DE347071C - Turbo ring nozzle hot air atomization - Google Patents
Turbo ring nozzle hot air atomizationInfo
- Publication number
- DE347071C DE347071C DE1918347071D DE347071DD DE347071C DE 347071 C DE347071 C DE 347071C DE 1918347071 D DE1918347071 D DE 1918347071D DE 347071D D DE347071D D DE 347071DD DE 347071 C DE347071 C DE 347071C
- Authority
- DE
- Germany
- Prior art keywords
- turbo
- air
- nozzle
- atomized
- hot air
- 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
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B01—PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
- B01D—SEPARATION
- B01D1/00—Evaporating
- B01D1/16—Evaporating by spraying
- B01D1/20—Sprayers
-
- A—HUMAN NECESSITIES
- A23—FOODS OR FOODSTUFFS; TREATMENT THEREOF, NOT COVERED BY OTHER CLASSES
- A23C—DAIRY PRODUCTS, e.g. MILK, BUTTER OR CHEESE; MILK OR CHEESE SUBSTITUTES; MAKING THEREOF
- A23C1/00—Concentration, evaporation or drying
- A23C1/04—Concentration, evaporation or drying by spraying into a gas stream
Landscapes
- Chemical & Material Sciences (AREA)
- Life Sciences & Earth Sciences (AREA)
- Engineering & Computer Science (AREA)
- Food Science & Technology (AREA)
- Polymers & Plastics (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Drying Of Solid Materials (AREA)
Description
Turbo-Ringdüsen-Heißluftzerstäubung.Turbo ring nozzle hot air atomization.
Beliebig zu temperierende, durch Düsen a und c geleitete Luftströme zerstäuben die aus Düse b ringförmig austretende flüssige Materie und führen dieselbe unter gleichzeitiger Mischung mit dem aus Düse d kommenden Heißluftsfrom gegen einen durch den aus Düse e kommenden beliebig temperierten Luftstrom zur Umdrehung gebrachten Turboverteiler (Windrad) H, welcher mit gegen die Luftströme im Winkel stehenden Flächen i versehen ist. Air streams that can be adjusted to any temperature and are directed through nozzles a and c atomize the liquid matter emerging from nozzle b in a ring shape and guide it while simultaneously mixing with the hot air from nozzle d against one made to rotate by the air stream of any temperature coming from nozzle e Turbo distributor (wind turbine) H, which is at an angle to the air currents Surfaces i is provided.
Durch den hierdurch entstehenden Wirbelwind wird die an und für sich bereits zerstäubte Materie bis in ihre kleinsten Teile zerteilt und getrocknet. Durch Anordnung der Düse b wird die kreisförmig austretende Materie sowohl im inneren wie auch im äußeren Umfange vom Luftstrom. bestrichen und gestalten sich hierdurch die Berührungslinien zu den denkbar günstigsten; auch kann durch jeweils voneinander unabhängige Regulierung des Druckes bzw. der Luftgeschwindigkeit in den Düsen a und c die Zerstäubungsstromrichtung sowohl konzentrisch wie exzentrisch gestaltet werden, so daß dieselbe in beliebiger Dimension zum Turboverteiler H (Windscheibe) geführt werden kann. The resulting whirlwind becomes that in and of itself matter that has already been atomized is broken down into its smallest parts and dried. By arranging the nozzle b, the circular emerging matter is both inside as well as in the outer circumference of the air flow. coated and designed as a result the lines of contact to the cheapest imaginable; also can by each of each other independent regulation of the pressure or the air speed in the nozzles a and c the atomization flow direction is made both concentric and eccentric so that the same in any dimension to the turbo distributor H (windshield) can be performed.
Auf Düse e ist ein mit Luftklappen versehenes Piston g, welches dazu dient, die aus e austretende Heißluft zu mischen und an die Windscheibe H zum Trocknen und Antrieb zu führen. On nozzle e there is a piston g with air flaps, which is used for this purpose serves to mix the hot air emerging from e and to dry it on the windshield H and drive to guide.
Die einzelnen Düsenzuführungen sind voneinander unabhängig. The individual nozzle feeds are independent of one another.
Die einzelnen Dimensionen der Düsen und die Dimension des Turboverteilers werden der jeweilig zu verarbeitenden Materie und der zu erzielendlen Menge angepaßt. The individual dimensions of the nozzles and the dimensions of the turbo distributor are adapted to the respective material to be processed and the amount to be achieved.
Claims (4)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE347071T | 1918-10-30 |
Publications (1)
Publication Number | Publication Date |
---|---|
DE347071C true DE347071C (en) | 1922-01-13 |
Family
ID=6255822
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE1918347071D Expired DE347071C (en) | 1918-10-30 | 1918-10-30 | Turbo ring nozzle hot air atomization |
Country Status (2)
Country | Link |
---|---|
DE (1) | DE347071C (en) |
NL (1) | NL6471C (en) |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3017854A (en) * | 1959-03-20 | 1962-01-23 | Edward D O'brien | Centrifugal coating apparatus |
-
1918
- 1918-10-30 DE DE1918347071D patent/DE347071C/en not_active Expired
-
1920
- 1920-01-09 NL NL13760A patent/NL6471C/xx active
Also Published As
Publication number | Publication date |
---|---|
NL6471C (en) | 1922-01-18 |
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