Investigation of Thermal Behavior and Orifice Flow Characteristics of Aeronautic Hydraulic Servoproportional Valve Spool-Sleeve Structure with Numerical Simulations
dc.authorid | 0000-0003-3385-5577 | en_US |
dc.authorid | 0000-0003-3188-2854 | en_US |
dc.contributor.author | Şen, Soner | |
dc.contributor.author | Şimşek, Rıza Deniz | |
dc.date.accessioned | 2023-08-05T08:37:11Z | |
dc.date.available | 2023-08-05T08:37:11Z | |
dc.date.issued | 2022 Aralık | en_US |
dc.department | Selçuk Üniversitesi, Yüksek Okullar, Sivil Havacılık Yüksekokulu | en_US |
dc.description.abstract | In this study, the mechanical behavior under highest thermal conditions and flow characteristics of the hydraulic fluid of the servo-characterized proportional valve, which is one of the indispensable components of the aviation industry and used for hydraulic flow control, were investigated numerically. In the simulations, 50, 75 and 100 °C were selected as temperatures, and 0.2 mm, 0.6 mm and 1.2 mm spool stroke openings were used for hydrodynamic flow. Simulations were carried out for a pressure difference of 35 bar. As a result of the analysis, it was observed that there was no restriction in the movement of the spool-sleeve structure for a temperature of 75°C, excessive friction occurred in the spool-sleeve structure at 100°C and the movement was restricted. In addition, it can be said that hydraulic turbulences are effective in dispersing polluting particulate matter for all three spool strokes at a pressure difference of 35 bar. | en_US |
dc.identifier.citation | Şen, S., Şimşek, R. D., (2022). Investigation of Thermal Behavior and Orifice Flow Characteristics of Aeronautic Hydraulic Servoproportional Valve Spool-Sleeve Structure with Numerical Simulations. International Journal of Aeronautics and Astronautics, 3(3), 120-131. DOI: 10.55212/ijaa.1208520 | en_US |
dc.identifier.doi | 10.55212/ijaa.1208520 | en_US |
dc.identifier.endpage | 131 | en_US |
dc.identifier.issn | 2757-6574 | en_US |
dc.identifier.issue | 3 | en_US |
dc.identifier.startpage | 120 | en_US |
dc.identifier.uri | https://hdl.handle.net/20.500.12395/49170 | |
dc.identifier.volume | 3 | en_US |
dc.institutionauthor | Şen, Soner | |
dc.institutionauthor | Şimşek, Rıza Deniz | |
dc.language.iso | en | en_US |
dc.publisher | Selçuk Üniversitesi | en_US |
dc.relation.ispartof | International Journal of Aeronautics and Astronautics | en_US |
dc.relation.publicationcategory | Makale - Uluslararası Hakemli Dergi - Kurum Öğretim Elemanı | en_US |
dc.rights | info:eu-repo/semantics/openAccess | en_US |
dc.selcuk | 20240510_oaig | en_US |
dc.subject | Hydraulic orifice | en_US |
dc.subject | Hydraulic turbulence | en_US |
dc.subject | Jet-flow | en_US |
dc.subject | Thermal stress | en_US |
dc.subject | Servo-proportional valve | en_US |
dc.title | Investigation of Thermal Behavior and Orifice Flow Characteristics of Aeronautic Hydraulic Servoproportional Valve Spool-Sleeve Structure with Numerical Simulations | en_US |
dc.type | Article | en_US |