Importance of Geometrical Factors on Spray Characteristics of Spill-return Atomisers
Identifikátory výsledku
Kód výsledku v IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00216305%3A26210%2F21%3APU138562" target="_blank" >RIV/00216305:26210/21:PU138562 - isvavai.cz</a>
Výsledek na webu
<a href="https://arc.aiaa.org/doi/full/10.2514/1.B38066" target="_blank" >https://arc.aiaa.org/doi/full/10.2514/1.B38066</a>
DOI - Digital Object Identifier
<a href="http://dx.doi.org/10.2514/1.B38066" target="_blank" >10.2514/1.B38066</a>
Alternativní jazyky
Jazyk výsledku
angličtina
Název v původním jazyce
Importance of Geometrical Factors on Spray Characteristics of Spill-return Atomisers
Popis výsledku v původním jazyce
An experimental investigation into small pressure-swirl spill-return atomizers was made to determine the effect of the entry port number, swirl chamber shape, spill-line design and the manufacturing precision on the spray quality and stability. The atomizers were experimentally studied using phase-Doppler anemometry, high-speed visualization and mechanical patternation. The Jet A-1 fuel was sprayed at inlet pressures of 0.5, 1.0 and 1.5 MPa and for spill-to-feed ratios of 0, 0.4 and 0.8. The chamber shape influenced the spray characteristics of the simplex atomizers only moderately with no systematic effect of conical chambers to the others. The spray was found to be circumferentially heterogeneous; its uniformity improved with increase in the pressure while the effect of swirling port number was negligible. Atomizers with axial spill orifice demonstrated strong spray pulsations at a spill-to-feed ratio of zero. A periodic decay of the air core was identified as a possible reason for the pulsations. Atomizers with the off-axis spill orifices always produced a stable spray. The atomizers with tangential inlet ports provided a finer spray than those with the helical ports. The manufacturing precision, axial symmetry and matching of the surfaces of connected parts were found important for the spray symmetry and homogeneity.
Název v anglickém jazyce
Importance of Geometrical Factors on Spray Characteristics of Spill-return Atomisers
Popis výsledku anglicky
An experimental investigation into small pressure-swirl spill-return atomizers was made to determine the effect of the entry port number, swirl chamber shape, spill-line design and the manufacturing precision on the spray quality and stability. The atomizers were experimentally studied using phase-Doppler anemometry, high-speed visualization and mechanical patternation. The Jet A-1 fuel was sprayed at inlet pressures of 0.5, 1.0 and 1.5 MPa and for spill-to-feed ratios of 0, 0.4 and 0.8. The chamber shape influenced the spray characteristics of the simplex atomizers only moderately with no systematic effect of conical chambers to the others. The spray was found to be circumferentially heterogeneous; its uniformity improved with increase in the pressure while the effect of swirling port number was negligible. Atomizers with axial spill orifice demonstrated strong spray pulsations at a spill-to-feed ratio of zero. A periodic decay of the air core was identified as a possible reason for the pulsations. Atomizers with the off-axis spill orifices always produced a stable spray. The atomizers with tangential inlet ports provided a finer spray than those with the helical ports. The manufacturing precision, axial symmetry and matching of the surfaces of connected parts were found important for the spray symmetry and homogeneity.
Klasifikace
Druh
J<sub>imp</sub> - Článek v periodiku v databázi Web of Science
CEP obor
—
OECD FORD obor
10305 - Fluids and plasma physics (including surface physics)
Návaznosti výsledku
Projekt
Výsledek vznikl pri realizaci vícero projektů. Více informací v záložce Projekty.
Návaznosti
P - Projekt vyzkumu a vyvoje financovany z verejnych zdroju (s odkazem do CEP)
Ostatní
Rok uplatnění
2021
Kód důvěrnosti údajů
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů
Údaje specifické pro druh výsledku
Název periodika
Journal of Propulsion and Power
ISSN
0748-4658
e-ISSN
1533-3876
Svazek periodika
37
Číslo periodika v rámci svazku
3
Stát vydavatele periodika
US - Spojené státy americké
Počet stran výsledku
11
Strana od-do
408-418
Kód UT WoS článku
000658185200007
EID výsledku v databázi Scopus
2-s2.0-85116463716