981 resultados para Wear-Fatigue-Lubrication-Interaction, Grinding, Inspection, Rail-Wheel Replacements


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Coordenação de Aperfeiçoamento de Pessoal de Nível Superior (CAPES)

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Coordenação de Aperfeiçoamento de Pessoal de Nível Superior (CAPES)

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Coordenação de Aperfeiçoamento de Pessoal de Nível Superior (CAPES)

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Coordenação de Aperfeiçoamento de Pessoal de Nível Superior (CAPES)

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Pós-graduação em Engenharia Mecânica - FEB

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Pós-graduação em Engenharia Mecânica - FEG

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This study attempted to observe the performance of three types of diamonds, two natural and one synthetic, to determine which features longer life and greater wear than the others. The methodology employed in this study was to dressed an aluminum oxide grinding wheel, and every twenty paces with a advance of depth dressing of 40 µm per passes, take an image of the tip in a horizontal position and the other in the vertical position of this diamond in a stereoscopic. Thereafter, the dresser was replaced in the rectifier to conduct a new dressing. The criteria to completion of the test was the spark generated by the grinding wheel contact with the base of the dresser, which indicates the end of the contact with the diamond wheel. After the tests, was calculated the areas worn of each diamond in accordance with each image obtained through the aid of a graphics software. The data were then arranged in graphs.

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Coordenação de Aperfeiçoamento de Pessoal de Nível Superior (CAPES)

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This project was originated from the national aircraft industry requirements to reduce the use of coated materials with electroplated chromium or cadmium that produce waste, which is harmful to health or the environment. The selected material is a Custom 465 stainless steel used in the aeronautical field due to its high mechanical strength. Considering the load sustained by the wheel axis of the landing gear, the Custom 465 is tested in axial fatigue. The objective is to compare the behavior of the Custom 465 with plated AISI 4340 steel coated with cadmium. X-ray diffraction method was used to determine the residual stress field induced by shot peening.

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This project was originated from the national aircraft industry requirements to reduce the use of coated materials with electroplated chromium or cadmium that produce waste, which is harmful to health or the environment. The selected material is a Custom 465 stainless steel used in the aeronautical field due to its high mechanical strength. Considering the load sustained by the wheel axis of the landing gear, the Custom 465 was tested in axial fatigue. The objective is to compare the behavior of the Custom 465 stainless steel with plated AISI 4340 steel coated with cadmium. Fractographic analysis was conducted using scanning electron microscopy. X-ray diffraction method was used to determine the residual stress field induced by shot peening.

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Pós-graduação em Engenharia Elétrica - FEB

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Fundação de Amparo à Pesquisa do Estado de São Paulo (FAPESP)

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Pós-graduação em Engenharia Mecânica - FEG