Estimation of High-Speed Liquid-Jet Velocity Using a Pyro Jet Injector.


Journal

Scientific reports
ISSN: 2045-2322
Titre abrégé: Sci Rep
Pays: England
ID NLM: 101563288

Informations de publication

Date de publication:
27 Dec 2019
Historique:
received: 13 06 2019
accepted: 06 12 2019
entrez: 29 12 2019
pubmed: 29 12 2019
medline: 29 12 2019
Statut: epublish

Résumé

The high-speed liquid-jet velocity achieved using an injector strongly depends on the piston motion, physical property of the liquid, and container shape of the injector. Herein, we investigate the liquid ejection mechanism and a technique for estimating the ejection velocity of a high-speed liquid jet using a pyro jet injector (PJI). We apply a two-dimensional numerical simulation with an axisymmetric approximation using the commercial software ANSYS/FLUENT. To gather the input data applied during the numerical simulation, the piston motion is captured with a high-speed CMOS camera, and the velocity of the piston is measured using motion tracking software. To reproduce the piston motion during the numerical simulation, the boundary-fitted coordinates and a moving boundary method are employed. In addition, we propose a fluid dynamic model (FDM) for estimating the high-speed liquid-jet ejection velocity based on the piston velocity. Using the FDM, we consider the liquid density variation but neglect the effects of the liquid viscosity on the liquid ejection. Our results indicate that the liquid-jet ejection velocity estimated by the FDM corresponds to that predicted by ANSYS/FLUENT for several different ignition-powder weights. This clearly shows that a high-speed liquid-jet ejection velocity can be estimated using the presented FDM when considering the variation in liquid density but neglecting the liquid viscosity. In addition, some characteristics of the presented PJI are observed, namely, (1) a very rapid piston displacement within 0.1 ms after a powder explosion, (2) piston vibration only when a large amount of powder is used, and (3) a pulse jet flow with a temporal pulse width of 0.1 ms.

Identifiants

pubmed: 31882780
doi: 10.1038/s41598-019-56511-x
pii: 10.1038/s41598-019-56511-x
pmc: PMC6934512
doi:

Types de publication

Journal Article

Langues

eng

Sous-ensembles de citation

IM

Pagination

19859

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Auteurs

Naohisa Takagaki (N)

Department of Mechanical Engineering, University of Hyogo, Himeji, 671-2280, Japan. takagaki@eng.u-hyogo.ac.jp.

Toru Kitaguchi (T)

Medical Device Division, Medical Device Research Center, Daicel Corporation, Toyonaka, Osaka, 560-8531, Japan.

Masashi Iwayama (M)

Corporate Research Center, R&D Headquarters, Daicel Corporation, Himeji, Hyogo, 671-1283, Japan.

Atsushi Shinoda (A)

Department of Mechanical Engineering, University of Hyogo, Himeji, 671-2280, Japan.

Hiroshige Kumamaru (H)

Department of Mechanical Engineering, University of Hyogo, Himeji, 671-2280, Japan.

Itsuro Honda (I)

Department of Mechanical Engineering, University of Hyogo, Himeji, 671-2280, Japan.

Classifications MeSH