TY - JOUR
T1 - Ultrafast X-ray study of multi-hole GDI injector sprays
T2 - Effects of nozzle hole length and number on initial spray formation
AU - Moon, Seoksu
AU - Komada, Keisuke
AU - Sato, Kiyotaka
AU - Yokohata, Hideaki
AU - Wada, Yoshitaka
AU - Yasuda, Nobuhiro
N1 - Publisher Copyright:
© 2015 Elsevier Inc.
PY - 2015/11/1
Y1 - 2015/11/1
N2 - Nozzle hole design factors, such as length, diameter, position and number of nozzle holes, significantly alter the near-field jet flow and following spray formation of fuel injection nozzles. This study investigates the effects of various nozzle hole design factors on near-field jet flow and spray formation of the multi-hole injectors for gasoline direct-injection (GDI) engines. The novelty of this study lies in intensive analysis in the near-field jet breakup, dynamics and droplet formation process that have rarely been characterized from previous studies by exploiting the potentials of synchrotron X-ray for near-field spray analysis. Among several nozzle hole design factors, the effects of the length and number of nozzle holes are investigated in the current paper as the first part. Four prototype injection nozzles, which have different lengths and numbers of nozzle holes with a substantially low needle lift of 35. μm, were used for this fundamental study. Single- and multi-exposed X-ray phase-contrast images were used to characterize the jet breakup, dynamics and droplet formation process from the nozzle exit to 30. mm downstream. The emerging jet flows from the multi-hole GDI injectors were highly turbulent and perturbed immediately from the nozzle exit. The decrease in nozzle hole length increased the axial and radial flow velocity of the emerging jet flow with an increased void fraction inside the nozzle hole at the nozzle exit. It promoted the jet breakup with formation of smaller and more circular liquid ligaments/droplets in the near-field when the nozzle hole length decreased, which accompanied the higher velocity decrease rate and turbulence strength along the spray axis. On the other hand, the increase in the number of nozzle holes decreased the axial and radial flow velocity of the emerging jet flow. It led to a slower breakup of the jet flow with a lower velocity decrease rate along the spray axis at larger number of nozzle holes.
AB - Nozzle hole design factors, such as length, diameter, position and number of nozzle holes, significantly alter the near-field jet flow and following spray formation of fuel injection nozzles. This study investigates the effects of various nozzle hole design factors on near-field jet flow and spray formation of the multi-hole injectors for gasoline direct-injection (GDI) engines. The novelty of this study lies in intensive analysis in the near-field jet breakup, dynamics and droplet formation process that have rarely been characterized from previous studies by exploiting the potentials of synchrotron X-ray for near-field spray analysis. Among several nozzle hole design factors, the effects of the length and number of nozzle holes are investigated in the current paper as the first part. Four prototype injection nozzles, which have different lengths and numbers of nozzle holes with a substantially low needle lift of 35. μm, were used for this fundamental study. Single- and multi-exposed X-ray phase-contrast images were used to characterize the jet breakup, dynamics and droplet formation process from the nozzle exit to 30. mm downstream. The emerging jet flows from the multi-hole GDI injectors were highly turbulent and perturbed immediately from the nozzle exit. The decrease in nozzle hole length increased the axial and radial flow velocity of the emerging jet flow with an increased void fraction inside the nozzle hole at the nozzle exit. It promoted the jet breakup with formation of smaller and more circular liquid ligaments/droplets in the near-field when the nozzle hole length decreased, which accompanied the higher velocity decrease rate and turbulence strength along the spray axis. On the other hand, the increase in the number of nozzle holes decreased the axial and radial flow velocity of the emerging jet flow. It led to a slower breakup of the jet flow with a lower velocity decrease rate along the spray axis at larger number of nozzle holes.
KW - Gasoline direct injection
KW - Multi-hole injector
KW - Nozzle hole geometry
KW - Spray formation
KW - X-ray phase-contrast imaging
UR - http://www.scopus.com/inward/record.url?scp=84928322337&partnerID=8YFLogxK
U2 - 10.1016/j.expthermflusci.2015.03.027
DO - 10.1016/j.expthermflusci.2015.03.027
M3 - Article
AN - SCOPUS:84928322337
SN - 0894-1777
VL - 68
SP - 68
EP - 81
JO - Experimental Thermal and Fluid Science
JF - Experimental Thermal and Fluid Science
ER -