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DISEÑO E IMPLEMENTACIÓN DE UN BANCO DE PRUEBAS VIRTUAL PARA EL MOTOR ROTAX 912 ULS DEL AVIÓN ULTRALIGERO FOX VECTOR V6 DE LA FUERZA AÉREA ECUATORIANA

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dc.contributor.advisor MORALES ARÉVALO, FLAVIO DAVID
dc.contributor.author SOLINA ARAUJO, JUAN MANUEL
dc.date.accessioned 2018-05-23T01:13:50Z
dc.date.available 2018-05-23T01:13:50Z
dc.date.issued 2018
dc.identifier.citation Solina Araujo, Juan Manuel (2018) Diseño E Implementación De Un Banco De Pruebas Virtual Para El Motor Rotax 912 Uls Del Avión Ultraligero Fox Vector V6 De La Fuerza Aérea Ecuatoriana Quito UISRAEL, ELECTRÓNICA DIGITAL Y TELECOMUNICACIONES Quito: Universidad Israel 2018, 144p. MG. FLAVIO DAVID MORALES ARÉVALO UISRAEL-EC-EDTL-378.242-2018-018 es_ES
dc.identifier.issn UISRAEL-EC-ELDT-378.242-2018-018
dc.identifier.uri http://repositorio.uisrael.edu.ec/handle/47000/1573
dc.description 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. es_ES
dc.description.abstract 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. es_ES
dc.description.sponsorship 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. es_ES
dc.format.extent 144p. es_ES
dc.language.iso spa es_ES
dc.publisher Quito es_ES
dc.relation.ispartofseries ELDT;018
dc.rights openAccess es_ES
dc.rights.uri http://creativecommons.org/licenses/by-nc-sa/3.0/ec/ es_ES
dc.subject Design, es_ES
dc.subject Control, FPGA, es_ES
dc.subject Propulsion System, es_ES
dc.subject Communication, Programming. es_ES
dc.subject.other Electrónica es_ES
dc.subject.other Digital es_ES
dc.title DISEÑO E IMPLEMENTACIÓN DE UN BANCO DE PRUEBAS VIRTUAL PARA EL MOTOR ROTAX 912 ULS DEL AVIÓN ULTRALIGERO FOX VECTOR V6 DE LA FUERZA AÉREA ECUATORIANA es_ES
dc.type bachelorThesis es_ES


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