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This paper aims to present two Anand’s model parameter sets for the multilayer silver–tin (AgSn) transient liquid phase (TLP) foils.

The AgSn TLP test samples are manufactured using pre-defined optimized TLP bonding process parameters. Consequently, tensile and creep tests are conducted at various loading temperatures to generate stress–strain and creep data to accurately determine the elastic properties and two sets of Anand model creep coefficients. The resultant tensile- and creep-based constitutive models are subsequently used in extensive finite element simulations to precisely survey the mechanical response of the AgSn TLP bonds in power electronics due to different thermal loads.

The response of both models is thoroughly addressed in terms of stress–strain relationships, inelastic strain energy densities and equivalent plastic strains. The simulation results revealed that the testing conditions and parameters can significantly influence the values of the fitted Anand coefficients and consequently affect the resultant FEA-computed mechanical response of the TLP bonds. Therefore, this paper suggests that extreme care has to be taken when planning experiments for the estimation of creep parameters of the AgSn TLP joints.

In literature, there is no constitutive modeling data on the AgSn TLP bonds.

THE work described in this paper is part of a programme concerned with the plastic, creep, and relaxation properties of metals under complex stress systems at elevated temperatures.which is being carried out in the Engineering Division of the N.P.L. It comprises data on the criterion of departure from elastic behaviour, of a low carbon steel over the temperature range 20–550 deg. C, and of an aluminium alloy over the temperature range 20–200 deg. C, and the creep properties under complex stress systems of the low carbon steel at 350 deg. C, and of the aluminium alloy at 150 and 200 deg. C.

This paper presents a review concerning the analytical and inverse methods of small punch creep test (SPCT) in order to evaluate the mechanical property of component material at elevated temperature.

In this work, the effects of temperature, specimen size and shape on material properties are mainly discussed using the finite element (FE) method. The analytical approaches including membrane stretching, empirical or semi-empirical solutions that are currently used for data interpretation have been presented.

The state-of-the-art research progress on the inverse method, such as non-linear optimization program and neutral network, is critically reviewed. The capabilities of the inverse technique, the uniqueness of the solution and future development are discussed.

The state-of-the-art research progress on the inverse method such as non-linear optimization program and neutral network is critically reviewed. The capabilities of the inverse technique, the uniqueness of the solution and future development are discussed.

To determine the role of microstructure in the creep and thermomechanical fatigue (TMF) properties of solder joints made with eutectic Sn‐Ag solder, and Sn‐Ag solder with Cu and/or Ni additions.

Quaternary alloys containing small amounts of Cu and Ni exhibit better high temperature creep resistance and also better resistance to damage under TMF cycles with a longer dwell time at the high temperature extreme, than eutectic Sn‐Ag, and Sn‐Ag‐Cu ternary alloy solder joints. Microstructural evaluation was conducted to investigate the effects of Ni additions to Sn‐Ag‐based solder joints.

Microstructural studies of the quaternary solder alloys revealed the presence of small ternary Cu‐Ni‐Sn intermetallic compound particles at Sn‐Sn grain boundaries. These precipitates can retard the grain boundary sliding that will occur during TMF with longer dwell times at the high temperature extreme, and during high temperature creep.

The findings of this paper will help to provide an understanding of the effects of alloying elements on Sn‐Ag based solder joints.

Conventional solder materials are generally low temperature and low strength materials which are particularly vulnerable to temperature and stress. Even under ambient temperature, 298±5°K, the homologous temperature of most soft solder compositions exceeds 0.5. It is therefore anticipated that the properties and behaviour of such solder compositions could alter significantly when they are exposed to temperature change, temperature rise and/or a moderate level of stresses. With the continued innovation and development of microelectronic packages along with the intense global competition, the reliability of solder joints and the quality and yield of making solder joints in production become increasingly important. This research is to address the fundamental material deficiencies of conventional solders in an effort to develop superior solder materials. Several material principles have been considered including both intrinsic material and soldering process approaches. This paper presents the preliminary results of strengthening effects from the intrinsic material approach. The soldering process effects will be presented in a separate paper. The strengthening effects were evaluated by the combined consideration of monotonic shearing, creep and isothermal low cycle fatigue tests. Fatigue fractography and microstructure of the strengthened solder were characterised in comparison with conventional 63Sn/37Pb solder. The results showed that the proprietary solder system possesses a higher monotonic flow resistance as cyclic frequency decreases to 10−4 Hz. Deformation mechanisms and fatigue failure modes are also discussed in this paper.

This paper aims to explore the capabilities of artificial neural network (ANN) for predicting the creep response of a rotating Al‐SiC_P composite disc operating at elevated temperature.

Mathematical modeling of the steady state creep behavior, as described by Sherby's law, of a rotating disc made of isotropic aluminium‐silicon carbide particulate composite has been carried out. The creep response has been calculated for various combinations of particle size, particle content and temperature by extracting creep parameters from the limited experimental creep data available on similar material. The results thus obtained are used to train the ANN based on back propagation learning algorithm with particle size, particle content and temperature as input and stress and strain rates as output parameters. The trained network is used to predict the stresses and strain rates in the disc for the data set not covered in the training of network. The predictions obtained from the ANN model have been compared with the corresponding analytical values.

A nice agreement between the ANN predicted and analytical values of the creep stresses and strain rates has been observed.

ANN can be used as a reliable tool for investigating the effect of operating temperature and, reinforcement‐size and ‐content, on the creep behavior of a rotating composite disc to reach at optimum design code.

This paper aims to propose a methodology to remove inherent implicit creep from the Eurocode 3 material model for steel and to present a creep-free analysis on simply supported steel members.

Most of the available material models of steel are based on transient coupon tests, which inherently include creep strain associated with particular heating rates and load ratios.

The creep-free analysis aims to reveal the influence of implicit creep by investigating the behaviour of simply supported steel beams and columns exposed to various heating regimes. The paper further evaluates the implicit consideration of creep in the Eurocode 3 steel material model.

A modified Eurocode 3 carbon steel material model for creep-free analysis is proposed for general structural fire engineering analysis.

This study aims to review the recent advancements in high entropy alloys (HEAs) called high entropy materials, including high entropy superalloys which are current potential alternatives to nickel superalloys for gas turbine applications. Understandings of the laser surface modification techniques of the HEA are discussed whilst future recommendations and remedies to manufacturing challenges via laser are outlined.

Materials used for high-pressure gas turbine engine applications must be able to withstand severe environmentally induced degradation, mechanical, thermal loads and general extreme conditions caused by hot corrosive gases, high-temperature oxidation and stress. Over the years, Nickel-based superalloys with elevated temperature rupture and creep resistance, excellent lifetime expectancy and solution strengthening L12 and γ´ precipitate used for turbine engine applications. However, the superalloy’s density, low creep strength, poor thermal conductivity, difficulty in machining and low fatigue resistance demands the innovation of new advanced materials.

HEAs is one of the most frequently investigated advanced materials, attributed to their configurational complexity and properties reported to exceed conventional materials. Thus, owing to their characteristic feature of the high entropy effect, several other materials have emerged to become potential solutions for several functional and structural applications in the aerospace industry. In a previous study, research contributions show that defects are associated with conventional manufacturing processes of HEAs; therefore, this study investigates new advances in the laser-based manufacturing and surface modification techniques of HEA.

The AlxCoCrCuFeNi HEA system, particularly the Al0.5CoCrCuFeNi HEA has been extensively studied, attributed to its mechanical and physical properties exceeding that of pure metals for aerospace turbine engine applications and the advances in the fabrication and surface modification processes of the alloy was outlined to show the latest developments focusing only on laser-based manufacturing processing due to its many advantages.

It is evident that high entropy materials are a potential innovative alternative to conventional superalloys for turbine engine applications via laser additive manufacturing.

The purpose of this study is to develop an analytical model that is capable of predicting the behavior of shear endplate beam-column assemblies when exposed to fire, taking into account the thermal creep effect.

An analytical model is developed and validated against finite element (FE) models previously validated against experimental tests in the literature. Major material and geometrical parameters are incorporated in the analysis to investigate their influence on the overall response of the shear endplate assembly in fire events.

The analytical model can predict the induced axial forces and deflections of the assembly. The results show that when creep effect is considered explicitly in the analysis, the beam undergoes excessive deformation. This deformation needs to be taken into account in the design. The results show the significance of thermal creep effect on the behavior of the shear endplate assembly as exposed to various fire scenarios.

However, the user-defined constants of the creep equations cannot be applied to other connection types. These constants are limited to shear endplate connections having the material and geometrical parameters specified in this study.

The importance of the analytical model is that it provides a time-effective, simple and comprehensive technique that can be used as an alternative to the experimental tests and numerical methods. Also, it can be used to develop a design procedure that accounts for the transient thermal creep behavior of steel connections in real fire.

The purpose of this paper is to found a life model for the single crystal (SC) turbine blade based on the rate‐dependent crystallographic plasticity theory.

This life model has taken into consideration the creep and fatigue damages by the linear accumulation theory. A SC blade was taken from an aero‐engine, which had worked for 1,000 hours, as the illustration to validate the life model.

The crystallographic life model has a good prediction to the life and damage of the SC turbine blade. In the mean time, the micro damage study of the miniature specimens showed that creep damage has more serious influence on the material performance in the blade body but it is fatigue damage in the blade rabbet.

The life model can reflect the crystalline slip and deformation and crystallographic orientation of nickel‐based SC superalloys.