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Design, manufacturing and operation of a small turbojet-engine for research purposes

Author

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  • Benini, Ernesto
  • Giacometti, Stefano

Abstract

A research project is on going, at the University of Padova, to develop a 200Â N static-thrust engine to be used for both didactic and research activities. This paper describes in detail all the phases required to set-up such an engine, including design, manufacturing and operation. The jet engine features a single-stage centrifugal compressor developing 2.66:1 compression ratio at 60,000Â rpm, a direct-flow annular combustion chamber and a single-stage axial turbine with 950Â K turbine-inlet temperature (TIT). All the design and manufacturing details are provided, as well as the operation procedure together with experimental results.

Suggested Citation

  • Benini, Ernesto & Giacometti, Stefano, 2007. "Design, manufacturing and operation of a small turbojet-engine for research purposes," Applied Energy, Elsevier, vol. 84(11), pages 1102-1116, November.
    • Handle: RePEc:eee:appene:v:84:y:2007:i:11:p:1102-1116
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    Cited by:

    1. Sogut, M. Ziya, 2020. "Assessment of small scale turbojet engine considering environmental and thermodynamics performance for flight processes," Energy, Elsevier, vol. 200(C).
    2. Aygun, Hakan & Cilgin, Mehmet Emin & Turan, Onder, 2021. "Exergo-sustainability indicators of a target drone engine at dynamic loads," Energy, Elsevier, vol. 221(C).
    3. Yurdusevimli Metin, Ece & Aygün, Hakan, 2019. "Energy and power aspects of an experimental target drone engine at non-linear controller loads," Energy, Elsevier, vol. 185(C), pages 981-993.
    4. Zhao, Yong-Ping & Hu, Qian-Kun & Xu, Jian-Guo & Li, Bing & Huang, Gong & Pan, Ying-Ting, 2018. "A robust extreme learning machine for modeling a small-scale turbojet engine," Applied Energy, Elsevier, vol. 218(C), pages 22-35.

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