Fatigue apparatus for geometrically complex non-standardized specimens

Standard Test Methods (e.g. ASTM, DIN) for materials characterization in general, and for fatigue in particular, do not contemplate specimens with complex geometries, as well as the combination of axial and in-plane bending loads in their methodologies. The present study refers to some patents and the new configuration or configurations of specimens (non-standardized by the status quo of test methods) and a device developed to induce axial and bending combined forces resultants from axial loads applied by any one test equipment (dynamic or monotonic) which possesses such limitation, towards obtaining more realistic results on the fatigue behavior, or even basic mechanical properties, from geometrically complex structures. Motivated by a specific and geometrically complex aeronautic structure (motor-cradle), non-standardized welded tubular specimens made from AISI 4130 steel were fatigue-tested at room temperature, by using a constant amplitude sinusoidal load of 20 Hz frequency, load ratio R = 0.1 with and without the above referred auxiliary fatigue apparatus. The results showed the fatigue apparatus was efficient for introducing higher stress concentration factor at the welded specimen joints, consequently reducing the fatigue strength when compared to other conditions. From the obtained results it is possible to infer that with small modifications the proposed apparatus will be capable to test a great variety of specimen configurations such as: squared tubes and plates with welded or melted junctions, as well as other materials such as aluminum, titanium, composites, polymeric, plastics, etc. © 2009 Bentham Science Publishers Ltd.

Fadiga e corrosão de aço inoxidável Custom 465 de aplicação aeronaútica

Coordenação de Aperfeiçoamento de Pessoal de Nível Superior (CAPES)

Um sistema com um bloco de teflon e um bastão abrasivo para a limpeza da superfície de corte de rebolos

Pós-graduação em Engenharia Mecânica - FEB

Efeito protetivo produzido pela aplicação de um filme de carbono amorfo na superfície de um ferramental para conformação

Pós-graduação em Ciência e Tecnologia de Materiais - FC

Estudo da transformação da austenita retida induzida por deformação, de um aço AISI4340 com estrutura multifásica

Coordenação de Aperfeiçoamento de Pessoal de Nível Superior (CAPES)

Analise mecânica e microestrutural em estruturas tubulares aeronáuticas soldadas de aço ABNT 4130

Airplane Motor Cradles have a complex geometry, since they require different conbinations between different tubes and TIG welded in several angles. In T-25 aircraft and Universal T-27 Tucano (EMBRAER / FAB), besides having to bear the engine balance, these components maintain fixed the nose landing gear in another extremity. They are considered critical to flight safety, and for this reason, the aviation standards are extremely rigid in their production, imposing a zero index” of defects on the final weld metal quality. These structures may be containing an historical of welding repairs, whose effects on their structural integrity are not computed. In this work we analyzed the standardised AISI 4130 steel and the raw steel of tubes to the Airplane Motor Cradles. First of all, microscopy and microanalysis of the base steel, then we analyzed the effects of the TIG weld. Tensile testing was conducted to measure the difference between the mechanical properties of standardised steel and without this treatment

Construção de um equipamento de ensaio de desgaste micro abrasivo por esfera rotativa fixa para análise do desgaste em revestimento duro aplicado por soldagem

Pós-graduação em Engenharia Mecânica - FEIS

Influência do tratamento superficial 3IP na vida em fadiga dos aços ABNT 4340 e 15-5PH para aplicação aeronáutica

Pós-graduação em Engenharia Mecânica - FEG

Fresamento de aço para moldes e matrizes em condições criogênicas

Pós-graduação em Engenharia Mecânica - FEIS

Experimental and numerical analysis of dry contact in the pin on disc test

The reduction of friction and wear in systems presenting metal-to-metal contacts, as in several mechanical components, represents a traditional challenge in tribology. In this context, this work presents a computational study based on the linear Archard's wear law and finite element modeling (FEM), in order to analyze unlubricated sliding wear observed in typical pin on disc tests. Such modeling was developed using finite element software Abaqus® with 3-D deformable geometries and elastic–plastic material behavior for the contact surfaces. Archard's wear model was implemented into a FORTRAN user subroutine (UMESHMOTION) in order to describe sliding wear. Modeling of debris and oxide formation mechanisms was taken into account by the use of a global wear coefficient obtained from experimental measurements. Such implementation considers an incremental computation for surface wear based on the nodal displacements by means of adaptive mesh tools that rearrange local nodal positions. In this way, the worn track was obtained and new surface profile is integrated for mass loss assessments. This work also presents experimental pin on disc tests with AISI 4140 pins on rotating AISI H13 discs with normal loads of 10, 35, 70 and 140 N, which represent, respectively, mild, transition and severe wear regimes, at sliding speed of 0.1 m/s. Numerical and experimental results were compared in terms of wear rate and friction coefficient. Furthermore, in the numerical simulation the stress field distribution and changes in the surface profile across the worn track of the disc were analyzed. The applied numerical formulation has shown to be more appropriate to predict mild wear regime than severe regime, especially due to the shorter running-in period observed in lower loads that characterizes this kind of regime.

Aluminum slurry coatings to replace cadmium for aeronautic applications

Cadmium has been widely used as a coating to provide protection against galvanic corrosion for steels and for its natural lubricity on threaded applications. However, it is a toxic metal and a known carcinogenic agent, which is plated from an aqueous bath containing cyanide salts. For these reasons, the use of cadmium has been banned in Europe for most industrial applications. However, the aerospace industry is still exempt due to the stringent technical and safety requirements associated with aeronautical applications, as an acceptable replacement is yet to be found. Al slurry coatings have been developed as an alternative to replace cadmium coatings. The coatings were deposited on AISI 4340 steel and have been characterized by optical and electron microscopy. Testing included salt fog corrosion exposure, fluid corrosion exposure (immersion), humidity resistance, coating-substrate and paint-coating adhesion, electric conductivity, galvanic corrosion, embrittlement and fatigue. The results indicated that Al slurry coatings are an excellent alternative for Cd replacement.

Caracterización de capas de óxidos en aceros inoxidables austeníticos. Impacto sobre la industria nuclear

Este trabajo tiene como objeto caracterizar las capas de óxido formadas en el acero AISI 316L en función de la deformación del material y de su contenido en Cr a distintas temperaturas. Este acero se utiliza en los internos de las vasijas de los reactores nucleares de agua ligera, y un mejor conocimiento de su proceso de oxidación puede suponer un avance en el desarrollo de los reactores de cuarta generación. Para ello se realizaron ensayos termogravimétricos y se analizaron los resultados con técnicas de microscopía óptica y electrónica, espectrometría y difracción de rayos X. Los resultados obtenidos muestran la similitud en morfología y composición elemental de los óxidos formados en muestras de este acero con distintos grados de deformación y contenido en Cr y las diferencias resultantes en cuanto a la ganancia de masa. Abstract The object of this work is to characterize the oxide layers formed in AISI 316L steel based on the material deformation and its Cr content at various temperatures. This kind of steel is used in the inside elements of the light water nuclear reactor vessels and further knowledge in the oxidation process could mean a greater development in fourth generation reactors. Thermogravimetric tests were undertaken for this purpose, leading to the results analysis with the use of optical and electronic microscopic techniques as well as spectrometry and X–ray diffraction. The obtained results show the resemblance in the morphology and elemental composition of the oxides formed in samples of this steel with different deformation and Cr content degrees. The results also showed differences in the mass gain.

Abrasão de ferro fundido cinzento: aplicação a motores automotivos.

Uma parte significativa das perdas por atrito num motor automotivo resulta da ação de partículas abrasivas. Dentre as fontes possíveis, podem ser citados o próprio meio ambiente - partículas que passam pelo filtro de ar - o desgaste de partes metálicas do motor ou mesmo resíduos de combustão. Essas partículas podem ficar encrustadas em anéis do pistão, ou ficar na interface entre pistão e bloco ou camisa, e são responsáveis por sulcos axiais, na direção do movimento do pistão, observáveis em motores usados. O objetivo deste trabalho foi obter um melhor entendimento dos mecanismos de desgaste relacionados com o sulcamento de camisa/bloco e identificar conjuntos de testes laboratoriais capazes de reproduzi-los sob condições controladas. Amostras de ferro fundido cinzento (FoFo) e de aço AISI 1070 com dureza de matriz próxima daquela encontrada em FoFo (?200HV30) foram submetidas a ensaios de riscamento em tribômetros. Verificou-se que riscos executados com um endentador cônico submetido a cargas na faixa de 20 a 50 mN eram similares aos sulcos observados em camisas ou blocos. Ensaios com outros materiais, como alumínio e latão e mesmo aço de diferentes durezas contribuíram para melhorar o entendimento dos resultados. Não foi observada transição brusca entre mecanismos de abrasão. O cálculo do fator de remoção de material, fab, a partir de perfilometria óptica resultou em valores com dispersão elevada; não foi possível associa-los aos diferentes mecanismos de abrasão observados. Valores obtidos para o coeficiente de atrito no riscamento permitiram fazer uma estimativa inicial de energia gasta nos processos abrasivos do motor.

Mild wear in dry and lubricated sliding systems

A vertical pin on horizontal disc machine has been used to conduct a series of experiments in air under dry and lubricating sliding conditions. For dry sliding low load and speed combinations were chosen to correspond to the mild wear region below the Welsh T1 transition. Lubricated tests were conducted under flooded conditions using Esso Technical White Oil alone and with a 0.1% stearic acid additive, for load and speed ranges that produced substantial amounts of asperity contact and thus a boundary lubricated regime of wear. The test material in all cases was AISI 52100 steel, for unlubricated sliding subjected to loads from 5 to 50 N and a range of speeds from 10-3 to 1.0 ms-1, and for lubricated sliding loads of 50 to 123 N and for speeds of 10-2 to 1.0 ms-1. Unlubricated wear debris was found to be a mixture of -Fe_2O_3 and -Fe. Unlubricated wear was found to occur via a thin film logarithmic oxide growth followed by agglomeration into thicker oxide plateaux 2 to 10 m in thickness. Lubricated wear occurred via thick film diffusion controlled oxide growth producing homogeneous oxide plateaux 0.1 to 0.2 m in thickness. X-ray photoelectron spectroscopy identified the presence of a surface film on pins worn in White Oil with stearic acid, which is thought to be iron stearate. A model has been developed for unlubricated wear based upon the postulated growth of thin film oxides by a logarithmic rate law. The importance of sliding geometry and environment to the dominant wear mechanism has been illustrated.

Análise tribo-termodinâmica da aplicação de nanopartículas de Al2O3 como aditivo lubrificante em compressor hermético de refrigeração

The thermodynamic performance of a refrigeration system can be improved by reducing the compression work by a particular technique for a specific heat removal rate. This study examines the effect of small concentrations of Al2O3 (50 nm) nanoparticles dispersion in the mineral oil based lubricant on the: viscosity, thermal conductivity, and lubrication characteristics as well as the overall performance (based on the Second Law of Thermodynamics) of the refrigerating system using R134a or R600a as refrigerants. The study looked at the influences of variables: i) refrigerant charge (100, 110, 120 and 130 g), ii) rotational speed of the condenser blower (800 and 1100 RPM) and iii) nanoparticle concentration (0.1 and 0.5 g/l) on the system performance based on the Taguchi method in a matrix of L8 trials with the criterion "small irreversibility is better”. They were carried pulldown and cycling tests according to NBR 12866 and NBR 12869, respectively, to evaluate the operational parameters: on-time ratio, cycles per hour, suction and discharge pressures, oil sump temperature, evaporation and condensation temperatures, energy consumption at the set-point, total energy consumption and compressor power. In order to evaluate the nanolubricant characteristics, accelerated tests were performed in a HFRR bench. In each 60 minutes test with nanolubricants at a certain concentration (0, 0.1 and 0.5 g/l), with three replications, the sphere (diameter 6.00 ± 0.05 mm, Ra 0.05 ± 0.005 um, AISI 52100 steel, E = 210 GPa, HRC 62 ± 4) sliding on a flat plate (cast iron FC200, Ra <0.5 ± 0.005 um) in a reciprocating motion with amplitude of 1 mm, frequency 20 Hz and a normal load of 1,96 N. The friction coefficient signals were recorded by sensors coupled to the HFRR system. There was a trend commented bit in the literature: a nanolubricant viscosity reduction at the low nanoparticles concentrations. It was found the dominant trend in the literature: increased thermal conductivity with increasing nanoparticles mass fraction in the base fluid. Another fact observed is the significant thermal conductivity growth of nanolubricant with increasing temperature. The condenser fan rotational speed is the most influential parameter (46.192%) in the refrigerator performance, followed by R600a charge (38.606%). The Al2O3 nanoparticles concentration in the lubricant plays a minor influence on system performance, with 12.44%. The results of power consumption indicates that the nanoparticles addition in the lubricant (0.1 g/L), together with R600a, the refrigerator consumption is reduced of 22% with respect to R134a and POE lubricant. Only the Al2O3 nanoparticles addition in the lubricant results in a consumption reduction of about 5%.