Publication detail

Inlet shape optimization of pneumobil engine pneumatic cylinder using CFD analysis

ČERNÁK, M. MICHALEC, M. VALENA, M. RANUŠA, M.

Original Title

Inlet shape optimization of pneumobil engine pneumatic cylinder using CFD analysis

Type

conference paper

Language

English

Original Abstract

The aim of this study is to minimize minor losses in cap-end ports of a pneumatic cylinder used in pneumobil vehicle engine. Six geometry arrangements of intake ports,including the currently used version, were designed assuming conventional machining technology.Boundary conditions for the analysis were acquired from experimental measurement. The airflow was analyzed by 3D stationary CFD analysis in ANSYS Fluent for all designs. Pressuredrop was used as the evaluation criteria. Two best configurations according to the obtainedresults were optimized using ANSYS Fluent Adjoint Solver. The pressure drop was reducedby 81.1% using this method. The obtained results will be used for design of solid geometrycustomized for production by lost wax casting process.

Keywords

pneumatic cylinder, boundary conditions, ANSYS Fluent

Authors

ČERNÁK, M.; MICHALEC, M.; VALENA, M.; RANUŠA, M.

Released

1. 6. 2021

Publisher

IOP Publishing

ISBN

1742-6588

Periodical

Journal of Physics: Conference Series

Year of study

1935

Number

1

State

United Kingdom of Great Britain and Northern Ireland

Pages from

012011

Pages to

012011

Pages count

8

URL

Full text in the Digital Library

BibTex

@inproceedings{BUT171725,
  author="Martin {Černák} and Michal {Michalec} and Martin {Valena} and Matúš {Ranuša}",
  title="Inlet shape optimization of pneumobil engine pneumatic cylinder using CFD analysis",
  booktitle="Journal of Physics: Conference Series",
  year="2021",
  series="1935",
  journal="Journal of Physics: Conference Series",
  volume="1935",
  number="1",
  pages="012011--012011",
  publisher="IOP Publishing",
  doi="10.1088/1742-6596/1935/1/012011",
  issn="1742-6588",
  url="https://iopscience.iop.org/article/10.1088/1742-6596/1935/1/012011"
}