DESIGN AND DEVELOPMENT OF A 70 N THRUST CLASS TURBOJET ENGINE

Autores

  • P. E. Trazzi

DOI:

https://doi.org/10.5380/reterm.v3i1.3484

Palavras-chave:

gas turbines, jet propulsion, centrifugal compressors, combustors, axial flow turbines.

Resumo

Small turbojet engines are being used for propulsion of radio-controlled model airplanes. The design and development of the model 505 small jet engine are reviewed. Small size gas turbines present special design and construction difficulties, some of which are addressed; design choices leading to the final configuration are discussed. Aero-thermodynamic aspects are covered along with experimental data when available. The unit is comprised of a radial compressor, an annular combustion chamber, and an axial turbine plus accessories; details on these components and on production aspects are presented.

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Publicado

2004-06-30

Como Citar

Trazzi, P. E. (2004). DESIGN AND DEVELOPMENT OF A 70 N THRUST CLASS TURBOJET ENGINE. Revista Da Engenharia Térmica, 3(1), 09–14. https://doi.org/10.5380/reterm.v3i1.3484

Edição

v. 3 n. 1 (2004)

Seção

Technology

Licença

Direitos Autorais para artigos publicados nesta revista são do autor, com direitos de primeira publicação para a revista. Em virtude da aparecerem nesta revista de acesso público, os artigos são de uso gratuito, com atribuições próprias, em aplicações educacionais e não-comerciais.