Influence of spray nozzle shape upon atomization process

2016 ◽  
Author(s):  
Marius Beniuga ◽  
Ioan Mihai
2021 ◽  
Vol 1 (1) ◽  
Author(s):  
Francisco Javier Salvador ◽  
Jaime Gimeno ◽  
Marcos Carreres ◽  
Lucas Gonzalez

Author(s):  
J. M. Walsh ◽  
K. P. Gumz ◽  
J. C. Whittles ◽  
B. H. Kear

During a routine examination of the microstructure of rapidly solidified IN-100 powder, produced by a newly-developed centrifugal atomization process1, essentially two distinct types of microstructure were identified. When a high melt superheat is maintained during atomization, the powder particles are predominantly coarse-grained, equiaxed or columnar, with distinctly dendritic microstructures, Figs, la and 4a. On the other hand, when the melt superheat is reduced by increasing the heat flow to the disc of the rotary atomizer, the powder particles are predominantly microcrystalline in character, with typically one dendrite per grain, Figs, lb and 4b. In what follows, evidence is presented that strongly supports the view that the unusual microcrystalline structure has its origin in dendrite erosion occurring in a 'mushy zone' of dynamic solidification on the disc of the rotary atomizer.The critical observations were made on atomized material that had undergone 'splat-quenching' on previously solidified, chilled substrate particles.


2005 ◽  
Vol 15 (6) ◽  
pp. 687-698 ◽  
Author(s):  
Jongmook Lim ◽  
Yudaya R. Sivathanu
Keyword(s):  

2019 ◽  
pp. 22-26
Author(s):  
А. Богоявленский ◽  
A. Bogoyavlenskiy

Snow-ice deposits formed on the outer surfaces of aircrafts on the ground during parking can have a negative impact during take-off due to the deterioration of aerodynamic and flight performance, a significant and even critical decrease in lift, increased drag, blocking controls, difficulty or blocking of landing gear retraction, damage to the blades of inlet guide vanes and/or the blades of an engine compressor. To exclude the influence of snow and ice deposits, anti-icing treatment is performed, including their removal and/or protection from subsequent formation. For this purpose, special anti-icing machines (deicers), equipped with such means of instrumental control as counters of anti-icing fluid pumps, measuring scales of anti-icing fluid tanks, thermometers and pressure gauges for temperature and pressure measuring at the outlet of a spray nozzle, are used. The article deals with the metrological aspects of civil aircrafts anti-icing prior to flight.


1981 ◽  
Vol 24 (2) ◽  
pp. 0526-0532 ◽  
Author(s):  
James M. Scott ◽  
David G. Dunsmore ◽  
Mark D. Keegan
Keyword(s):  

2010 ◽  
Vol 21 (7) ◽  
pp. 075403 ◽  
Author(s):  
Mohamed Esmail ◽  
Nobuyuki Kawahara ◽  
Eiji Tomita ◽  
Mamoru Sumida

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