DEVICE FOR GENERATING A JET OF TWO-PHASE FLUID
20230405379 ยท 2023-12-21
Inventors
Cpc classification
B05B1/32
PERFORMING OPERATIONS; TRANSPORTING
B05B7/1209
PERFORMING OPERATIONS; TRANSPORTING
B01F25/4335
PERFORMING OPERATIONS; TRANSPORTING
B05B7/0483
PERFORMING OPERATIONS; TRANSPORTING
B05B12/002
PERFORMING OPERATIONS; TRANSPORTING
B01F25/25
PERFORMING OPERATIONS; TRANSPORTING
A62C31/03
HUMAN NECESSITIES
B01F25/3141
PERFORMING OPERATIONS; TRANSPORTING
International classification
Abstract
A device for generating a jet of two-phase fluid, comprising a nozzle having a main duct that is fed with a pressurized gaseous fluid and opens into a mixing chamber, and at least one secondary duct that is fed by at least one pressurized fluid and opens into the mixing chamber in a direction forming a non-zero angle with the axis of the main duct. The mixing chamber has a convergent-divergent cylindrical wall having a constriction defining an opening in the plane perpendicular to the axis of the main duct. The convergent part of the wall has a frustoconical region in the continuation of the axis of the at least one secondary duct so as to form a fragmentation chamber for the liquid phase.
Claims
1. A device for generating a jet of two-phase fluid comprising a nozzle having a main duct supplied with a pressurized gaseous fluid and opening into a mixing chamber, as well as at least one secondary duct supplied with at least one pressurized liquid fluid opening into the mixing chamber in a direction forming a non-zero angle with the axis of the main duct, wherein: the mixing chamber has a convergent-divergent cylindrical wall having a constriction defining a disc opening in the plane perpendicular to the axis of the main duct; and the convergent part of the wall has a frustoconical region in the continuation of the axis of the at least one secondary duct so as to form a fragmentation chamber for the liquid phase.
2. The device of claim 1, wherein the axis of the at least one secondary duct forms, with the axis of the main duct, an angle of between 2 and 20.
3. The device of claim 1, wherein the axis of the at least one secondary duct defines with the generator of the cone of the convergent part, an angle of between 0 and 60.
4. The device of claim 1, wherein the diameter of the opening of the constriction is between 0.8 and 1.2 times the diameter of the main duct.
5. The device of claim 1, wherein the at least one secondary duct comprises a plurality of secondary ducts converging toward the mixing chamber, the secondary ducts of the plurality distributed at the periphery of the main duct.
6. The device of claim 1, wherein the ejection channel of the nozzle is located in the divergent part and has a truncated bullet shape.
7. The device of claim 1, wherein an ejection channel of the nozzle is extended by a deformable ejection tip.
8. The device of claim 7, wherein the deformable ejection tip comprises a deformable sleeve arranged between two movable jaws articulated between a position in which the movable jaws cause pinching of a front portion of the deformable sleeve and a spaced position in which the sleeve has a nominal section.
9. The device of claim 8, wherein the movable jaws have a ramp against which the connecting rods are supported to control tightening of front ends of the movable jaws.
10. The device of claim 1, wherein the device is integrated into a body having a fixed rear handle and a front tilting handle controlling variation of parameters of the jet.
11. The device of claim 10, wherein the body has a fitting for connecting a supply pipe of an air mask.
12. The device of claim 3, wherein the axes of the secondary ducts define, with the generator of the cone of the convergent part, an angle of 4510.
13. The device of claim 2, wherein the axes of the at least one secondary duct defines, with the generator of the cone of the convergent part, an angle of between 0 and 60
14. The device of claim 13, wherein the diameter of the opening of the constriction is between 0.8 and 1.2 times the diameter of the main duct.
15. The device of claim 14, wherein the at least one secondary duct comprises a plurality of secondary ducts converging toward the mixing chamber, the second ducts of the plurality distributed at the periphery of the main duct.
16. The device of claim 15, wherein an ejection channel of the nozzle is located in the divergent part and has a truncated bullet shape.
17. The device of claim 16, wherein an ejection channel of the nozzle is extended by a deformable ejection tip.
18. The device of claim 17, wherein the deformable ejection tip comprises a deformable sleeve arranged between two movable jaws articulated between a position in which the movable jaws cause pinching of a front portion of the deformable sleeve and a spaced position in which the sleeve has a nominal section.
19. The device of claim 18, wherein the movable jaws have a ramp against which the connecting rods are supported to control tightening of front ends of the movable jaws.
20. The device of claim 19, wherein the device is integrated into a body having a fixed rear handle and a front tilting handle controlling variation of parameters of the jet.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
[0016] The present disclosure will be better understood from reading the following description, which refers to non-limiting exemplary embodiments illustrated by the accompanying drawings, in which:
[0017]
[0018]
[0019]
[0020]
[0021]
[0022]
[0023]
[0024]
[0025]
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[0027]
[0028]
DETAILED DESCRIPTION
[0029] It is specified that the complete system comprises a nozzle, optionally being able to be extended by a variable-geometry ejection tip, with a multifunction control handle and optionally peripheral elements to form, for example, a portable equipment. The aim is to form a mist of water droplets with a section of less than 400 micrometers and preferably less than micrometers. For an extinguisher, the water mist finely divided into droplets constitutes a two-phase extinguishing agent produced in situ at the nozzle.
[0030] The action of the water mist is based on several mechanisms, often combined: [0031] a) Cooling the flame resulting from the large exchange surface area and the high vaporization speed. Water is a very good thermal trap. Raising a kilogram of liquid water from 20 C. to 100 C. requires 335 kJ/kg and its vaporization additionally requires 2257 kJ/kg, which is a total of 2592 kJ/kg. The fineness of the droplets of the water mist involves a significant exchange surface making it possible to exploit its potential of evaporation and absorption of calories. By evaporating, the droplets, in contact with the hot zones (vicinity of the flame) generate a vapor volume, which contributes to depleting the oxygen concentration locally. Cooling the flame contributes to its extinguishing. It should also be noted that cooling a smoke cloud can prevent it from igniting when it comes in contact with fresh air (flashover). [0032] b) Cooling solid fuels (materials): The water-solid contact (materials) is limited by the surface of the fire fuel (material). The fineness of the water mist is not essential but can be used to limit thermal shocks. In contrast, efficient cooling requires sufficient water flow and a good liquid-solid overlap. If, for example, it is desired to optimize the cooling of a hot atmosphere, a very fine water mist is preferable. On the other hand, if the cooling of a solid fuel is desired to be maximized, a water mist comprising a greater proportion of large droplets will give better results. [0033] c) Decreasing the overall or local oxygen concentration: Depleting the oxygen content in two cases: [0034] Near the seat of the fire, the water droplets are turned into steam, which contributes to locally reducing the oxygen concentration. [0035] In the rooms, the formation of water vapor comparable to an inert gas contributes mechanically to lowering the oxygen concentration in the air of the enclosed premises. For a large amount of focus in a small volume, the water mist can vaporize and the action of the vapor produces a smothering effect that can lead to extinguishing. A sufficient ambient minimum temperature (65 C.-75 C.) is necessary to observe this effect related to water vapor because, for a volume saturated with water (caused by the mist), the proportion of water in vapor form by volume is limited by the saturated vapor pressure of water in the air. [0036] d) Mitigating thermal radiation: Influence of the propagation energy. Like conduction and convection, thermal radiation is a heat transfer mode. It contributes to the propagation of a fire. A suitably sized water mist can significantly reduce thermal radiation. The preponderant mechanisms in the mitigation are absorption, reflection and diffraction. The main parameters involved in the effectiveness of the mitigation are: [0037] The density of the water mist [0038] The thickness of the water mist screen [0039] The class of the water mist [0040] The homogeneity of the distribution of the water mist
[0041] An overall mitigation rate of 50% can be easily achieved.
[0042] The description of one of these items naturally extends to subassemblies including this element combined with another element, even if the first element is not repeated in detail in the part regarding the detailed description of that other element. The non-repeated characteristics must be considered included in the detailed description, except for features that would be clearly technically impossible. Likewise, each of the elements can be used with a complementary element other than that described or even subject of the present patent, the nozzle that is the subject matter of the patent can be extended by a tip other than that proposed by the present patent, and likewise the described tip can be used with nozzles other than those of the present patent. The same applies to all elements in a detailed description.
[0043]
[0044] The nozzle is composed, in the non-limiting example described, of several parts connected by screwing or any other mechanical connection with sealing gaskets: a connection plate (100), a control body (200), an intermediate body (300) and a mixing chamber (400).
[0045] The nozzle is crossed by an axial main channel (1) opening into the coaxial mixing chamber (400). The main channel (1) extends from an eccentric threaded fitting (101) to a ring or secondary duct (301) opening into the mixing chamber (400). It passes through a plug valve (201) for controlling the gas flow rate provided with a spherical body (202) actuated by a rod not visible in
[0046] The main channel (1) is intended to supply the gas phase, for example, compressed air, or a neutral gas such as nitrogen. For a particular application, the compressed gas is air, serving both to produce the mist and secondarily to supply a respiratory mask intended for a human operator.
[0047] The connection plate (100) has a second threaded fitting (151) for connecting a supply pipe with the liquid phase, for example, pressurized water. It opens into the control body (200) by a duct placed in a plane not visible in
[0048] The outlet of this second plug valve (251) opens into a radial duct (270) opening into an annular chamber (260) coaxial with the main channel (1). Optionally, this radial duct (270) also opens onto the outer wall of the control body (200) by a threaded fitting (271) allowing the connection of a supply pipe for a secondary fluid. When not in use, this threaded fitting (271) is hermetically sealed by a screw cap (272).
[0049] The intermediate body (300) provides transmission of the two fluids from the control body (200) to the mixing chamber (400). It comprises the main channel (1), arranged along the longitudinal axis of the intermediate body (300) and the mixing chamber (400), and one or more secondary ducts (301, 302), typically a bundle of secondary ducts extending from the annular chamber (260) to the inlet of the mixing chamber (400). These secondary ducts (301, 302) are oriented along axes (311, 312) forming, relative to the longitudinal axis (10), an angle of approximately 10, typically between 8 and 15. The main channel (1) of air and the secondary pipe(s) (301, 302) of liquid open into the same transverse plane (306), perpendicular to the axis of the main channel (1) of air, in a hollow space located in the convergent part (410) of the mixing chamber.
[0050] The axes (311, 312) defining with the generator (413) of the cone of the convergent part (410) an angle of approximately 30.
[0051] Other configurations may be provided, for example, a conical chamber extending from the annular chamber (260) to an annular outlet in the inlet of the mixing chamber (400). This conical chamber can be longitudinally partitioned to ensure the rigidity of the peripheral walls.
[0052] The mixing chamber (400) forms a tip called a de Laval nozzle. It is formed by a rectilinear duct having a variable section, consisting of a convergent part (410) extended by a divergent part (420) with a constriction (430) between these two parts (410, 420). The tubular volume passing longitudinally through the chamber is completely free and devoid of any obstacle and member capable of restricting the flow of the mixed fluid.
[0053] The convergent part (410) is configured such that an annular zone (411) is in the continuation of the axes (311, 312) of the secondary ducts respectively (301 to 305), without any obstacle or wall between the opening of the secondary ducts (301 to 305) and the wall of this convergent annular zone (411). The frustoconical volume defined by the convergent part (410) is devoid of any obstacle in order to form a hollow volume, into which there opens at the upstream base defined by the transverse plane (306) the main air supply channel (1) and the secondary liquid ducts (301 to 305) which are oriented at a non-zero angle relative to the axis of the main air supply channel (1) such that the open water jet of these secondary liquid ducts (301 to 305) is oriented directly toward the surface of the convergent part (410) of the mixing chamber, upstream of the narrowed part.
[0054] This configuration is essential for the liquid jet to break against the surface of the convergent part (410) and to atomize the liquid drop flow projected into the central vein in the jet of the gas phase and to create turbulence in the convergent part (410) before being driven by the central vein through the constriction (430) in the divergent part (420) of the tip, called a de Laval nozzle configuration. This divergent part (420), also of a flared frustoconical shape, is completely hollow and devoid of any obstacle or part that could totally or partially obstruct the vein passing through the convergent-divergent mixing chamber.
[0055] This convergent-divergent mixing chamber directly opens into a deformable tip connected in a sealed manner, without any passage of air coming from outside the nozzle.
[0056] Detailed Description of a Deformable Tip
[0057]
[0058] This deformable nozzle device constitutes a complement to the nozzle described above. However, it could also adapt to other solutions of two-phase mixing generators under pressure, in particular, to solutions already marketed or known from the prior art.
[0059]
[0060] At its outlet, the sleeve (500) forms a variable configuration between a circular shape and a flattened shape where it has a slot (501) of small height delimited by the edges of the sleeve forming two transverse lips. The front end of the sleeve (500) matches the inner shape of the movable jaws (530, 540).
[0061] The front portions of the fixed jaws (510, 520) have series of striations (512, 522) oriented in parallel transverse planes. These striations (512, 522) are sandwiched between complementary ridges (532, 542) oriented in parallel transverse planes, provided at the front portion of the movable jaws (530, 540), to provide guidance upon angular displacement of the movable jaws (530, 540) to change the configuration of the sleeve (500).
[0062] The jet composed of the gas and liquid mixture has different fluidic characteristics depending on whether the sleeve is pinched (movable jaws (530, 540) closed) or in the open position (movable jaws (530, 540) spaced apart.
[0063] The droplet size is finer and the opening cone angle of the jet is more open when the outlet is pinched.
[0064] The geometric configuration in the open or pinched position is not limited to a circular or pinched shape, but may take other forms.
[0065] The sleeve (500) shown in
[0066] The front portion (501) of the sleeve (500) has two diametrically opposed protuberances (504, 505). They allow an anchoring of the front portion (501) in complementary cavities (535, 545) provided at the front inner surface of the two movable jaws (530, 540).
[0067] The rear portion of the movable jaws (530, 540) has inclined ramps (536, 546) against which the ends of the control pistons (531 541) press to control the tilting of the movable jaws (530, 540).
[0068]
[0069] The rigid base (550) has two diametrically opposed notches (551, 552) to allow the passage of the control pistons (531; 541), which have the form of connecting rods.
[0070] The assembly between the rigid base (550) and the movable jaws (530, 540) is achieved by transverse axes (537, 547).
[0071] Multi-Functional Control Handle
[0072]
[0073] The diffusion assembly includes a main body (700) wherein the two-phase jet production nozzle is enclosed, for example, a nozzle according to the present disclosure. This body (700) has at its rear part a base (701) for connecting a supply pipe (600) fitting (601). At the front, the body (700) is extended by a secondary body (702) enclosing the jet-shaping tip, for example, the deformable tip previously described. This secondary body (702) has a front plate (708) cut by an outlet orifice (710).
[0074] The body (700) is provided with a fixed handle (703) for directing and holding the body (700) in the direction of the fire to be extinguished. It has a side button (709) for controlling an electrical function, for example, the use of the pressurized air production turbine or the opening of a pressurized oxygen supply valve.
[0075] The body (700) has a connector (704) allowing the connection of an oxygen or breathable air supply pipe of a protective mask carried by the operator in order to allow that person to continue their work in a fouled or smoke-filled environment.
[0076] The body (700) and/or the secondary body (702) further includes rails (706, 707) for attaching accessories, for example, a flashlight or a camera.
[0077] Finally, the body (700) comprises a tilting handle (705) actuating a transmission member controlling the configuration of the outlet jet. In the case of a deformable tip according to the present disclosure described above, the transmission member is constituted by the two control pistons (531, 541) actuated by cams driven by the tilting handle (705). Pivots (715) provide the articulated connection between the tilting handle (705) and the body (700).
[0078] This multifunction handle allows the operator to progress toward the fire and to act on the different parameters of the two-phase jet in a very intuitive manner. The operation of this handle is illustrated by
[0079] The mechanism comprises a cam (720) articulated in rotation relative to an eccentric transverse pivot (721). The outer face (722) of the cam (720) pushes the piston (730) against which the control pistons (531, 541) bear in order to control the tightening of the front end of the movable jaws (530, 540), or loosening by releasing the handle.
[0080] The pivoting of the cam (720) thus serves to position the nozzle shape via the movable jaws (530, 540) of the deformable nozzle, with a synchronization of the opening(s) of the gas and/or liquid channels.
[0081] The valves are controlled via the cam track (740) (for example, the left-hand side pilots the gas and the other side pilots the water. The whole is actuated by the handle (705), therefore no adjustment is necessary. All the opening/closing/flow rate and jet-shaping sequences are programmed by the different positions of the handle (705).