...Abstract Abstract Accurate thermal prediction of gas turbine blades is essential to ensure successful operation throughout the design life. Large Gas turbines operate in different conditions based on customer requirements, due to which turbine blades are subjected to variations in thermal...

... Proceedings of the ASME 2021 Gas Turbine India Conference GTINDIA2021 December 2-3, 2021, Virtual, Online GTINDIA2021-75952 INFLUENCE OF DEGRADATION, FUEL COST AND ELECTRICITY PRICE FACTORS ON COMBINE CYCLE POWER PLANT COST ANALYSIS Pugalenthi Nanadagopal1, Matthias Duerr2, Ole Fahrendorf2, Dan...

... Proceedings of the ASME 2021 Gas Turbine India Conference GTINDIA2021 December 2-3, 2021, Virtual, Online GTINDIA2021-76443 AERODYNAMIC PERFORMANCE EVALUATION OF AXIAL FLOW FAN USING NUMERICAL TECHNIQUES Raghuvaran D 1, Satvik Shenoy 1, Srinivas G 1 1 Department of Aeronautical and Automobile...

... Proceedings of the ASME 2021 Gas Turbine India Conference GTINDIA2021 December 2-3, 2021, Virtual, Online GTINDIA2021-76058 MACHINE LEARNING BASED CLASSIFICATION MODEL FOR PREDICTING CYCLIC FAILURE IN RADIALLY COOLED GAS TURBINE BLADES Rishabh Shrivastava1, Ankush Kapoor1, Stuti Kaushal1, Amit...

... Proceedings of the ASME 2021 Gas Turbine India Conference GTINDIA2021 December 2-3, 2021, Virtual, Online GTINDIA2021-75844 COMBINED CYCLE POWERPLANT COST SENSITIVITY ANALYSIS Pugalenthi Nanadagopal1, Animesh Pandey1, Manjunath More1, Pertik Kamboj1 1Siemens AG, Gurgaon, India ABSTRACT Fuel cost...

...ENERGY AND EXERGY ANALYSIS OF A GAS TURBINE POWER PLANT INTEGRATED WITH VAPOR ADSORPTION REFRIGERATION SYSTEM Sanchit Agarwal1, Darshika Gupta1, Devendra Dandotiya2, Nitin D Banker3 1Shiv Nadar University, Dadri, UP, India 2Presidency University, Bangalore, Karnataka, India 3Ahmedabad University...

... Tripoli3 Baker Hughes a GE Company (BHGE) Via F. Matteucci 2, 50127, Florence, Italy ABSTRACT Gas Turbine shroud is a static component, which forms the outer flow path surface and sealing clearances to turbine blade tip. It also protects the casing from hot gases ingestion and radiation. Shrouds...

...EXERGY ANALYSIS OF A COMBINED GAS TURBINE AND ORGANIC RANKINE CYCLE BASED POWER AND ABSORPTION COOLING SYSTEMS Joy Nondy and Tapan Kr. Gogoi Department of Mechanical Engineering, Tezpur University, Tezpur 784028 , India ABSTRACT In this paper, a combined power and cooling system...

...-shaped ribs in a rectangular channel with an aspect ratio of 6:1. The rib-roughened copper plates were located at the bottom of the channel to simulate the backside wall cooling of gas turbine combustor liners. The rib height-to-hydraulic diameter ratio (e/Dh) was 0.05834 and the rib pitch-to-height...

.... The plant is basically the captive power plant (CPP) of Numaligarh Refinery Limited (NRL), lo- cated in Golaghat district of Assam, India. The plant consists of a gas turbine (GT) plant as topping and a steam turbine (ST) plant as bottoming cycle. In the CPP, there was also provision for extracting steam...

...ANALYSIS OF PART ELECTRIC GAS TURBINE: A NOVEL HYBRID PROPULSION CONCEPT MSN Murthy1,2, Subhash Kumar1, Sheshadri Sreedhara1 1Indian Institute of Technology, Bombay, Powai, Mumbai, India 2Naval Dockyard, Visakhapatnam, India ABSTRACT A gas turbine engine (GT) is very complex to design...

...EXPERIMENTAL ANALYSIS OF COMBUSTION IN GAS TURBINE MSN Murthy1,2, Subhash Kumar1, Sheshadri Sreedhara1 1Indian Institute of Technology, Bombay, Powai, Mumbai, India 2Naval Dockyard, Visakhapatnam, India ABSTRACT This paper presents the methodology and results of an experimental analysis...

...TURBINE REAR FRAME DESIGN FOR AN AERO DERIVATIVE GAS TURBINE Anil Kumar Chippa1, Santhana G Babu2 Baker Hughes a GE company (BHGE) GE JFWTC, Whitefield, Bangalore-66, India Casadio Federico3 ,Gianfranco Pittella4 Baker Hughes a GE company (BHGE) Via F. Matteucci 2, 50127, Florence, Italy ABSTRACT...

...Abstract Abstract The gas turbine combustion chamber is a vital part of a gas turbine engine. Proper mixing of air in the combustor plays an important role in combustion. Increasing mixing rate is an important factor for better combustion efficiency. The injection of air in crossflow is widely...

...ARTIFICIAL INTELLIGENCE BASED GAS TURBINE COMPRESSOR WASH: A PREDICTIVE APPROACH Shaiju M.Raghavan 1, Arun Palatel2, Jayaraj Simon3 1Deputy General Manager, NTPC Limited, Mumbai, India 2Associate Professor, 3Professor, Department of Mechanical Engineering, National Institute of Technology Calicut...

...Abstract Abstract Gas turbines Lifting devices (such as lifting lugs, eye bolts, trunnions, are provided on large stationary gas turbine parts as an aid in manufacturing, assembly, transport, shipping, test, installation, repair, and serviceability. Trunnions are used to lift the entire turbine...

.... In the Arcadia framework this is represented at system analysis level. Further studies capture the logical and physical architecture which is representative in nature. gas turbine tip clearance control TCC MBSE Capella Export Control Information (ECI). This document is subject to the following...

... in pressure ratio with crenulation was surprising and might be due to increased mixing losses downstream of the blade. Axial Transonic Compressor Trailing Edge Crenulation Stall Margin CFD Gas Turbine EFFECT OF TRAILING EDGE CRENULATION ON THE PERFORMANCE AND STALL MARGIN OF A TRANSONIC AXIAL...

... 1 Copyright © 2012 by ASME PART-LOAD PERFORMANCE OF GAS TURBINES-PART I: A NOVEL COMPRESSOR MAP GENERATION APPROACH SUITABLE FOR ADAPTIVE SIMULATION E. Tsoutsanis1,2 Y. G. Li2 P. Pilidis2 M. Newby3 1 Qatar University, Doha, Qatar 2 Cranfield University, Cranfield, Beds, UK 3 Manx Electricity...

... Gas Turbine Off-Design Performance Multi-point Adaptation Genetic Algorithms 1 Copyright © 2012 by ASME PART-LOAD PERFORMANCE OF GAS TURBINES-PART II: MULTI-POINT ADAPTATION WITH COMPRESSOR MAP GENERATION AND GA OPTIMIZATION E. Tsoutsanis1,2 Y. G. Li2 P. Pilidis2 M. Newby3 1 Qatar...