Fatigue crack growth of Al 7475 T761 under constant and variable amplitude loading

Experimental programs in constant and variable amplitude loading were performed to obtain a x N curves and to study retardation in fatigue crack growth due to overloads. The main aim of this research program was to analyse the effect of overload ratio and number of overload peaks. The effect of underloads, before and after the overload blocks was also studied. The generalised equation of Paris-Erdogan type was used for modelling of obtained data on crack propagation under constant amplitude load.

Simulation of delamination in composites under quasi-static and fatigue loading using cohesive zone models

Es desenvolupa una eina de disseny per l'anàlisi de la tolerància al dany en composites. L'eina pot predir el inici i la propagació de fisures interlaminars. També pot ser utilitzada per avaluar i planificar la necessitat de reparar o reemplaçar components durant la seva vida útil. El model desenvolupat pot ser utilitzat tan per simular càrregues estàtiques com de fatiga. El model proposat és un model de dany termodinàmicament consistent que permet simular la delaminació en composites sota càrregues variables. El model es formula dins el context de la Mecànica del Dany, fent ús dels models de zona cohesiva. Es presenta un metodologia per determinar els paràmetres del model constitutiu que permet utilitzar malles d'elements finits més bastes de les que es poden usar típicament. Finalment, el model és també capaç de simular la delaminació produïda per càrregues de fatiga.

The influence ofvariable amplitude loading on the fatigue strength of rhs corners

Rectangular hollow section (RHS) members are components widely used in engineering applications because of their good-looking, good properties in engineering areas and inexpensive cost comparing to members with other sections. The increasing use of RHS in load bearing structures makes it necessary to analyze the fatigue behavior of the RHS members. In this thesis, concentration will be given to the fatigue behavior of the RHS members under variable amplitude pure torsional loading. For the RHS members, failure will normally occur in the corner region if the welded regions are under full penetration. This is because of the complicated stress components' distributions at the RHScorners, where all of three fracture mechanics modes will happen. Mode I is mainly caused by the residual stresses that caused by the manufacturing process. Modes II and III are caused by the applied torsional loading. Stress based Findleymodel is also used to analyze the stress components. Constant amplitude fatigue tests have been done as well as variable amplitude fatigue tests. The specimens under variable amplitude loading gave longer fatigue lives than those under constant amplitude loading. Results from tests show an S-N curvewith slope around 5.

Constant and variable amplitude fatigue strength of high strength steel welds treated with ultrasonic impact treatment

Hitsattujen rakenteiden väsymiskestävyyttä pystytään parantamaan jälkikäsittelymenetelmillä, joistayksi, ultraäänikäsittely muokkaa hitsin geometriaa ja aiheuttaa puristusjäännösjännitystilan. Tässä tutkimuksessa verrataan kokeellisesti kuormaa kantamattoman hitsatun ja ui -käsitellyn rivan väsymislujuutta toisiinsa. Tutkimusohjelmaan kuuluu kahta teräslajia ja sekä vakio - että vaihtuva - amplitudista kuormitusta. Ultraäänikäsittelyllä saavutetaan väsymiskestoiän parantuminen vakio - ja vaihtuva - amplitudisella kuormituksella. Perusaineen lujuudella ei ole merkittää vaikutusta väsymislujuuteen kun liitos on hitsatussa tilassa. Tällöin väsymiskestävyyden määrää hitsin rajaviivan jännityskeskittymä. Ultraäänikäsitellyn hitsatunliitoksen väsymiskestävyys on suurempi korkeamman lujuuden omaavilla teräksillä. Tästä syystä korkealujuuksisten terästen käyttö ultraäänikäsiteltynä väsyttävästi kuormitetuissa kevytrakenteissa on perusteltua.

Identifying the Impact of Incomplete Datasets on Process Cycle Time Prediction in an Aerospace Assembly Line

Supply Chain Simulation (SCS) is applied to acquire information to support outsourcing decisions but obtaining enough detail in key parameters can often be a barrier to making well informed decisions.
One aspect of SCS that has been relatively unexplored is the impact of inaccurate data around delays within the SC. The impact of the magnitude and variability of process cycle time on typical performance indicators in a SC context is studied.
System cycle time, WIP levels and throughput are more sensitive to the magnitude of deterministic deviations in process cycle time than variable deviations. Manufacturing costs are not very sensitive to these deviations.
Future opportunities include investigating the impact of process failure or product defects, including logistics and transportation between SC members and using alternative costing methodologies.

Arthrodesis of the equine proximal interphalangeal joint: a biomechanical comparison of 3-Hole 4.5 mm locking compression plate and 3-hole 4.5 mm narrow dynamic compression plate, with two transarticular 5.5 mm cortex screws

Objectives To compare the biomechanical characteristics of 2 arthrodesis techniques for the equine proximal interphalangeal joint (PIP) using either a 3-hole 4.5 mm locking compression plate (LCP) or 3-hole 4.5 mm narrow dynamic compression plate (DCP), both with 2 transarticular 5.5 mm cortex screws. Study Design Experimental. Sample Population Cadaveric adult equine forelimbs (*n=6 pairs). Methods For each forelimb pair, 1 limb was randomly assigned to 1 of 2 treatment groups and the contralateral limb by default to the other treatment group. Construct stiffness, gap formation across the PIP joint, and rotation about the PIP joint were determined for each construct before cyclic axial loading and after each of four, 5000 cycle loading regimens. After the 20,000 cycle axial loading regimen, each construct was loaded to failure. Results There were no significant differences in construct stiffness, gap formation, or sagittal plane rotation between the LCP and DCP treatment groups at any of the measured time points. Conclusion Biomechanically, fixation of the equine PIP joint with a 3-hole 4.5 mm LCP is equivalent to fixation with a 3-hole 4.5 mm narrow DCP under the test conditions used.

Kylmämuovatun putkipalkin väsyminen metsätyökoneen puomirakenteessa

Työssä on tutkittu kylmämuovatun suorakaideputkipalkin väsymistä metsätyökoneen puomirakenteen osana. Kylmämuovatun putkipalkin sisäpintaan syntyy käytössä puristavan ulkoisen kuormituksen vaikutuksesta putkipalkin pituussuunnassa sekä seinämän läpi kasvavia säröjä. Työn tarkoituksena on ollut selvittää rakenteen väsymiskestoikä sekä säröytymisen aiheuttavat tekijät. Työssä on verrattu kestoikälaskentaan ja särönkasvuun sovellettujen murtumismekaniikan ja elementtimenetelmän tuloksia laboratoriokokeista saatuihin tuloksiin. Toisiaan tukevien tulosten perusteella kylmämuovausprosessissa syntyneiden jäännösjännitysten osuus särön ydintymisessä, kasvussa ja sen käyttäytymisessä on ulkoisen kuorman paikallisen vaikutuksen lisänä erittäin merkittävä. Putkipalkin väsyminen onkin jäännösjännityksistä riippuva särönkasvuilmiö.

Testiohjelmiston kehittäminen väsytyskokeiden suorittamiseksi mielivaltaisilla kuormituksilla

Väsytyskokeita on väsymisilmiön keksimisestä lähtien tehty pääasiallisesti vakioamplitudisella kuormituksella. Paremmin todellisuutta kuvaavaan testitilanteeseen päästään kuitenkin vain käyttämällä testattavan rakenteen reaalikuormitusta simuloivaa muuttuva-amplitudista kuormitusta. Tällaisen kuormituksen testaaminen käytännössä on kuitenkin huomattavasti vaikeampaa kuin perinteisen vakioamplitudisen kuormituksen, koska muuttuva-amplitudisen kuormituksen spektri on ensin kehitettävä jostain – joko käytännön mittausten kautta tai rakenteen käyttötilaa analysoimalla. Myöskään tiedossa olevan spektrin tuottaminen käytännön kokeissa ei ole aivan yksinkertaista. Tässä kandidaatintyössä pyrittiin ratkaisemaan näitä ongelmia suunnittelemalla ja toteuttamalla testiohjelmisto, joka pystyy sekä generoimaan että käytännössä toistamaan käyttäjän haluaman kuormitusspektrin laboratoriokokeissa. Jälkimmäistä varten oli olemassa ohjelma, jota haluttiin hyödyntää tässä työssä. Tehtävä jaettiin kolmeen osioon: kuormitusspektrien generoiminen, kuormitusspektrien yhdistäminen ja lopuksi spektrien toistaminen itse väsytyskokeessa. Kahdessa ensimmäisessä osiossa käytettiin ohjelmointiympäristönä Matlab-ohjelmaa; kolmannessa käytettiin pohjana olemassa olevaa väsytyskoeohjelmaa ja käytännön ohjelmointi suoritettiin näin ollen ANSI C –kielellä käyttäen kääntäjänä Microsoft Visual Studio 6.0:aa. Alkuperäinen väsytyskoeohjelma vaati useita merkittäviä muutoksia, ennen kuin se soveltui käytettäväksi tässä yhteydessä. Työssä on kuvattu periaatetasolla ohjelmien suunnittelu- ja toteuttamisvaiheet. Lisäksi työn on tarkoitus toimia yksinkertaisena käyttöohjeena ja opastuksena koko ohjelmiston käyttöön.

Evaluation of WC-10Ni thermal spraying coating by HVOF on the fatigue and corrosion AISI 4340 steel

Shot peening is a surface process widely used to improve the fatigue strength of materials, through compressive residual stresses induced in their surface layers. Considering mechanical components for high responsible applications, wear and corrosion control is currently accomplished by the use of coated materials.In the case of chrome plating or hard anodizing, lower fatigue strength in comparison to uncoated parts are associated to high residual tensile stresses and microcracks density. Under constant or variable amplitude loading microcracks will propagate and cross the interface coating substrate without impediment.The aim of the present study is to analyze the influence of WC-10Ni coating applied by HVOF process on the axial fatigue strength of AISI 4340 steel. The shot peening effect on the fatigue performance of coated AISI 4340 steel was also evaluated. The fractured fatigue specimens were investigated using a scanning electron microscope in order to obtain information about the crack initiation points. (C) 2010 Published by Elsevier Ltd.

Modelling of fatigue crack growth following overloads

In variable-amplitude loading there are interaction effects between the loading history and the crack propagation rate. The most important of these effects is the retardation in the crack propagation, which may raise the life of the cracked structureconsiderably. The main objective of this research is to analyse and quantify the retardation of crack propagation in a thin plate of the high-resistance aluminium alloy 2024-T3, comparing the results obtained from the mathematical models proposed to account for the retardation effect. The specimens were tested under high-low loading sequences, for different crack sizes and overload ratios. A simplified model was developed, based on crack closure theory, that could represent the crack behaviour during retardation very well. © 1991.

Effects of electroplated zinc-nickel alloy coatings on the fatigue strength of AISI 4340 high strength steel

It is well known that fatigue behaviour is an important parameter to be considered in mechanical components subjected to constant and variable amplitude loadings. In combination with corrosion phenomenon, fatigue effects were responsible for proximally 64% of fails that occur in metallic parts of aeronautical accidents in the last 30 years. Recovered substrates have been extensively used in the aerospace field. Cadmium electroplating has been widely applied to promote protective coatings in aeronautical components, resulting in excellent corrosion protection combined with a good performance in cyclic loading. Ecological considerations allied to the increasing demands for corrosion resistance, resulted in the search for possible alternatives. Zinc-nickel alloys received considerable interest recently, since these coatings showed some advantages such as a good resistance to white and red rust, high plating rates and acceptation in the market. In this study the effects of zinc-nickel coatings electroplated on AISI 4340 high strength steel were analysed on rotating bending and axial fatigue strength, corrosion and adhesion resistance. Compressive residual stress field was measured by a X-ray tensometry prior to fatigue tests. Optical microscopy images showed coating thicknesses, adhesion and the existence of an uniform coverage of nearly all substrates. The fractured fatigue specimens were investigated using a scanning electron microscope. Three different zinc-nickel coating thicknesses were tested and comparison with rotating bending fatigue data from specimens cadmium electroplated and heat treated at 190°C for 3, 8 and 24 hours to avoid the diffusion of hydrogen in the substrate, was performed. Experimental results showed effect of coatings on the AISI 4340 steel behaviour when submitted to fatigue testing and the existence of coating thickness influence on the fatigue strength.

Estudo da propagação de trinca por fadiga sob carregamento de amplitude variável

For engineering projects that require high reliability levels, is often not enough know only physical and chemical material properties. It’s necessary understand the failure mode of these materials in operation to ensure security level in the project and establish more stringent criteria in the analysis of structural integrity. Due to this need, aircraft industry has been using aluminum alloys in their designs and projects. “Currently more than 70% of aircraft structures are built of high strength aluminum alloys among which stand out 7075-T6 and 2024-T3 alloys, which are considered basics for being used in the new alloys development.” (PASTOUKHOV & VOORWALD, 1995). Some years ago ALCOA develops Al 2524 alloy that has emerged as refinement of Al 2024 (Al, Cu. Mg) alloy, with purpose of improve fracture toughness and fatigue resistance on structural components. The present research addresses testing of fatigue crack propagation under variable amplitude loading for Al 2024 alloy, observing the interaction effects from application of overhead blocks and plastic zone at the crack tip and makes an analysis of fracture surface images

Estudo do efeito de pausas introduzidas em testes de fadiga de amplitude variável.

É muito importante para a indústria fornecer produtos competitivos e que exerçam corretamente as suas funções perante o cliente. Uma das ferramentas existentes para atingir estes objetivos é a realização de testes de fadiga e durabilidade cada vez mais refinados e em espaço mais curto de tempo. Uma das maneiras de se executar testes de fadiga mais precisos é utilizando parâmetros que sejam fiéis à solicitação que o produto sofre durante o seu uso. Com esse intuito surgiram os testes de fadiga sob amplitude variável. Juntamente com eles surgem as particularidades deste tipo de solicitação, que é de natureza complexa. Algumas particularidades são a dependência do resultado na história de carregamento (também chamada de \"interação de cargas\") e a variação abrupta do nível de carga durante o tempo de aplicação. Fenômenos estes chamados de sobrecarga ou subcarga (overload e underload), que aqui serão agrupados, muitas vezes de forma simplista, de perturbações no espectro de fadiga. A finalidade principal deste trabalho é descrever a influência das perturbações ocorridas nas solicitações nos testes de fadiga em regime de amplitude variável, mais precisamente em testes de bancada, em que se busca a reprodução de situações de trabalho reais de um componente. Apesar de esse assunto ser alvo de diversas investigações recentes, nenhum trabalho tem como foco a influência das paradas (completa remoção de carga) realizadas durante um teste de fadiga acelerado. Essas paradas são extremamente comuns na prática laboratorial, seja por manutenção do equipamento, inspeção da amostra ou necessidade de operação. O objeto alvo de estudo nesta pesquisa é um suporte metálico de buzina, utilizado em automóveis de passeio. Apesar de sua concepção simples, tal componente é responsável por exercer funções importantes e é sujeito a uma interessante gama de solicitações. Como resultado observou-se que a aplicação das paradas durante os testes de fadiga simulados no componente automotivo, provoca variações em sua vida útil total. E o tempo de parada também exerce influência nesta variação observada. Essas paradas não se encaixam perfeitamente nas classificações de perturbações no espectro registradas na literatura. Por esse motivo o trabalho se propõe ainda a sintetizar e uniformizar a terminologia para as variações abruptas de tensão aplicadas no tempo (as sobrecargas e as subcargas), tendo em vista que ocorre a falta de consenso entre os termos utilizados atualmente na literatura e seus respectivos conceitos.

Life-Cycle Effects on Household Expenditures: A Latent-Variable Approach

Using data from the Spanish household budget survey, we investigate life- cycle effects on several product expenditures. A latent-variable model approach is adopted to evaluate the impact of income on expenditures, controlling for the number of members in the family. Two latent factors underlying repeated measures of monetary and non-monetary income are used as explanatory variables in the expenditure regression equations, thus avoiding possible bias associated to the measurement error in income. The proposed methodology also takes care of the case in which product expenditures exhibit a pattern of infrequent purchases. Multiple-group analysis is used to assess the variation of key parameters of the model across various household life-cycle typologies. The analysis discloses significant life-cycle effects on the mean levels of expenditures; it also detects significant life-cycle effects on the way expenditures are affected by income and family size. Asymptotic robust methods are used to account for possible non-normality of the data.

Lyfe-cycle effects on household expenditures: A latent-variable approach

Using data from the Spanish household budget survey, we investigate life-cycle effects on several product expenditures. A latent-variable model approach is adopted to evaluate the impact of income on expenditures, controlling for the number of members in the family. Two latent factors underlying repeated measures of monetary and non-monetary income are used as explanatory variables in the expenditure regression equations, thus avoiding possible bias associated to the measurement error in income. The proposed methodology also takes care of the case in which product expenditures exhibit a pattern of infrequent purchases. Multiple-group analysis is used to assess the variation of key parameters of the model across various household life-cycle typologies. The analysis discloses significant life-cycle effects on the mean levels of expenditures; it also detects significant life-cycle effects on the way expenditures are affected by income and family size. Asymptotic robust methods are used to account for possible non-normality of the data.