Resumen:
El presente proyecto describe las etapas de análisis, diseño e implementación de un
sistema electrónico para realizar pruebas de funcionamiento del motor ROTAX 912 ULS
del avión ultraligero FOX VECTOR V6 que se encuentra en el Centro de Investigación
y Desarrollo de la Fuerza Aérea Ecuatoriana (CIDFAE).
El sistema electrónico que desarrollar recibe la denominación de Banco de Pruebas,
adquiere señales físicas como temperatura, presión, nivel y revoluciones por minuto
(RPM’s), generadas por el sistema de propulsión (motor), las variables adquiridas se
digitalizan, empacan y transmiten a una interfaz hombre-máquina (HMI) para que el
operador pueda evaluar el funcionamiento de los componentes del sistema de propulsión.
La adquisición y transmisión de datos se realiza en tiempo real y de manera determinista.
En la HMI, los valores recibidos se almacenan en archivos planos. Los archivos planos
se utilizan para analizar el comportamiento de los componentes en pruebas operacionales
previas.
Este documento contiene toda la información necesaria que explica de forma detallada
como se llevó y se desarrolló los componentes de hardware y software.
DESCRIPTORES:
Diseño, Control, FPGA, Sistema de Propulsión, Comunicación, Programación.
Descripción:
This project describes the stages of analysis, design and implementation of an
electronic system to perform tests of the ROTAX 912 ULS engine of the ultralight aircraft
FOX VECTOR V6 that is in the Research and Development Center of the Ecuadorian
Air Force (CIDFAE).
The electronic system to be developed receives the denomination of Test Bank,
acquires physical signals such as temperature, pressure and revolutions per minute
(RPMs), generated by the propulsion system (engine), the acquired variables are
digitized, packaged and transmitted to an Interface Man Machine (HMI) so that the
operator can assess the operation of the components of the propulsion system. The
acquisition and transmission of data is done in real time and deterministically. In the HMI
the received values are stored in flat files. Flat files are used to analyze the behavior of
components in previous operational tests.
This document contains all the necessary information that explains in detail how the
hardware and software components were carried and developed.
KEY WORDS:
Design, Control, FPGA, Propulsion System, Communication, Programming. This project describes the stages of analysis, design and implementation of an
electronic system to perform tests of the ROTAX 912 ULS engine of the ultralight aircraft
FOX VECTOR V6 that is in the Research and Development Center of the Ecuadorian
Air Force (CIDFAE).
The electronic system to be developed receives the denomination of Test Bank,
acquires physical signals such as temperature, pressure and revolutions per minute
(RPMs), generated by the propulsion system (engine), the acquired variables are
digitized, packaged and transmitted to an Interface Man Machine (HMI) so that the
operator can assess the operation of the components of the propulsion system. The
acquisition and transmission of data is done in real time and deterministically. In the HMI
the received values are stored in flat files. Flat files are used to analyze the behavior of
components in previous operational tests.
This document contains all the necessary information that explains in detail how the
hardware and software components were carried and developed.
KEY WORDS:
Design, Control, FPGA, Propulsion System, Communication, Programming.
Excepto si se señala otra cosa, la licencia del ítem se describe como openAccess