Matches in SemOpenAlex for { <https://semopenalex.org/work/W2306933940> ?p ?o ?g. }
- W2306933940 abstract "With the introduction of welding as joining method, the welding technology was applied as major joining technique in hi-tech industries to the welding of steels for manufacturing of different structures like pressure vessels and aerospace applications.Mostly high strength low alloy steels in thin cylindrical shell form are being used for aerospace structures due to high strength and low weight ratio. Despite being high strength and light weight by numerous advantages, the welding of thin walled structure of high strength low alloy steel (also known as HSLA Steel) comes also with a major problems of weld induced imperfections due to high temperatures like residual stresses and distortions with shortening of weld strength and it is a still major challenge for the welding professionals due to the complex nature of the welding phenomenon despite many innovations in welding technology. The most of the weld induced imperfections are the result of transient temperature distributions and subsequent cooling of the welds followed by transient and residual stress fields.Where as, the reliability of thin-walled structures used for any aerospace or pressure vessel application is on the prime importance every time for safe operational.Usually, thin walled cylindrical structures contain two types of weld as longitudinal and circumferential. The major design and industry constraints are weld strength and cost competitive. Gas Tungsten Arc Welding (GTAW) or TIG process is mostly applied due to the excellent weld strength and cost competitiveness.The main aim of this research work is to analyze and experimentally investigate the TIG welding parameters for purpose of minimizing residual stresses and distortion with the requirements of maximizing of weld strength of thin walled structures of HSLA steel respectively. To achieve the aforementioned targets, the following strategy was applied keeping in view the complex phenomena of welding, time and cost of extensive experimentations involved.Weld experiments were subdivided into linear and circumferential welding.Initially for linear welding, TIG welding parameters were analyzed to determine their significance on thin plates of HSLA steel of different thicknesses (3 to 5 mm) by following design of experiments (DOE) with employing 2-level full factorial and response surface method (RSM) designs to have response (weld strength, distortion residual stress). Whereas for circumferential welding, a hybrid numerical simulation and experimental based analysis approach was employed to model and predict TIG welding process to investigate the transient temperature distributions, transient/residual stress fields and distortion for circumferentially welded thin-walled cylinders of HSLA steel.The simulations strategy was developed and implemented by using commercial available general purpose finite element software ANSYS® enhanced with subroutines. First thermal analysis was completed followed by a separate mechanical analysis based on the thermal history. From the three dimensional FE model developed for TIG welding process of circumferential welding, a series of virtual welding experiments based on statistical designs (DOE) were performed for response (residual stresses and distortion) with different thicknesses by using full factorial and RSM as applied for linear welding.The effects of following six parameters, four numeric and two categorical: welding current, welding voltage, welding speed, sheet/cylinder thickness and trailing (Ar) & weld type (linear and circumferential) were investigated upon following three performance measures: weld strength, residual stresses and distortions for different thicknesses of material of HSLA steel. The experimental results were analyzed using ANOVA and significance of effects of all the tested parameters upon performance measures was determined.Empirical models for weld strength, distortion and residual stresses, in terms of significant parameters, were also developed and numerical optimization was performed according to the desirability for the maximization of weld strength and minimization of distortion residual stresses. All the statistical analyses were performed by using commercial available statistical software Design-Expert® and MINITAB From the results of post-experimental analyses, it was noticed that the effects of welding current, welding voltage and welding speed upon weld strength, residual stresses and distortion are extremely significant, while the effect of trailing and weld type is also considerably significant with respect to material thicknesses. The residual stresses are highly sensitive to heat input (weld temperatures). The residual stresses and distortion in circumferential welding are low as compared to linear welding for the same welding parameters and material thickness respectively. The vital recommendation, in this regard, is to use the parameters of welding resulting low input heat (low current, low voltage and high speed) with application of trailing with respect to material thicknesses for the maximum weld strength and minimum residual stresses and distortion in thin walled structures of HSLA steel.For the trade-off among aforementioned opposing targets and for prediction of values of performance measures at different settings of TIG welding parameters, the expert system tool, employing fuzzy reasoning mechanism, was utilized. Initially, an expert system was developed for the optimization of parameters according to objectives of maximization and/or minimization of weld strength, distortion and residual stresses.The expert system also provided the predicted values of various performance measures based upon the finalized values of the welding parameters. The analyses, simulations, experimental and ANOVA results were utilized for the making of fuzzy rule-base.The fuzzy rule-base was adjusted for maximum accuracy by employing the simulated annealing (SA) algorithm. In the next stage, a machine learning (ML) technique was utilized for creation of a expert system, named as EXWeldHSLASteel, that can: self-retrieve and self-store the experimental data; automatically develop fuzzy sets for numeric variables involved; automatically generate rules for optimization and prediction rule-bases; resolve the conflict among contradictory rules; and automatically update the interface of expert system according to newly introduced TIG welding process variables. The algorithms for these constituents were coded using a pointer-enabled language in C++. The coding involves a data structure named as doubly linked list, which provide the means for fast and efficient processing.The presented expert system is used for deciding the values of important welding process parameters as per objective before the start of actual welding process on shop floor. The user should be absolutely clear about the nature and requirements of any given TIG welding process, e.g., the setting parameters, fixed parameters, and geometric parameters etc. The expert system developed in the domain of welding for optimizing welding process of thin walled HSLA steel structure possesses all capabilities to adapt effectively to the unpredictable and continuously changing industrial environment of mechanical fabrication and manufacturing and to serve the newly emerging field of knowledge management by transforming individual (expert) knowledge into organizational knowledge i.e. implicit to explicit knowledge" @default.
- W2306933940 created "2016-06-24" @default.
- W2306933940 creator A5070757969 @default.
- W2306933940 date "2009-01-01" @default.
- W2306933940 modified "2023-09-28" @default.
- W2306933940 title "Expert System For Optimization Of Welding Process Of Thin Walled HSLA Steel Structures" @default.
- W2306933940 cites W1494372196 @default.
- W2306933940 cites W1498051694 @default.
- W2306933940 cites W1520308067 @default.
- W2306933940 cites W1527048048 @default.
- W2306933940 cites W1536701623 @default.
- W2306933940 cites W160144529 @default.
- W2306933940 cites W1614603984 @default.
- W2306933940 cites W1964593220 @default.
- W2306933940 cites W1970654831 @default.
- W2306933940 cites W1970743889 @default.
- W2306933940 cites W1975653502 @default.
- W2306933940 cites W1978068017 @default.
- W2306933940 cites W1980579543 @default.
- W2306933940 cites W1982795239 @default.
- W2306933940 cites W1983212471 @default.
- W2306933940 cites W1984954515 @default.
- W2306933940 cites W1985783989 @default.
- W2306933940 cites W1985907525 @default.
- W2306933940 cites W1985925863 @default.
- W2306933940 cites W1997882034 @default.
- W2306933940 cites W1998108927 @default.
- W2306933940 cites W1999092057 @default.
- W2306933940 cites W2001542066 @default.
- W2306933940 cites W2002735107 @default.
- W2306933940 cites W2004332806 @default.
- W2306933940 cites W2010430496 @default.
- W2306933940 cites W2010929081 @default.
- W2306933940 cites W2012971947 @default.
- W2306933940 cites W2013457547 @default.
- W2306933940 cites W2014120343 @default.
- W2306933940 cites W2014440588 @default.
- W2306933940 cites W2014793246 @default.
- W2306933940 cites W2020701003 @default.
- W2306933940 cites W2022045978 @default.
- W2306933940 cites W2022534905 @default.
- W2306933940 cites W2023773401 @default.
- W2306933940 cites W2028490802 @default.
- W2306933940 cites W2028507541 @default.
- W2306933940 cites W2031387545 @default.
- W2306933940 cites W2031856589 @default.
- W2306933940 cites W2033613435 @default.
- W2306933940 cites W2037412399 @default.
- W2306933940 cites W2042414664 @default.
- W2306933940 cites W2043872038 @default.
- W2306933940 cites W2044427658 @default.
- W2306933940 cites W2047359581 @default.
- W2306933940 cites W2049474363 @default.
- W2306933940 cites W2051040066 @default.
- W2306933940 cites W2052813570 @default.
- W2306933940 cites W2052868811 @default.
- W2306933940 cites W2053779066 @default.
- W2306933940 cites W2053979815 @default.
- W2306933940 cites W2061576113 @default.
- W2306933940 cites W2064142149 @default.
- W2306933940 cites W2064564766 @default.
- W2306933940 cites W2067159767 @default.
- W2306933940 cites W2069368991 @default.
- W2306933940 cites W2069989075 @default.
- W2306933940 cites W2075887670 @default.
- W2306933940 cites W2076777938 @default.
- W2306933940 cites W2079210660 @default.
- W2306933940 cites W2080051980 @default.
- W2306933940 cites W2080738730 @default.
- W2306933940 cites W2081990853 @default.
- W2306933940 cites W2088592288 @default.
- W2306933940 cites W2090534477 @default.
- W2306933940 cites W2090829412 @default.
- W2306933940 cites W2104314722 @default.
- W2306933940 cites W2106094353 @default.
- W2306933940 cites W2110724133 @default.
- W2306933940 cites W2115188296 @default.
- W2306933940 cites W2121792131 @default.
- W2306933940 cites W2123544733 @default.
- W2306933940 cites W2124595981 @default.
- W2306933940 cites W2144374868 @default.
- W2306933940 cites W2146934839 @default.
- W2306933940 cites W2161690462 @default.
- W2306933940 cites W2166566803 @default.
- W2306933940 cites W2167358684 @default.
- W2306933940 cites W2171776966 @default.
- W2306933940 cites W2301087314 @default.
- W2306933940 cites W2319345640 @default.
- W2306933940 cites W2320075668 @default.
- W2306933940 cites W2345438584 @default.
- W2306933940 cites W2433548967 @default.
- W2306933940 cites W2472084709 @default.
- W2306933940 cites W2472737503 @default.
- W2306933940 cites W2497524209 @default.
- W2306933940 cites W2509315528 @default.
- W2306933940 cites W2523217629 @default.
- W2306933940 cites W257500642 @default.
- W2306933940 cites W2800361446 @default.
- W2306933940 cites W2887033271 @default.
- W2306933940 cites W2946554447 @default.