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Desenvolvimento de um ve?culo a?reo n?o tripulado com sustenta??o e propuls?o h?brida

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Previous issue date: 2018-01-31 / Este trabalho busca apresentar o desenvolvimento de um Ve?culo A?reo n?o Tripulado (VANT) duplamente h?brido, capaz de conciliar as vantagens de dois tipos de aeronaves (asa fixa e multirotor), utilizando motores a combust?o e el?tricos para a propuls?o e para a sustenta??o em voo a asa e o multirotor, capaz de decolar e pousar verticalmente, executar voos lentos ou parados, tamb?m executar voo horizontal com sustenta??o pela asa e propuls?o por motor a combust?o que garante maior autonomia. Para a realiza??o desse estudo foram desenvolvidas tr?s aeronaves, inicialmente uma asa voadora e um multirotor tric?ptero com objetivo de analisar separadamente cada tipo de aeronave, ap?s os testes e an?lises foi desenvolvido um VANT duplamente h?brido, uma asa voadora e um hexac?ptero, propuls?o por motores el?tricos e ? combust?o. A partir dos testes e c?lculos te?ricos da aeronave h?brida observou-se a viabilidade de um novo tipo de aeronave, com caracter?sticas pr?prias, capaz de conciliar as vantagens de dois tipos de aeronaves. / This work aims to present the development of a double hybrid unmanned aerial vehicle (UAV), capable of reconciling the advantages of two types of aircraft (fixed wing and multirotor), using combustion and electric motors for propulsion and in flight support the wing and the multirotor, able to take off and land vertically, to perform slow or stopped flights, also to execute horizontal flight with support by the wing and propulsion by combustion engine that guarantees greater autonomy. In order to carry out this study, three aircraft were developed, initially a flying wing and a tricopter multirotor with the objective of analyzing separately each type of aircraft, after the tests and analyzes a double hybrid VANT was developed, a flying wing and a hexacopter, motor propulsion electrical and combustion. From the theoretical tests and calculations of the hybrid aircraft, the viability of a new type of aircraft, with its own characteristics, was able to reconcile the advantages of two types of aircraft.

Identiferoai:union.ndltd.org:IBICT/oai:repositorio.ufrn.br:123456789/24977
Date31 January 2018
CreatorsLucena, Alysson Nascimento de
Contributors02306444498, Coutinho, Karilany Dantas, 03557257460, Bessa, Wallace Moreira, 05362438751, Amorim J?nior, Wanderley Ferreira de, 87244152434, Freire J?nior, Raimundo Carlos Silverio
PublisherPROGRAMA DE P?S-GRADUA??O EM ENGENHARIA MEC?NICA, UFRN, Brasil
Source SetsIBICT Brazilian ETDs
LanguagePortuguese
Detected LanguageEnglish
Typeinfo:eu-repo/semantics/publishedVersion, info:eu-repo/semantics/masterThesis
Sourcereponame:Repositório Institucional da UFRN, instname:Universidade Federal do Rio Grande do Norte, instacron:UFRN
Rightsinfo:eu-repo/semantics/openAccess

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