Journal of Chemical Engineering and Energy Materials

Abstract The two combustion chambers are located vertically around the turbine and are connected to the turbine housing by side flanges. This type of design makes it possible to keep the inlet air from the compressor to the combustion chamber and from the combustion chamber to the turbine in one direction and causes the least relative pressure drop and relative velocity. Compressed air from the compressor entering the combustion chamber cools the outer shell of the hot gas. In addition, the symmetrical inlet and dual variable airflow results in a symmetrical temperature distribution with minimal pressure change in front of the first row of rotating vanes. Each combustion chamber consists of 8 burners (BURNER) designed for both gas and diesel fuel. Fuel burners operate in accordance with the law of reverse flow. This arrangement of the combustion chamber creates a great flexibility in the dimensions as well as the shape of the combustion system and provides a good possibility for inspection as well as the possibility of easy assembly and disassembly. Combined burners 1 cause diffusion as well as premixing of the flame and produce nitrous oxide and low carbon monoxide without spraying water and steam injection. However, a gas turbine engine can use a water or steam injection system to reduce pollution.

Abstract KKS identification codes used to identify various components in the P&I diagram, equipment list, electrical load list, instrumentation list, function diagrams, terminal diagrams, system descriptions, and other documents. In this regard, the specification of power plant units not recounted in general. In addition, as a simple rule, the 4 digits of the equipment key (for example "-S01") are not listed in P&ID. Most valves, precision measuring instruments, etc. have a NAME PLATE installed on which the complete KKS code of the instrument inserted, which also includes the unit number of the power plant. The KKS technical issues in question fully recounted to determine which equipment discussed. For example, the phrase "solenoid valve" MBA41AA010A should be used instead of the phrase "solenoid valve" operating BLOW OFF 1.2, 1.1. KKS coding used to order spare parts. The uniaxial arrangement of the turbine allows the compressor to operate directly and independently of the generator. Combustion of gas or liquid fuel done in two symmetrical combustion chambers with several burners located on both sides of the turbine. Each combustion chamber has 8 burners. Air enters the compressor through the suction channel and through filters and mufflers. In the compressor, the air pressure increases by almost 11 times. Compressed air directed to the burners (above each combustion chamber) and burned in the combustion chambers. Hot gases burned and converted into mechanical power through a turbine. The generator connected to the turbine compressor through the shaft. The electrical power generated by the generator delivered to the transformer through the generator terminals. Exhaust gases reach atmospheric pressure at an approximate temperature of 545 C through an axial diffuser. Exhaust gas enters the open air through a vertical exhaust.

Abstract Computational modeling and simulation have emerged as indispensable tools for understanding corrosion phenomena across multiple length and time scales, bridging the gap between atomistic mechanisms and component-level lifetime prediction . This comprehensive review systematically examines the multiscale computational framework for corrosion research, from electronic structure calculations to continuum-scale predictive models. Density functional theory (DFT) provides quantum-level insights into corrosion inhibitor adsorption, with frontier molecular orbital analysis revealing that a lower energy gap (ΔE = ELUMO - EHOMO) correlates with enhanced inhibition efficiency through increased molecular reactivity . Reactive molecular dynamics (ReaxFF) enables tracking of chemical reactions, bond formation and breaking during initial corrosion stages, though time scales remain considerably shorter than realistic corrosion phenomena . Multiscale approaches integrating atomistic insights with finite element method have emerged, preserving grain boundary crystallography while enabling realistic large-scale simulations of corrosion-induced intergranular strain . Phase-field modeling has become a powerful mesoscale tool for simulating autonomous evolution of corrosion pits, capturing the complex interactions between electrochemical processes and mechanical deformation . Machine learning applications have revolutionized lifetime prediction, with hybrid models achieving R² > 0.99 for corrosion rate forecasting and service life prediction . The review concludes that next-generation corrosion modeling requires integrated frameworks combining physics-based mechanistic understanding with data-driven approaches.