Small scale gas turbine combustor sizing

Authors

  • Michal Czarnecki Rzeszow University of Technology

DOI:

https://doi.org/10.24136/atest.2019.032

Keywords:

gas turbine, micro scale, flame tube, distribution

Abstract

Presented article is focused on initial design of small scale combustors for micro scale jest engines. In comparison to the full size equivalent, small combustor are design and manufactured in experimental way. To try building universal numeric model for micro size design is important to acquire as many data as possible to identify boundary conditions for a model. Major advantage of analyzing different design is possibility to quick building prototype design without investigating complex process of combustion.

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References

Czarnecki, M., Olsen, J. , Influence of selected parameters on micro gas turbine compressor design, Journal of KONES, 2017 vol. 24 p.45-52,

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Скубачевский Г.С.,. Авиационные газотурбинные двигатели. Конструкция и расчет деталей. Машиностроение, 1969.

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Published

2019-02-28

How to Cite

Czarnecki, M. (2019). Small scale gas turbine combustor sizing. AUTOBUSY – Technika, Eksploatacja, Systemy Transportowe, 20(1-2), 180–184. https://doi.org/10.24136/atest.2019.032

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Articles