Diseño preliminar de un rotor de onda para motores con microturbina

  • Gina P. Pérez B. Universidad de San Buenaventura
  • Arnold Escobar G. Instituto Militar Aeronáutico
Palabras clave: Termodinamica, cámara de combustion, rotor de onda

Resumen

Este trabajo presenta un analisis preliminar sobre los beneficios de ia implementacion de un rotor de onda en una micro-turbina convencional. Este estudio se enfoca en la consecución de un punto de disefio por medio de cálculos térmicos para así lograr una geometría adecuada, la cual podra ser evaluada por medio de Dinámica de Flujo Computacional CFD para determinar la viabilidad de la implementacion de este dispositive en un motor con micro-turbina a gas de 30 lb, de empuje.

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Biografía del autor/a

Gina P. Pérez B., Universidad de San Buenaventura

Grupo de investigación motor combustión GIMOC categoría B colciencias, Universidad de San Buenaventura- Bogotá

Arnold Escobar G., Instituto Militar Aeronáutico

Grupo de investigación en tecnología y desarrollo en logística y seguridad aérea, GITELS registrado en Colciencias, Instituto Militar Aeronáutico- Fuerza Aérea Colombiana

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Cómo citar
Pérez B., G., & Escobar G., A. (2009). Diseño preliminar de un rotor de onda para motores con microturbina. Ciencia Y Poder Aéreo, 4(1), 38-41. https://doi.org/10.18667/cienciaypoderaereo.53
Publicado: 2009-01-01
Sección
Tecnología