US3240254A - Compressible fluid sonic pressure wave apparatus and method - Google Patents

Compressible fluid sonic pressure wave apparatus and method Download PDF

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Publication number
US3240254A
US3240254A US332502A US33250263A US3240254A US 3240254 A US3240254 A US 3240254A US 332502 A US332502 A US 332502A US 33250263 A US33250263 A US 33250263A US 3240254 A US3240254 A US 3240254A
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Prior art keywords
gas
nozzle
passageway
stream
exit opening
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US332502A
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Hughes Nathaniel
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Sonic Development Corporation of America
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Sonic Development Corporation of America
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Priority to BE657350D priority Critical patent/BE657350A/xx
Application filed by Sonic Development Corporation of America filed Critical Sonic Development Corporation of America
Priority to US332502A priority patent/US3240254A/en
Priority to GB51677/64A priority patent/GB1092119A/en
Priority to DE19641447334 priority patent/DE1447334A1/de
Priority to SE15526/64A priority patent/SE347169B/xx
Priority to NL6414944A priority patent/NL6414944A/xx
Priority to CH1651564A priority patent/CH438164A/fr
Priority to US511010A priority patent/US3371869A/en
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    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23D—BURNERS
    • F23D11/00—Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space
    • F23D11/34—Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space by ultrasonic means or other kinds of vibrations
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B05—SPRAYING OR ATOMISING IN GENERAL; APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
    • B05B—SPRAYING APPARATUS; ATOMISING APPARATUS; NOZZLES
    • B05B7/00—Spraying apparatus for discharge of liquids or other fluent materials from two or more sources, e.g. of liquid and air, of powder and gas
    • B05B7/24—Spraying apparatus for discharge of liquids or other fluent materials from two or more sources, e.g. of liquid and air, of powder and gas with means, e.g. a container, for supplying liquid or other fluent material to a discharge device
    • B05B7/2489—Spraying apparatus for discharge of liquids or other fluent materials from two or more sources, e.g. of liquid and air, of powder and gas with means, e.g. a container, for supplying liquid or other fluent material to a discharge device an atomising fluid, e.g. a gas, being supplied to the discharge device
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23D—BURNERS
    • F23D11/00—Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space
    • F23D11/24—Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space by pressurisation of the fuel before a nozzle through which it is sprayed by a substantial pressure reduction into a space
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B05—SPRAYING OR ATOMISING IN GENERAL; APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
    • B05B—SPRAYING APPARATUS; ATOMISING APPARATUS; NOZZLES
    • B05B13/00—Machines or plants for applying liquids or other fluent materials to surfaces of objects or other work by spraying, not covered by groups B05B1/00 - B05B11/00
    • B05B13/06—Machines or plants for applying liquids or other fluent materials to surfaces of objects or other work by spraying, not covered by groups B05B1/00 - B05B11/00 specially designed for treating the inside of hollow bodies
    • B05B13/0627—Arrangements of nozzles or spray heads specially adapted for treating the inside of hollow bodies

Definitions

  • An object of the present invention is to provide stable and eflicient apparatus and methods -for expanding and accelerating compressible fluids to supersonic speeds wherein the expanding and accelerating apparatus and methods automatically adapt themselves to provide at all times substantially optimum treatment of the compressible fluids despite changing ambient or other process conditions.
  • Another object of this invention is to provide simple, elfective and efl'icient control means and methods for such apparatus and methods.
  • a further object of the present invention is to provide compressible fluid-operated sonic pres-sure Wave generating, atomizing, and fuel burning apparatus and methods providing substantially improved performance.
  • Still another object of this invention is to provide convenient and advantageous methods and apparatus for introducing fluent materials into the sonic energy field of such sonic devices.
  • Another object of the present invention is to provide sonic atomization and fuel burning apparatus and methods having improved stability.
  • a still further object of the present invention is to provide apparatus and methods for controlling the pattern of the atomized spray cloud produced by such sonic apparatus.
  • Another object of the present invention is to provide such apparatus and methods which are simple, economical and inexpensive to practice commercially.
  • FIGURE 1 is a perspective view of compressible fluid expanding and accelerating apparatus constructed in accordance with the present invention
  • FIGURE 2 is a partially sectional view of a sonic pressure wave generator and atomizer utilizing the apparatus shown in FIGURE 1;
  • FIGURE 3 is a view, similar to that of FIGURE 2, of another sonic pressure wave generator and atomizer in accordance with the present invention
  • FIGURE 4 is a perspective view of another sonic pressure wave generating and atomizing unit embodying the present invention.
  • FIGURE 5 is a sectional view taken along line 55 of FIGURE 4, in the direction of the arrows;
  • FIGURE 6 is a perspective view of still another sonic pressure wave generating and atomizing unit embodying the present invention.
  • FIGURE 7 is a sectional view taken along line 77 of FIGURE 6;
  • FIGURE 8 is a sectional view taken along line 8-8 of FIGURE 6;
  • FIGURE 9 is a perspective view of yet another sonic 'ice pressure-wave generating and atomizing unit embodying the present invention.
  • FIGURE 10 is a sectional view taken along the line 1010 of FIGURE 9;
  • FIGURE 11 is a sectional view, like that of FIGURE 10, of another sonic pressure-wave generating and atomizing unit of the present invention.
  • FIGURE 12 is a perspective view of another sonic pressure wave generating and atomizing unit embodying the present invention.
  • FIGURE 13 is a sectional view taken along line 13-13 of FIGURE 12;
  • FIGURE 14 is a sectional View, like that of FIG- URE 13, of another sonic pressure-wave generating and atomizing unit of the present invention.
  • FIGURE 15 (which is located on the same sheet as FIGURES 4 and 5) is a perspective, partly sectional view of a fuel burning unit constructed in accordance with the present invention.
  • the compressible fluid expanding and accelerat ing method of the present invention comprises passing the compressible fluid (e.g., gas) through a nozzle, and introducing an incompressible fluid (e.g., liquid) into the nozzle in a manner such that the liquid forms barriers which control the expansion and acceleration of the gas.
  • the liquid is injected into the gas flowing in the nozzle so as to form liquid-walled orifices and surfaces adapted to cause the gas to expand, accelerate, and issue from the nozzle in the form of a low pressure stream having supersonic velocity.
  • FIGURE 1 Apparatus for performing the above-described method is shown in FIGURE 1.
  • the nozzle structure indicated generally at 20 in FIGURE 1 also is shown in FIGURE 2.
  • the nozzle structure 20 includes a gas supply tube 22 which has a solid-walled nozzle portion, generally indicated at 24, at its exit end.
  • Nozzle 24 has a converging inlet section 26, a cylindrically-shaped exit section 28, and four symmetrically-positioned liquid feed holes 30.
  • the axis of each feed hole 30 is perpendicular to the longitudinal axis of the nozzle
  • Nozzle 24 has an outwardly-flaring exterior portion 32 at its exit end.
  • a liquid feed tube 34 is fitted concentrically around the gas feed tube 22 and nozzle 24. The forward end of tube 34 is brazed at 35 to the flaring portion 32 of nozzle 24, so as to form a concentric liquid feed passage 36 to supply liquid to holes 30-.
  • spherical metal spacers 38 are welded to the exterior surface of tube 22. Their outside surfaces are ground down so as to fit into the interior of tube 34. This arrangement provides solid support for tube 34 with respect to tube 22 without appreciably hindering the flow of liquid through passage 36.
  • the nozzle structure 20 operates as follows: a gas such as air is compressed and supplied to nozzle 24 at a pressure P greater than the pressure of the ambient gas surrounding the nozzle structure 20. A liquid is supplied under pressure through passageway 36 and feed holes 39 into exit section 28 of the nozzle. The gas flows through nozzle section 28 swiftly and forms a boundary layer, indicated by dashed lines 39, along the interior walls of the nozzle. The fast-flowing gas causes the liquid entering through holes 30 to spread around the nozzle and form liquid barriers whose outlines are indicated by dashed lines 40 in FIGURE 2. The gas boundary layer 39 merges with the liquid barriers 40 so that the liquid barriers serve as the new boundary layer for the nozzle.
  • a gas such as air is compressed and supplied to nozzle 24 at a pressure P greater than the pressure of the ambient gas surrounding the nozzle structure 20.
  • a liquid is supplied under pressure through passageway 36 and feed holes 39 into exit section 28 of the nozzle.
  • the gas flows through nozzle section 28 swiftly and forms a boundary layer, indicated by dashed lines 39
  • the liquid barriers 40 constrict the flow of air through section 28. As can be seen in FIGURE 2, their shape is such as to form a virtual converging-diverging nozzle. That is, barriers 40 tend to occlude the nozzle at the exits of feed holes 30, and then spread and become thinner at positions progressively further downstream from the feed holes.
  • the liquid is partially atomized bythe shear forces between it and the high-speed gas stream.
  • the new boundary layer for the nozzle is an intimate mixture of gas and liquid particles.
  • the partially atomized liquid and the gas stream emerge from the nozzle structure as indicated at 42 in FIGURE 1.
  • the liquid is believed to be formed into a column having a generally conical shape when it emerges from the nozzle.
  • this liquid-walled nozzle functions in a manner similar to a solid-wall converging-diverging nozzle. That is, barriers 40 accelerate the incoming gas to a speed of Mach 1.0, and then, in the liquid-walled diverging section, further accelerate and expand the flowing gas.
  • Solid-walled converging nozzle section 26 can be used as shown in FIGURE 1 to aid in the initial accelation of the gas, but such a section is not necessary. The acceleration and expansion provided vby barriers 40 is fully effective. Applicant has found that nozzles constructed with only a straight section 28 operate in a highly satisfactory manner.
  • the effective exit opening diameter for the virtual nozzle is the diameter D of cylindrical section 28.
  • the effective choked orifice or neck diameter D of the liquid-walled nozzle is located approximately in the plane formed by the longitudinal axes of feed holes 30.
  • the pressure P and Mach number M at the exit of the nozzle can be computed by use of the following equations which are taken from The Thermodynamics of Compressible Fluid Flow, Shapiro, volume 1, chapter 4; Ronald Press, New York, 1953.
  • M the Mach number of the flowing gas at any point along the nozzles longitudinal axis at which the nozzles cross-sectional area is A and the pressure of the gas flowing is P.
  • k the ratio of specific heats of the gas flowing through the nozzle.
  • P the pressure, in pounds per square inch absolute, of the gas'in the nozzle at any point along its longitudinal axis.
  • the feed holes 30 are located such that the length L of the liquid-walled diverging nozzle section is optimum for the range of operation desired.
  • the length L can be optimized for use in a sonic pressure wave generator by considering the distance L as the length of a solid-walled diverging nozzle section and utilizing the principles set forth in my co-pending US. patent application Serial No. 239,236, filed November 21, 1962 to determine the optimum value for L.
  • C a constant whose value is a function of the fixed diameter D of each nozzle and the type of liquid supplied and other conversion factors.
  • the gas be supplied at a relatively constant flow rate.
  • P is a function of D* and Q and D* is a function of Q and Q
  • the liquid-walled nozzle is one in which the operational characteristics such as exit Mach number M and pressure P can be controlled by deliberately varying the gas flow rate Q, and/or the liquid supply rate Q This method of control is extremely simple and provides variability not previously available.
  • this liquid-walled nozzle is self-adjusting. For example, if the inlet pressure P drops suddenly (with the gas being supplied at a constant rate), the diameter D* decreases automatically. The nozzle reacts to this change automatically to return i D* and the pressure P to their initial values, thus maintaining constant the Mach number and pressure of the gas stream producer by the nozzle.
  • An advantageous result of this is that the power input, which is the product of inlet gas pressure and air flow rate P X Q is sub- 1 stantially constant throughout a wide range of variation of liquid viscosity.
  • the flow through this liquid-walled nozzle also is unexpectedly stable; that is, there is, practically speaking, no separation of the gas from the liquid or solid walls of the nozzle, and no turbulence in the gas boundary layer.
  • One reason for this stability it is believed, is that the liquid is introduced into the boundary region of the nozzle and blends with the gas boundary layer 39. It is believed that the high speed gas forces the liquid toward the walls of the nozzle and, as explained above, breaks it up into globules which become intimately dispersed in the gas boundary layer. This increases the mass and, therefore, the fluid momentum in the gas boundary layer, thus reducing the likelihood that the boundary layer will become turbulent or separate. Furthermore, it is believed that the liquid cools the boundary layer gas and increases its density, thus further reducing the tendency toward turbulence or separation and further improving the stability of the nozzle.
  • Another advantage of this expanding and accelerating method and apparatus is that the liquid wall of the nozzle provides excellent insulation against heat transfer between the flowing gas and the solid nozzle walls. Thus, if the flowing gas is very hot the solid nozzle walls are protected by the liquid wall and are not likely to become overheated.
  • liquid feed holes Although four liquid feed holes are shown in FIG URE 1, the number used may be varied as desired. It is preferred to use them in pairs, with the pairs being spaced symmetrically around the nozzle 24, and the holes of each pair being positioned opposite one another.
  • FIGURE 2 illustrates sonic pressure wave generating and atomizing apparatus and methods in accordance with the present invention.
  • the generating and atomizing apparatus indicated generally at 43, includes the nozzle structure 20 and a pulsator unit 44.
  • FIGURE 2 The apparatus and methods illustrated in FIGURE 2, as well as in the other figures of the drawings, represent improvements over those disclosed in my copending applications for United States Letters Patent Serial No. 260,738 filed February 25, 1963; No. 247,221 filed December 26, 1962; and No. 239,236 filed November 21, 1962.
  • the disclosures of those patent applications hereby are incorporated into this application.
  • Those patent applications describe sonic pressure wave generation and atomization apparatus and methods utilizing means such as a pressurized-gas-supplied nozzle having a diverging exit section for creating a high-speed, low-pressure, gas jet which is directed into a cavity pulsator to create a sonic pressure wave output.
  • the pulsator unit shown in FIGURE 2 includes a member 46 with a pulsator cavity 48 in it.
  • Member 46 is secured to nozzle structure 20 by means of a pair of legs 50 with rounded outer edges. Legs 50 are brazed to member 46 and are brazed into holes 52 in the forward end of nozzle member 24.
  • the cavity 48 is positioned and has dimensions determined in the manner disclosed in my above-identified co-pending patent application Ser. No. 239,236. Other details of the pulsator structure are described more fully in that application and my other coepending patent applications identified above.
  • nozzle structure 20 is operated so that the exit pressure P of the gas emerging from the section 28 is lower than the pressure of the ambient gas, and preferably is below one or two pounds per square inch absolute.
  • the ratio A /a* of the exit opening area to the choked orifice area is greater than 1.0 and preferably is greater than 1.5.
  • the Mach number M of the gas emerging from the nozzle is greater than 1.0 and preferably greater than 1.6.
  • ambient gas will be drawn in or imploded into the emerging high-speed gas stream as indicated by arrows 54 in FIGURE 1.
  • This inward fiow or implosion of ambient gas into the emerging gas stream 42 increases the mass and pressure and, therefore, the momentum of the stream 42 and greatly increases the sonic :power output and efiiciency of the unit. It is believed that this unit develops a highly concentrated core of sonic pressure wave energy in the region between the exit of nozzle and pulsator cavity 48. Powerful sonic pressure waves then spread outwardly from this intense core of energy. The liquid is intimately subjected to energy in this core and is thereby broken up into minute particles.
  • the reflecting rear wall is located between 7 ⁇ and 3/2A downstream from the plane of location of the diameter D the diameter of the gas passageway of the nozzle at the position where the pressure of the gas in the passageway equals ambient pressure, where 7 ⁇ is given approximately by the following equation:
  • the liquid-walled nozzle structure 20 is self-adjusting.
  • the flow characteristics of the gas stream emerging from the nozzle remain relatively constant despite fluctuations in operating conditions.
  • This stability means that the pulsator cavity 48 will be at an approximately optimum location at all times, and the other dimensions of the unit 43 will be similarly optimum.
  • unit 43 is capable of producing a very high power sonic output, e.-g., well over 5,000 acoustic watts.
  • the sonic generator and atomizer unit 56 shown is the same as unit 43 shown in FIGURE 2 except that liquid feed holes 30 are smaller (optionally) and a cylindrical recess or step section 58 is formed in section 28.
  • Step section 58 is provided to give the nozzle a larger exit diameter D to provide liquid storage space in the nozzle conduit, and to provide a flexible liquid wall in the diverging nozzle section. Equations 1 through 3 above are applicable to compute flow conditions through the nozzle of unit 56, as in nozzle unit 20 of FIGURES 1 and 2.
  • the larger exit diameter D provides means for producing lower exit pressures and higher speeds in the gas stream emerging from the nozzle. It is believed that the flexible liquid wall is formed when the liquid emerges from holes 30 and forms a liquid boundary indicated by dashed lines 60. Since the step section 58 is abruptly offset from section 28, the main liquid and gas leaves the solid walls of the nozzle. It is believed that a low-speed gas-liquid mixture is stored in the offset section between boundary 60 and the solid walls of the nozzle. This produces increased atomizing efficiency.
  • the liquid wall 60 is termed a flexible wall because it is believed to move inwardly and outwardly to change the rate of acceleration and expansion of the gas in response to changes in ambient pressure inlet pressure fluctuations, etc. Thus, the flexible wall 60 improves the stability and performance of the device because, it is believed, the flexible wall automatically compensates for changing conditions in much the same manner as do the liquid walls in the unit shown in FIG- URE 2.
  • the generating and atomizing devices shown in the remaining figures of the drawings are like those shown in FIGURES 2 and 3 in that the fluid to be atomized is introduced into the gas stream while the stream is still contained within the solid-walled nozzle.
  • the liquid forms new boundary layers in the solid-walled nozzle, and the gas flow through the nozzle is modified as described with respect to FIGURES 1, 2 and 3, and as described by Equations 1 through 3.
  • the fluid is introduced into the nozzle in various arrangements which provide advantageous liquid walls for the nozzle. These arrangements also provide means for controlling the shape of the spray and allow the fluid to be introduced into the unit in a simple and highly eflicient manner.
  • the sonic atomizer unit 62 includes a nozzle housing, indi cated generally at 64, which comprises a. tubular-shaped section 66 connected to a pair of leg-like members 68 terminating in an end portion 70 containing a pulsator cavity 72 with its open end facing towards tubular section 12.
  • a cylindrical nozzle member is mounted inside nozzle housing member 64 with its forward end abutting under-cut portions 76 of the rear ends of legs 68 (see FIGURE 5).
  • Nozzle member 74 has a converging inlet section 78, a cylindrical middle or stabilizing section 80, and a diverging outlet section 82.
  • a source of pressurized gas (not shown) is connected to tubular portion 66 of nozzle housing 64. Pressurized gas flows from the supply through nozzle 74 and emerges in the form of a gas jet which is intercepted by pulsator cavity 72.
  • the nozzle 74 When constructed and operated in accordance with the above-mentioned patent applications, the nozzle 74, like the nozzle structure described above, produces a gas jet having a Mach number substantially greater than 1.0, and preferably greater than 1.6, at the exit of the nozzle.
  • the Mach number of the stream in the stabilizing section is approximately 1.0.
  • the nozzle also produces at its exit a pressure appreciably less than the pressure of the ambient gas surrounding the nozzle and preferably less than 1 or 2 pounds per square inch absolute (p.s.i.a.).
  • the ratio of the cross-sectional area of the nozzle exit opening to the cross-sectional area of the stabilizing section 80 is made greater than 1 to 1 and preferably 1.5 to 1 or greater.
  • the substantial difference between the pressure at the exit of the nozzle and the ambient gas causes the ambient gas to be drawn in or imploded into the intense sonic energy core produced in the region between the exit of nozzle 74 and the entrance of pulsator cavity 72.
  • This implosion greatly enhances the power output and efficiency of the sonic generator.
  • fluid delivery holes 84, 86, 88 and 90 are formed through tubular section 66 and nozzle member 74 into the stabilizing section 80 of the nozzle.
  • tubes 92, 94, 96 and 98 are secured to tubular housing 66 so as to communicate, respectively, with holes 84, 86, 88 and 90.
  • the fluid (e.g., liquid) to be atomized is supplied through tubes 84, 86, 88 and 90 and, holes 92, 94, 96 and 98 into the gas stream flowing through the nozzle in the stabilizing section 80.
  • the highspeed gas stream flowing through the nozzle forces the liquid toward the solid walls of the nozzle and breaks it up into globules which become intimately dispersed in the gas boundary layer 91.
  • the fluid then flows through the nozzle in the boundary regions and, if the rate of flow through each fluid feed hole is substantially the same, the fluid is emitted from the nozzle in the form of an evenly-distributed, cylindrically-shaped sheet.
  • This sheet of fluid globules then is violently agitated and further broken-up into microscopic particles by the intense sonic energy developed in and emitted from pulsator cavity 72.
  • the resulting spray formed is made up of microscopic fluid droplets of substantially uniform size.
  • This arrangement has many advantages, including the advantages of the FIGURES 1 through 3 embodiments. It has improved stability and, as in the FIGURES 2 and 3 arrangements, its operational characteristics are easily controlled by varying the rates of fluid input to the device in accordance with Equations 1 through 3 above.
  • Another advantage is that the fluid is emitted from the nozzle in an evenly-distributed pattern at substantially all rates of fluid input to the unit.
  • the atomizer produces a fine, even spray that is substantially free from large drops or globules of unatomized fluid. This is an improvement over some previous atomizers in which relatively large globules of unatomized fluid dropped or drooled from the nozzle occasionally, especially when the fluid input rate was very high or very low.
  • the spray cone angle is relatively small and the spray is projected forward with considerable force.
  • a further advantage of this arrangement is that multiple inlet tubes are provided for mixing different fluids with one another. By injecting the fluids into the gas stream in the nozzle, more time is provided for them to become mixed before being atomized by the sonic pressure waves. Thus, the device produces a more thorough mixing of such fluids.
  • the fluids supplied through the feed tubes 92, 94, 96 and 98 may be supplied at various different flow rates so as to provide a means for con-trolling the pattern of the spray produced by the atomizer.
  • fluids can be supplied to opposing holes 84 and 88 .at one flow rate and to opposing holes 816 and 90 at a different rate.
  • the shape of the spray produced bulges outwardly from the longitudinal axis of the unit in the plane of the holes through which the greater quantity of fluid flows, and dips inwardly in the plane of the holes through which less fluid flows.
  • the generally ovalshaped spray pattern (shown in section in FIGURE 4) is produced when the fluid flow rate through holes 84 and 88 is greater than that through holes 86 .and 90.
  • the pattern bulges outwardly in the longitudinal plane coincident with holes 84 and '88 and dips inwardly in the plane of holes 86 and 90.
  • the spray pattern developed by the atomizer can be given an oval, flat, or some other shape desirable for use in a given application.
  • a gas may be supplied to one pair of opposing tubes such as tubes 92 and 96 while a liquid is supplied to the other set of opposing tubes 94 and 98.
  • the gas supply may, if desired, be the same as that used to supply gas to the nozzle 74. This arrangement provides for easy and effective control of the spray pattern of the atomizer.
  • the atomizer unit 62 shown in FIGURES 6, 7 and 8 has the same construction as the unit shown in FIGURES 1 and 2 except that the four fluid supply tubes 84, 86, 88 and 90 are replaced by a single tube 102, and four additionai fluid supply holes 104 exiting outside of nozzle structure 74 are provided.
  • a portion of the fluid to be atomized is supplied through tube 102 to all four of the stabilizer section holes 84, 86, 88 and 90 at substantially the same pressure.
  • This fluid flows into nozzle section 80, forms a liquid-walled nozzle in solid-walled nozzle 74 and is atomized in the manner described above with respect to FIGURES 1 through 5.
  • the remainder of the fluid flows into the sonic field through holes 104 which exit outside the nozzle 74. Outside nozzle 74 all of the fluid is atomized by the high-energy sonic pressure waves emanating from pulsator cavity 72.
  • An advantage of this arrangement is that its spray has an increased forward throw and a narrow cone angle.
  • the spray shape can be changed from circular to some other shape desired by making the diameter of each of one pair of opposing holes 84 and 8 8 different from that of the others 86 and 90.
  • the flow rate through the pairs of holes then will be different and the spray shape will be altered in the manner described above with respect to FIGURES 4 and 5.
  • the atomizer 62 shown in FIGURES 9 and 10 is similar to the atomizer shown in FIGURES 4 and 5 except that the fluid to be atomized is supplied into nozzle 74 at a position up-stream from converging section 78 instead of being fed into stabilizing section 80.
  • Converging section 78 is shaped so that the edge of its inlet opening lies flush against the inside wall of housing 66, there by providing a smooth inclined surface for guiding fluid into the nozzle.
  • the front end of pulsator unit 70 is given a pointed shape in accordance with the principles disclosed in my co-pending United States patent application Serial No. 260,737 filed February '25, 1963.
  • the fluid supply structure is uncomplicated and inexpensive.
  • 'Fluid to be atomized is supplied through a tube 106 and into the atomizing unit by means of a standard screw fitting 108 which is mounted in a threaded hole in housing 66.
  • a small orifice plate 110 blocks the exit opening of tube 106.
  • Orifice plate 110 has a small hole in its center which serves to meter the fluid flow into the atomizer unit. The fluid flow rate can he changed easily and inexpensively merely by exchanging the orifice plate 110 for another having a different size orifice.
  • the fluids flows through tube 106 and fitting 8 into housing 66 where it is spread evenly around the inside circumference of the converging nozzle section 22 by the high-speed stream. It forms a boundary layer 111 and creates a liquid-walled nozzle in solid-walled nozzle 74 and functions in the manner described above and in accordance with Equations 1 through 3 to control the gas flow through the nozzle.
  • the fluid then is atomized in the manner described above.
  • the fluid feed apparatus for this arrangement is extremely simple in construction, and its use prevents cluttering the forward portions of the atomizer unit with equipment. This is especially advantageous in situations where a minimum amount of space is available in which to house or mount the forward part of the atomizer unit.
  • the generating and atomizing unit 62 shown in FIG- URE 1 1 is the same as that shown in FIGURES 9 and 10 except that the unit has been modified to form a flexible liquid-walled nozzle similar to that shown in FIG- URE 3.
  • a cylindrically-shaped exit section 112 is provided. Section 112 is like section 58 of the FIGURE 3 embodiment; it is stepped or offset from stabilizing section 8t).
  • no solid-walled converging nozzle section is provided. Instead, an abrupt inlet surface ⁇ 114 is provided for the nozzle 74, and the fluid inlet [fitting 108 is positioned close to surface .114.
  • the fastmoving gas stream draws the liquid entering from fitting 108 into stabilizing section where it is spread around in the nozzle and forms a boundary layer .115, thus forming a liquid-walled nozzle as in the embodiments described previously.
  • the liquid then forms a flexible dive-r-ging liquid wall which expands and accelerates the gas in the stream in the manner described above in connection with the FIGURE 3 embodiment.
  • the unit has the advantage of even greater simplicity of construction. Also, the unit has automatic self-adjustment to compensate for operational fluctuations, liquid-storage in the stepped section 112, and the other advantages of the FIGURE 3 embodiment.
  • the atomizer 62 shown in FIGURES l2 and 13 is similar to that shown in FIGURES 6, 7 and 8 except that stabilizer section feed holes 84, 88 and 90 and external feed holes 104 are not provided. Instead, there are provided four fluid feed holes 116 which exit into the diverging section 82 of the nozzle, thus guiding the fluid into the interior of the nozzle as in the previously-described embodiments of the present invention. Also, the end of pulsator unit 70 is given a pointed shape as in the FIG- URES 9 and 10 embodiment.
  • the fluid supplied through holes 116 spreads into an even, symmetrical boundary layer sheet 117 before emerging from the nozzle and being atomized.
  • the flow of fluid in the gas boundary layers 119 improves the stability of operation the atomizer, it is believed, in the manner described above. That is, the injection of liquid into the diverging solid-walled section forms a liquid-walled diverging nozzle section. In addition, this mode of injection seems to cause a build-up and thickening of the gas boundary layer 119 upstream from the point of liquid injection so that the stabilizing section is occluded so as to regulate the gas flow through the nozzle in the same manner as in the other embodiments described previously.
  • the forward throw of the spray is increased and the spray cone angle is decreased in this device.
  • the generating and atomizing unit 62 shown in FIG- URE 14 is the same as that shown in FIGURES l2 and 13 except that the structure has been modified to align the axes of fluid feed holes 116 to be approximately perpendicular to the longitudinal axis of the nozzle 74.
  • holes 116 direct the fluid to be atomized into the gas stream at an angle approaching 90 to the nozzle axis. This arrangement provides further improved atomization, forward spray throw, and cone-angle definition.
  • FIGURE 15 shows a fuel burner using a sonic atomizer 43 of the type shown in FIGURE 2 mounted in a fluid feed unit indicated generally at 118.
  • This fuel atomizer projects through a hole 120 in a wall 122 of a furnace which may be used to heat boiler tubes 124 or the like.
  • Atomizer unit 43 is fitted into a coupling device 126 which permits its easy insertion and removal, thus providing easy interchangeability of atomizing units in the furnace.
  • Liquid fuel such as furnace oil
  • pressurized air to operate atomizing unit 62 is fed from a supply 132 through a pipe 134 to feed unit 118.
  • the atomized cloud of fuel emitted from atomizing unit 62 may be ignited initially by a gas flame 136, a spark or other suitable igniting device, and thereafter it immediately bursts into a flame 138 and continues to burn without the need for further ignition.
  • the flame produced by this fuel burner is a brilliant flame; that is, a flame in which combustion is essentially complete and is substantially uniform throughout. Further aspects of the quality of this flame are described more fully in my above-mentioned co-pending patent application Serial No. 260,738.
  • the improved fuel burning apparatus and method provided by the present invention produces a flame which has a greater forward velocity than in previous fuel burners of this type.
  • a flame which is very soft i.e., one that billows with a low forward velocity
  • the fuel burning unit shown in FIGURE 15 provides a flame having a forward velocity great enough to resist significant deflection by furnace gusts. It is believed that this increased forward velocity is a result of feeding fuel into the gas stream before the stream leaves the nozzle. This fuel is accelerated to relatively high velocities, thus giving the resulting spray and flame a higher forward velocity and momentum.
  • Apparatus for atomizing fluent materials comprising, in combination, a gas-operated pressure wave generator including a gas-expanding and accelerating nozzle comprising a body member forming a gas flow passageway having an exit opening for issuing a high-speed gas stream, means in said body member for constricting said gas flow passageway upstream from said exit opening, means in said body member downstream from said constricting means and adjacent said exit opening of said gas flow passageway for giving said passageway a cross-sectional area increasing in the direction of flow of gas through said nozzle, said last-named means giving said passageway the shape of a frustum of a cone, resonator means, means located outside said passageway for positioning said resonator means downstream from said exit opening of said nozzle and intercepting the highspeed gas stream issuing from said exit opening, and means for feeding said fluent materials into the gas forming said high-speed gas stream at a position within said nozzle, subjecting said fluent materials to pressure waves developed by said generator and effecting the
  • Apparatus for atomizing fluent materials comprising, in combination, a gas-operated pressure wave generator including a gas-expanding and accelerating nozzle comprising a body member forming a gas flow passageway having an exit opening for issuing a high-speed gas stream, means in said body member for constricting said gas flow passageway upstream from said exit opening, means in said body member downstream from said constricting means and adjacent said exit opening of said gas flow passageway for giving said passageway a cross-sectional area increasing in the direction of flow of gas through said nozzle, the rate of increase in area provided by said last-named means being less than the rate which would cause substantial separation of the gas flow from the walls of said gas passageway, the ratio of the maximum cross-sectional area of said passageway to the minimum cross-sectional area of said passageway being suificient to produce acceleration of a compressed gasv to supersonic velocities, resonator means, means located outside said passageway for positioning said resonator means downstream from said exit opening of said exit opening of said
  • Apparatus for atomizing fluent materials comprising, in combination, a gas-operated pressure wave generator including a gas-expanding and accelerating nozzle comprising a body member forming a gas flow passageway having an exit opening for issuing a high-speed gas stream, means in said body member for constricting said gas flow passageway upstream from said exit opening, means in said body member downstream from said constricting means and adjacent said exit opening of said gas flow passageway for giving said passageway a cross-sectional area increasing in the direction of flow of gas through said nozzle, the ratio of the maximum cross-sectional area of said passageway to the minimum cross-sectional area of said passageway being suflicient to produce acceleration of a compressed gas to supersonic velocities and being at least 1.5, resonator means positioned downstream from said exit opening of said nozzle and intercepting the high-speed gas stream issuing from said exit opening, and means for feeding said fluent materials into the gas forming said stream at a position within said nozzle, and for subjecting
  • Apparatus for atomizing fluent materials comprising, in combination, a gas-operated pressure wave generator including a gas-accelerating and stream-forming nozzle comprising a body member forming a gas flow passageway, first and second longitudinal positions in said body member, restrictor means reducing the cross-sectional area of said gas flow passageway and forming a reduced orifice at said first longitudinal position, expansion means in said gas flow passageway between said orifice and said second longitudinal position, said expansion means providing an increasing cross-sectional area for said passageway between said orifice and said second longitudinal position in the direction of flow of gas through said nozzle, resonator means, means for positioning said resonator means adjacent the exit opening of said gas passageway, the ratio of the cross-sectional area of said gas passageway at said second longitudinal position to the cross-sectional area of said gas passageway at said first longitudinal position being at least 1.5, and means for feeding said fluent materials into the gas forming said stream at a position within said nozzle, and sub jecting said fluent materials to
  • Apparatus for atomizing fluent materials comprising, in combination, a gas-operated pressure wave generator including a nozzle body having a gas-passageway therethrough with a frustro-conical converging inlet section, a frustro-conical diverging outlet section, and a throat connecting said converging and diverging sections, the ratio of the cross-sectional area of said gas passageway at the exit of said nozzle being at least 1.5 times as great as the cross-sectional area of said gas passageway in said throat, a resonator member forming a cylindrical resonator cavity, support means secured to said nozzle body and said resonator member to position said resonator cavity with its open end facing said outlet section of said nozzle, and means for feeding said fluent materials into the gas forming said stream within said nozzle, and subjecting said fluent materials to pressure waves developed by said generator and effecting the atomization of said fluent materials.
  • a method of atomizing fluent materials in a gaseous ambient medium comprising the steps of generating pressure waves in said medium by expanding and accelerating a gas to form a supersonic gas stream flowing in said ambient medium, the supersonic flow in said stream producing shock waves in a region of said stream, controlling said expansion and acceleration so that it creates a region of sub-ambient pressure in said stream and creates an inrush of ambient gas into said subambient pressure region of said stream, performing resonant action on said supersonic stream, and feeding said fluent materials into the gas forming said supersonic stream at a position upstream from the position at which the pressure of said gas in said stream is a minimum.
  • An atomizing method utilizing an atomizer having a gas-operated pressure wave generator including a gasexpanding and accelerating nozzle comprising a body member forming a gas flow passageway having an exit opening for issuing a high-speed gas stream, means in said body member for constricting said gas flow passageway upstream from said exit opening, means in said body member downstream from said constricting means and adjacent said exit opening of said gas flow passageway for giving said passageway a cross-sectional area increasing in the direction of flow of gas through said nozzle, and means for feeding materials to be atomized into the gas forming said gas stream within said nozzle and subjecting said materials to the field of said pressure waves, said method comprising supplying a compressed gas to said atomizer and maintaining the absolute pressure P of said compressed gas within range in which P, the absolute pressure of said gas stream at said exit opening of said nozzle is less than the absolute pressure of the gaseous ambient medium into which said gas stream is issued, the upper limit of said range corresponding to the value for P given by the following equation when the
  • M is the Mach number of said gas jet at said nozzle exit; and k is the ratio of specific heats for said gas in said jet.
  • Apparatus for atomizing fluent materials comprising, in combination, a gas-operated pressure wave generator including a gas-expanding and accelerating nozzle comprising a body member forming a gas flow passageway having an exit opening for issuing a high-speed gas stream, means in said body member for constricting said gas flow passageway upstream from said exit opening, means in said body member downstream from said constricting means and adjacent said exit opening of said gas flow passageway for giving said passage way a cross-sectional area increasing in the direction of flow of gas through said nozzle, resonator means, means for positioning said resonator means adjacent said exit opening of said nozzle, said generator being operative to generate pressure waves when the pressure of said compressed gas is less than the approximate value of P given by the following equation when P equals the absolute pressure of said gaseous ambient medium and M is equal in which P is the absolute pressure of said compressed gas, and k is the ratio of specific heats for said compressed gas, and means for feeding said fluent materials into the gas forming said stream
  • An atomizer comprising, in combination, a gasoperated pressure wave generator including a gas-expanding and accelerating nozzle comprising a body member forming a gas flow passageway having an exit opening for issuing a high-speed gas stream, means in said body member for constricting said gas flow passageway upstream from said exit opening, means in said body member downstream from said constricting means and adjacent said exit opening of said gas flow passageway for giving said passageway a cross-sectional area increasing in the direction of flow of gas through said nozzle, said high-speed gas stream having oblique shock waves forming a periodic shock-wave outline pattern, the first of said waves downstream from said exit opening of said nozzle means being a compressional shock wave, and cavity resonator means positioned downstream from said exit opening and intercepting said jet with the reflecting surface of said cavity resonator means being located within said first shock wave, and means for feeding said fluent materials into the gas forming said stream within said nozzle, and subjecting said fluent materials to pressure waves de veloped by said generator
  • Apparatus for atomizing fluent materials comprising, in combination, a gas-operated pressure wave generator including a gas-accelerating and stream-forming nozzle com-prising a body member forming a gas flow passageway, first, second and third longitudinal positions in said body member, said second position being spaced from said first position in the direction of flow of gas through said nozzle and said third position being spaced from said second position in the direction of flow of gas through said nozzle, restrictor means reducing the cross-sectional area of said gas flow passageway and forming a reduced orifice at said first longitudinal position, stabilizing means in said gas flow passageway between said reduced orifice and said second longitudinal position, said stabilizing means providing a substantially constant cross-sectional area for said passage.- way between said reduced orifice and said second longitudinal position, said stabilizing means also providing another orifice at said second longitudinal position, said other orifice having a cross-sectional area substantially equal to that of said reduced orifice, expansion means in said gas flow passageway between said other orific
  • Fuel combustion apparatus comprising, in combination, a combustion enclosure having walls subject to being detrimentally coated with unburned fuel residues, fuel burner means for atomizing a fluid fuel, spraying the atomized fuel into said enclosure, and burning said fuel with high efficiency and relatively little unburned residue, said fuel burner means comprising a gas-operated pressure wave generator including a gas-expanding and accelerating nozzle comprising a body member forming a gas flow passageway having an exit opening for issuing a high-speed gas stream, means in said body member for constricting said gas flow passageway upstream from said exit opening, means in said body member downstream from said constricting means and adjacent said exit opening of said gas flow passageway for giving said passageway a cross-sectional area increasing in the direction of flow of gas through said nozzle, resonator means, means located outside said passageway for positioning said resonator means downstream from said exit opening of said nozzle and intercepting the high-speed gas stream issuing from said exit opening, means for feeding said fluid fuel into the gas forming said stream
  • Boiler apparatus comprising, in combination, a furnace enclosure, boiler tubes mounted in said enclosure and adapted to carry fluids to be heated, said boiler tubes and the walls of said furnace enclosure being subject to being detrimentally coated with unburned fuel residues, fuel burner apparatus for atomizing fluid fuel, burning said atomized fuel and projecting the flaming fuel into said furnace and against said boiler tubes, said fuel burner comprising, in combination, a gas-operated pressure wave generator including a gas-accelerating and stream-forming nozzle comprising a body member forming a gas flow passageway, first and second longitudinal positions in said body member, restrictor means reducing the cross-sectional area of said gas flow passageway and forming a reduced orifice at said first longitudinal position, expansion means in said gas flow passageway between said orifice and said second longitudinal position, said expansion means providing an increasing crosssectional area for said passageway between said orifice and said second longitudinal position in the direction of flow of gas through said nozzle, resonator means, means for positioning said resonator means adjacent the exit opening of said
  • said feeding means includes means for injecting said fluent materials into said gas forming said high-speed gas stream at a position within the increasing-area portion of said nozzle created by said constricting means.
  • said feeding means includes means for injecting said fluent materials into said gas forming said high-speed gas stream at a position upstream from said constricting means.
  • Apparatus as in claim 15 including means for injecting said fluent materials into said high-speed gas stream at a position within said stabilizing means.
  • M is the Mach number of the gas in said stream at. said exit of said passageway.
  • resonator means comprises a resonator member with a resonator cavity in it, and means for positioning said resonator member with said cavity intercepting said gas stream and with the rear wall of said cavity being located downstream from said exit opening of said nozzle at a point between A and 3/ 2x distant from the plane of location of the nozzle diameter D where A is given approximately by the following equation:
  • D equals the internal diameter of said nozzle means at the position where the pressure of the gas in said nozzle equals atmospheric pressure; and M equals the Mach number of the gas in said jet at said nozzle exit opening.
  • Apparatus for atomizing fluent materials comprising, in combination, a gas-operated. pressure wave generator including a gas-expanding and accelerating nozzle comprising a body member forming a gas flow passageway having an exit opening for issuing a high-speed gas stream, means in said body member for constricting said gas flow passageway upstream from said exit opening, means in said body member downstream from said constricting means and adjacent said exit opening of 'said gas flow passageway for giving said passageway a cross-sectional area increasing in the direction of flow of gas through said nozzle, resonator means positioned downstream from said exit opening of said nozzle and intercepting the high-speed gas stream issuing from said exit opening, and means for injecting said fluent materials into a boundary layer of gas between a wall of said passageway and the gas stream flowing in said passageway, thereby effecting the atomization of said fluent materials.
  • a gas-operated. pressure wave generator including a gas-expanding and accelerating nozzle comprising a body member

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Nozzles (AREA)
  • Nozzles For Spraying Of Liquid Fuel (AREA)
US332502A 1963-12-23 1963-12-23 Compressible fluid sonic pressure wave apparatus and method Expired - Lifetime US3240254A (en)

Priority Applications (8)

Application Number Priority Date Filing Date Title
BE657350D BE657350A (cs) 1963-12-23
US332502A US3240254A (en) 1963-12-23 1963-12-23 Compressible fluid sonic pressure wave apparatus and method
GB51677/64A GB1092119A (en) 1963-12-23 1964-12-18 Methods and apparatus for generating sonic pressure waves
DE19641447334 DE1447334A1 (de) 1963-12-23 1964-12-21 Vorrichtung und Verfahren zur Erzeugung von Schall-Druckwellen und zur Zerstaeubung von fluessigen Stoffen
SE15526/64A SE347169B (cs) 1963-12-23 1964-12-22
NL6414944A NL6414944A (cs) 1963-12-23 1964-12-22
CH1651564A CH438164A (fr) 1963-12-23 1964-12-22 Procédé pour atomiser une matière fluide dans un milieu ambiant gazeux et appareil pour la mise en oeuvre de ce procédé
US511010A US3371869A (en) 1963-12-23 1965-10-19 Compressible fluid sonic pressure wave atomizing apparatus

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BE (1) BE657350A (cs)
CH (1) CH438164A (cs)
DE (1) DE1447334A1 (cs)
GB (1) GB1092119A (cs)
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SE (1) SE347169B (cs)

Cited By (35)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3320744A (en) * 1965-11-15 1967-05-23 Sonic Dev Corp Gas turbine engine burner
US3337135A (en) * 1965-03-15 1967-08-22 Sonic Dev Corp Spiral fuel flow restrictor
US3556401A (en) * 1968-11-22 1971-01-19 Energy Sciences Inc Streaming
US3643623A (en) * 1967-08-30 1972-02-22 Lin Eng Corp Method of and apparatus for purifying polluted gases
US3667679A (en) * 1969-04-08 1972-06-06 Dumag Ohg Dr Ludwig Kaluza & C Apparatus for mixing a plurality of gaseous streams
US3668869A (en) * 1971-01-28 1972-06-13 Westinghouse Electric Corp Fuel spray ignition atomizer nozzle
US3677525A (en) * 1969-12-31 1972-07-18 Sonic Dev Corp Pressure wave atomizing apparatus
US3774846A (en) * 1969-12-31 1973-11-27 Sonic Dev Corp Pressure wave atomizing apparatus
US3806029A (en) * 1973-01-24 1974-04-23 Energy Sciences Inc Shock enhancement of pressure wave energy
US3814567A (en) * 1972-02-22 1974-06-04 Zink Co John Smokeless flare using liquid water particles
US3839994A (en) * 1972-03-30 1974-10-08 Steamotive Inc Steam generator
US3899130A (en) * 1974-02-28 1975-08-12 Sonic Dev Corp Atomizer with graduated liquid feed and manufacturing method
US4036581A (en) * 1976-09-03 1977-07-19 The United States Of America As Represented By The Secretary Of The Navy Igniter
US4069004A (en) * 1975-06-20 1978-01-17 Societe Nationale Elf Aquitaine (Production) Device to emit shock waves, with adjustable capacity
US4070424A (en) * 1976-09-21 1978-01-24 Uop Inc. Method and apparatus for conditioning flue gas with a mist of H2 SO4
FR2377576A1 (fr) * 1977-01-14 1978-08-11 Italimpianti Bruleur du type rayonnant pour combustibles liquides et gazeux
DE2806479A1 (de) * 1978-02-16 1979-08-23 Uop Inc Verfahren und vorrichtung fuer das ausfaellen von flugasche aus rauchgasen
US4252844A (en) * 1978-07-26 1981-02-24 Union Carbide Corporation Process for mixing liquid additives with solid materials under sonic velocity conditions
FR2481782A1 (fr) * 1980-05-05 1981-11-06 Wanson Constr Mat Therm Ajutage de pulverisation de liquides, notamment pour pulveriser des effluents liquides destines a etre brules
US4302226A (en) * 1978-10-27 1981-11-24 Quad Environmental Technologies Corp. Apparatus for neutralizing odors
US4308040A (en) * 1979-12-14 1981-12-29 Quad Environmental Technologies Corp. Apparatus for neutralizing odors
US4378088A (en) * 1979-06-25 1983-03-29 Ewing James W Liquid atomizing method and apparatus
EP0085583A2 (en) * 1983-02-22 1983-08-10 Lee, Smith & Zickert Liquid atomizing method and apparatus
US4678125A (en) * 1984-08-13 1987-07-07 G S I Holdings (Proprietary) Limited Nozzle
EP0234077A1 (en) * 1986-02-25 1987-09-02 Council of Scientific and Industrial Research Improved burner for furnaces employing acoustic energy
US4726934A (en) * 1982-10-27 1988-02-23 Cabot Corporation Carbon black burner
US4828182A (en) * 1984-04-19 1989-05-09 Spraying Systems Co. Spray nozzle assembly with recessed deflector
US5232164A (en) * 1990-05-09 1993-08-03 Resch D R Precisely adjustable atomizer
US6098897A (en) * 1998-12-23 2000-08-08 Lockwood; Hanford N. Low pressure dual fluid atomizer
US20100025502A1 (en) * 2006-12-14 2010-02-04 Tronox Llc Jet for Use in a Jet Mill Micronizer
US20110023359A1 (en) * 2009-07-29 2011-02-03 David Raring Aeroponic growing apparatus and method
US20110192910A1 (en) * 2008-10-16 2011-08-11 Urea Casale S. A. Spraying Method and Nozzle for Atomization of a Liquid
US20130186982A1 (en) * 2011-08-03 2013-07-25 Spraying Systems Co. Pressurized air assisted spray nozzle assembly
WO2019223848A1 (en) * 2018-05-21 2019-11-28 Wärtsilä Moss As A burner nozzle
WO2023193958A1 (en) * 2022-04-06 2023-10-12 Brookes Jonathan Pneumatic liquid injection device/method

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4919853A (en) * 1988-01-21 1990-04-24 The United States Of America As Represented By The United States Department Of Energy Apparatus and method for spraying liquid materials

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US1593497A (en) * 1926-02-25 1926-07-20 Thomas C Kerr Fuel-oil atomizer and burner
US1860136A (en) * 1928-04-02 1932-05-24 John C Bowman Liquid spreading apparatus
US2532554A (en) * 1946-01-29 1950-12-05 Thomas D Joeck Method for atomizing by supersonic sound vibrations
US2770501A (en) * 1952-09-23 1956-11-13 Sebac Nouvelle Sa Means for the atomization of liquids
US2875578A (en) * 1950-06-16 1959-03-03 Snecma Device for controlling the flow direction of a reaction jet issuing from a nozzle
US2944029A (en) * 1957-09-16 1960-07-05 Aeroprojects Inc Aerosolization process
FR1256669A (fr) * 1960-02-12 1961-03-24 Siderurgie Fse Inst Rech Brûleur pour produire une flamme à forte concentration calorifique stabilisée par onde de choc
US3070313A (en) * 1962-03-05 1962-12-25 Astrosonics Inc Apparatus for the acoustic treatment of liquids

Patent Citations (8)

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Publication number Priority date Publication date Assignee Title
US1593497A (en) * 1926-02-25 1926-07-20 Thomas C Kerr Fuel-oil atomizer and burner
US1860136A (en) * 1928-04-02 1932-05-24 John C Bowman Liquid spreading apparatus
US2532554A (en) * 1946-01-29 1950-12-05 Thomas D Joeck Method for atomizing by supersonic sound vibrations
US2875578A (en) * 1950-06-16 1959-03-03 Snecma Device for controlling the flow direction of a reaction jet issuing from a nozzle
US2770501A (en) * 1952-09-23 1956-11-13 Sebac Nouvelle Sa Means for the atomization of liquids
US2944029A (en) * 1957-09-16 1960-07-05 Aeroprojects Inc Aerosolization process
FR1256669A (fr) * 1960-02-12 1961-03-24 Siderurgie Fse Inst Rech Brûleur pour produire une flamme à forte concentration calorifique stabilisée par onde de choc
US3070313A (en) * 1962-03-05 1962-12-25 Astrosonics Inc Apparatus for the acoustic treatment of liquids

Cited By (42)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3337135A (en) * 1965-03-15 1967-08-22 Sonic Dev Corp Spiral fuel flow restrictor
US3320744A (en) * 1965-11-15 1967-05-23 Sonic Dev Corp Gas turbine engine burner
US3643623A (en) * 1967-08-30 1972-02-22 Lin Eng Corp Method of and apparatus for purifying polluted gases
US3556401A (en) * 1968-11-22 1971-01-19 Energy Sciences Inc Streaming
US3667679A (en) * 1969-04-08 1972-06-06 Dumag Ohg Dr Ludwig Kaluza & C Apparatus for mixing a plurality of gaseous streams
US3677525A (en) * 1969-12-31 1972-07-18 Sonic Dev Corp Pressure wave atomizing apparatus
US3774846A (en) * 1969-12-31 1973-11-27 Sonic Dev Corp Pressure wave atomizing apparatus
US3668869A (en) * 1971-01-28 1972-06-13 Westinghouse Electric Corp Fuel spray ignition atomizer nozzle
US3814567A (en) * 1972-02-22 1974-06-04 Zink Co John Smokeless flare using liquid water particles
US3839994A (en) * 1972-03-30 1974-10-08 Steamotive Inc Steam generator
US3806029A (en) * 1973-01-24 1974-04-23 Energy Sciences Inc Shock enhancement of pressure wave energy
US3899130A (en) * 1974-02-28 1975-08-12 Sonic Dev Corp Atomizer with graduated liquid feed and manufacturing method
US4069004A (en) * 1975-06-20 1978-01-17 Societe Nationale Elf Aquitaine (Production) Device to emit shock waves, with adjustable capacity
US4036581A (en) * 1976-09-03 1977-07-19 The United States Of America As Represented By The Secretary Of The Navy Igniter
US4070424A (en) * 1976-09-21 1978-01-24 Uop Inc. Method and apparatus for conditioning flue gas with a mist of H2 SO4
FR2377576A1 (fr) * 1977-01-14 1978-08-11 Italimpianti Bruleur du type rayonnant pour combustibles liquides et gazeux
DE2806479A1 (de) * 1978-02-16 1979-08-23 Uop Inc Verfahren und vorrichtung fuer das ausfaellen von flugasche aus rauchgasen
US4252844A (en) * 1978-07-26 1981-02-24 Union Carbide Corporation Process for mixing liquid additives with solid materials under sonic velocity conditions
US4302226A (en) * 1978-10-27 1981-11-24 Quad Environmental Technologies Corp. Apparatus for neutralizing odors
US4378088A (en) * 1979-06-25 1983-03-29 Ewing James W Liquid atomizing method and apparatus
US4308040A (en) * 1979-12-14 1981-12-29 Quad Environmental Technologies Corp. Apparatus for neutralizing odors
FR2481782A1 (fr) * 1980-05-05 1981-11-06 Wanson Constr Mat Therm Ajutage de pulverisation de liquides, notamment pour pulveriser des effluents liquides destines a etre brules
US4726934A (en) * 1982-10-27 1988-02-23 Cabot Corporation Carbon black burner
EP0085583A2 (en) * 1983-02-22 1983-08-10 Lee, Smith & Zickert Liquid atomizing method and apparatus
EP0085583A3 (en) * 1983-02-22 1983-09-14 James William Ewing Liquid atomizing method and apparatus
US4828182A (en) * 1984-04-19 1989-05-09 Spraying Systems Co. Spray nozzle assembly with recessed deflector
US4678125A (en) * 1984-08-13 1987-07-07 G S I Holdings (Proprietary) Limited Nozzle
EP0234077A1 (en) * 1986-02-25 1987-09-02 Council of Scientific and Industrial Research Improved burner for furnaces employing acoustic energy
US5232164A (en) * 1990-05-09 1993-08-03 Resch D R Precisely adjustable atomizer
US6098897A (en) * 1998-12-23 2000-08-08 Lockwood; Hanford N. Low pressure dual fluid atomizer
US8387901B2 (en) * 2006-12-14 2013-03-05 Tronox Llc Jet for use in a jet mill micronizer
US20100025502A1 (en) * 2006-12-14 2010-02-04 Tronox Llc Jet for Use in a Jet Mill Micronizer
US8991721B2 (en) * 2008-10-16 2015-03-31 Casale Sa Spraying method and nozzle for atomization of a liquid
US20110192910A1 (en) * 2008-10-16 2011-08-11 Urea Casale S. A. Spraying Method and Nozzle for Atomization of a Liquid
US9421508B2 (en) 2008-10-16 2016-08-23 Casale Sa Spraying method and nozzle for atomization of a liquid
US20110023359A1 (en) * 2009-07-29 2011-02-03 David Raring Aeroponic growing apparatus and method
US20130186982A1 (en) * 2011-08-03 2013-07-25 Spraying Systems Co. Pressurized air assisted spray nozzle assembly
US8820663B2 (en) * 2011-08-03 2014-09-02 Spraying Systems Co. Pressurized air assisted spray nozzle assembly
WO2019223848A1 (en) * 2018-05-21 2019-11-28 Wärtsilä Moss As A burner nozzle
CN112189112A (zh) * 2018-05-21 2021-01-05 瓦锡兰莫斯公司 燃烧器喷嘴
KR20210013055A (ko) * 2018-05-21 2021-02-03 바르질라 모스 에이에스 버너 노즐
WO2023193958A1 (en) * 2022-04-06 2023-10-12 Brookes Jonathan Pneumatic liquid injection device/method

Also Published As

Publication number Publication date
BE657350A (cs)
GB1092119A (en) 1967-11-22
SE347169B (cs) 1972-07-31
CH438164A (fr) 1967-06-15
NL6414944A (cs) 1965-06-24
DE1447334A1 (de) 1969-09-04

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