US3230924A - Sonic pressure wave generator - Google Patents

Sonic pressure wave generator Download PDF

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Publication number
US3230924A
US3230924A US247221A US24722162A US3230924A US 3230924 A US3230924 A US 3230924A US 247221 A US247221 A US 247221A US 24722162 A US24722162 A US 24722162A US 3230924 A US3230924 A US 3230924A
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Prior art keywords
gas
nozzle
orifice
sonic
passageway
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Expired - Lifetime
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US247221A
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English (en)
Inventor
Hughes Nathaniel
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Sonic Development Corporation of America
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Sonic Development Corporation of America
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Application filed by Sonic Development Corporation of America filed Critical Sonic Development Corporation of America
Priority to US247221A priority Critical patent/US3230924A/en
Priority to SE14247/63A priority patent/SE331604B/xx
Priority to DE1963S0088808 priority patent/DE1447333B2/de
Priority to NO151318A priority patent/NO122811B/no
Priority to GB50458/63A priority patent/GB1063859A/en
Priority to CH1558763A priority patent/CH457937A/fr
Priority to DE1964S0089650 priority patent/DE1475154B2/de
Application granted granted Critical
Publication of US3230924A publication Critical patent/US3230924A/en
Anticipated expiration legal-status Critical
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    • G—PHYSICS
    • G10—MUSICAL INSTRUMENTS; ACOUSTICS
    • G10K—SOUND-PRODUCING DEVICES; METHODS OR DEVICES FOR PROTECTING AGAINST, OR FOR DAMPING, NOISE OR OTHER ACOUSTIC WAVES IN GENERAL; ACOUSTICS NOT OTHERWISE PROVIDED FOR
    • G10K5/00—Whistles
    • G10K5/02—Ultrasonic whistles
    • G—PHYSICS
    • G10—MUSICAL INSTRUMENTS; ACOUSTICS
    • G10K—SOUND-PRODUCING DEVICES; METHODS OR DEVICES FOR PROTECTING AGAINST, OR FOR DAMPING, NOISE OR OTHER ACOUSTIC WAVES IN GENERAL; ACOUSTICS NOT OTHERWISE PROVIDED FOR
    • G10K5/00—Whistles

Definitions

  • sonic generators in accordance with the abovementioned co-pending application utilize a convergingdiverging nozzle supplied with a pressurized gas to create a high-speed, low-pressure, gas jet which is directed into a cavity pulsator to create a sonic pressure wave output. While such generators provide performance which is substantially better than that of generators previously avail-- able, generators in accordance with the present invention provide even further improved performance.
  • an object of this invention is to provide a gas-operated sonic generator having a high-velocity-gas jet-producing nozzle of simple construction which readily maintains such a flow in the boundary layers of gas at the interior surfaces of the diverging section of the nozzle as to minimize the growth of these boundary layers and retard separation of this gas from these surfaces.
  • Another object of this invention is to provide a sonic generator incorporating a highspeed, lowpressure-gas jet-producing nozzle which produces shock waves at its exit which are stable in location and have relatively unchanging dimensions throughout a relatively wide range of variations of input pressure.
  • a further object of this invention is to provide such a generator which is of a simple construction and is ecoriomical to build and operate.
  • a still further object of this invention is to provide a gas-operated sonic generator of such construction as to produce a sonic pressure wave output having frequencies falling within a narrow range and having a minimal amount of extraneous noise.
  • FIGURE 1 is a perspective view of a gas-operated sonic pressure wave generator embodying the present invent1on;
  • FIGURE 2 is a sectional view of this generator taken along line 22 of FIGURE 1, in the direction of the arrows;
  • FIGURE 3 is a sectional view of another gas-operated sonic wave generator embodying the present invention.
  • the gas-operated sonic wave generator shown in FIG- URES 1 and 2 comprises a nozzle portion, generally indicated at 10, having a converging inlet section 12, an essentially cylindrical mid or stabilizing section 13, and a diverging outlet section 14.
  • a source of pressurized gas (not shown) is connected through a pipe 16 to one end of nozzle portion 10, and a pulsator unit 18 is attached to its other end.
  • Pulsator unit 18 includes a pulsator chamber 20 which intercepts the gas jet produced by the nozzle 10 and emits sonic pressure waves, all in the manner described in my above-mentioned co-pending patent application.
  • the provision of the cylindrical stabilizing section 13 joining converging section 12 and diverging section 14 in nozzle 10 substantially increases the stability, and also the power output and efl iciency, of the sonic generator in which the nozzle is used. Furthermore, it allows the generator to be operated over a relatively wide range of variations of input air pressure levels without the previously-experienced drop-off in power and efliciency.
  • stabilizing section 13 creates such improved results is that the flow lines of the gas flowing through the nozzle are straightened in section 13 and are not bent as abruptly as they otherwise might when they pass from converging section 12 to diverging section 14. This creates an overall smoothing effect in the flow which reduces the tendency toward turbulence in and build-up of the boundary layers of gas flowing along the interior surfaces of diverging section 14. At the same time, this smoothing effect reduces the likelihood of the gas separating from the walls of this section.
  • this construction prevents the plane at which the gas pressure equals ambient pressure (the ambient pressure plane) from moving into the converging or diverging sections of the nozzle and thereby causing a deflection of the gas flow which would tend to increase boundary layer thickness and enhance the possibility of separation of the gas from the interior of the nozzle.
  • a further advantage of this construction is demonstrable when the pressure of the input gas is varied, either deliberately over a moderate range, or due to the pressure fluctuations which might be encountered in the usual industrial pressurized gas supplies. Under such conditions the increased tendency toward separation and excessive boundary layer turbulence caused by such pressure variations is minimized.
  • the output of the generator is predictable and stable despite such variations in the input pressure, in contrast to the erratic and unpredictable output often developed by nozzles not provided with such a stabilizing section, a lack of stability which, it is believed, may be caused by a shifting of the ambient pressure plane.
  • the overall effect is to provide a generator whose sonic output power is relatively stable and predictable despite the usual fluctuations of pressure encountered in most pressurized gas supply systems used in industry.
  • the sonic output power of 'this generator can be effectively varied over a moderate range of output values in a stable and predictable manner by varying the input gas pressure.
  • generators constructed and operated in accordance with this invention give steady and predictable sonic power outputs when operated with input gas pressures varying between approximately 10 and 30 pounds per square inch gage (p.s.i.g.).
  • generators in which the stabilizing section of the present invention is added to a converging-diverging nozzle have produced at least 50 percent more sonic output power than without such a stabilizing section.
  • a further beneficial effect is that the frequency of the sonic pressure wave output produced by the generator is cleaner; that is, the frequencies produced fall within a band which is narrower than previously obtained with devices of this nature so that the output is more nearly free from extraneous noise.
  • the pulsator cavity 20 should be located, centered, and dimensioned as precisely as possible with respect to the location and dimensions of this shock wave, a pulsator with fixed dimensions may be used in a generator in accordance with this invention to produce a sonic power output deviating only slightly from optimum values as the input gas pressure varies. Furthermore, the reduction of fflutter of the shock wave tends greatly to clean up the frequency distribution of the sonic output.
  • the length I of stabilizing section 13 should have a minimum value equal to the axial shift in position of the ambient pressure plane that would occur in an ordinary converging-diverging nozzle having converging and diverging sections with the same dimensions as those of the proposed nozzle, when the input pressure varies within certain expected limits.
  • the distance of this axial shift can be determined by using the following equations to determine the nozzle diameters at which the ambient pressure plane will appear when first the maximum and then the minimum expected input pressures are supplied, and then computing the axial distance between the points along the nozzle axis at which these diameters are located.
  • A the cross sectional area of the nozzles conduit at any point along its longitudinal axis.
  • A* the cross sectional area of the nozzle conduit at the point where the Mach number of the gas in the noz- Z18:
  • 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 absolute pressure of the gas in the nozzle at any point along its longitudinal axis.
  • the length I of the stabilizing section 13 is made somewhat longer than the above-described minimum value.
  • the ratio between the length I of stabilizing section 13 and the length L of diverging section 14 usually falls between 1/ 3 and 1/2. Nozzles using a ratio of J to L of 1/ 3 have proved especially desirable.
  • the pulsator cavity 20' in pulsator unit 18 is held in the desired spaced relationship to nozzle 10 by means of a pair of leg-like members 22 afiixed to a ring-shaped portion 24 which is attached to nozzle portion 10 by means of screw threads 26. This threaded engagement may be used to provide for adjustment of the distance between pulsator unit 18 and nozzle 10.
  • the length I and convergence angle (a) of converging section 12, and the length L and divergence angle ([2) of diverging section 14 necessary to give a preferred output from the sonic generator all can be determined from Equations 1 and 2 in accordance with the principles set forth in my above-mentioned co-pending patent application.
  • the distance Y of the forward end of pulsator cavity 20 from the exit of nozzle 10, and the depth Z of cavity 20 to be used in obtaining optimum performance from the generator may be determined by use of the principles set forth in my above-mentioned copending patent application.
  • the pulsator cavity 20 comprises a cylindrical hole hav ing a conically-shaped rear wall 28.
  • the provision of conical rear wall 28 for cavity 20 improves the performance of the sonic generator in that the frequencies of the sound waves emanating from cavity 26 fall within a substantially narrower band than in previous devices of this nature. That is, the sonic pressure wave output is cleaner and contains less extraneous noise.
  • the cone angle (c) of rear wall 28 of comically-bottomed pulsator cavity 20 should be, desirably, between and 150. An angle of about has proved highly satisfactory in actual use. It is believed that this pulsator cavity bottom intercepts and reflects the shock waves of the gas jet produced by nozzle 10 in a manner such that the development of sonic pressure waves at undesired frequencies is reduced.
  • the sonic generator shown in FIGURE 3 includes a a housing member, generally indicated at 30, which comprises a ring-shaped section 32 with a set of interior screw threads 34, a pair of leg-like members 36 connecting an end portion 38 of housing 30 to threaded support section 32, with a pulsator cavity 40 formed in end portion 38.
  • a cylindrical nozzle member is threaded on its outside surface and is mounted inside housing member 30 by engagement with screw threads 34.
  • Nozzle member 42 has an axial passage or conduit which includes an initial straight cylindrical stabilizing section 44 followed by a diverging section 46.
  • a source of pressurized gas (not shown) is connected to housing 30 through a pipe 48 having a threaded end 50 engaged with screw threads 34.
  • the construction of the generator shown in FIGURE 3 is simpler than that of previous sonic generators.
  • the machining of sections 44 and 46 of nozzle member 42 is simpler since member 42 may be prepared as a separate element and can be fitted into housing 30 when it is completed.
  • member 42 is constructed without a converging section corresponding to section 12 of the nozzle shown in FIGURES 1 and 2. This further simplifies the construction of the nozzle. It has been found that the use of a converging section in a nozzle for use in gas-operated sonic generators is not necessary if a stabilizing section such as section 44 is used. It has been discovered that this is true whether the inside diameter of the pipe 48 supplying air to the generator is equal to or is greater than the diameter of stabilizing section 44.
  • the minimum value for the length K of stabilizing section 44 can be determined by the method outlined above for determining the minimum length of stabilizing section I of nozzle 10.
  • the ratio of stabilizer section length K to diverging section length N is usually between 1/3 and 1/2. Nozzles using a ratio of K to N of 1/3 have proved especially desirable. Since the gas flowing in stabilizing section 44 has a Mach number of 1.0, the length N and divergence angle ((1) of diverging section 46 can be determined in the same way that the corresponding values (b) and L of section 14 of nozzle are determined. Similarly, the optimum values for the placement and depth dimensions Q and R of pulsator 40 can be determined in accordance with the principles set forth in my above-mentioned co-pending application.
  • the operating characteristics of three examples of nozzles built and operated in accordance with the embodiment of the invention shown in FIGURES 1 and 2 are given in the table below.
  • the input air pressure and the output power of each of the units tested vary from relatively low values (4 p.s.-i.g. and 400 watts) for the unit shown in Example 1, to relatively high values (30 p.s.i.g. and 1400 watts) for the unit shown in Example 3.
  • Example 1 Example 2
  • Example 3 4 p.s.i.g 8 p.s.i.g 30 p s.i.g. 12.87--.” 15.62 30.76.
  • the frequency of the sonic output is given in cycles per second.
  • the sonic power output was measured at the source.
  • a gas operated pressure wave generator said generator compnising, in combination, a gas-accelerating nozzle comprising 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 oi 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 crossseotional 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 passageway between said reduced orifice and said second longitudinal position, said stabilizing means also providing another orifice at said second longitudinal position, said other onifice having a cross-sectional area substantially equal to that or said reduced orifice, expansion means in said gas flow passageway between said other orifice and said third longitudinal position, said expansion means providing an increasing cross-sectional area for said
  • a gas-operated pressure wave generator comprising, in combination, a gas-accelerating nozzle comprising 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 crosssectional area of said gas flow passageway and forming a reduced orifice at said first longitudinal position, stabilizing means between said reduced orifice and second longitudinal position providing a cylindrical shape for said gas flow, 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 orifice and said third longitudinal position, said expansion means providing a irustro-conical shape for said passageway between said other orifice and said third longitudinal position in the direction of flow of gas through said nozzle, reson
  • a gas-operated pressure wave generator said generator co-mtpnising, in combination, a gas-accelerating nozzle comprising 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 crosssectional area ot 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 passageway 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 orifice and said third longitudinal position, said expansion means providing an increasing cross-sectional area for said passageway between said other orifice and.
  • said generator being adapted to be supplied with a compressed gas, to convert said compressed gas into a highspeed gas stream flowing in an ambient gaseous medium, and to generate pressure waves in said medium 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 to 1.0:
  • a gaso-perated pressure wave generator comprising, in combination, a gas-accelerating nozzle comprising a body member forming a gas flow passageway, first, second and third longitudinal positions in said body mernber, 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 crosssectional 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 passageway 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 orifice and said third longitudinal position, said expansion means providing an increasing cross-sectional area for said
  • a gas-operated sonic pressure wave generator comprising, in combination, a nozzle for producing a highspeed, low-pressure gas jet, said nozzle comprising a body having a conduit therethrough, said conduit including a converging frustro-conical shaped inlet section, a diverging frust-ro-conical shaped outlet section, and a cylindrical mid-section interconnecting the small ends of said inlet and outlet sections, a resonator member with a resonator cavity in it, and means for positioning said resonator member with said cavity facing the exit opening of said outlet section.
  • Apparatus as in claim 1 including a compressed gas supply tube, and in which said resonator means comprises a resonator cavity in said positioning means, said positioning means being adapted to engage and secure to gether said gas supply tube and said nozzle with said supply tube feeding compressed gas to said nozzle.

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  • Physics & Mathematics (AREA)
  • Engineering & Computer Science (AREA)
  • Acoustics & Sound (AREA)
  • Multimedia (AREA)
  • Nozzles (AREA)
  • Jet Pumps And Other Pumps (AREA)
  • Percussion Or Vibration Massage (AREA)
  • Toys (AREA)
US247221A 1962-11-21 1962-12-26 Sonic pressure wave generator Expired - Lifetime US3230924A (en)

Priority Applications (7)

Application Number Priority Date Filing Date Title
US247221A US3230924A (en) 1962-12-26 1962-12-26 Sonic pressure wave generator
SE14247/63A SE331604B (enEXAMPLES) 1962-12-26 1963-12-19
DE1963S0088808 DE1447333B2 (de) 1962-11-21 1963-12-19 Vorrichtung zur erzeugung von schalldruckwellen
NO151318A NO122811B (enEXAMPLES) 1962-12-26 1963-12-20
GB50458/63A GB1063859A (en) 1962-12-26 1963-12-20 Sonic pressure wave generator
CH1558763A CH457937A (fr) 1962-12-26 1963-12-24 Procédé pour produire de l'énergie sonique et appareil pour la mise en oeuvre de ce procédé
DE1964S0089650 DE1475154B2 (de) 1962-11-21 1964-02-24 Verwendung eines Hartmann-Generators bei einer Einrichtung zur Zerstäubung von Flüssigkeiten

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US247221A US3230924A (en) 1962-12-26 1962-12-26 Sonic pressure wave generator

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GB (1) GB1063859A (enEXAMPLES)
NO (1) NO122811B (enEXAMPLES)
SE (1) SE331604B (enEXAMPLES)

Cited By (8)

* 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
US3484914A (en) * 1966-06-13 1969-12-23 Bemberg Spa Method and means for treating with a gasiform stream a thread bundle made of a plurality of elementary threads
US3937445A (en) * 1974-02-11 1976-02-10 Vito Agosta Process and apparatus for obtaining the emulsification of nonmiscible liquids
US4690332A (en) * 1983-11-28 1987-09-01 Nathaniel Hughes Single inlet prepackaged inhaler
US6098897A (en) * 1998-12-23 2000-08-08 Lockwood; Hanford N. Low pressure dual fluid atomizer
US6584774B1 (en) * 2001-10-05 2003-07-01 The United States Of America As Represented By The Secretary Of The Air Force High frequency pulsed fuel injector
US20090214990A1 (en) * 2006-07-22 2009-08-27 Egon Evertz Flame burner and method for flame burning a metallic surface
CN111295342A (zh) * 2017-08-04 2020-06-16 创意和喊叫有限公司 发声瓶盖

Citations (16)

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Publication number Priority date Publication date Assignee Title
DE285330C (enEXAMPLES) *
US1127320A (en) * 1911-03-16 1915-02-02 Harry P Tiffner Resonator.
US1413113A (en) * 1918-03-15 1922-04-18 Good Inventions Co Liquid-fuel burner
US1462680A (en) * 1922-09-01 1923-07-24 Bliss John Burner for fluid fuel
US1779009A (en) * 1928-02-15 1930-10-21 Negro Luigo Nozzle
FR722233A (fr) * 1931-08-31 1932-03-14 Perfectionnements aux trompes sonores et appareils avertisseurs acoustiques similaires
US1953990A (en) * 1932-12-07 1934-04-10 Vilbiss Co Fluid ejecting nozzle
US1980171A (en) * 1932-01-27 1934-11-13 Amy Aceves & King Inc Dispersing particles suspended in air
US2044697A (en) * 1935-12-28 1936-06-16 Huss Henry Nozzle
US2052926A (en) * 1935-08-23 1936-09-01 John A Frisk Whistle
US2297726A (en) * 1938-04-02 1942-10-06 Thermo Plastics Corp Method and apparatus for drying or the like
US2519619A (en) * 1944-08-04 1950-08-22 Inst Gas Technology Acoustic generator
US2532554A (en) * 1946-01-29 1950-12-05 Thomas D Joeck Method for atomizing by supersonic sound vibrations
US2815985A (en) * 1954-12-14 1957-12-10 Joseph D Pesce Oil burner
US3009826A (en) * 1957-05-24 1961-11-21 Aeroprojects Inc Process of forming a dispersion of aerosol particles and process for coating solid particles with said dispersion
US3064619A (en) * 1960-03-11 1962-11-20 Gen Precision Inc Acoustic generator and shock wave radiator

Patent Citations (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE285330C (enEXAMPLES) *
US1127320A (en) * 1911-03-16 1915-02-02 Harry P Tiffner Resonator.
US1413113A (en) * 1918-03-15 1922-04-18 Good Inventions Co Liquid-fuel burner
US1462680A (en) * 1922-09-01 1923-07-24 Bliss John Burner for fluid fuel
US1779009A (en) * 1928-02-15 1930-10-21 Negro Luigo Nozzle
FR722233A (fr) * 1931-08-31 1932-03-14 Perfectionnements aux trompes sonores et appareils avertisseurs acoustiques similaires
US1980171A (en) * 1932-01-27 1934-11-13 Amy Aceves & King Inc Dispersing particles suspended in air
US1953990A (en) * 1932-12-07 1934-04-10 Vilbiss Co Fluid ejecting nozzle
US2052926A (en) * 1935-08-23 1936-09-01 John A Frisk Whistle
US2044697A (en) * 1935-12-28 1936-06-16 Huss Henry Nozzle
US2297726A (en) * 1938-04-02 1942-10-06 Thermo Plastics Corp Method and apparatus for drying or the like
US2519619A (en) * 1944-08-04 1950-08-22 Inst Gas Technology Acoustic generator
US2532554A (en) * 1946-01-29 1950-12-05 Thomas D Joeck Method for atomizing by supersonic sound vibrations
US2815985A (en) * 1954-12-14 1957-12-10 Joseph D Pesce Oil burner
US3009826A (en) * 1957-05-24 1961-11-21 Aeroprojects Inc Process of forming a dispersion of aerosol particles and process for coating solid particles with said dispersion
US3064619A (en) * 1960-03-11 1962-11-20 Gen Precision Inc Acoustic generator and shock wave radiator

Cited By (9)

* 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
US3484914A (en) * 1966-06-13 1969-12-23 Bemberg Spa Method and means for treating with a gasiform stream a thread bundle made of a plurality of elementary threads
US3937445A (en) * 1974-02-11 1976-02-10 Vito Agosta Process and apparatus for obtaining the emulsification of nonmiscible liquids
US4690332A (en) * 1983-11-28 1987-09-01 Nathaniel Hughes Single inlet prepackaged inhaler
US4702415A (en) * 1983-11-28 1987-10-27 Vortran Corporation Aerosol producing device
US6098897A (en) * 1998-12-23 2000-08-08 Lockwood; Hanford N. Low pressure dual fluid atomizer
US6584774B1 (en) * 2001-10-05 2003-07-01 The United States Of America As Represented By The Secretary Of The Air Force High frequency pulsed fuel injector
US20090214990A1 (en) * 2006-07-22 2009-08-27 Egon Evertz Flame burner and method for flame burning a metallic surface
CN111295342A (zh) * 2017-08-04 2020-06-16 创意和喊叫有限公司 发声瓶盖

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NO122811B (enEXAMPLES) 1971-08-16
GB1063859A (en) 1967-03-30
SE331604B (enEXAMPLES) 1971-01-04

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