Simulation of a liquid propellant rocket engine manufacturing assembly line utilizing the PFS/PN methodology

Autores/as

  • Jhonatan Ribeiro dos Santos Polytechnic School of the University of São Paulo
  • Eduardo Seiji Suguimoto Miyazato Ferrer Polytechnic School of the University of São Paulo

DOI:

https://doi.org/10.11606/issn.2526-8260.mecatrone.2023.221035

Palabras clave:

Liquid Propellant Rocket Engine, Discrete Event System, Metal Additive Manufacturing, Industry 4.0

Resumen

The system addressed in this paper pertains to an assembly line for liquid propellant rocket engines equipped with turbopump. The challenge involves automating the process of metal 3D printing for the turbopump and combustion chamber, followed by heat treatment for stress relief, X-ray computed tomography inspection, and the subsequent movement of components throughout the factory. To achieve this, the PFS/PN methodology was employed to facilitate a detailed analysis of the system, ensuring control over its inputs and outputs. The system was simulated using the ProModel Discrete Event Simulator, and the results were scrutinized, indicating the robustness of the simulation. Following the Ladder methodology, programming for Programmable Logic Controllers was also developed.

Descargas

Los datos de descarga aún no están disponibles.

Biografía del autor/a

  • Jhonatan Ribeiro dos Santos, Polytechnic School of the University of São Paulo

    Jhonatan Ribeiro dos Santos is a Mechatronics Engineering student at the Polytechnic School of the University of São Paulo, earning a technical degree from SENAI. Noteworthy for his active involvement as a monitor in the "Noite com as Estrelas" project by the Institute of Astronomy, Geophysics, and Atmospheric Sciences (IAG) at USP, Jhonatan combines theoretical knowledge with practical experience. His commitment to community outreach and passion for mechatronics mirrors his dedication to academia. Inspired by the prospect of bridging technology and education, Jhonatan aspires to contribute significantly to the field as he advances in his academic journey.

  • Eduardo Seiji Suguimoto Miyazato Ferrer, Polytechnic School of the University of São Paulo

    Eduardo Seiji Suguimoto Miyazato Ferrer is a Mechatronics Engineering student at the Polytechnic School of the University of São Paulo, holding a prior degree in Molecular Sciences, also from the University of São Paulo. He was a member of the motorsports and the rocket team, focusing on the design, simulation, manufacturing, and testing of power transmission systems, as well as solid and hybrid rocket engines. Currently, he is involved in research at the Combustion and Propulsion Laboratory of the National Institute for Space Research. Eduardo is deeply passionate about aerospace and automotive engineering, harboring a dream of contributing to humanity's return to the Moon and journey to Mars.

Referencias

D SYSTEMS. German Aerospace Center (DLR) Designs Liquid Rocket Engine Injector with 3D Systems. 2020. Retrieved from https://www.3dsystems.com/customer-stories/german-aerospace-center-dlr-designs-liquid-rocket-engine-injector-3d-systems

BAO, B., ZHOU, L., WANG, J., & XIAO, S. Application and challenges of additive manufacturing in the liquid rocket engines. 2022. SPIE-Intl Soc Optical Eng, 240.

BECK et al. Rocket Engine Thrust Chamber, Injector, and Turbopump. 2019.

BLAKEY-MILNER, B., GRADL, P., SNEDDEN, G., BROOKS, M., PITOT, J., LOPEZ, E., ... & PLESSIS, A. Metal additive manufacturing in aerospace: A review. Materials and Design, 2019, 209.

CARDOSO, J.; VALETTE, R. Redes de Petri. Florianópolis, 1997.

GRADL, P., MIRELES, O., & ANDREWS, N. Introduction to Additive Manufacturing for Propulsion Systems.

MORIYA, S., INOUE, T., SASAKI, M., NAKAMOTO, T., KIMURA, T., NOMURA, N., ... & MASUDA, I. Feasibility Study on Additive Manufacturing of Liquid Rocket Combustion Chamber. TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN, 2020, 16(3), 261–266.

MIYAGI, P.E. Controle Programável: Fundamentos do Controle de Sistemas a Eventos Discretos. Brasil: Blucher, 1996, 206p.

REI, M. Rocket Engine Made by Additive Manufacturing. IHI Corporation, Tech. Rep, 2018.

SALMI, B. 3D-Printing a Rocket. IEEE Spectrum, 2019.

SOLLER, S., & ARIANE GROUP. Development of Liquid Rocket Engine Injectors Using Additive Manufacturing. 2015. Retrieved from https://www.researchgate.net/publication/280561310

SOLLER, S., BARATA, A., BEYER, S., DAHLHAUS, A., GUICHARD, D., HUMBERT, E., ... & ZEISS, W. Selective Laser Melting (Slm) Of Inconel 718 And Stainless Steel Injectors For Liquid Rocket Engines. 2016. Retrieved from https://www.researchgate.net/publication/303331194

YUSUF, S. M., CUTLER, S., & GAO, N. Review: The impact of metal additive manufacturing on the aerospace industry, 2019.

Descargas

Publicado

2024-02-22

Número

Vol. 6 Núm. 1 (2023)

Sección

Artigos

Licencia

Derechos de autor 2023 Jhonatan Ribeiro dos Santos, Eduardo Seiji Suguimoto Miyazato Ferrer

Creative Commons License

Esta obra está bajo una licencia internacional Creative Commons Atribución-NoComercial-CompartirIgual 4.0.

Cómo citar

Simulation of a liquid propellant rocket engine manufacturing assembly line utilizing the PFS/PN methodology. (2024). Mecatrone, 6(1), 1-18. https://doi.org/10.11606/issn.2526-8260.mecatrone.2023.221035