Diseño y construcción de un TURBOEJE

Authors

  • Arnold Escobar Instituto Militar Aernáutico
  • M. Cabrera Instituto Militar Aernáutico
  • F. Ramírez Instituto Militar Aernáutico
  • J. Zapata Instituto Militar Aernáutico

DOI:

https://doi.org/10.18667/cienciaypoderaereo.58

Keywords:

Turboeje, flujo másico, potencia, rendimiento, poder calorífico, relación de compresión, turbina de impulso

Abstract

This study focuses on the design and construction of a jet engine which uses its power to drive a shaft connected to an electrical generator. This turbo-shaft engine uses natural gas as fu el, reducing costs in electricity generation approximately 70% compared to conventional suppliers.

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Author Biographies

  • Arnold Escobar, Instituto Militar Aernáutico

    Instituto Militar Aeronáutico. Departamento de Investigación FAC. Universidad de San Buenaventura, grupo de investigación GIMOC categoria B COLCIENCIAS.

  • M. Cabrera, Instituto Militar Aernáutico

    Universidad de San Buenaventura grupo de investigación GIMOC categoria B COLCIENCIAS

  • F. Ramírez, Instituto Militar Aernáutico

    Universidad de San Buenaventura grupo de investigación GIMOC categoria B COLCIENCIAS

  • J. Zapata, Instituto Militar Aernáutico

    Universidad de San Buenaventura grupo de investigación GIMOC categoria B COLCIENCIAS

References

ESCOBAR, A. Metodología de diseño para Turborreactores de bajo flujo másico. Bogotá. 2005.

http://www.soliclima.com/termoelectrica.html

http:/ /tha les.cica .es/rd/Recu rsos/rd99/ ed99-0226-011.capitulo3.html

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Published

2008-01-01

Issue

Vol. 3 No. 1 (2008): Enero - Diciembre

Section

Artículos

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How to Cite

Diseño y construcción de un TURBOEJE. (2008). Ciencia Y Poder Aéreo, 3(1), 16-20. https://doi.org/10.18667/cienciaypoderaereo.58