EP0604741B1 - Buse à tourbillonnement pour pulvériser un liquide - Google Patents

Buse à tourbillonnement pour pulvériser un liquide Download PDF

Info

Publication number
EP0604741B1
EP0604741B1 EP93118034A EP93118034A EP0604741B1 EP 0604741 B1 EP0604741 B1 EP 0604741B1 EP 93118034 A EP93118034 A EP 93118034A EP 93118034 A EP93118034 A EP 93118034A EP 0604741 B1 EP0604741 B1 EP 0604741B1
Authority
EP
European Patent Office
Prior art keywords
whirl
nozzle
swirl
central axis
nozzle outlet
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.)
Expired - Lifetime
Application number
EP93118034A
Other languages
German (de)
English (en)
Other versions
EP0604741A2 (fr
EP0604741A3 (fr
Inventor
Zoltan Farago
Tom Schork
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.)
Deutsches Zentrum fuer Luft und Raumfahrt eV
Original Assignee
Deutsches Zentrum fuer Luft und Raumfahrt eV
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 Deutsches Zentrum fuer Luft und Raumfahrt eV filed Critical Deutsches Zentrum fuer Luft und Raumfahrt eV
Publication of EP0604741A2 publication Critical patent/EP0604741A2/fr
Publication of EP0604741A3 publication Critical patent/EP0604741A3/fr
Application granted granted Critical
Publication of EP0604741B1 publication Critical patent/EP0604741B1/fr
Anticipated expiration legal-status Critical
Expired - Lifetime 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
    • B05B1/00Nozzles, spray heads or other outlets, with or without auxiliary devices such as valves, heating means
    • B05B1/34Nozzles, spray heads or other outlets, with or without auxiliary devices such as valves, heating means designed to influence the nature of flow of the liquid or other fluent material, e.g. to produce swirl
    • B05B1/3405Nozzles, spray heads or other outlets, with or without auxiliary devices such as valves, heating means designed to influence the nature of flow of the liquid or other fluent material, e.g. to produce swirl to produce swirl
    • B05B1/341Nozzles, spray heads or other outlets, with or without auxiliary devices such as valves, heating means designed to influence the nature of flow of the liquid or other fluent material, e.g. to produce swirl to produce swirl before discharging the liquid or other fluent material, e.g. in a swirl chamber upstream the spray outlet
    • B05B1/3478Nozzles, spray heads or other outlets, with or without auxiliary devices such as valves, heating means designed to influence the nature of flow of the liquid or other fluent material, e.g. to produce swirl to produce swirl before discharging the liquid or other fluent material, e.g. in a swirl chamber upstream the spray outlet the liquid flowing at least two different courses before reaching the swirl chamber
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B05SPRAYING OR ATOMISING IN GENERAL; APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
    • B05BSPRAYING APPARATUS; ATOMISING APPARATUS; NOZZLES
    • B05B1/00Nozzles, spray heads or other outlets, with or without auxiliary devices such as valves, heating means
    • B05B1/34Nozzles, spray heads or other outlets, with or without auxiliary devices such as valves, heating means designed to influence the nature of flow of the liquid or other fluent material, e.g. to produce swirl
    • B05B1/3405Nozzles, spray heads or other outlets, with or without auxiliary devices such as valves, heating means designed to influence the nature of flow of the liquid or other fluent material, e.g. to produce swirl to produce swirl
    • B05B1/341Nozzles, spray heads or other outlets, with or without auxiliary devices such as valves, heating means designed to influence the nature of flow of the liquid or other fluent material, e.g. to produce swirl to produce swirl before discharging the liquid or other fluent material, e.g. in a swirl chamber upstream the spray outlet
    • B05B1/3421Nozzles, spray heads or other outlets, with or without auxiliary devices such as valves, heating means designed to influence the nature of flow of the liquid or other fluent material, e.g. to produce swirl to produce swirl before discharging the liquid or other fluent material, e.g. in a swirl chamber upstream the spray outlet with channels emerging substantially tangentially in the swirl chamber
    • B05B1/3431Nozzles, spray heads or other outlets, with or without auxiliary devices such as valves, heating means designed to influence the nature of flow of the liquid or other fluent material, e.g. to produce swirl to produce swirl before discharging the liquid or other fluent material, e.g. in a swirl chamber upstream the spray outlet with channels emerging substantially tangentially in the swirl chamber the channels being formed at the interface of cooperating elements, e.g. by means of grooves
    • B05B1/3442Nozzles, spray heads or other outlets, with or without auxiliary devices such as valves, heating means designed to influence the nature of flow of the liquid or other fluent material, e.g. to produce swirl to produce swirl before discharging the liquid or other fluent material, e.g. in a swirl chamber upstream the spray outlet with channels emerging substantially tangentially in the swirl chamber the channels being formed at the interface of cooperating elements, e.g. by means of grooves the interface being a cone having the same axis as the outlet

Definitions

  • the invention relates to a swirl nozzle for atomizing a Liquid with a spread over a swirl chamber floor uplifting and opposite to the swirl chamber floor Swirl chamber tapering towards the nozzle outlet opening at least one opposite a central axis of the swirl chamber laterally offset into this swirl channel, with a Swirl parameters of> 1, with a different from the swirl chamber floor uplifting and the formation of an air core in one displacement body preventing swirl chamber at the bottom, which is arranged concentrically to the central axis and has an outer diameter in the bottom part, the at least one diameter of the nozzle outlet opening corresponds.
  • the one to be atomized flows Liquid through the swirl channel preferably in tangential direction in the swirl chamber in which it itself in the direction of the central axis of the swirl chamber with enlargement their peripheral speed moves. Since the Liquid with a swirl parameter of the swirl nozzle of> 1 due to the centrifugal forces not to the central axis can flow around the central axis air core extending the entire height of the swirl chamber which the liquid flows around and thus as rotating Liquid film ring passes through the nozzle outlet opening and then forms a liquid film cone that due to its own instability in small droplets of liquid disintegrates.
  • a swirl nozzle of the type mentioned is in FR-A-1 560 603. This also shows a swirl nozzle, at which with a high probability the swirl parameters> 1 and which is also a conical displacement body having.
  • a twist parameter ⁇ 0.5 was determined in GB-A-162 172 and in DE-A-175 561 it can be assumed that none at all Air core is present. It also follows from this Documentation that the cone body serves the opening angle of the spray cone to change what is against displacement of an air core speaks. For the rest, became a swirl parameter of approximately 0.4.
  • the invention is therefore based on the object To improve swirl nozzle of the generic type in such a way that this increases the input swirl pulse allows constant or lower swirl losses.
  • the height of the swirl chamber and thus the length of the air core keep it as low as possible that the swirl chamber wall has a conical surface with the largest possible cone angle, which, however, has a poor positive fit of the Partially would result, so that the wall surfaces of the recess which is the truncated cone seat for the truncated cone trained inner part form a smaller cone angle has as an adjoining the nozzle outlet opening Part of the swirl chamber wall.
  • the swirl nozzle according to the invention has it as Proven useful if the displacer is a cone with one that adjoins the nozzle outlet opening Partial range is corresponding cone angle.
  • the displacement body with at least the diameter of the nozzle outlet openings corresponding average diameter over at least about two thirds of the height of the swirl chamber extends.
  • a width of the annular portion of an extension the mouth opening from an outer edge of this Area in the radial direction corresponds to the inside means that this annular area is only as wide is chosen that this the mouth of the swirl channel can record.
  • the swirl channel in the mouth area with its center line essentially tangential to the swirl chamber wall runs.
  • a particularly large swirl channel eccentricity can be achieved, however, if the swirl channel with a mouth opening designed as a segment of a circle along an outer edge region of the swirl chamber floor opens into the swirl chamber, since in this case the radial extension of the mouth opening in the direction of the central axis is only a width of the swirl channel corresponds and the liquid jet when entering the swirl chamber thus flows along the swirl chamber wall and with a given swirl chamber diameter in greatest possible distance from the central axis into the swirl chamber flows in.
  • the swirl nozzle it is expedient when the swirl duct is straightened from a pressure chamber runs to the swirl chamber.
  • the swirl channel is spiraling with respect to the Central axis runs from a pressure chamber to the swirl chamber, because in this case the swirl channel with respect to the central axis can be provided with a lower slope and thus based on a constant flow rate the liquid in this swirl channel the one from this escaping liquid jet as large as possible Tangential velocity component in one plane perpendicular to the central axis and as small as possible Speed component parallel to the central axis having.
  • the swirl channels are preferably one have a substantially constant cross section.
  • the provision of the displacement body according to the invention has the advantage that the swirl chamber in the bottom area the shape of an annular space encircling the displacement body has so that there is no air core in this area can train who to those already described Twist loss leads.
  • the swirl channel eccentricity chosen larger without increasing the overall twist losses, so that a good atomization quality of the invention Swirl nozzles can be reached. It is even possible that Swirl channel eccentricity increase so far that the tangential velocity of the liquid jet less and thus a larger cross section of the swirl channels can be, so that the risk of clogging of the nozzle decreased.
  • the present invention offers Solution the possibility of the return hole to be arranged eccentrically to the displacement body.
  • the return bore in a distance from the central axis of the sinker is arranged, which is at least a radius of the nozzle outlet opening corresponds, so that a possibly in Area of residual air arising in the outlet opening does not stand above the return hole and thus influences it.
  • the return holes are arranged at a distance from the central axis, which is smaller than the distance of the mouth opening of the swirl channels.
  • a swirl nozzle for atomizing a liquid like it from is known in the art, shown in Fig. 1 and 2 shows an outer body 10, starting from the outer side 12 thereof there is a nozzle outlet opening designed as a cylindrical bore 13 into an interior of the outer body 10 extends.
  • This nozzle outlet opening 14 adjoins an essentially conical recess 16 at whose wall surfaces 18 the lateral surfaces of a coaxial to Nozzle outlet opening 14 arranged and to a central axis 20 form a rotationally symmetrical truncated cone.
  • an inner body 22 is used, which has a circular cylindrical region 24 which is followed by a frustoconical region 26 whose base area 28 is identical to the circular area.
  • This frustoconical region 26 is formed such that Are lateral surfaces 30 of the same section of the cone shell, on which the wall surfaces 18 of the recess 16 also lie.
  • the inner body 22 is form-fitting through a conical seat held in the recess 16, the area of the wall surfaces 18 of the recess 16, in which the lateral surfaces 30 of the frustoconical Area 26 of the inner body 22 abut as Tapered seats 32 of the recess 16 are designated.
  • Area 26 of the inner body 22 extends perpendicularly to the central axis 20 and forms a swirl chamber floor 34.
  • An area lying above this swirl chamber floor 34 the recess 16 is referred to as a swirl chamber 36, the wall surfaces 18 delimiting the swirl chamber 36 the recess 16 referred to as swirl chamber walls 38 are.
  • One enclosed by the recess 16 and on one of the swirl chamber 36 opposite side of the The inner body 22 is arranged as the pressure space 40 referred to, in which the intended for atomization Liquid is kept under pressure. From this pressure room 40 lead several swirl channels 42 into the swirl chamber 36, these swirl channels 42, such as in particular Fig.
  • notches in the lateral surfaces 30 are formed, which in the pressure chamber 40 with a rectangular and approximately square Cross section in the circular cylindrical region 24 of the inner body 22 open and in the swirl chamber 36 in the area of the swirl chamber base 34 and preferably in one area lying radially outside with respect to the central axis 20 open, with a centerline 44 of each swirl channel 42, at least in the area of an opening 46 the same, in the swirl chamber base 34 a distance e of the central axis 20 and thus from the mouth opening 46 a liquid jet 48 emerges, which when leaving the mouth opening 46 in a to the central axis 20 parallel and at a distance e from this Level 50 is a speed component 52 has parallel to the swirl chamber floor 34 and a speed component 54 parallel to Central axis 20.
  • the distance e is commonly called eccentricity e of the swirl nozzle.
  • a definition of the swirl parameter can also be found in the research report DFVLR-FB 87-25 (ISSN 0171-1342), page 22.
  • an air core always occurs with a swirl nozzle if the swirl parameter So> 1.
  • the occurrence of an air core can also be made dependent on the ratio of the sum of all swirl channel areas f 1 , f 2 , f 3 , f 4 to the cross-sectional area of the nozzle outlet opening, which should be less than 5 for this purpose.
  • a known Swirl nozzle shows a first embodiment of an inventive Swirl nozzle, shown in FIGS. 3 to 5, the same parts and features, thus in Figs. 3 to 5 are also provided with the same reference numerals.
  • the entire displacement body 62 is rotationally symmetrical to the central axis 20, the cylindrical base 64 with respect to the radial direction the central axis 20 to the mouth openings 46 of the swirl channels 42 extends outwards, so that the displacement body 62 the swirl chamber floor 34 in his central area 72 covered and a cylindrical Outer surface 74 of the cylindrical base 64 a subject to change annular region 76 of the swirl chamber base 34 limited internally.
  • cylindrical outer surface 74 form the cylindrical Base and a swirl chamber bottom opposite this arranged section of the swirl chamber wall 38 and the circular area of the swirl chamber base 34 an annular space 80, in which the liquid jet 48 tangential to the outer surface 74 of the cylindrical Base 64 is injected.
  • a surface 82 designed as a conical surface the conical tip 66 extends as in FIG. 3 shown, preferably at a distance b from one outlet-side section 84 of swirl chamber wall 38 and parallel to this, preferably the width b corresponds approximately to a width b of the swirl channels 42.
  • the swirl chamber 36 includes in the first embodiment the swirl nozzle according to the invention Annulus 80 arranged on the swirl chamber bottom which one of the conical surface 82 of the displacement body 62 and the outlet side Section 84 of the swirl chamber wall of limited cone-shaped Connects room 86, which in turn is in the cylindrical bore of the nozzle outlet opening 14 transforms.
  • FIGS. 6 and 7 A second embodiment of an inventive Swirl nozzle, shown in FIGS. 6 and 7, is so far than with the first embodiment of FIG. 3 to 5 is identical, provided with the same reference numerals, so that regarding the description of the corresponding Parts referred to the above statements becomes.
  • the Displacer 62 no longer a conical tip, but one sitting on the cylindrical base 64 Truncated cone 88 with a base 68 opposite it and parallel to the swirl chamber floor 34 Front surface 90, which lies in the swirl chamber 36 and has a diameter larger than a diameter of the nozzle outlet opening 14.
  • the displacement body in this embodiment 62 not over the entire height of the swirl chamber from the swirl chamber floor 34 to a transition 92 of the swirl chamber walls 38 into the nozzle outlet opening 14, but ends with the front surface 90 in Distance from this.
  • Swirl nozzle shown in Figs. 8 and 9, are insofar as the same parts as those described above Embodiments are available, the same Reference numerals are used so that the above Description can be referenced.
  • the swirl channels 42 are not notches with a straight center line 44 more, but run although along the lateral surfaces 30 of the inner body 22 as Straight, but show one designed as a circular ring segment 94 Mouth opening 46, which is therefore the possibility offers the annular region 76 of the Swirl body bottom 34 to the width b of the swirl channel 42 to reduce, so that the distance e from the mouth 46 emerging beam 48 from the central axis 20 almost with an outer radius of the swirl chamber base 34 is identical.
  • the displacement body 62 can thus only be in the form of a cone Tip 66 be formed, the base 68 of the conical tip 66 with respect to the central axis 20 has a radial extension that is up to an inner edge 96 of the circular ring segment Mouth openings 46 of the swirl channels 42 are sufficient.
  • Swirl chamber reduced to the cone-shaped space 86, which is between the conical surface 82 of the displacement body 62 and the swirl chamber wall 38 lies.
  • FIGS. 10 and 11 show insofar as the same reference numerals are used, the same parts as the above-described embodiments.
  • the fourth embodiment differs in that the wall surfaces of the recess 16 have two different partial areas 98 and 100, which is located directly at the nozzle outlet opening 14 adjoining partial area 98 of a truncated cone surface whose cone angle is greater than that of a truncated cone lateral surface of the Subarea 98 adjoining subarea 100, wherein the truncated cone surface of the portion 98 along a line of contact 102 in the truncated cone surface of section 100 passes over.
  • the conical seat surface becomes part 100 32 formed on which the inner body 22 with its Shell surfaces 30 abuts.
  • This inner body 22 is with regard to the formation of the swirl channels 42 and their Mouth openings 46 with the inner body 22 of the third Embodiment identical.
  • runs the conical surface 82 is now parallel to the partial area 98 at a distance b, which is approximately corresponds to the width of the swirl channels 42.
  • annular region 76 of the swirl chamber base 34 can be kept in the width of the swirl channel 42 can and also the conical surface 82 of the displacer 62 in one of the width of the Swirl channels 42 corresponding distance b from the partial area 98 can extend advantageously extends the partial area 100 over the conical seat surface 32 towards the nozzle outlet opening 14 to the line of contact 102 so that the swirl chamber 36 in the fourth embodiment, an annular space 104, formed by the cone seat surface 32 out to the contact line 102 extending portion 100, the annular region 76 and one Part of the surface 82 of the displacer 62 and the cone-shaped space 86 limited through section 98 and the rest of the Surface 82 of the displacer 62 comprises.
  • a fifth embodiment of the invention Swirl nozzle shown in FIGS. 12 and 13, is largely identical to the fourth embodiment, so that the same parts with the same reference numerals are provided.
  • the swirl channels 42 run from the pressure chamber 40 to the swirl chamber 36 in the area of Shell surface 30 of the inner body 22 spirally with respect the central axis 20 so that these swirl channels 42, based on the central axis 20, a smaller slope have than the swirl channels 42 in the fourth embodiment.
  • An exemplary embodiment is additionally a return bore 104 provided, which is concentric to the central axis 20 is arranged and in the swirl chamber 36 of the Nozzle outlet opening 14 opposite in the area of the displacer 62 opens.
  • the sinker 62 is no longer a cone, but only a truncated cone, the front surface of which is now covered by a Mouth opening 106 of the return bore 104 is formed.
  • This return bore 104 thus extends through the entire displacement body 62 and also through the inner body 22 through and is with a usual return flow path connected, which for example in the German Patent application P 37 03 075.2 is described.
  • a sixth embodiment shown in the 14 to 16 shows a variant of the first embodiment, shown in Figs. 3 to 5, so far used as the same parts, they are also the same Provide reference numerals so that with regard to their Description on the explanations of the first embodiment can be referred.
  • This sixth embodiment shows in contrast to first embodiment in the conical surface 82 of the conical tip 66 incorporated return holes 110, which is perpendicular to the conical Surface 82 standing longitudinal axes 112 in the displacement body 62 penetrate towards its central axis 20, being arranged in a coaxial to the central axis Return channel 114 open, which of the conical Tip 66 of the sinker in opposite Direction leads to an interior of the nozzle.
  • the return bores 110 are not in the Area of the nozzle outlet opening 14 arranged, but in one of the exit-side section 84 of the swirl chamber wall 38 overlapped so that the return bore 110th not in the area of one in the nozzle outlet opening 14 emerging air core.
  • a fifth embodiment of the invention Swirl nozzle shown in Figs. 17 and 18 has similarities with the second embodiment so that the same Parts are also provided with the same reference numerals.
  • the mouth openings 46 form a ring segment cutout 120 expanded, the width of the width of the annular swirl chamber bottom 34 between the frustoconical Displacement body 62 and the swirl chamber walls 38 corresponds.
  • the displacement body 62 without the cylindrical Approach as a truncated cone 88 directly from the swirl chamber floor 34 and extends to the front surface 90, which is approximately the diameter of the nozzle outlet bore 14 corresponding diameter.
  • Particularly advantageous in the seventh embodiment is the fact that this is easy to manufacture and that the cross-sectional area of the orifices 46 is large is what leads to relatively low viscosity-related pressure drops leads.

Landscapes

  • Nozzles (AREA)

Claims (12)

  1. Buse à tourbillonnement pour pulvériser un liquide, comportant une chambre de buse (36), qui s'élève au-dessus d'un fond (34) de la chambre de buse et se rétrécit en direction d'une ouverture (14) de sortie de la buse, qui est située à l'opposé du fond (34) de la chambre de buse, au moins un canal à tourbillonnement qui débouche dans la chambre à tourbillonnement (36) en en étant décalé latéralement par rapport à un axe médian de la chambre à tourbillonnement, avec un paramètre de tourbillonnement > 1, un corps de refoulement (62), qui s'élève à partir du fond (34) de la chambre à tourbillonnement et empêche la formation d'un noyau d'air (58) dans une zone de la chambre à tourbillonnement, située du côté du fond, et qui est disposée concentriquement par rapport à l'axe médian (20) et possède, dans la partie située du côté du fond, un diamètre extérieur, qui correspond au moins à un diamètre de l'ouverture (14) de sortie de la buse, et dans lequel la buse à tourbillonnement possède un corps extérieur (10), qui entoure l'ouverture (14) de sortie de la buse et un évidement (16), qui se raccorde à ladite ouverture, s'étend le long de l'axe médian (20) et possède une section transversale qui augmente dans la direction croissante d'extension, et un corps intérieur (22) peut être inséré selon une liaison par formes complémentaires dans cet évidement (16), le fond (34) de la chambre à tourbillonnement étant perpendiculaire à l'axe médian (20), de sorte que le fond (34) de la chambre à tourbillonnement et des surfaces (18) de l'évidement (16), situées entre ce fond et l'ouverture (14) de sortie de la buse, délimitent la chambre à tourbillonnement (36), et dans lequel une zone partielle (100) des surfaces de paroi (18) de l'évidement (16) forme une surface de siège conique (32) pour le bord intérieur (22) réalisé avec une forme tronconique, caractérisée en ce que les surfaces de paroi (18) de l'évidement (16) sont formées par des surfaces enveloppes de troncs de cône coaxiaux à l'axe médian (20), que la surface de siège conique (32) possède un angle au sommet inférieur à celui d'une autre zone partielle (98) de la paroi (38) de la chambre à tourbillonnement, qui se raccorde à l'ouverture (14) de sortie de la buse, de sorte que la chambre à tourbillonnement (36) est réalisée avec une hauteur aussi faible que possible, et que le corps de refoulement (62) s'étend, sur au moins la moitié de la hauteur de la chambre à tourbillonnement (36) en direction de l'ouverture (14) de sortie de la buse, en moyenne avec un diamètre qui correspond au moins au diamètre de l'ouverture (14) de sortie de la buse.
  2. Buse à tourbillonnement selon la revendication 1, caractérisée en ce que le corps de refoulement (62) s'étend, avec un diamètre moyen correspondant au moins au diamètre de l'ouverture (14) de sortie de la buse, sur au moins les deux tiers de la hauteur de la chambre à tourbillonnement (36) en direction de l'ouverture de sortie de la buse (14).
  3. Buse à tourbillonnement selon l'une des revendications précédentes, caractérisée par une surface (74,82) du corps de refoulement (62), qui est tournée vers la paroi (38) de la chambre à tourbillonnement, est située annulairement dans chaque plan de coupe transversal par rapport au plan médian (20) respectivement à une distance constante de la paroi (38) de la chambre à tourbillonnement.
  4. Buse à tourbillonnement selon la revendication 3, caractérisée en ce que dans une partie du corps de refoulement (62) tournée vers l'ouverture (14) de sortie de la buse, la surface (82), tournée vers la paroi (38) de la chambre à tourbillonnement, s'étend à une distance constante de cette paroi.
  5. Buse à tourbillonnement selon la revendication 4, caractérisée en ce que la distance correspond approximativement à une largeur (b) du canal à tourbillonnement (42).
  6. Buse à tourbillonnement selon l'une des revendications précédentes, caractérisée en ce qu'une ouverture d'embouchure (46) du canal à tourbillonnement (42) est située dans une partie annulaire (76), qui s'étend autour du corps de refoulement (62), du fond (34) de la chambre à tourbillonnement.
  7. Buse à tourbillonnement selon la revendication 6, caractérisée en ce que la largeur de la zone annulaire (76) est choisie de telle sorte qu'elle correspond à l'étendue de l'ouverture d'embouchure (46) dans une direction radiale vers l'intérieur, à partir d'un bord extérieur de cette zone (76).
  8. Buse à tourbillonnement selon la revendication 7, caractérisée en ce que le canal à tourbillonnement (42) débouche, par une ouverture d'embouchure agencée sous la forme d'un segment de cercle (94), dans la chambre à tourbillonnement (36), le long d'une zone de bord extérieur du fond (34) de la chambre à tourbillonnement.
  9. Buse à tourbillonnement selon l'une des revendications précédentes, caractérisée en ce que le corps de refoulement (62) est pourvu d'un perçage central de retour (104).
  10. Buse à tourbillonnement selon l'une des revendications précédentes, caractérisée en ce que le corps de refoulement (62) est pourvu d'au moins un perçage de retour (110) disposé de façon excentrée.
  11. Buse à tourbillonnement selon la revendication 10, caractérisée en ce que le perçage de retour (110) est situé à une distance de l'axe médian (20), qui correspond au moins au rayon de l'ouverture (14) de sortie de la buse.
  12. Buse à tourbillonnement selon la revendication 11, caractérisée en ce que le perçage de retour (110) est disposé à une distance de l'axe médian (20), qui est inférieure à la distance de l'ouverture d'embouchure (46) du canal à tourbillonnement (42).
EP93118034A 1987-12-11 1988-12-09 Buse à tourbillonnement pour pulvériser un liquide Expired - Lifetime EP0604741B1 (fr)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
DE3742015 1987-12-11
DE3742015 1987-12-11
EP89900234A EP0346417B1 (fr) 1987-12-11 1988-12-09 Ajutage a tourbillon vaporisateur de liquides

Related Parent Applications (2)

Application Number Title Priority Date Filing Date
EP89900234A Division EP0346417B1 (fr) 1987-12-11 1988-12-09 Ajutage a tourbillon vaporisateur de liquides
EP89900234.9 Division 1988-12-09

Publications (3)

Publication Number Publication Date
EP0604741A2 EP0604741A2 (fr) 1994-07-06
EP0604741A3 EP0604741A3 (fr) 1994-11-30
EP0604741B1 true EP0604741B1 (fr) 1998-05-13

Family

ID=6342366

Family Applications (2)

Application Number Title Priority Date Filing Date
EP89900234A Expired - Lifetime EP0346417B1 (fr) 1987-12-11 1988-12-09 Ajutage a tourbillon vaporisateur de liquides
EP93118034A Expired - Lifetime EP0604741B1 (fr) 1987-12-11 1988-12-09 Buse à tourbillonnement pour pulvériser un liquide

Family Applications Before (1)

Application Number Title Priority Date Filing Date
EP89900234A Expired - Lifetime EP0346417B1 (fr) 1987-12-11 1988-12-09 Ajutage a tourbillon vaporisateur de liquides

Country Status (4)

Country Link
US (1) US5067655A (fr)
EP (2) EP0346417B1 (fr)
DE (2) DE3856185D1 (fr)
WO (1) WO1989005195A1 (fr)

Families Citing this family (86)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE69210603T2 (de) * 1991-05-20 1996-09-12 Goeran Tuusula Sundholm Ausrüstung zur brandbekämpfung
US5655608A (en) * 1991-05-20 1997-08-12 Sundholm; Goeran Fire fighting equipment
US5392993A (en) * 1994-01-21 1995-02-28 Grinnell Corporation, Fire protection nozzle
US5522549A (en) * 1994-10-24 1996-06-04 Sheu; Kun N. Jet nozzle assembly for removing pests from crops
US5697553A (en) * 1995-03-03 1997-12-16 Parker-Hannifin Corporation Streaked spray nozzle for enhanced air/fuel mixing
SE504838C2 (sv) * 1995-08-31 1997-05-12 Astra Ab Anordning vid ett sprayrörsmunstycke
US5765752A (en) * 1996-01-26 1998-06-16 Dgh Systems, L.L.C. Airless atomizing nozzle and system for humidity control
US5921470A (en) * 1997-03-20 1999-07-13 Kamath; Bola R. Air-atomizing oil burner utilizing a low pressure fan and nozzle
US6470980B1 (en) 1997-07-22 2002-10-29 Rex A. Dodd Self-excited drill bit sub
US6029746A (en) * 1997-07-22 2000-02-29 Vortech, Inc. Self-excited jet stimulation tool for cleaning and stimulating wells
US5954047A (en) * 1997-10-17 1999-09-21 Systemic Pulmonary Development, Ltd. Methods and apparatus for delivering aerosolized medication
US6745763B2 (en) * 1998-10-27 2004-06-08 Garth T. Webb Vaporizing device for administering sterile medication
AU755989B2 (en) * 1999-05-20 2003-01-02 Kos Life Sciences, Inc. Low spray force, low retention atomization system
US6367471B1 (en) * 1999-11-01 2002-04-09 Sheffield Pharmaceuticals, Inc. Internal vortex mechanism for inhaler device
JP2001137349A (ja) * 1999-11-16 2001-05-22 Asahi Optical Co Ltd 内視鏡用噴霧具
JP3798928B2 (ja) * 1999-11-16 2006-07-19 ペンタックス株式会社 内視鏡用処置具のチューブと口金の接続構造
FR2802446B1 (fr) * 1999-12-16 2002-04-12 Oreal Buse pour recipient aerosol
DE10010881B4 (de) * 2000-02-29 2006-09-07 Torsten Dipl.-Ing. Clauß Verfahren und Vorrichtung zum Ausbringen von flüssigen Medien
US6962152B1 (en) * 2000-05-02 2005-11-08 Salter Labs Respiratory equipment spacer assembly
DE10024888B4 (de) * 2000-05-16 2008-10-16 Gea Wtt Gmbh Plattenwärmeübertrager mit Kältemittelverteiler
IT1318646B1 (it) * 2000-07-26 2003-08-27 Medical Internat Licensing N V Ugello pr somministrazioni e lavaggi nasali.
US8235919B2 (en) 2001-01-12 2012-08-07 Celleration, Inc. Ultrasonic method and device for wound treatment
DE10129367A1 (de) * 2001-06-20 2003-01-09 Klingenburg Gmbh Luftbefeuchtungsvorrichtung
US7231919B2 (en) 2001-09-28 2007-06-19 Kurve Technology, Inc. Particle dispersion device for nasal delivery
DE10154237A1 (de) * 2001-11-07 2003-05-15 Steag Microparts Gmbh Zerstäuber für manuelle Betätigung
US20030102392A1 (en) * 2001-12-03 2003-06-05 Illinois Tool Works Inc. Internal impingement nozzle
US6814307B2 (en) * 2002-01-24 2004-11-09 Combustion Components Associates, Inc. Low NOx liquid fuel oil atomizer spray plate and fabrication method thereof
US8122881B2 (en) * 2002-05-09 2012-02-28 Kurve Technology, Inc. Particle dispersion device for nasal delivery
US6659369B1 (en) * 2002-06-12 2003-12-09 Continental Afa Dispensing Company High viscosity liquid sprayer nozzle assembly
US6808122B2 (en) * 2002-08-19 2004-10-26 Illinois Tool Works, Inc. Spray gun with improved pre-atomization fluid mixing and breakup
DE50312628D1 (de) * 2002-10-17 2010-05-27 Braun Gmbh Munddusche und sprühdüse zur erzeugung eines flüssigkeitsstrahls sowie zahnreinigungssystem
GB0300939D0 (en) * 2003-01-16 2003-02-12 Unilever Plc Method of creating a cosmetic spray
US7174717B2 (en) * 2003-12-24 2007-02-13 Pratt & Whitney Canada Corp. Helical channel fuel distributor and method
DE102005037972A1 (de) * 2005-08-11 2007-02-22 Krauss-Maffei Kunststofftechnik Gmbh Düse für Sprühkopf
MX2008011252A (es) * 2006-03-07 2008-09-10 Boehringer Ingelheim Int Tobera de remolino.
JP5400609B2 (ja) * 2006-05-17 2014-01-29 メッドミックス システムズ アーゲー 噴霧アセンブリを有する注出装置
US8491521B2 (en) * 2007-01-04 2013-07-23 Celleration, Inc. Removable multi-channel applicator nozzle
KR101450122B1 (ko) * 2007-06-04 2014-10-21 렉티셀 오토모빌시스템 게엠베하 경화성 조성물을 분무하기 위한 압력 선회 분무 노즐과 관련 제조 방법 및 사용 방법
US7712313B2 (en) * 2007-08-22 2010-05-11 Pratt & Whitney Canada Corp. Fuel nozzle for a gas turbine engine
EP2077132A1 (fr) 2008-01-02 2009-07-08 Boehringer Ingelheim Pharma GmbH & Co. KG Dispositif distributeur, dispositif de stockage et procédé pour la distribution d'une formulation
US8517009B2 (en) 2008-07-13 2013-08-27 Map Pharmaceuticals, Inc. Methods and apparatus for delivering aerosolized medication
RU2485245C2 (ru) * 2008-11-11 2013-06-20 Геннадий Петрович Кузнецов Способ создания условий для предотвращения попадания иловых отложений с дна воронежского водохранилища в пруд-охладитель нововоронежской атомной электростанции
US10011906B2 (en) 2009-03-31 2018-07-03 Beohringer Ingelheim International Gmbh Method for coating a surface of a component
EP3508239B1 (fr) 2009-05-18 2020-12-23 Boehringer Ingelheim International GmbH Adaptateur, dispositif d'inhalation et pulvérisateur
CA2671171C (fr) 2009-07-06 2017-12-12 Northbasin Energy Services Inc. Trepan avec interrupteur de debit
US10016568B2 (en) 2009-11-25 2018-07-10 Boehringer Ingelheim International Gmbh Nebulizer
EP2504051B1 (fr) 2009-11-25 2019-09-04 Boehringer Ingelheim International GmbH Nébuliseur
WO2011064164A1 (fr) 2009-11-25 2011-06-03 Boehringer Ingelheim International Gmbh Nébuliseur
US8517124B2 (en) 2009-12-01 2013-08-27 Northbasin Energy Services Inc. PDC drill bit with flute design for better bit cleaning
US20110303767A1 (en) * 2010-06-11 2011-12-15 Scott Edward Smith Dispenser having convergent flow path
US9174229B2 (en) * 2010-06-11 2015-11-03 The Procter & Gamble Company Dispenser having non-frustro-conical funnel wall
WO2011160932A1 (fr) 2010-06-24 2011-12-29 Boehringer Ingelheim International Gmbh Nébuliseur
US9332776B1 (en) * 2010-09-27 2016-05-10 ZoomEssence, Inc. Methods and apparatus for low heat spray drying
RU2594244C2 (ru) * 2011-01-31 2016-08-10 Син Ниппон Байомедикал Лэборэтэриз, Лтд. Устройства для интраназальной доставки
EP2694220B1 (fr) 2011-04-01 2020-05-06 Boehringer Ingelheim International GmbH Appareil médical pourvu d'un récipient
US9827384B2 (en) 2011-05-23 2017-11-28 Boehringer Ingelheim International Gmbh Nebulizer
EP2570110B1 (fr) * 2011-09-15 2017-05-03 Noxell Corporation Produit de laque aérosol pour styliser et/ou mettre en place les cheveux
EP2570190A1 (fr) * 2011-09-15 2013-03-20 Braun GmbH Buse de pulvérisation pour distribuer un fluide et pulvérisateur comportant une telle buse de pulvérisation
US9188063B2 (en) 2011-11-03 2015-11-17 Delavan Inc. Injectors for multipoint injection
US20140339339A1 (en) * 2011-11-03 2014-11-20 Delavan Inc Airblast injectors for multipoint injection and methods of assembly
WO2013152894A1 (fr) 2012-04-13 2013-10-17 Boehringer Ingelheim International Gmbh Pulvérisateur comprenant des moyens de détrompage
EP3030298B1 (fr) 2013-08-09 2017-10-11 Boehringer Ingelheim International GmbH Nébuliseur
EP2835146B1 (fr) 2013-08-09 2020-09-30 Boehringer Ingelheim International GmbH Atomiseur
CA2931612C (fr) 2013-11-26 2023-03-21 Alliqua Biomedical, Inc. Systemes et procedes pour produire et administrer des ultrasonotherapies pour un traitement de plaie et une cicatrisation
CN103691587B (zh) * 2013-12-12 2017-03-29 中国神华能源股份有限公司 布液喷头和海水淡化喷淋装置
US9689571B2 (en) * 2014-01-15 2017-06-27 Delavan Inc. Offset stem fuel distributor
PL3139979T3 (pl) 2014-05-07 2023-12-27 Boehringer Ingelheim International Gmbh Jednostka, nebulizator i sposób
US10722666B2 (en) 2014-05-07 2020-07-28 Boehringer Ingelheim International Gmbh Nebulizer with axially movable and lockable container and indicator
EA032459B1 (ru) 2014-05-07 2019-05-31 Бёрингер Ингельхайм Интернациональ Гмбх Небулайзер
US9897321B2 (en) 2015-03-31 2018-02-20 Delavan Inc. Fuel nozzles
US10385809B2 (en) 2015-03-31 2019-08-20 Delavan Inc. Fuel nozzles
CA3068887C (fr) 2016-06-21 2021-07-06 I3-Edge Ltd. Procede et systeme d'extraction d'elements tubulaires et similaires
DE202016103825U1 (de) * 2016-07-14 2017-10-20 SWEDEX GmbH Industrieprodukte Drallkörper sowie Kegeldüse mit einem solchen Drallkörper
FR3055560B1 (fr) * 2016-09-02 2021-05-07 Albea Le Treport Tete de distribution d'un fluide sous pression et bombe aerosol ou pompe a actionnement manuel comprenant une telle tete de distribution
CN106621785A (zh) * 2017-02-23 2017-05-10 东方电气集团东方锅炉股份有限公司 一种锅炉烟气三氧化硫脱除装置及方法
DE102017113207A1 (de) * 2017-06-15 2018-12-20 Alfons Kenter Zerstäuberdüse zum Zerstäuben eines Fluids
US9993787B1 (en) 2017-08-04 2018-06-12 ZoomEssence, Inc. Ultrahigh efficiency spray drying apparatus and process
US10486173B2 (en) 2017-08-04 2019-11-26 ZoomEssence, Inc. Ultrahigh efficiency spray drying apparatus and process
BR112020002403A2 (pt) 2017-08-04 2020-07-28 ZoomEssence, Inc. método de processamento de uma composição líquida secável por pulverização, sistemas de secagem por pulverização e processo para a produção de um material seco por pulverização
US10155234B1 (en) 2017-08-04 2018-12-18 ZoomEssence, Inc. Ultrahigh efficiency spray drying apparatus and process
US9861945B1 (en) 2017-08-04 2018-01-09 ZoomEssence, Inc. Ultrahigh efficiency spray drying apparatus and process
US10569244B2 (en) 2018-04-28 2020-02-25 ZoomEssence, Inc. Low temperature spray drying of carrier-free compositions
DE102020204849A1 (de) 2020-04-16 2021-10-21 Siemens Aktiengesellschaft Dralldüse mit äußerer Führungsrille
FR3112292A1 (fr) * 2020-07-07 2022-01-14 Aptar France Sas Tête de pulvérisation et dispositif de distribution de produit fluide comportant une telle tête
US20230090908A1 (en) * 2021-09-23 2023-03-23 GM Global Technology Operations LLC Paint spray nozzle for a paint spray system
CN116116590B (zh) * 2023-04-18 2023-06-13 箭牌家居集团股份有限公司 出水装置及花洒

Family Cites Families (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE314080C (fr) *
US1008119A (en) * 1911-06-12 1911-11-07 Union Iron Works Co Liquid-atomizer.
DE280632C (fr) * 1912-08-19 1914-11-21
US1650128A (en) * 1920-04-05 1927-11-22 Babcock & Wilcox Co Method of and apparatus for spraying liquids
GB162172A (en) * 1920-04-09 1921-04-28 John Graves Mckean Improvements in atomisers for liquid fuel and other liquids
US1757023A (en) * 1926-10-20 1930-05-06 Ira E Smith Oil burner
DE556863C (de) * 1928-04-23 1932-08-15 Gustav Schlick Zerstaeuberduese
US2017467A (en) * 1934-11-23 1935-10-15 Leavitt R Loomis Spray nozzle
US2065161A (en) * 1935-01-28 1936-12-22 Thompson Mfg Company Full circle sprinkler
US2176356A (en) * 1936-05-23 1939-10-17 Jens A Paasche Fluid spraying apparatus
US2374041A (en) * 1942-01-31 1945-04-17 Gen Furnaces Corp Variable capacity atomizing device
US2984421A (en) * 1958-08-11 1961-05-16 Sarah A Hession Adjustable aerosol device
FR1560603A (fr) * 1968-01-30 1969-03-21
DE1750561B2 (de) * 1968-05-14 1976-08-05 Hoechst Ag, 6000 Frankfurt Trommelfoermig gestaltete spiralduese zum zerstaeuben verunreinigter fluessigkeiten
US3684194A (en) * 1970-10-29 1972-08-15 Delavan Manufacturing Co Spray nozzle
DE2814246A1 (de) * 1978-04-03 1979-10-11 Metallgesellschaft Ag Ruecklaufduese
DE3703075A1 (de) * 1987-02-03 1988-08-11 Deutsche Forsch Luft Raumfahrt Drallduese zum zerstaeuben einer fluessigkeit

Also Published As

Publication number Publication date
US5067655A (en) 1991-11-26
DE3856185D1 (de) 1998-06-18
WO1989005195A1 (fr) 1989-06-15
DE3851750D1 (de) 1994-11-10
EP0346417B1 (fr) 1994-10-05
EP0604741A2 (fr) 1994-07-06
EP0346417A1 (fr) 1989-12-20
EP0604741A3 (fr) 1994-11-30

Similar Documents

Publication Publication Date Title
EP0604741B1 (fr) Buse à tourbillonnement pour pulvériser un liquide
EP1046426B1 (fr) Buse de pulvérisation haute pression
EP1243343B1 (fr) Buse de vaporisation à deux fluides
EP0619457B1 (fr) Brûleur à prémélange
DE1601958B2 (fr)
DE2542240A1 (de) Hohlkegelduese zum zerstaeuben von fluessigkeit
DE102011078508A1 (de) Vollkegeldüse
DE68926396T2 (de) Plasmabrenner für übertragenen lichtbogen
DE1063989B (de) Drallduese
DE102011078857A1 (de) Sprühdüse und Verfahren zum Erzeugen wenigstens eines rotierenden Sprühstrahls
EP1543882B1 (fr) Buse à jet conique
EP0801990B1 (fr) Buse de pulvérisation, en particulier pour la pulvérisation d'eau dans les installations de protection contre l'incendie
DE2141291C3 (de) Sprühdüse zur Erzielung eines kegelstumpfförmigen Sprühnebels
DE19841401C2 (de) Zweistoff-Flachstrahldüse
EP1343591B1 (fr) Gicleur
DE3309742C2 (fr)
DE69913442T2 (de) Flüssigkeits-Zerstäuber
DE3640818C1 (en) Spray head for producing an air-liquid mixture, in particular for a cooling device
DE2919074C2 (fr)
DE1942022A1 (de) Einteiliger Spruehkopf fuer Aerosolbehaelter
EP0413173B1 (fr) Injecteur de combustible pour moteurs à combustion interne
DE19750068C1 (de) Axial-Hohlkegeldüse zum Versprühen flüssiger Medien
DE3703075C2 (fr)
DE19949236A1 (de) Zweistoff-Sprühdüse
DE2604264A1 (de) Spruehduese

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

17P Request for examination filed

Effective date: 19931106

AC Divisional application: reference to earlier application

Ref document number: 346417

Country of ref document: EP

AK Designated contracting states

Kind code of ref document: A2

Designated state(s): CH DE LI

PUAL Search report despatched

Free format text: ORIGINAL CODE: 0009013

AK Designated contracting states

Kind code of ref document: A3

Designated state(s): CH DE LI

17Q First examination report despatched

Effective date: 19951005

GRAG Despatch of communication of intention to grant

Free format text: ORIGINAL CODE: EPIDOS AGRA

GRAG Despatch of communication of intention to grant

Free format text: ORIGINAL CODE: EPIDOS AGRA

GRAH Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOS IGRA

RAP1 Party data changed (applicant data changed or rights of an application transferred)

Owner name: DEUTSCHES ZENTRUM FUER LUFT- UND RAUMFAHRT E.V.

GRAH Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOS IGRA

GRAA (expected) grant

Free format text: ORIGINAL CODE: 0009210

AC Divisional application: reference to earlier application

Ref document number: 346417

Country of ref document: EP

AK Designated contracting states

Kind code of ref document: B1

Designated state(s): CH DE LI

REG Reference to a national code

Ref country code: CH

Ref legal event code: EP

REF Corresponds to:

Ref document number: 3856185

Country of ref document: DE

Date of ref document: 19980618

REG Reference to a national code

Ref country code: CH

Ref legal event code: NV

Representative=s name: KIRKER & CIE SA

PLBE No opposition filed within time limit

Free format text: ORIGINAL CODE: 0009261

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT

26N No opposition filed
PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: DE

Payment date: 19991117

Year of fee payment: 12

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: CH

Payment date: 19991220

Year of fee payment: 12

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: LI

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20001231

Ref country code: CH

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20001231

REG Reference to a national code

Ref country code: CH

Ref legal event code: PL

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: DE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20011002