EP1908526A1 - Düse für eine Zwei-Phasenmischung - Google Patents

Düse für eine Zwei-Phasenmischung Download PDF

Info

Publication number
EP1908526A1
EP1908526A1 EP06291557A EP06291557A EP1908526A1 EP 1908526 A1 EP1908526 A1 EP 1908526A1 EP 06291557 A EP06291557 A EP 06291557A EP 06291557 A EP06291557 A EP 06291557A EP 1908526 A1 EP1908526 A1 EP 1908526A1
Authority
EP
European Patent Office
Prior art keywords
liquid
nozzle
gas
mixture
particle size
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Withdrawn
Application number
EP06291557A
Other languages
English (en)
French (fr)
Inventor
Thibault Bourrilhon
Bernard Dusser
Patrick Fernandes
Jean-Paul Thibaut
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Le Centre National de la Recherche Scientifique - LEGI
Universite Joseph Fourier Grenoble 1
Siemens SAS
Original Assignee
Le Centre National de la Recherche Scientifique - LEGI
Universite Joseph Fourier Grenoble 1
Siemens SAS
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Le Centre National de la Recherche Scientifique - LEGI, Universite Joseph Fourier Grenoble 1, Siemens SAS filed Critical Le Centre National de la Recherche Scientifique - LEGI
Priority to EP06291557A priority Critical patent/EP1908526A1/de
Priority to CA2665265A priority patent/CA2665265C/en
Priority to UAA200903212A priority patent/UA99264C2/ru
Priority to PCT/EP2007/007488 priority patent/WO2008040418A1/fr
Priority to US12/444,432 priority patent/US9352340B2/en
Priority to KR1020097009237A priority patent/KR101384012B1/ko
Priority to EP07801913.0A priority patent/EP2069073B1/de
Publication of EP1908526A1 publication Critical patent/EP1908526A1/de
Withdrawn legal-status Critical Current

Links

Images

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B05SPRAYING OR ATOMISING IN GENERAL; APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
    • B05BSPRAYING APPARATUS; ATOMISING APPARATUS; NOZZLES
    • B05B7/00Spraying apparatus for discharge of liquids or other fluent materials from two or more sources, e.g. of liquid and air, of powder and gas
    • B05B7/0012Apparatus for achieving spraying before discharge from the apparatus
    • AHUMAN NECESSITIES
    • A62LIFE-SAVING; FIRE-FIGHTING
    • A62CFIRE-FIGHTING
    • A62C31/00Delivery of fire-extinguishing material
    • A62C31/02Nozzles specially adapted for fire-extinguishing
    • AHUMAN NECESSITIES
    • A62LIFE-SAVING; FIRE-FIGHTING
    • A62CFIRE-FIGHTING
    • A62C31/00Delivery of fire-extinguishing material
    • A62C31/02Nozzles specially adapted for fire-extinguishing
    • A62C31/05Nozzles specially adapted for fire-extinguishing with two or more outlets
    • AHUMAN NECESSITIES
    • A62LIFE-SAVING; FIRE-FIGHTING
    • A62CFIRE-FIGHTING
    • A62C99/00Subject matter not provided for in other groups of this subclass
    • A62C99/0009Methods of extinguishing or preventing the spread of fire by cooling down or suffocating the flames
    • A62C99/0072Methods of extinguishing or preventing the spread of fire by cooling down or suffocating the flames using sprayed or atomised water
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B05SPRAYING OR ATOMISING IN GENERAL; APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
    • B05BSPRAYING APPARATUS; ATOMISING APPARATUS; NOZZLES
    • B05B3/00Spraying or sprinkling apparatus with moving outlet elements or moving deflecting elements
    • B05B3/02Spraying or sprinkling apparatus with moving outlet elements or moving deflecting elements with rotating elements
    • B05B3/04Spraying or sprinkling apparatus with moving outlet elements or moving deflecting elements with rotating elements driven by the liquid or other fluent material discharged, e.g. the liquid actuating a motor before passing to the outlet
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B05SPRAYING OR ATOMISING IN GENERAL; APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
    • B05BSPRAYING APPARATUS; ATOMISING APPARATUS; NOZZLES
    • B05B3/00Spraying or sprinkling apparatus with moving outlet elements or moving deflecting elements
    • B05B3/02Spraying or sprinkling apparatus with moving outlet elements or moving deflecting elements with rotating elements
    • B05B3/04Spraying or sprinkling apparatus with moving outlet elements or moving deflecting elements with rotating elements driven by the liquid or other fluent material discharged, e.g. the liquid actuating a motor before passing to the outlet
    • B05B3/0409Spraying or sprinkling apparatus with moving outlet elements or moving deflecting elements with rotating elements driven by the liquid or other fluent material discharged, e.g. the liquid actuating a motor before passing to the outlet with moving, e.g. rotating, outlet elements
    • B05B3/0418Spraying or sprinkling apparatus with moving outlet elements or moving deflecting elements with rotating elements driven by the liquid or other fluent material discharged, e.g. the liquid actuating a motor before passing to the outlet with moving, e.g. rotating, outlet elements comprising a liquid driven rotor, e.g. a turbine
    • B05B3/0422Spraying or sprinkling apparatus with moving outlet elements or moving deflecting elements with rotating elements driven by the liquid or other fluent material discharged, e.g. the liquid actuating a motor before passing to the outlet with moving, e.g. rotating, outlet elements comprising a liquid driven rotor, e.g. a turbine with rotating outlet elements
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B05SPRAYING OR ATOMISING IN GENERAL; APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
    • B05BSPRAYING APPARATUS; ATOMISING APPARATUS; NOZZLES
    • B05B3/00Spraying or sprinkling apparatus with moving outlet elements or moving deflecting elements
    • B05B3/02Spraying or sprinkling apparatus with moving outlet elements or moving deflecting elements with rotating elements
    • B05B3/04Spraying or sprinkling apparatus with moving outlet elements or moving deflecting elements with rotating elements driven by the liquid or other fluent material discharged, e.g. the liquid actuating a motor before passing to the outlet
    • B05B3/06Spraying or sprinkling apparatus with moving outlet elements or moving deflecting elements with rotating elements driven by the liquid or other fluent material discharged, e.g. the liquid actuating a motor before passing to the outlet by jet reaction, i.e. creating a spinning torque due to a tangential component of the jet
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B05SPRAYING OR ATOMISING IN GENERAL; APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
    • B05BSPRAYING APPARATUS; ATOMISING APPARATUS; NOZZLES
    • B05B7/00Spraying apparatus for discharge of liquids or other fluent materials from two or more sources, e.g. of liquid and air, of powder and gas
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B05SPRAYING OR ATOMISING IN GENERAL; APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
    • B05BSPRAYING APPARATUS; ATOMISING APPARATUS; NOZZLES
    • B05B7/00Spraying apparatus for discharge of liquids or other fluent materials from two or more sources, e.g. of liquid and air, of powder and gas
    • B05B7/0018Spraying 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 devices for making foam
    • B05B7/0025Spraying 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 devices for making foam with a compressed gas supply
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B05SPRAYING OR ATOMISING IN GENERAL; APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
    • B05BSPRAYING APPARATUS; ATOMISING APPARATUS; NOZZLES
    • B05B7/00Spraying apparatus for discharge of liquids or other fluent materials from two or more sources, e.g. of liquid and air, of powder and gas
    • B05B7/02Spray pistols; Apparatus for discharge
    • B05B7/04Spray pistols; Apparatus for discharge with arrangements for mixing liquids or other fluent materials before discharge
    • B05B7/0416Spray pistols; Apparatus for discharge with arrangements for mixing liquids or other fluent materials before discharge with arrangements for mixing one gas and one liquid
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B05SPRAYING OR ATOMISING IN GENERAL; APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
    • B05BSPRAYING APPARATUS; ATOMISING APPARATUS; NOZZLES
    • B05B7/00Spraying apparatus for discharge of liquids or other fluent materials from two or more sources, e.g. of liquid and air, of powder and gas
    • B05B7/02Spray pistols; Apparatus for discharge
    • B05B7/04Spray pistols; Apparatus for discharge with arrangements for mixing liquids or other fluent materials before discharge
    • B05B7/0416Spray pistols; Apparatus for discharge with arrangements for mixing liquids or other fluent materials before discharge with arrangements for mixing one gas and one liquid
    • B05B7/0441Spray pistols; Apparatus for discharge with arrangements for mixing liquids or other fluent materials before discharge with arrangements for mixing one gas and one liquid with one inner conduit of liquid surrounded by an external conduit of gas upstream the mixing chamber
    • B05B7/0475Spray pistols; Apparatus for discharge with arrangements for mixing liquids or other fluent materials before discharge with arrangements for mixing one gas and one liquid with one inner conduit of liquid surrounded by an external conduit of gas upstream the mixing chamber with means for deflecting the peripheral gas flow towards the central liquid flow
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B05SPRAYING OR ATOMISING IN GENERAL; APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
    • B05BSPRAYING APPARATUS; ATOMISING APPARATUS; NOZZLES
    • B05B7/00Spraying apparatus for discharge of liquids or other fluent materials from two or more sources, e.g. of liquid and air, of powder and gas
    • B05B7/02Spray pistols; Apparatus for discharge
    • B05B7/04Spray pistols; Apparatus for discharge with arrangements for mixing liquids or other fluent materials before discharge
    • B05B7/0416Spray pistols; Apparatus for discharge with arrangements for mixing liquids or other fluent materials before discharge with arrangements for mixing one gas and one liquid
    • B05B7/0483Spray pistols; Apparatus for discharge with arrangements for mixing liquids or other fluent materials before discharge with arrangements for mixing one gas and one liquid with gas and liquid jets intersecting in the mixing chamber
    • CCHEMISTRY; METALLURGY
    • C21METALLURGY OF IRON
    • C21CPROCESSING OF PIG-IRON, e.g. REFINING, MANUFACTURE OF WROUGHT-IRON OR STEEL; TREATMENT IN MOLTEN STATE OF FERROUS ALLOYS
    • C21C5/00Manufacture of carbon-steel, e.g. plain mild steel, medium carbon steel or cast steel or stainless steel
    • C21C5/28Manufacture of steel in the converter
    • C21C5/42Constructional features of converters
    • C21C5/46Details or accessories
    • C21C5/4606Lances or injectors

Definitions

  • the present invention relates to a device for ejecting an at least two-phase mixture according to the preamble of claim 1, as well as various advantageous uses of this device according to claims 16 to 20.
  • a known way to fight effectively against a fire is the water lance, allowing to "drown" a fire, especially under a large range of ejection but at the cost of a large flow of water.
  • Another ejection device uses a two-phase mixture, for example by means of, inter alia, water and pressurized gas, and adapts itself in the field of extinguishing fire in order to create a mist of water or fire-fighting foam, such as a conventional fire extinguisher.
  • the amount of water required is therefore reduced.
  • Other agents may also be included in the pressurized water-gas phase, such as an emulsifying agent or another agent of a non-obligatorily emulsifying nature such as carbon dioxide.
  • agent remains however binding for example because of the limited storage of a fire extinguisher.
  • the scope of conventional fire extinguishers is also limited because they are designed for small-scale fire suppression.
  • a device of this type comprises a wall delimiting a chamber where this two-phase pressure flow is produced, perforated by at least one opening through which a gas under a so-called "supply pressure" pressure, equipped with a first upstream end connected to a liquid supply source substantially at the same pressure, and a second downstream end connected to a fluid accelerating nozzle where it relaxes, and from which it escapes in the form of jet at high speed.
  • Such a device makes it possible to create a two-phase jet of water and non-oxidizing gas at the site of the fire intervention, from the existing water resource, and from a source of non-oxidizing gas.
  • the supply pressure is increased to obtain jets at such speeds that they can reach fires at great distances, the operation of the devices becomes defective.
  • This device for ejecting a two-phase mixture comprises two separate inputs for a liquid injection inlet and the injection inlet gas, an emulsion chamber for producing a liquid-gas mixture and an ejection nozzle of the first liquid-gas mixture in a main direction defined by a vector axis.
  • the gas is injected perpendicularly into the water inlet pipe and through perforated elements promoting the emulsion of the liquid-gas mixture.
  • partition elements such as lamellae are arranged parallel to the flow of the water pipe so as to form separate channels of flow. These slats can be spaced angularly on a section of the water pipe surrounded by the perforated elements for the entry of gas into the channels. Admittedly, this device makes it possible to generate a constant two-phase jet for various pressures, but may be subject to disturbances due to untimely obstructions at the level of the lamellae or perforated elements, for example when introducing impurities (sand, pebble, dirt, etc.) via the water pipe or via the gas line. This can also result in a point or prolonged degeneration of the diphasic mixture which makes the extinction of a fire less manageable.
  • the elements internally arranged at the levels of the pipes require the manufacture and maintenance of the complex device.
  • An object of the present invention is to provide a simple device for ejecting a mixture at least two-phase that allows at least a precise control of its ejection range in two-phase assured.
  • this device should adapt to various liquid and gas injection pressures, or even in the low pressure range while reaching long spans of the two-phase jet.
  • the device should be able to overcome internal elements with shutter potential and complex and remain insensitive to input impurity factors, in that the two-phase mixture at the device outlet is provided over the entire length of the jet and permanently .
  • the invention thus proposes a solution based on a device for ejecting an at least two-phase mixture, comprising at least one injection inlet for a liquid and a gas, an emulsion chamber for producing a first liquid-gas mixture. , an ejection nozzle of the first liquid-gas mixture in a main direction defined by a vector axis.
  • the ejection nozzle has a geometry with at least a minimum cross-sectional area along its length, at a location of the vector axis, not only is an expansion effect within the nozzle created as known in any Venturi type flow, but it is important to note that the geometry of the nozzle is adapted such that a relaxation within the ejection nozzle is induced allowing the first liquid-gas mixture from the chamber of emulsion to be converted, in the direction of the flow configuration, into a second liquid-gas mixture at the outlet of the nozzle, the ejection range of the second mixture and the particle size of the liquid in the form of droplets can be controlled according to the mass flow rates of the liquid and gas and the absolute pressure at the injection inlet.
  • the invention makes it possible to optionally use a common inlet for the liquid and the gas, which decreases the complexity favorably vis-à-vis device with two separate inputs whose relative position is to be taken into account in particularly for the emulsion.
  • the invention does not require the use of sharing or perforation elements in one of the injection inlets to allow quality emulsion and two-phase mixing, because the geometry of the nozzle coupled to the generating conditions at the inlet of the device (mass flow rates of the liquid and the gas and the absolute pressure at the injection inlet) ensure optimum emulsion and in addition allow the two-phase mixture at the nozzle inlet to be transformed, in the direction of the flow configuration, in a second two-phase mixture at the outlet of nozzles whose particle size and range are clearly related to the generating conditions, thus controlled.
  • the device is very simplified and moreover avoids any shutter effect by the absence of elements arranged in the complete flow.
  • such elements perforated cone, grid, stirrer, etc.
  • the geometry of the nozzle is adapted so that the ejected mixture, called the second mixture to distinguish it from the first mixture at the nozzle inlet, forms a fog jet mainly along the vector axis of the nozzle and whose particle size, the range and volume deployment out of the vector axis (also commonly referred to as jet divergence) are controllable and assured up to the desired fire attack surface.
  • the impurities or even grains of sand do not cause significant disturbances at the two-phase ejected mixture. It is even possible to add to the water-gas mixture an abrasive product such as consisting of fine solid particles.
  • the nozzle inlet consists of a first high gradient convergent access zone followed by a second low gradient convergent zone, a transition to the minimum cross section also referred to as the nozzle neck, and possibly a third divergent area ending in the nozzle outlet section. It is thanks to such a configuration or to similar configurations that the expansion within the nozzle makes it possible to control the particle size of the fog jet and its range, as a function of generating conditions that are simply definable at the inlet of the device.
  • a strong advantage of the invention is that the device can be used for a low absolute pressure (generally of the order of 5 to 10 bar) at the inlet to the emulsion chamber or the nozzle.
  • a fog jet flow at the outlet of the nozzle is, however, perfectly ensured in a range from 50 to 150 m / s and a particle size of droplets of 50 to 150 microns.
  • the device therefore does not require a high input pressure or at least a considerable increase, in order to guarantee a larger jet range, such as for a long range light.
  • untimely and abrupt variations in its particle size (and therefore its diphasic state) are discarded.
  • the geometry of the nozzle allows a liquid-gas emulsion at its inlet to provide particle size uniformity as well as controlled range (and vice versa). It could then be understood that to vary the range thus obtained without modifying the particle size of the jet and the generating conditions, it would be necessary to modify the geometry of the nozzle, which would be practically impossible.
  • nozzle geometry has also been calculated and adapted to allow range variation of the jet for a stable particle size factor by simply varying one or more of the generating conditions at the inlet or in the device.
  • the input pressure (liquid-gas injection) of the device is for example adjustable by a single valve.
  • the invention also has a second advantageous aspect coupling several nozzles as described above and arranged on a rotary support, allowing in addition to a gyratory action by the detents of the nozzles and their particular provisions on the rotor and between them, of sweep targeted surfaces in a complete and extensive way or to project jets of fog over a large volume without trying to reach precisely a flame zone for example.
  • the rotational speed can also be favorably controlled for a desired exercise, depending on the generating conditions of the multi-nozzle device, similar to that of a single nozzle.
  • the ejection device according to the invention satisfies the requirements of the control of large particle size in practice.
  • the size of the droplets must be adapted according to the type of fire, for example by means of finer drops to attack hydrocarbon foci or to cool very hot environments, or by means of larger drops for wet fires forming embers.
  • a set of subclaims also has advantages of the invention.
  • the particle size and range characteristics of the second ejected MLG2 liquid-gas mixture are controllable by said generator conditions such as the total inlet pressure of the EMC emulsion chamber or of the EJ nozzle (s) and the mass flow rates of the liquid. L1 and gas G1. These generating conditions relating to a nozzle flow are adapted for operating points of the nozzle with targeted particle size and range.
  • the feed conditions pressure of the first mixture MLG1 inlet nozzle EJ, incoming flow of the liquid L1, incoming flow of the gas G1 are not arbitrary.
  • jet outlet conditions are entirely a function of the conditions generating the flow, directly also related to the geometry of the nozzle. It is thus possible to map, for a nozzle geometry, operating points according to the generating and output conditions for each desired ejection application.
  • the network arrangements and the multi-head device have the disadvantage of leaving unprotected areas of the volume, while the solution of a rotating body on which several nozzles are fixed can scan all a set of direction and optimally cover the volume to be protected.
  • FIG. 2 such a device for ejecting a two-phase fluid MLG1 injected into a multi-nozzle rotary system is shown in cross-section.
  • the system comprises a stator STAT rotating guide a rotor ROT, on which are arranged nozzles EJ, EJ1, EJ2.- according to Figure 1.
  • the gas G1 and liquid L1 are directly injected to the inputs nozzles via the single input IN of the stator STAT leading to a free inner space of the rotor ROT which simply serves as an EMD distribution chamber for the MLG1 mixture.
  • an effective emulsion chamber for example with perforated or partition elements, is no longer indispensable insofar as the mixture is admitted directly into the distribution chamber.
  • EMC emulsion chamber
  • the axis AX of a nozzle EJ can be superimposed on the axis of rotation RX of the rotor ROT, but does not contribute to the rotation of the rotor.
  • This nozzle EJ can also be fixed on the stator STAT to simplify the construction of the complete device and avoid a rotation of the nozzle on itself.
  • Separate jets are disposed on the walls of the EMD distribution chamber, in particular so as to obtain a surface or a fog cover volume extended to at least one defined range.
  • Some vector axes AX1, AX2, ... ejector nozzles EJ1, EJ2, - can be arranged on the rotor ROT asymmetrically about a plane comprising the axis of rotation RX, and are in particular oriented from staggered at an angle between 0 ° and 90 ° in a plane perpendicular to the axis of rotation RX. To simply favor the jet distribution, this angle is different between at least two adjacent nozzles.
  • the expansions at the outlet of the ejector nozzles EJ1, EJ2, ... or / and the directions distinct from the vector axes AX1, AX2,... are thus adapted so that a rotating effect of the rotor ROT with controlled rotation speed is produced.
  • the vector axes AX1, AX2,... May also be free from any intersection with the axis of rotation RX in order to generate on the rotor ROT by the reaction forces in a nozzle a torque component laterally to the nozzle inducing an angular displacement of the rotor ROT about its axis RX.
  • the fog obtained can have various properties useful for various exercises (close and far extinction, several controlled diameters of drops).
  • the pressure of the liquid L1 or / and the gas G1 at the injection inlet is adaptable according to the ratio of the inlet flow rates for the liquid L1 and the gas G1 .
  • the device is designed with geometrically studied nozzles, so that particle size characteristics and scope of the second ejected MLG2 liquid-gas mixture are controllable by generating conditions such as the total inlet pressure of the EMD distribution chamber or / of the nozzle (s) EJ, EJ1, EJ2, ... and mass flow rates of the liquid L1 and gas G1.
  • the rotary device responds to generating conditions relating to a nozzle flow and which are adapted for operating points of the device for one (or more) granulometry (s) and / or one (or several) targeted reach (s).
  • liquid flow rates L1 of the order of less than 2 kg / s are made possible.
  • Figure 2 corresponding to an embodiment suitable for the rotary multi-nozzle device has one of the ideal geometries of the nozzle according to the invention.
  • This geometry has been detailed for the nozzle EJ2 seen in section at the level of its axis-vector AX2 (axis of symmetry of the nozzle).
  • the nozzle EJ2 consists of three portions of length La, Lb, LC along its vector axis AX2.
  • the nozzle inlet consists of a first zone, of length La, converging with a strong gradient followed by a second zone, of length Lb, converging at a low gradient, of a passage at the minimum section also called neck of the nozzle, and optionally to a third zone, of length Lc, diverging ending in the nozzle outlet section of dimension D2 (usually greater than 1 mm for extinguishing or cooling applications over a few tens of meters).
  • the first zone with high gradient favors a rapid atomization of the flow, the increase of the exchange surface resulting from this atomization allows intense transfers of momentum and energy, between liquid and gas, in the together the nozzle which thus jointly ensures atomization and acceleration of the liquid during relaxation. It is thanks to such a geometry and such dimensions that the two-phase mixture can be ejected after expansion into a fog nozzle with particle size, range and volume controlled as the invention describes it.
  • Figures 3 and 4 show a bottom view and a side view (right) of rotary multi-nozzle device according to Figure 2.
  • the arrangement of the nozzles EJ1, EJ2, ..., EJ6 relative to the axis of rotation RX of the rotor ROT is asymmetrical considering two nozzles whose vector axes are included in a single plane also comprising the axis of rotation.
  • RX rotation of the rotor for example the EJ4 and EJ6 nozzles with their vector axes AX4 and AX6).
  • the neighboring nozzles are also angularly offset relative to the axis of rotation RX of the rotor ROT. This arrangement promotes the controlled rotational effect of the rotor ROT, but also offers an extended jet scan on volumes to be humidified.
  • this system provides an ecological advantage because it operates at low water flow rates with respect to current devices for ejecting a two-phase water-gas mixture (weakly compressed gas). It therefore allows a low consumption of water coupled to a precisely controlled distribution of water.
  • This device could therefore also be advantageously used, outside a building, for the prevention of fire in natural environments.
  • the water could come from any source (especially a water table).
  • a humidification or even watering function is also possible over large spaces while minimizing water consumption without the need for high pressure at the inlet of the device.
  • Other media such as flammable industrial surfaces may also be protected against suspicious heating or fire.
  • the present invention is potentially adaptable to other types of applications such as propellant feed / atomization for rocket engines, or for fuel injection optimization for combustion heat engines.
  • the device for the propulsion of a vehicle comprising the nozzle as a means of propulsion is also possible, such as for the propulsion of a marine or air vehicle (submarine, jet-ski, airplane, etc.).

Landscapes

  • Health & Medical Sciences (AREA)
  • Public Health (AREA)
  • Business, Economics & Management (AREA)
  • Emergency Management (AREA)
  • Nozzles (AREA)
EP06291557A 2006-10-04 2006-10-04 Düse für eine Zwei-Phasenmischung Withdrawn EP1908526A1 (de)

Priority Applications (7)

Application Number Priority Date Filing Date Title
EP06291557A EP1908526A1 (de) 2006-10-04 2006-10-04 Düse für eine Zwei-Phasenmischung
CA2665265A CA2665265C (en) 2006-10-04 2007-08-27 Device for ejecting a diphasic mixture
UAA200903212A UA99264C2 (ru) 2006-10-04 2007-08-27 Устройство для выпуска двухфазной смеси
PCT/EP2007/007488 WO2008040418A1 (fr) 2006-10-04 2007-08-27 Dispositif d'éjection d'un mélange diphasique
US12/444,432 US9352340B2 (en) 2006-10-04 2007-08-27 Device for ejecting a diphasic mixture
KR1020097009237A KR101384012B1 (ko) 2006-10-04 2007-08-27 이상성 혼합물의 분사 장치
EP07801913.0A EP2069073B1 (de) 2006-10-04 2007-08-27 Düse für eine zwei-phasenmischung

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
EP06291557A EP1908526A1 (de) 2006-10-04 2006-10-04 Düse für eine Zwei-Phasenmischung

Publications (1)

Publication Number Publication Date
EP1908526A1 true EP1908526A1 (de) 2008-04-09

Family

ID=37781664

Family Applications (2)

Application Number Title Priority Date Filing Date
EP06291557A Withdrawn EP1908526A1 (de) 2006-10-04 2006-10-04 Düse für eine Zwei-Phasenmischung
EP07801913.0A Active EP2069073B1 (de) 2006-10-04 2007-08-27 Düse für eine zwei-phasenmischung

Family Applications After (1)

Application Number Title Priority Date Filing Date
EP07801913.0A Active EP2069073B1 (de) 2006-10-04 2007-08-27 Düse für eine zwei-phasenmischung

Country Status (6)

Country Link
US (1) US9352340B2 (de)
EP (2) EP1908526A1 (de)
KR (1) KR101384012B1 (de)
CA (1) CA2665265C (de)
UA (1) UA99264C2 (de)
WO (1) WO2008040418A1 (de)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2011087383A1 (en) * 2010-01-12 2011-07-21 Telesto Sp. Z.O.O. Apparatus for regulating two-phase flow and portable atomizer based on two-phase flow
CN109485168A (zh) * 2019-01-08 2019-03-19 威海百克环保工程有限公司 一种射流混合曝气器
CN114602104A (zh) * 2022-03-15 2022-06-10 刘龙平 一种室内消防用可定向大范围喷淋的自动喷淋装置

Families Citing this family (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR101383605B1 (ko) * 2010-08-11 2014-04-11 주식회사 엘지화학 플로트 유리 제조용 플로트 배스 및 플로트 배스 냉각 방법
KR101383604B1 (ko) * 2010-08-12 2014-04-11 주식회사 엘지화학 플로트 유리 제조용 플로트 배스 및 플로트 배스 냉각 방법
DK177678B1 (da) * 2011-12-19 2014-02-24 Vid Fire Kill Aps Modulært fast installeret tunnel brand beskyttelses system.
US20160325129A1 (en) * 2015-05-08 2016-11-10 International Fog Inc. Fluid discharge nozzle
US10081091B2 (en) * 2015-06-12 2018-09-25 Postech Academy-Industry Foundation Nozzle, device, and method for high-speed generation of uniform nanoparticles
US10324104B2 (en) * 2016-01-04 2019-06-18 Bradley Charles Ashmore Device for measuring the speed and direction of a gas flow
CN105749463A (zh) * 2016-05-03 2016-07-13 曹景怡 一种新型车载灭火***和防火方法
USD849226S1 (en) * 2017-05-24 2019-05-21 Hamworthy Combustion Engineering Limited Atomizer
CN107470049B (zh) * 2017-09-30 2023-04-18 江西远达环保有限公司 具有防汽化作用的脱硫脱硝用喷枪管
CN107470050B (zh) * 2017-09-30 2023-04-18 江西远达环保有限公司 具冷却效果的脱硫脱硝用喷枪
US10815046B2 (en) * 2018-03-03 2020-10-27 Byoplanet International, LLC Size-selective aerosol nozzle device
US11364510B2 (en) * 2018-11-20 2022-06-21 Willis Dane Multiple nozzle system
US11181544B2 (en) 2020-02-20 2021-11-23 Bradley Charles Ashmore Configurable flow velocimeter
CN111853776B (zh) * 2020-07-09 2022-05-27 芜湖中燃城市燃气发展有限公司 一种具有空气混合功能的天然气烧嘴及方法
CN114681845B (zh) * 2022-04-22 2022-11-25 海天消防科技股份有限公司 一种具有降温作用的变电站细水雾化灭火设备

Citations (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2548052A1 (fr) 1983-06-28 1985-01-04 Cebal Tete pour production de mousse avec de l'air et du liquide
WO1990005000A1 (en) * 1988-10-31 1990-05-17 Dale Gordon Jones Devices and method for cleaning gases
EP0608140A2 (de) * 1993-01-22 1994-07-27 Cca, Inc. Mechanische Schaumfeuerlöschvorrichtung und Verfahren
WO1995030452A1 (en) * 1994-05-10 1995-11-16 Ada Technologies, Inc. Apparatus and method to control deflagration of gases
CA2131109A1 (en) * 1994-08-30 1996-03-01 George P. Crampton Foam nozzle
FR2766108A1 (fr) 1997-07-17 1999-01-22 France Etat Dispositif de generation d'un fluide diphasique
WO2000012177A1 (en) * 1998-08-12 2000-03-09 Edvardsen Odd J Method for production of a fire fighting foam, nozzle head and an arrangement in a fire extinguishing installation
EP1072320A1 (de) * 1998-04-13 2001-01-31 Nauchno-Issledovatelsky Inst. Nizkikh Temperatur pri MAI(Mosk. Gosudarstvennom Aviatsionnom Inst.-Tekhnicheskom Univers.) Vorrichtung zur aerosolerzeugung und ventil
WO2002076624A1 (en) * 2001-03-22 2002-10-03 Dushkin Andrey L Liquid sprayers
WO2003041805A2 (en) * 2001-11-15 2003-05-22 National Research Council Of Canada Rotary foam nozzle
EP1629899A1 (de) * 2004-08-23 2006-03-01 Delphi Technologies, Inc. Auswechselbarer Düseneinsatz für eine kinetische Sprühdüse

Family Cites Families (36)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1484684A (en) * 1922-09-18 1924-02-26 William C Todd Water sprinkler
US2175160A (en) * 1935-07-02 1939-10-03 Linde Air Prod Co Nozzle for cutting blowpipes
US2583726A (en) * 1948-01-26 1952-01-29 Chalom Joseph Aaron Nozzle
US2678845A (en) * 1952-05-29 1954-05-18 Emil H Fitter Automatically adjustable hydraulic mechanism
US2970771A (en) * 1956-11-09 1961-02-07 Dancing Waters Inc Nozzle arrangement for fountain displays
US3302882A (en) * 1964-07-01 1967-02-07 Leland H Hutton Oxygen alnce construction
US3430939A (en) * 1965-04-02 1969-03-04 Berry Metal Co Oxygen injection nozzle with externally projecting conduits
US3428131A (en) * 1966-08-16 1969-02-18 Bliss Co Method and apparatus for generating fire-fighting foam
US3743814A (en) * 1970-12-18 1973-07-03 G Oakes Oxygen lance
US4052005A (en) * 1976-03-11 1977-10-04 Berry Metal Company Oxygen lance nozzle
US4301969A (en) * 1980-02-25 1981-11-24 Sharp Kenneth C Oxygen lance nozzle
DE3412319C1 (de) * 1984-04-03 1985-06-27 Woma-Apparatebau Wolfgang Maasberg & Co Gmbh, 4100 Duisburg Als hydraulische Wirbelstrahlduese ausgebildetes Arbeitswerkzeug
US4815665A (en) * 1984-04-19 1989-03-28 Spraying Systems Air assisted nozzle with deflector discharge means
GB8724973D0 (en) * 1987-10-24 1987-11-25 Bp Oil Ltd Fire fighting
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
AT389710B (de) * 1988-04-25 1990-01-25 Voest Alpine Ind Anlagen Blaslanze
US5169069A (en) * 1989-02-21 1992-12-08 Sybron Chemicals, Inc. Fluid driven tank cleaning apparatus
US5706842A (en) * 1995-03-29 1998-01-13 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Balanced rotating spray tank and pipe cleaning and cleanliness verification system
AT406234B (de) * 1996-02-02 2000-03-27 Voest Alpine Ind Anlagen Verfahren zum entzundern eines werkstückes
US6991362B1 (en) * 1998-04-02 2006-01-31 Seaman Anthony E Agitators for wave-making or mixing as for tanks, and pumps and filters
US6599464B1 (en) * 1999-10-06 2003-07-29 Bernd Feldhaus Steelmaking lance with integral temperature probe
US6315221B1 (en) * 1999-12-22 2001-11-13 Visteon Global Tech., Inc. Nozzle
US6988676B2 (en) * 2000-03-14 2006-01-24 Crane Pumps & Systems, Inc. Turbine drive rotary spray cleaner
US6241164B1 (en) * 2000-08-31 2001-06-05 The United States Of America As Represented By The Secretary Of The Navy Effervescent liquid fine mist apparatus and method
JP2002336370A (ja) * 2001-05-16 2002-11-26 Yamato Protec Co 微細水噴射ノズルヘッダー
CA2468209C (en) * 2001-12-11 2012-03-27 Nivis Gmbh-Srl Snow making apparatus and method for operating the same
US7311004B2 (en) * 2003-03-10 2007-12-25 Capstan Ag Systems, Inc. Flow control and operation monitoring system for individual spray nozzles
US20050011652A1 (en) * 2003-07-17 2005-01-20 Jinsong Hua Spray head and nozzle arrangement for fire suppression
US20060027679A1 (en) * 2004-08-03 2006-02-09 Mr. Jack Gratteau Ejector Nozzle
US7131598B2 (en) * 2004-10-04 2006-11-07 Ratnik Industries, Inc. Snow-gun
EP1830964B1 (de) * 2004-12-30 2015-10-14 Tempress Technologies, Inc. Überdruckturbinenrotor mit schwebekopf und verbesserter düsenqualität
BRPI0612215A2 (pt) * 2005-03-31 2016-09-06 William Henry Richards dispositivo e lanceta portátil de dispersão e aeração para sistemas de espuma de ar comprimido e sistemas para liberação de nutrientes a uma planta
EP1728535B1 (de) * 2005-05-26 2010-09-29 Kidde IP Holdings Limited Löschen von Bränden und Unterdrückung von Explosionen
US7494071B2 (en) * 2006-04-25 2009-02-24 Shamrock Research & Development, Inc. Energy efficient water sprinkler
US7878419B2 (en) * 2006-09-19 2011-02-01 Sta-Rite Industries, Llc Spray head with covers
US8133328B2 (en) * 2008-09-03 2012-03-13 Gamajet Cleaning Systems Inc. Rotary apparatus and method for cleaning liquid storage tanks

Patent Citations (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2548052A1 (fr) 1983-06-28 1985-01-04 Cebal Tete pour production de mousse avec de l'air et du liquide
WO1990005000A1 (en) * 1988-10-31 1990-05-17 Dale Gordon Jones Devices and method for cleaning gases
EP0608140A2 (de) * 1993-01-22 1994-07-27 Cca, Inc. Mechanische Schaumfeuerlöschvorrichtung und Verfahren
WO1995030452A1 (en) * 1994-05-10 1995-11-16 Ada Technologies, Inc. Apparatus and method to control deflagration of gases
CA2131109A1 (en) * 1994-08-30 1996-03-01 George P. Crampton Foam nozzle
FR2766108A1 (fr) 1997-07-17 1999-01-22 France Etat Dispositif de generation d'un fluide diphasique
EP1072320A1 (de) * 1998-04-13 2001-01-31 Nauchno-Issledovatelsky Inst. Nizkikh Temperatur pri MAI(Mosk. Gosudarstvennom Aviatsionnom Inst.-Tekhnicheskom Univers.) Vorrichtung zur aerosolerzeugung und ventil
WO2000012177A1 (en) * 1998-08-12 2000-03-09 Edvardsen Odd J Method for production of a fire fighting foam, nozzle head and an arrangement in a fire extinguishing installation
WO2002076624A1 (en) * 2001-03-22 2002-10-03 Dushkin Andrey L Liquid sprayers
WO2003041805A2 (en) * 2001-11-15 2003-05-22 National Research Council Of Canada Rotary foam nozzle
EP1629899A1 (de) * 2004-08-23 2006-03-01 Delphi Technologies, Inc. Auswechselbarer Düseneinsatz für eine kinetische Sprühdüse

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2011087383A1 (en) * 2010-01-12 2011-07-21 Telesto Sp. Z.O.O. Apparatus for regulating two-phase flow and portable atomizer based on two-phase flow
CN102612387A (zh) * 2010-01-12 2012-07-25 特利斯多公司 用于调节两相流体的装置和基于两相流体的便携式雾化器
RU2534912C2 (ru) * 2010-01-12 2014-12-10 Телесто Сп. З.О.О. Устройство для регулирования двухфазного потока и переносной распылитель двухфазного потока
CN102612387B (zh) * 2010-01-12 2014-12-31 特利斯多公司 用于调节两相流体的装置和基于两相流体的便携式雾化器
US9248460B2 (en) 2010-01-12 2016-02-02 Telesto Sp. Z.O.O. Apparatus for regulating two-phase flow and portable atomizer based on two-phase flow
CN109485168A (zh) * 2019-01-08 2019-03-19 威海百克环保工程有限公司 一种射流混合曝气器
CN114602104A (zh) * 2022-03-15 2022-06-10 刘龙平 一种室内消防用可定向大范围喷淋的自动喷淋装置

Also Published As

Publication number Publication date
CA2665265A1 (en) 2008-04-10
WO2008040418A1 (fr) 2008-04-10
UA99264C2 (ru) 2012-08-10
EP2069073A1 (de) 2009-06-17
US9352340B2 (en) 2016-05-31
EP2069073B1 (de) 2016-01-13
KR101384012B1 (ko) 2014-04-09
US20100006670A1 (en) 2010-01-14
KR20090098788A (ko) 2009-09-17
CA2665265C (en) 2012-12-11

Similar Documents

Publication Publication Date Title
EP2069073B1 (de) Düse für eine zwei-phasenmischung
CA2320270C (en) Method for extinguishing fires from an aircraft and related device
EP2257704B1 (de) Vorrichtung zur reduzierung des durch ein flugzeugdüsentriebwerk erzeugten lärms mit gleich ausgerichteten flüssigkeitsdüsen
Rizk et al. Prediction of velocity coefficient and spray cone angle for simplex swirl atomizers
EP0933594B1 (de) Verfahren zum Betreiben einer Gasturbinenbrennkammer für flüssigen Kraftstoff
CA2198420C (fr) Dispositif d'injection de combustible pour statoreacteur d'aeronef
FR2987081A1 (fr) Ensemble et procede propulsifs
JP2016001078A (ja) 噴霧ノズル、噴霧ノズルを備えた燃焼装置、及びガスタービンプラント
EP3368826B1 (de) Aerodynamisches einspritzsystem für flugzeugtriebwerk mit verbesserter luft-kraftstoff-mischung
RU2007104170A (ru) Авиационный турбореактивный двигатель, снабженный устройством снижения акустического шума от реактивных сопел
Lacava et al. Design procedure and experimental evaluation of pressure-swirl atomizers
Livingston et al. Penetration and spreading of liquid jets in an external-internal compression inlet
EP0956883B1 (de) Feuerlöscheinrichtung mit einem thermochemischen Gasgenerator
da Silva Couto et al. Experimental evaluation of a low pressure-swirl atomizer applied engineering design procedure
EP2874870B1 (de) Verschleierungsverfahren und -vorrichtung sowie wasserfahrzeug mit mindestens einer solchen vorrichtung
Peretz et al. Development of a laboratory-scale system for hybrid rocket motor testing
CA1153685A (fr) Procede et dispositif de dispersion de gaz combustibles dans l'atmosphere
EP3019746A1 (de) Zweiphasige expansionsvorrichtung zur maximierung des durch eine zweiphasenströmung erzeugten bewegungsvolumens
EP4132664A1 (de) Feuerlöscheinrichtung mit feuerlöschdüse
JPH0861150A (ja) ハイブリッドロケットのための噴射装置
EP3303232A1 (de) Schallinjektionsofen
Ferreira et al. Experimental investigation of polyethylene combustion in a solid fuel ramjet
FR3061948A1 (fr) Chambre de combustion de turbomachine a haute permeabilite
RU2096625C1 (ru) Устройство для пылегазоподавления
Strokin et al. Compact Combustor Integrated (CI) with Compressor and Turbine for Perspective Turbojet Engine

Legal Events

Date Code Title Description
PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

Free format text: ORIGINAL CODE: 0009012

AK Designated contracting states

Kind code of ref document: A1

Designated state(s): AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HU IE IS IT LI LT LU LV MC NL PL PT RO SE SI SK TR

AX Request for extension of the european patent

Extension state: AL BA HR MK RS

AKX Designation fees paid
STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: THE APPLICATION IS DEEMED TO BE WITHDRAWN

18D Application deemed to be withdrawn

Effective date: 20081010

REG Reference to a national code

Ref country code: DE

Ref legal event code: 8566