to form a first spray plume. Imaginary extensions of the second group of passageways converge to create at least one second focal point, such that the plurality of stream jets passing through the second group of passageways impinge on each other to form a second spray plume. The first group of orifices are arranged on a first imaginary circle on an exterior surface of the fluid flow guide. The first group of orifices are radially asymmetrically distributed on the first imaginary circle with respect to the central axis of the first imaginary circle. The second group of orifices are arranged on a second imaginary circle on the exterior surface of the fluid flow guide. The second group of orifices are radially asymmetrically distributed on the second imaginary circle with respect to the central axis of the second imaginary circle.
According to still another exemplary aspect of the present disclosure, an injector nozzle used with an internal combustion engine for guiding and shaping a fluid flow is provided. The injector nozzle includes a nozzle body that includes an inlet for admitting the fluid flow and an outlet. The injector nozzle further includes a fluid flow guide in fluid communication with the outlet of the nozzle body. The fluid flow guide includes a plurality of fluid passageways for creating a plurality of stream jets. Each passageway has an orifice through which a respective stream jet is discharged from a respective passageway. The plurality of fluid passageways includes a first group of fluid passageways. The first group of fluid passageways includes a first subgroup of passageways and a first subgroup of orifices corresponding to the first subgroup of fluid passageways, respectively. The first subgroup of orifices are arranged on a first imaginary circle on an exterior surface of the fluid flow guide. The first subgroup of orifices are radially asymmetrically distributed on the first imaginary circle with respect to the central axis of the first imaginary circle. The first group of fluid passageways further includes a second subgroup of passageways and a second subgroup of orifices corresponding to the second subgroup of fluid passageways, respectively. The second subgroup of orifices are arranged on a second imaginary circle on the exterior surface of the fluid flow guide. The second subgroup of orifices are radially asymmetrically distributed on the second imaginary circle with respect to the central axis of the second imaginary circle. The first group of fluid passageways further includes a third subgroup of at least one passageway and a third subgroup of at least one orifice corresponding to the third subgroup of at least one passageway, respectively. The third subgroup of at least one orifice is arranged on a third imaginary circle on the exterior surface of the fluid flow guide. The third subgroup of at least one orifice is radially asymmetrically distributed on the third imaginary circle with respect to the central axis of the third imaginary circle. The first imaginary circle, the second imaginary circle and the third imaginary circle are concentric. The first group of fluid passageways further includes a first central passageway passing through the central axis of the first to third imaginary circles and a first central orifice corresponding to the first central passageway. Imaginary extensions of the first subgroup of passageways, imaginary extensions of the second subgroup of passageways, imaginary extensions of the third subgroup of at least one passageway and an imaginary extension of the first central passageway converge to create at least one first focal point, such that the plurality of stream jets passing through the first group of passageways impinge on each other to form a first spray plume.
Detailed embodiments of the present disclosure are described herein; however, it is to be understood that the disclosed embodiments are merely illustrative of the compositions, structures and methods of the disclosure that may be embodied in various forms. In addition, each of the examples given in connection with the various embodiments is intended to be illustrative, and not restrictive. Further, the figures are not necessarily drawn to scale; some features may be exaggerated to show details of particular components. Therefore, specific structural and functional details disclosed herein are not to be interpreted as limiting, but merely as a representative basis for teaching one skilled in the art to variously employ the compositions, structures and methods disclosed herein. References in the specification to “one embodiment”, “an embodiment”, “an example embodiment”, etc., indicate that the embodiment described may include a particular feature, structure, or characteristic, but every embodiment may not necessarily include the particular feature, structure, or characteristic. Moreover, such phrases are not necessarily referring to the same embodiment.
One aspect of the present disclosure provides an injector or nozzle for injecting liquids into reciprocating or rotary internal combustion engines. Such liquids include, but are not limited to, fuels, water or aqueous solutions. When the injector is in use, two or more liquid jets are aimed at an impingement point under pressure. The collision of the jets at the impingement point efficiently atomizes the liquid.
Although the spray plume shaping methodology according to the disclosure will be described with respect to the injector nozzle having a nozzle body and an orifice plate associated with the nozzle body, it should be understood that the spray plume shaping methodology is equally applicable to other types of injector nozzles, which include but are not limited to injector nozzles having integrated passageways. In addition, the structure and mechanism of the injector nozzle, for guiding and discharging the fluid flow, are not limited to an orifice plate.
The orifice plate 300 has an exterior surface 302 and an opposite interior surface 304. The exterior surface 302 is downstream with respect to the interior surface 304, in view of the flowing direction of a liquid jet. The exterior surface 302 and the interior surface 304 are substantially planar and parallel to each other, thereby defining a thickness A of the orifice plate 300, which thickness may be substantially uniform. In an embodiment, the thickness A of the orifice plate 300 can range from about 0.25 mm to about 4.0 mm, while, in another embodiment, from about 0.25 mm to about 2.5 mm, and in a still further embodiment from about 0.25 mm to about 0.95 mm. For example, the thickness A can be 0.25 mm, 0.3 mm, 0.35 mm, 0.4 mm, 0.45 mm, 0.5 mm, 0.55 mm, 0.6 mm, 0.65 mm, 0.7 mm, 0.75 mm, 0.8 mm, 0.85 mm, 0.9 mm, 0.95 mm, 10 mm, 1.1 mm, 1.2 mm, 1.3 mm, 1.4 mm, 1.5 mm, 1.6 mm, 1.7 mm, 1.8 mm, 1.9 mm, 2.0 mm, 2.1 mm, 2.2 mm, 2.3 mm, 2.4 mm, 2.5 mm, 3.0 mm or 4.0 mm The orifice plate 300 has a diameter B, which can range from about 4.0 mm to about 14.0 mm; in another embodiment, from about 5 mm to about 10 mm; the diameter can be 4.0 mm, 4.1 mm, 4.2 mm, 4.3 mm, 4.4 mm, 4.5 mm, 4.6 mm, 4.7 mm, 4.8 mm, 4.9 mm, 5.0 mm, 5.1 mm, 5.2 mm, 5.3 mm, 5.4 mm, 5.45 mm, 5.5 mm, 5.6 mm, 5.7 mm, 5.8 mm, 5.9 mm, 6.0 mm, 6.1 mm, 6.2 mm, 6.3 mm, 6.4 mm, 6.5 mm, 6.6 mm, 6.7 mm, 6.8 mm, 6.9 mm, 7.0 mm, 7.1 mm, 7.2 mm, 7.3 mm, 7.4 mm, 7.5 mm, 7.6 mm, 7.7 mm, 7.8 mm, 7.9 mm, 8.0 mm, 8.1 mm, 8.2 mm, 8.3 mm, 8.4 mm, 8.5 mm, 8.6 mm, 8.7 mm, 8.8 mm, 8.9 mm, 9.0 mm, 9.1 mm, 9.2 mm, 9.3 mm, 9.4 mm, 9.5 mm, 9.6 mm, 9.7 mm, 9.8 mm, 9.9 mm, 10.0 mm, 10.1 mm, 10.2 mm, 10.3 mm, 10.4 mm, 10.5 mm, 10.6 mm, 10.7 mm, 10.8 mm, 10.9 mm, 11.0 mm, 11.1 mm, 11.2 mm, 11.3 mm, 11.4 mm, 11.5 mm, 11.6 mm, 11.7 mm, 11.8 mm, 11.9 mm, 12.0 mm, 12.1 mm, 12.2 mm, 12.25 mm, 12.3 mm, 12.4 mm, 12.5 mm, 12.6 mm, 12.7 mm, 12.8 mm, 12.9 mm, 13.0 mm, or 14.0 mm
In the shown embodiment, the first fluid passageway 312 forms a part of an imaginary cylinder extending along axis I-I′. The first fluid passageway 312 can be radially consistent along its axis and has a constant diameter D. For example, the diameter D can range from about 80 um to about 1000 um and; in another embodiment, from about 200 um to about 350 um. For example, the diameter D of each passageway can be 80 um, 90 um, 100 um, 110 um, 120 um, 130 um, 140 um, 150 um, 160 um, 170 um, 180 um, 190 um, 200 um, 210 um, 220 um, 230 um, 240 um, 250 um, 260 um, 270 um, 280 um, 290 um, 300 um, 310 um, 320 um, 330 um, 340 um, 350 um, 360 um, 370 um, 380 um, 390 um, 400 um, 500 um, 600 um, 700 um, 800 um, 900 um or 1000 um.
The fluid passageways 312-318 are arranged, such that the fluid jets from each passageway substantially impinge on each other at a focal point F, as shown in
As shown in
An angle of about 60° is formed between the first orifice 411 and the second orifice 412, between the second orifice 412 and the third orifice 413, between the third orifice 413 and the fourth orifice 414, and between the fourth orifice 414 and the fifth orifice 415. However, in an embodiment, the various angles may be the same or different, even though they are all approximately 60°. An angle of about 120° is formed between the first orifice 411 and the fifth orifice 415. This configuration of the orifices can be referred to as a “six minus one” orifice arrangement. Although in an embodiment, these angles may be substantially the same measure in degrees; however, in some embodiments, all of the angles are the same, while in other embodiments, some or all of the of the angles are different in measure of degrees , although each of the angles are substantially the same measure of degrees. However, the angles can be of any suitable combination as long as the sum of the angles is 360° and the orifices are asymmetrically distributed along the imaginary circle. For example, an angle of about 50° to 70° is independently is formed between the first orifice 411 and the second orifice 412, between the second orifice 412 and the third orifice 413, between the third orifice 413 and the fourth orifice 414, and between the fourth orifice 414 and the fifth orifice 415. An angle of about 80° to about 160° is formed between the first orifice 411 and the fifth orifice 415. In each of the above-shown embodiments, the orifices are arranged radially in a single virtual circle. However, the orifices can be arranged radially in multiple virtual circles, which are concentric and share the same central axis Z-Z′ of the orifice plate.
The resultant spray plume emitted from the impingement focal point of the orifice plate 400 is oriented asymmetrically and biased toward the quadrant or direction, which lacks a corresponding orifice. The asymmetrical colliding set results in a biased spray, which is emitted outward from the focal point and, due to the unbalanced lateral liquid momentum, biased toward the side of orifice plate between the first orifice 411 and the fifth orifice 415.
An angle of about 60° is formed between the first orifice 511 and the second orifice 512, between the second orifice 512 and the third orifice 513, and between the third orifice 513 and the fourth orifice 514. However, in an embodiment, the various angles may be the same or different, even though they are all approximately 60°. An angle of about 180° is formed between the first orifice 511 and the fourth orifice 514. However, the angles can be of any suitable combination as long as the sum of the angles is 360° and the orifices are asymmetrically distributed along the imaginary circle. For example, an angle of about 50° to about 70° is formed between the first orifice 511 and the second orifice 512, an angle of about 50° to about 70° is formed between the between the second orifice 512 and the third orifice 513, and an angle of about 50° to about 70° is formed between the between the third orifice 513 and the fourth orifice 514, wherein each of the aforementioned angles may be the same or different; and an angle of about 150° to about 210° can be formed between the fourth orifice 514 and the first orifice 511. This configuration of the orifices can be referred to as a “six minus two” orifice arrangement. In each of the above-shown embodiments, the orifices are arranged radially in a single virtual circle. However, the orifices can be arranged radially in multiple virtual circles, which are concentric and share the same central axis Z-Z′ of the orifice plate. The resultant spray plume emitted from the impingement focal point of the orifice plate 500 is oriented asymmetrically and biased toward the quadrant or direction, which lacks a corresponding orifice. The asymmetrical colliding set results in a biased spray, which is emitted outward from the focal point and, due to the unbalanced lateral liquid momentum, biased toward the side of orifice plate between the first orifice 511 and the fourth orifice 514.
An angle α1 of about 20° is formed between the first orifice 611 and the second orifice 612 and between the fourth orifice 614 and the fifth orifice 615. However, individually, the measure of the aforesaid angles may be the same or different. An angle β1 of about 70° is formed between the second orifice 612 and the third orifice 613 and between the third orifice 613 and the fourth orifice 614. However, individually, the measure of the aforesaid angles may be the same or different. An angle θ1 of about 180° is formed between the first orifice 611 and the fifth orifice 615. However, the angles can be of any suitable combination as long as the sum of the angles is 360° and the orifices are asymmetrically distributed along the imaginary circle. For example, an angle α1 of about 10° to about 30° is formed between the first orifice 611 and the second orifice 612 and an angle of about 10° to about 30° is formed between the fourth orifice 614 and the fifth orifice 615. However, individually, the measure of the aforesaid angles may be the same or different. An angle β1 of about 60° to about 80° is formed between the second orifice 612 and the third orifice 613 and between the third orifice 613 and the fourth orifice 614. However, individually, the measure of the aforesaid angles may be the same or different. An angle θ1 of about 140° to about 220° is formed between the first orifice 611 and the fifth orifice 615. In each of the above-shown embodiments, the orifices are arranged radially in a single virtual circle. However, the orifices can be arranged radially in multiple virtual circles, which are concentric and share the same central axis Z-Z′ of the orifice plate. The resultant spray plume emitted from the impingement focal point of the orifice plate 600 is oriented asymmetrically and biased toward the quadrant or direction, which lacks a corresponding orifice. The asymmetrical colliding set results in a biased spray, which is emitted outward from the focal point and, due to the unbalanced lateral liquid momentum, biased toward the side of orifice plate between the first orifice 611 and the fifth orifice 615.
An angle α2 of about 75° is formed between the first orifice 711 and the second orifice 712 and between the third orifice 713 and the fourth orifice 714. However, individually, the measure of the aforesaid angles may be the same or different. An angle β2 of about 20° is formed between the second orifice 712 and the third orifice 713. An angle θ2 of about 190° is formed between the first orifice 711 and the fourth orifice 714. However, the angles can be of any suitable combination as long as the sum of the angles is 360° and the orifices are asymmetrically distributed along the imaginary circle. For example, an angle of about 65° to about 85° is formed between the first orifice 711 and the second orifice 712 and an angle of about 65° to about 85° is formed between the third orifice 713 and the fourth orifice 714. However, individually, the measure of the aforesaid angles may be the same or different. An angle β2 of about 10° to about 30° is formed between the second orifice 712 and the third orifice 713. An angle θ2 of about 160° to about 220° is formed between the first orifice 711 and the fourth orifice 714. In each of the above-shown embodiments, the orifices are arranged radially in a single virtual circle. However, the orifices can be arranged radially in multiple virtual circles, which are concentric and share the same central axis Z-Z′ of the orifice plate. The resultant spray plume emitted from the impingement focal point of the orifice plate 700 is oriented asymmetrically and biased toward the quadrant or direction, which lacks a corresponding orifice. The asymmetrical colliding set results in a biased spray, which is emitted outward from the focal point and, due to the unbalanced lateral liquid momentum, biased toward the side of orifice plate between the first orifice 711 and the fourth orifice 714.
An angle α3 of about 80° is formed between the first orifice 811 and the second orifice 812. An angle β3 of about 52° is formed between the second orifice 812 and the third orifice 813. An angle γ3 of about 48° is formed between the third orifice 813 and the fourth orifice 814. An angle θ3 of about 180° is formed between the first orifice 811 and the fourth orifice 814. However, the combination of the four individual angles can be of any suitable combination as long as the sum of the angles is 360° and the orifices are asymmetrically distributed along the imaginary circle. For example, in an embodiment, the angle α3 can be in a range of about 70° to about 90°; the angle β3 can be in a range from about 42° to about 62°; the angle γ3 can be in a range from about 38° to about 58°; and the angle θ3 can be in a range from about 150° to about 210°. In each of the above-shown embodiments, the orifices are arranged radially in a single virtual circle. However, the orifices can be arranged radially in multiple virtual circles, which are concentric and share the same central axis Z-Z′ of the orifice plate. The resultant spray plume emitted from the impingement focal point of the orifice plate 800 is oriented asymmetrically and biased toward the quadrant or direction, which lacks a corresponding orifice. The asymmetrical colliding set results in a biased spray, which is emitted outward from the focal point and, due to the unbalanced lateral liquid momentum, biased toward the side of orifice plate between the first orifice 811 and the fourth orifice 814.
An angle α4 of about 45° is formed between the first orifice 911 and the second orifice 912, between the second orifice 912 and the third orifice 913, and between the third orifice 913 and the fourth orifice 914; however, the measure of each of the aforesaid angles may be the same or different. An angle β4 of about 90° is formed between the fourth orifice 914 and the fifth orifice 915. An angle θ4 of about 135° is formed between the first orifice 911 and the fifth orifice 915. However, the angles can be of any suitable combination as long as the sum of the angles is 360° and the orifices are asymmetrically distributed along the imaginary circle. For example, an angle of about 35° to about 55° is formed between the first orifice 911 and the second orifice 912, an angle of about 35° to about 55° is formed between the second orifice 912 and the third orifice 913, and an angle of about 35° to about 55° is formed between the third orifice 913 and the fourth orifice 914; however, the measure of each of the aforesaid angles may be the same or different. An angle β4 of about 80° to about 100° is formed between the fourth orifice 914 and the fifth orifice 915. An angle θ4 of about 95° to about 175° is formed between the first orifice 911 and the fifth orifice 915. In each of the above-shown embodiments, the orifices are arranged radially in a single virtual circle. In an embodiment, the orifices can be arranged radially in multiple virtual circles, which are concentric and share the same central axis Z-Z′ of the orifice plate. The resultant spray plume emitted from the impingement focal point of the orifice plate 900 is oriented asymmetrically and biased toward the quadrant or direction, which lacks a corresponding orifice. The asymmetrical colliding set results in a biased spray, which is emitted outward from the focal point and, due to the unbalanced lateral liquid momentum, biased toward the side of orifice plate between the first orifice 911 and the fifth orifice 915. According to this embodiment, the fifth orifice 915 can effectively bias the spray plume emitted by the colliding set of the other four holes for the purpose of spray targeting. In addition, the fifth orifice 915 can also provide the ability to shape the spray plume, so as to generate plume sections that are irregular, concavely or convexly polygonal, or of any freehand shapes required for a particular application.
An angle α5 of about 30° is formed between the first orifice 1011 and the second orifice 1012 and between the second orifice 1012 and the third orifice 1013. However, individually, the measure of each of the aforesaid angles may be the same or different. An angle β5 of about 300° is formed between the first orifice 1011 and the third orifice 1013. However, the angles can be of any suitable combination as long as the sum of the angles is 360° and the orifices are asymmetrically distributed along the imaginary circle. For example, an angle α5 of about 20° to about 40° is formed between the first orifice 1011 and the second orifice 1012 and of about 20° to about 40° is formed between the second orifice 1012 and the third orifice 1013. However, individually, the measure of each of the aforesaid angles may be the same or different. An angle β5 of about 280° to about 320° is formed between the first orifice 1011 and the third orifice 1013. In each of the above-shown embodiments, the first to third orifices are arranged radially in a single virtual circle. However, the orifices can be arranged radially in multiple virtual circles, which are concentric and share the same central axis Z-Z′ of the orifice plate. The resultant spray plume emitted from the impingement focal point of the orifice plate 100 is oriented asymmetrically and biased toward the quadrant or direction, which lacks corresponding orifices. The asymmetrical colliding set results in a biased spray, which is emitted outward from the focal point and, due to the unbalanced lateral liquid momentum, biased toward the side of orifice plate with no orifices. According to this embodiment, the fourth and central orifice 1014 can effectively bias the spray plume emitted by the colliding set of the other three holes for the purpose of spray targeting. In addition, the fourth and central orifice 1014 can also provide the ability to shape the spray plume, so as to generate plume sections that are irregular, concavely or convexly polygonal, or of any freehand shapes required for a particular application.
Within the first colliding set on imaginary circle 1111, an angle of about 45 degrees is formed between the first orifice 1121 and the second orifice 1122, between the second orifice 1122 and the third orifice 1123, between the third orifice 1123 and the fourth orifice 1124, and between the fourth orifice 1124 and the fifth orifice 1125. An angle of about 180 degrees is formed between the fifth orifice 1125 and the first orifice 1121. Within the second colliding set on imaginary circle 1112, an angle of about 45 degrees is formed between the sixth orifice 1126 and the seventh orifice 1127, between the seventh orifice 1127 and the eighth orifice 1128, between the eighth orifice 1128 and the ninth orifice 1129, and between the ninth orifice 1129 and the tenth orifice 1130. An angle of about 180 degrees is formed between the tenth orifice 1130 and the sixth orifice 1126. However, the angles can be of any suitable combination as long as the sum of the angles is 360 degrees and the orifices are asymmetrically distributed along the imaginary circles. This configuration of the orifices can be referred to as a “split gamma eight minus three” orifice arrangement. The term “split gamma” refers to the two configurations of orifices in two separate imaginary circles. Each configuration defines its own focal point and is adapted individually in an asymmetrical set of five holes. Each asymmetrical set generates a spray plume emitted from the impingement focal point 1113 and 1114, respectively. Each spray plume is biased toward the quadrant or direction, which lacks the corresponding orifice, resulting in two biased sprays, each emitted outward from the each focal point. Due to the unbalanced lateral liquid momentum, each spray plume is biased toward the side of each colliding set between the first orifice 1121 and the fifth orifice 1125 or between the sixth orifice 1126 and the tenth orifice 1130, thereby generating two plumes in the split gamma, or split spray, configuration.
Within the first colliding set on imaginary circle 1213, an angle of about 36 degrees is formed between the first orifice 1221 and the second orifice 1222, between the second orifice 1222 and the third orifice 1223, between the third orifice 1223 and the fourth orifice 1224, and between the fourth orifice 1224 and the fifth orifice 1225. At the center of the first colliding set on imaginary circle 1213 is a sixth orifice 1231. An angle of about 216 degrees is formed between the fifth orifice 1225 and the first orifice 1221. Within the second colliding set on imaginary circle 1214, an angle of about 36 degrees is formed between the seventh orifice 1226 and the eighth orifice 1227, between the eighth orifice 1227 and the ninth orifice 1228, between the ninth orifice 1228 and the tenth orifice 1229, and between the tenth orifice 1229 and the eleventh orifice 1230. At the center of the second colliding set on imaginary circle 1214 is a twelfth orifice 1232. An angle of about 216 degrees is formed between the eleventh orifice 1230 and the seventh orifice 1226. However, the angles can be of any suitable combination as long as the sum of the angles is 360 degrees and the orifices are asymmetrically distributed along the imaginary circles. This configuration of the orifices can be referred to as a “split gamma ten minus five plus one” orifice arrangement. The term “split gamma” as used in this expression, refers to the two configurations of orifices in two separate imaginary circles, each with its own focal point. In addition, each set is configured individually in an asymmetrical set of five holes with an additional hole at the center of the imaginary circle. Each asymmetrical set generates a spray plume emitted from each respective impingement focal point 1215 and 1216. Each spray plume is biased toward the quadrant or direction, which lacks the corresponding orifice, resulting in two biased sprays, each emitted outward from the each focal point. Due to the unbalanced lateral liquid momentum, the spray plume is biased toward the side of each colliding set between the first orifice 1221 and the fifth orifice 1225 and between the seventh orifice 1226 and the eleventh orifice 1230, thereby generating two plumes in the split gamma, or split spray, configuration.
Within the first colliding set on the imaginary circle 1315, an angle of about 30 degrees is formed between the first orifice 1321 and the second orifice 1322 and between the second orifice 1322 and the third orifice 1323; and an angle of about 300 degrees is formed between the third orifice 1323 and the first orifice 1321. On the imaginary circle 1316, an angle of about 40 degrees is formed between the fourth orifice 1324 and the fifth orifice 1325, and an angle of about 320 degrees is formed between the fifth orifice 1325 and the fourth orifice 1324. On the imaginary circle 1317, a single sixth orifice 1326 is aligned with the second orifice 1322 of the imaginary circle 1315. At the center of the first colliding set on the imaginary circles 1315-1317, a seventh orifice 1327 is provided. The center lines of the orifices aligned on the imaginary circle 1315 and 1317 are radially aligned with respect to the center lines of the orifices on the imaginary circle 1316 by about 20 degrees. Within the second colliding set, on the imaginary circle 1318, an angle of about 30 degrees is formed between the eighth orifice 1328 and the ninth orifice 1329 and also between the ninth orifice 1329 and the tenth orifice 1330; an angle of about 300 degrees is formed between the tenth orifice 1330 and the eighth orifice 1328. On the imaginary circle 1319, an angle of about 40 degrees is formed between the eleventh orifice 1331 and the twelfth orifice 1332; and an angle of about 320 degrees is formed between the twelfth orifice 1332 and the eleventh orifice 1331. On the imaginary circle 1320, a single thirteenth orifice 1333 is aligned with the ninth orifice 1329 of the imaginary circle 1318. At the center of the second colliding set on the imaginary circles 1318-1320, a fourteenth orifice 1334 is provided. The center lines of the orifices aligned in imaginary circle 1318 and 1320 are radially aligned in relation to the center lines of the orifices on imaginary circle 1319 by about 20 degrees. However, the angles can be of any suitable combination as long as the sum of the angles is 360 degrees and the orifices are asymmetrically distributed along the imaginary circles. This configuration of the orifices can be referred to as a “split gamma, single focal point, twelve minus 9, nine minus 7, six minus 5, plus one” orifice arrangement. The term “split gamma”, as used in this expression, refers to the two configurations of orifices in two separate colliding sets, each with its own focal point and each set configured individually in an asymmetrical set of six holes along three concentric imaginary circles, with an additional hole at the center of the imaginary circles. The first asymmetrical set generates a spray plume emitted from the first impingement focal point 1335. The second asymmetrical set generates a spray plume emitted from the second impingement focal point 1336. Each spray plume is biased toward the quadrant or direction, which lacks the corresponding orifice. As a result, two separate biased sprays, each emitted outwardly from a respective focal point, are generated. Due to the unbalanced lateral liquid momentum, each spray plume is biased toward the side of each colliding set directly opposite the cluster of orifices 1321-1326 or the cluster of orifices 1328-1333. As a result, two plumes in the split gamma, or two split sprays outward from the center of the plate 1300 and both with downward bend angle, are generated.
Within the first colliding set on the imaginary circle 1415, an angle of about 30 degrees is formed between the first orifice 1421 and the second orifice 1422 and between the second orifice 1422 and the third orifice 1423; an angle of about 300 degrees is formed between the third orifice 1423 and the first orifice 1421. On the imaginary circle 1416, an angle of about 40 degrees is formed between the fourth orifice 1424 and the fifth orifice 1425; and an angle of about 320 degrees is formed between the fifth orifice 1425 and the fourth orifice 1424. On the imaginary circle 1417, a single sixth orifice 1426 is aligned with the second orifice 1422 of imaginary circle 1415. At the center of the first colliding set on the imaginary circles 1415-1417, a seventh orifice 1427 is provided. The center lines of the orifices aligned in the imaginary circle 1415 and 1417 are radially aligned with respect to the center lines of the orifices on the imaginary circle 1416 by about 20 degrees. Within the second colliding set, on imaginary circle 1418, an angle of about 30 degrees is formed between the eighth orifice 1428 and the ninth orifice 1429 and between the ninth orifice 1429 and the tenth orifice 1430; an angle of about 300 degrees is formed between the tenth orifice 1430 and the eighth orifice 1428. On the imaginary circle 1419, an angle of about 40 degrees is formed between the eleventh orifice 1431 and the twelfth orifice 1432; an angle of about 320 degrees is formed between the twelfth orifice 1432 and the eleventh orifice 1431. On the imaginary circle 1420, a single thirteenth orifice 1433 is aligned with the ninth orifice 1429 of the imaginary circle 1418. At the center of the second colliding set on the imaginary circles 1418-1420, a fourteenth orifice 1334 is provided. The center lines of the orifices aligned in the imaginary circle 1418 and 1420 are radially aligned with respect to the center lines of the orifices on the imaginary circle 1419 by about 20 degrees. However, the angles can be of any suitable combination as long as the sum of the angles is 360 degrees and the orifices are asymmetrically distributed along the imaginary circles. This configuration of the orifices can be referred to as a “split gamma, stacked focal point, twelve minus 9, nine minus 7, six minus 5, plus one” orifice arrangement. The term “split gamma” refers to the two configurations of orifices in two separate colliding sets, each with three stacked focal points and each set configured individually in an asymmetrical set of six holes along three concentric imaginary circles, with an additional hole at the center of the imaginary circles. Each of the asymmetrical sets generates a spray plume emitted from each respective impingement focal points 1435-1437 and 1338-1440, respectively. Each spray plume is biased toward the quadrant or direction, which lacks the corresponding orifice. As a result, two separate biased sprays, each emitted outward from each focal point are generated. Due to the unbalanced lateral liquid momentum, each spray plume is biased toward the side of each colliding set directly opposite the cluster of orifices 1421-1426 and directly opposite the cluster of orifices 1428-1433. As a result, two plumes in the split gamma, or two split sprays outward from the center of the plate 1400 and both with downward bend angle, are generated.
Although the above-described orifice plates 1100-1400 each have two colliding sets of orifices for generating two spray plumes, the present disclosure encompass orifice plates that have more colliding sets of orifices. For example, the orifice plates can have three colliding sets of orifices for generating three spray plumes each having a central axis; each colliding set can have orifices aligned on between one and six imaginary circles, which circles may or not be concentric to another; each colliding set can have between two and twenty-six holes; and each colliding set can have between one and six focal points, which focal points may or not be along the same axis. For example, the orifice plates can have four colliding sets of orifices for generating three spray plumes each having a central axis; each colliding set can have orifices aligned on between one and six imaginary circles, which circles may or not be concentric to another; each colliding set can have between two and twenty-six holes; and each colliding set can have between one and six focal points, which focal points may or not be along the same axis.
The orifice plate may be useful for a variety of fluids, such as liquid fuels, oxidizers, fuel-alcohol blends including Ethanol blends ranging from E0 to E100, water, salt, urea, adhesive, finish coatings, paint, lubricants or any solutions or mixtures therein. For example, the fluid can be a volatile fuel of any gasoline-alcohol blends including E0, E1, E2, E3, E4, E5, E6, E7, E8, E9, E10, E15, E20, E25, E30, E40, E50, E60, E70, E75, E85, E90, E95, E97, E98, E99, E100. The fluid can be water and alcohol and any mixture therein. The fluid can be water and salt, and any mixture therein. The fluid can be water and urea, and any mixture therein.
Accordingly, the orifice plate may be constructed of any grade of steel, aluminum, brass, copper, alloys therein, composites including graphite, ceramic, carbon or fiber blends, or a multitude of plastic chemistries.
Although the disclosure has been described with respect to the exemplary embodiments in view of
Furthermore, with respect to these additional embodiments referred to in the previous paragraphs, the angle(s) between each of these adjacent orifices can range from about 18 degrees to about 342 degrees and the angles may be the same or different. Furthermore, in embodiments, each of the aforesaid angles may be the same or different. Each orifice can be equiangular with respect to another orifice or other orifices. Alternatively, each orifice can also be non-equiangular with respect to another orifice or other orifices. Alternatively, the orifices can be a combination of equiangular orifices and non-equiangular orifices. For example, the above angle(s) can be about 18.00°, 18.95°, 19.00°, 20.00°, 21.00°, 21.18°, 22.00°, 22.50°, 23.00°, 24.00°, 25.00°, 25.71°, 26.00°, 27.00°, 27.69°, 28.00°, 29.00°, 30.00°, 31.00°, 32.00°, 32.73°, 33.00°, 34.00°, 35.00°, 36.00°, 37.00°, 37.89°, 38.00°, 39.00°, 40.00°, 42.35°, 45.00°, 48.00°, 50.00°, 51.43°, 52.00°, 53.00°, 54.00°, 55.38°, 56.84°, 60.00°, 62.00°, 63.53°, 65.45°, 67.50°, 72.00°, 75.00°, 75.79°, 77.14°, 80.00°, 83.08°, 84.71°, 90.00°, 94.74°, 96.00°, 98.18°, 100.00°, 102.86°, 105.88°, 108.00°, 110.77°, 112.50°, 113.68°, 120.00°, 126.00°, 127.06°, 128.57°, 130.91°, 132.63°, 135.00°, 138.46°, 140.00°, 144.00°, 148.24°, 150.00°, 151.58°, 154.29°, 157.50°, 160.00°, 162.00°, 163.64°, 166.15°, 168.00°, 169.41°, 170.53°, 180.00°, 190.00°, 190.59°, 192.00°, 193.85°, 196.36°, 200.00°, 202.50°, 205.71°, 210.00°, 216.00°, 221.54°, 225.00°, 229.09°, 231.43°, 240.00°, 249.23°, 252.00°, 257.14°, 261.82°, 270.00°, 280.00°, 288.00°, 294.55°, 300.00°, 308.57°, 315.00°, 320.00°, 324.00°, 325.00°, 330.00°, 335.00°, 340.00°, and 342.00° degrees.
According to another aspect of the present disclosure, a method of spray targeting and plume shaping for colliding jets is provided. The colliding jets pass through and are guided by an orifice plate (such as, the orifice plates 300-1000 as described previously), such that the colliding jets are not radially symmetry along the central axis of the orifice plate. The asymmetry distribution of the colliding jets causes biasing of the center line of the spray plume center line. As a result, the center line is not parallel to the central longitudinal axis. A plurality of orifices is provided to produce fluid jets. The fluid jets impinge on each other to form a focal point, which is distanced from the exit face of the orifice plate and is positioned along the central axis of the orifice plate. The asymmetrical arrangement of the colliding jets result in unbalanced lateral momentum components. The asymmetrical arrangement of the colliding jets also results in a corresponding spray plume emitted from the focal point, which is biased radially toward the area of least lateral momentum, or conversely, away from the side with most lateral momentum.
Accordingly to another aspect of the present disclosure, a method of spray targeting and plume shaping for colliding jets is provided. The colliding jets pass through and are guided by an orifice plate (such as, the orifice plates 1100-1400 as described previously), such that the colliding jets are clustered into asymmetrical colliding sets, which sets are not aligned along the central axis of the orifice plate. The asymmetrical distribution, which can be executed within multiple concentric imaginary circles and aligned in each colliding set, causes compound biasing of the center line of the spray plumes. As a result, the center line of each two or more spray plumes is not parallel to the central longitudinal axis of the plate; rather, the centerline can be compound to the plate, with two or more plumes targeted away from the central axis and from each other.
Accordingly, the spray plume can be selectively shaped to one or more plume sections, which are other than a conical section. The plume sections can be perpendicular to the spray plume centerline and can have cross sections that are linear, oval, concave polygonal, convex polygonal, regular or irregular, or a multitude of freehand shapes desirable for a particular application.
Accordingly, the spray plume can be selectively shaped to generate a split gamma, or split spray pattern, which plume sprays at a compound angle from the plate, with both a bend angle, or a bias in the same direction as the other, and a gamma angle, or an angle that splits the two or more plumes away from the other.
The method can be applied to colliding jets used with a nozzle, an orifice plate, and/or an insert for fluid fitting and channeling. The method can also be applied to an injector with metering means of providing a precise quantity of liquid flow at a precise start and stop time.
The method can be used with a wide variety of fluids, including but not limited to liquid fuels, oxidizers, fuel-alcohol blends including Ethanol blends ranging from E0 to E100, water, salt, urea, adhesive, finish coatings, paint, lubricants or any solutions or mixtures thereof.
While the fundamental novel features of the disclosure as applied to various specific embodiments thereof have been shown, described and pointed out, it will also be understood that various omissions, substitutions and changes in the form and details of the devices illustrated and in their operation, may be made by those skilled in the art without departing from the spirit of the disclosure. For example, it is expressly intended that all combinations of those elements and/or method steps which perform substantially the same function in substantially the same way to achieve the same results are within the scope of the disclosure. Moreover, it should be recognized that structures and/or elements and/or method steps shown and/or described in connection with any disclosed form or embodiment of the disclosure may be incorporated in any other disclosed or described or suggested form or embodiment as a general matter of design choice. It is the intention, therefore, to be limited only as indicated by the scope of the claims appended hereto.
Filing Document | Filing Date | Country | Kind |
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PCT/US16/54754 | 9/30/2016 | WO | 00 |
Number | Date | Country | |
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62235221 | Sep 2015 | US |