DE1949449B - Swirl nozzle for evenly atomizing liquids - Google Patents
Swirl nozzle for evenly atomizing liquidsInfo
- Publication number
- DE1949449B DE1949449B DE1949449B DE 1949449 B DE1949449 B DE 1949449B DE 1949449 B DE1949449 B DE 1949449B
- Authority
- DE
- Germany
- Prior art keywords
- swirl
- nozzle
- cone
- face
- atomization
- 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.)
- Pending
Links
- 239000007788 liquid Substances 0.000 title claims description 8
- 238000000889 atomisation Methods 0.000 claims description 11
- 230000035515 penetration Effects 0.000 claims description 9
- 238000009826 distribution Methods 0.000 claims description 4
- 238000011068 load Methods 0.000 claims 2
- 210000003608 Feces Anatomy 0.000 claims 1
- 238000010348 incorporation Methods 0.000 claims 1
- 239000010871 livestock manure Substances 0.000 claims 1
- 238000005461 lubrication Methods 0.000 claims 1
- 239000002245 particle Substances 0.000 claims 1
- 239000007787 solid Substances 0.000 claims 1
- 239000007921 spray Substances 0.000 claims 1
- 238000004544 sputter deposition Methods 0.000 claims 1
- 238000009827 uniform distribution Methods 0.000 claims 1
- 238000006073 displacement reaction Methods 0.000 description 1
Description
Die Parameter für die Beeinflussung der Beaufschlagungsverteilung durch den Drallkörper sind:The parameters for influencing the impact distribution by the swirl body are:
Die Tiefe der Drallkanäle durch paralleles Verschieben
der Begrenzungsebene vor oder hinter die Rotationsachse des Drallkörpers,
seitliche Versetzung der Durchdringung der Drallkanäle an der Stirnfläche des Drallkörpers
gegenüber dem Radius,
die Breite der Drallkanäle,
die Höhe des Drallkörpers.The depth of the swirl channels by parallel displacement of the boundary plane in front of or behind the axis of rotation of the swirl body,
lateral offset of the penetration of the swirl channels on the face of the swirl body compared to the radius,
the width of the swirl channels,
the height of the swirler.
Durch die unterschiedliche Durchdringung der Drallkanäle an den beiden Stirnflächen der Drallkörper ergeben sich unterschiedliche Ein- bzw. Austrittsquerschnitte für die Flüssigkeit. Diese Unterschiede können dadurch ausgeglichen werden, daß die Tiefe der Drallkanäle von der radialen zur gegenüberliegenden Durchdringungsseite kontinuierlich vergrößert wird. Der Querschnittsausgleich kann auch durch konische Ausbildung des Drallkörpers erfolgen. Dies schränkt jedoch die unveränderte Verwendbarkeit des Drallkörpers für Vollkegel- und Hohlkegel-Due to the different penetration of the swirl channels on the two end faces of the swirl body there are different inlet and outlet cross-sections for the liquid. Those differences can be compensated by the fact that the depth of the swirl channels from the radial to the opposite Penetration side is continuously enlarged. The cross-sectional adjustment can also take place by conical design of the swirl body. However, this limits the unchanged usability of the swirl body for full cone and hollow cone
zerstäubung ein. Die Beaufschlagungsverteilung kann auch durch entsprechende Ausbildung des Düsendrallraumcs beeinflußt werden.atomization. The surcharge distribution can also through appropriate training of the nozzle swirl space to be influenced.
Die unterschiedliche Durchdringung der Drallkanäle an den Stirnflächen des Drallkörpers gibt dieThe different penetration of the swirl channels on the end faces of the swirl body gives the
ίο Möglichkeit zur Erzeugung einer Hohlkegelzcrstäubung dadurch, daß die Stirnfläche des Drallkörpers mit radialer Durchdringung der Drallkanäle dem Flüssigkeitszulauf zugekehrt in den Düsenkörper eingebaut wird. Diese Mehrzweckverwendungsmöglich-ίο Possibility to generate a hollow cone atomization in that the end face of the swirl body with radial penetration of the swirl channels Liquid inlet facing is installed in the nozzle body. This multi-purpose use
keit bedeutet vor allem im Hinblick auf die bei Düsen erforderlichen Leistungsbaureihen eine wesentliche Verbesserung der Kostensituation.Above all, speed means in terms of nozzles required performance series a significant improvement in the cost situation.
Hierzu 1 Blatt Zeichnungen1 sheet of drawings
Claims (3)
Drallkörpers mit radialer Durchdringung der 25 Die A b b. 1 bis 4 zeigen das Prinzip der Erfindung Drallkanäle dem Flüssigkeitszulauf zugekehrt ist, am Beispiel einer Dralldüse mit vier Drallkanälen im wodurch eine Hohlkegelbeaufschlagung erzielt Drallkörper.3. Swirl nozzle according to claims 1 and 2, can, can achieve a very uniform Beaufschladakter that the end face of the supply distribution of the atomizing cone.
Swirl body with radial penetration of the 25 The A b b. 1 to 4 show the principle of the invention swirl channels facing the liquid inlet, using the example of a swirl nozzle with four swirl channels in the swirl body, whereby a hollow cone is applied to the swirl body.
großer Drallraum erforderlich. Die Beaufschlagung kann im Rahmen der ErHn-Der Erfindung liegt die Aufgabe zugrunde, einen dung durch verschiedene konstruktive Maßnahmen Drallkörper zu finden, der über einen großen Druck- am Drallkörper beeinflußt werden, so daß wahlweise bereich sowohl für eine gleichmäßige Vollkegel- wie die inneren oder äußeren Zonen des Düsenstrahl Hohlkcgelzerstäubung geeignet ist. Zur Lösung des 65 stärker oder schwächet beaufschlagt werden. Dies Problems wird gemäß der Erfindung vorgeschlagen, kann z. B. dann von Bedeutung sein, wenn mehrere daß je ein Drallkanal in einer windschief zur Längs- Düsen im Verband spritzen, wie beim Pflanzenschutz, achse der Dralldüse liegenden Ebene angeordnet ist, und die einzelnen Düsenstrahlen sich überlappen.Full cone sparging relatively difficult, before the liquid flowing from direction A of the nozzle under pressure, especially with regard to a uniform surface area, flows upwards, increasing its impact on the sputtering cone. Flow velocity in the circumference of the swirl. For the solution of this problem there are different channels 2 lying on the body 1. Became known through the oblique designs. According to the German position of the swirl channel 2 to the axis of rotation of the swirl patent specification 448 008, swirl bodies, for example, how the liquid particles are used for the hollow cone lubrication, are axially deflected in the inflow direction and are provided with a central bore in order to create the oblique flow direction more or less to be filled in as a concentric hollow cone. E ; Such a partial flow of preferably rectangular, transversely uniform distribution can only be cut into the swirl space. Achieve the pressure range limited there by the Abeincn. The swirl caused by the steering is the greater, the further. This consists in the wcscnt swirl body are removed. The swirl components borrowed from two inclined guide surfaces, which are interrupted by recesses in the flow that forms in the swirl space. This swirl body therefore has the disadvantage, continuously in the direction towards the center, that the division into two from the load to zero, so that this occurring impact becomes apparent. In order to keep this unevenness in the speed distribution a uniform, fully tolerable limit, a relatively 60 jet is created from the nozzle orifice 4 between the cone impact at the exit of the atomizing nozzle orifice and the swirl body,
large swirl space required. The application can in the context of the ErHn-The invention is based on the task of finding a manure through various structural measures swirl body, which can be influenced by a large pressure on the swirl body, so that either area for a uniform full cone as the inner or outer zones of the nozzle jet hollow cone atomization is suitable. To solve the 65 stronger or weaker pressures. This problem is proposed according to the invention, e.g. B. be of importance when several that each spray a swirl channel in a skewed to the longitudinal nozzle in the association, as in plant protection, axis of the swirl nozzle lying plane is arranged, and the individual nozzle jets overlap.
Family
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Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE3235080A1 (en) * | 1982-09-22 | 1984-03-22 | Kraftwerk Union AG, 4330 Mülheim | Return-flow injection nozzle for the atomisation of liquids |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE3235080A1 (en) * | 1982-09-22 | 1984-03-22 | Kraftwerk Union AG, 4330 Mülheim | Return-flow injection nozzle for the atomisation of liquids |
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