Análise estrutural de uma torre tubular sob acção do vento

Com a realização deste trabalho, pretende-se essencialmente dar a conhecer a influência que a acção do vento possui no dimensionamento de determinadas estruturas, neste caso específico, em torres tubulares de telecomunicações. É por todos sabido, da importância de um capaz e evoluído sistema de comunicações, no desenvolvimento sustentado do mundo moderno. Nesse sentido, o avanço galopante, principalmente nas últimas duas décadas, das tecnologias de Telecomunicações, implicou uma rápida resposta em consonância na implantação e proliferação de infraestruturas de suporte aos equipamentos dessas tecnologias. Assim, a estrutura em forma de torre tubular, entre as demais variadas secções que as constituem, foi adquirindo preponderância neste campo, constituindo a mais vasta utilização de estruturas de suporte aos equipamentos de telecomunicações, nomeadamente em meios rurais, onde escasseiam edificações com alturas suficientes para fazer face às necessidades das operadoras licenciadas para os devidos efeitos. Será efectuada uma breve descrição sobre as diversas e mais comuns tipologias de torres utilizadas no âmbito do suporte de equipamentos de telecomunicações. Descreve-se, em forma de relatório e levantamento fotográfico, a ocorrência do colapso de uma torre tubular de telecomunicações. Por último, e na sequência do incidente referido no ponto anterior, será efectuada com detalhe, a análise estrutural da torre tubular que foi instalada na posição da anteriormente instalada.

Design optimization of cruciform specimens for biaxial fatigue loading

In order to correctly assess the biaxial fatigue material properties one must experimentally test different load conditions and stress levels. With the rise of new in-plane biaxial fatigue testing machines, using smaller and more efficient electrical motors, instead of the conventional hydraulic machines, it is necessary to reduce the specimen size and to ensure that the specimen geometry is appropriated for the load capacity installed. At the present time there are no standard specimen’s geometries and the indications on literature how to design an efficient test specimen are insufficient. The main goal of this paper is to present the methodology on how to obtain an optimal cruciform specimen geometry, with thickness reduction in the gauge area, appropriated for fatigue crack initiation, as a function of the base material sheet thickness used to build the specimen. The geometry is optimized for maximum stress using several parameters, ensuring that in the gauge area the stress is uniform and maximum with two limit phase shift loading conditions. Therefore the fatigue damage will always initiate on the center of the specimen, avoiding failure outside this region. Using the Renard Series of preferred numbers for the base material sheet thickness as a reference, the reaming geometry parameters are optimized using a derivative-free methodology, called direct multi search (DMS) method. The final optimal geometry as a function of the base material sheet thickness is proposed, as a guide line for cruciform specimens design, and as a possible contribution for a future standard on in-plane biaxial fatigue tests. © 2014, Gruppo Italiano Frattura. All rights reserved.

Optimization of cruciform specimens for biaxial fatigue loading with direct multi search

In order to correctly assess the biaxial fatigue material properties one must experimentally test different load conditions and stress levels. With the rise of new in-plane biaxial fatigue testing machines, using smaller and more efficient electrical motors, instead of the conventional hydraulic machines, it is necessary to reduce the specimen size and to ensure that the specimen geometry is appropriate for the load capacity installed. At the present time there are no standard specimen's geometries and the indications on literature how to design an efficient test specimen are insufficient. The main goal of this paper is to present the methodology on how to obtain an optimal cruciform specimen geometry, with thickness reduction in the gauge area, appropriate for fatigue crack initiation, as a function of the base material sheet thickness used to build the specimen. The geometry is optimized for maximum stress using several parameters, ensuring that in the gauge area the stress distributions on the loading directions are uniform and maximum with two limit phase shift loading conditions (delta = 0 degrees and (delta = 180 degrees). Therefore the fatigue damage will always initiate on the center of the specimen, avoiding failure outside this region. Using the Renard Series of preferred numbers for the base material sheet thickness as a reference, the reaming geometry parameters are optimized using a derivative-free methodology, called direct multi search (DMS) method. The final optimal geometry as a function of the base material sheet thickness is proposed, as a guide line for cruciform specimens design, and as a possible contribution for a future standard on in-plane biaxial fatigue tests