Orientador: Antonio Jorge Abdalla / Coorientador: Marcelo dos Santos Pereira / Banca: Tomaz Manabu Hashimoto / Banca: Marcelino Pereira do Nascimento / Banca: Miguel Justino Ribeiro Barbosa / Banca: Dilermando Nagle Travessa / Resumo: Este trabalho tem como objetivo caracterizar mecanica e metalograficamente, juntas soldadas de chapas finas em aço Maraging 300, submetidas a até três reparos, usadas na fabricação de envelopes motores foguete a propelente sólido desenvolvidos no Instituto de Aeronáutica e Espaço (IAE) em atendimento às necessidades de sua gama de lançadores. O envelope motor atua como elemento estrutural e também possui a função primária de suportar a pressão de trabalho durante a queima do propelente. Atualmente, o envelope motor é fabricado em aço 300M-ESR e o IAE tomou a decisão de substituí-lo pelo aço Maraging 300. Em função dos processos existentes no Instituto, neste trabalho utilizaram-se os processos de soldagem Plasma Arc Welding - PAW com a técnica keyhole e Gas Tungsten Arc Welding - GTAW, ambos em passe único, com metal de adição. Antes de serem submetidas aos ensaios, as juntas passaram por inspeção não destrutiva de acordo com os critérios da norma AWS D17.1. Os reparos foram feitos de forma manual e processo GTAW. Amostras da junta soldada e reparadas foram submetidas a ensaios de tração, dureza Vickers (HV) por microindentações, análises químicas, análises metalográficas e fractográficas. Corpos de prova dos cordões adjacentes aos reparos também foram avaliados. Os resultados mostram que após a solda e reparos e o tratamento térmico de solubilização e envelhecimento, a zona fundida e a região da linha de fusão da solda apresentam uma dureza abaixo das outras regiões afetadas termicamente. Para as condições da solda sem reparo e reparadas, o processo PAW apresentou um valor menor de dureza em todas estas regiões com relação ao processo GTAW. As análises da superfície dos corpos de prova soldados rompidos indicam o predomínio de um processo de ruptura iniciado próximo à linha de fusão da solda e que se propaga em direção ao interior do ... (Resumo completo, clicar acesso eletrônico abaixo) / Abstract: This work aims at mechanic and metallographic characterization of Maraging 300 welded joints sheets, submitted to up to three repairs, used for the fabrication of solid propellant rocket motors at the Institute of Aeronautics and Space - IAE as to comply with its range of launchers. The rocket motor is a structural part and also has the primary function of supporting the nominal pressure during the propellant burning. At present, the rocket motor is fabricated in 300M-ESR steel and IAE has decided to replace such a steel for the Maraging 300 one. Due to IAE's existing processes, Plasma Arc Welding - PAW with the keyhole technique and the Gas Tungsten Arc Welding - GTAW have been used, both single-pass welding with filler. Before they have been submitted to the tests, the joints went through non-destructive inspection according to AWS D17.1 Standard. Manual repairs and GTAW process have been made. Samples of the welded and repaired joints were submitted to tensile testing, Vickers hardness, chemical analysis, fractrographic and metallographic analysis. Body tests of the beads adjacent to the repairs have also been assessed. Results show that after welding, repairs and solubilization and aging heating treatment, the melted zone as well as the weld joins lines zone present hardness below other heat affected zones. As for the conditions of the non-repaired and repaired welds, the PAW process has demonstrated lower hardness values in all zones in what regards the GTAW process. The welded and fractured body tests surfaces analysis indicate the predominance of a fracture process started next to the weld joins lines which goes towards the bead interior. The nature of the fracture has shown the predominance of dimples. The GTAW welded body tests presented higher mechanical strength than that of the PAW process. Similarly, the PAW welded body tests obtained from the beads of the zones ... (Complete abstract click electronic access below) / Doutor

Spot friction welding (SFW) was performed on ultra high strength steel (UHSS) steel sheet commonly used in automobile manufacturing. Alloys studied included DP780, DP780EG, DP980, and DF140T sheet steel of varying thickness from 1.2 mm to 1.4 mm. Welding was accomplished using a PCBN standard tool. Weld strengths were then compared to a proposed AWS standard. Initial hardness readings were taken in cross sectioned samples. Grain structure in a SFW is presented. Resistance spot welds were created in three steels. This study focuses on the strength of SFW joints as compared to traditional resistance spot welding (RSW) in welding like materials to one another. Cycle times of SFW were also evaluated and compared to production rate cycle times of RSW.

Design of a new steel structure administrative building in Zlín. Structure is consist of three parts. The part A is designed of three fields in the transverse direction and five fields in the longitudinal direction. This part is two-storey. The part B is designed of two fields in the transverse direction and three fields in the longitudinal direction. This part is six-storey (five-storey). The part C is designed of two fields in the transverse direction and five fields in the longitudinal direction. This part is four-storey (three, two-storey). In both directions in all parts of the building is the distance between the columns in all fields of 6,0 meters. Structural elevation of all floors is 3,5 meters. Shape and dimension design. Fixed, utility, climatic load. The purpose is confrontation of inner forces and dimensioning of main supporting elements in three variations of structure. Comparsion of variations. More detailed static calculation, drawings for the selected variant. Detailed drawings for part of building.