Gas Turbine By V Ganesan Pdf UPD Download
Gas Turbine By V Ganesan Pdf Download
abstract. a concept for a hybrid gas turbine-steam turbine is presented, which uses a simple steam turbine as a starter. the steam turbine is connected via a pipe to the turbine exhaust of a gas turbine. the steam generated by this starter is used to drive a compressor on the gas turbine. the main idea is to use a simple steam turbine, such as the standard industrial-grade one. this has the advantages that such turbines are easy to find and are inexpensive. the conventional starter is a gas turbine combined-cycle, which has a complicated air-gas-steam circuit. the problem with this is that it needs a large amount of steam to drive a compressor. the approach described here can be used to replace a gas-steam circuit with a steam circuit and thereby save the cost and complexity of the starter. this paper describes the concept, its feasibility, the basic design of the system, and the expected technical and economical results.
abstract. the goal of this thesis is to investigate the influence of the parameters gas velocity, pressure, temperature and pipe length on the pressure drop in a pipe, and hence the efficiency of a gas turbine-driven compressor. the work is a part of the thesis project of a student at the delft university of technology. the particular interest is in the applicability of non-dimensional parameters, which are defined in the thesis. by the application of these non-dimensional parameters, the influence of the aforementioned parameters on the pressure drop can be investigated without the need of three-dimensional modeling. by so doing the work can be reduced from a full-blown finite element model to a simple linear relation between the non-dimensional parameters. the pressure drop in a pipe is modeled by means of the continuity and the navier-stokes equations. the results of this thesis can be used to investigate the application of the gas turbine-driven compressor. moreover, the results can be used for example in the development of an optimal control model of the compressor of a gas turbine.
the paper describes how the state-of-the-art carbon fiber honeycomb manufacturing technology used for the production of the six-blade, fully composite variable pitch turbine fan in the repower system can be adapted to fabricate a three-blade, fully composite variable pitch system. this work is being performed for the united states navy and the united states air force. this paper is a comparative study of the atmospheric corrosion behavior of low-alloyed steels used in gas turbine engines and the corresponding protection. the experimental results of the atmospheric corrosion behavior of the different alloys, in terms of the concentrations of the different species at the surface, are compared with the corrosion models developed for the different alloys. it is shown that the real protection of the gas turbine alloys is lower than predicted by the models, and that a new model for the protection of these alloys should be developed. in this study, the intergranular corrosion of the blade base material in steam turbine blades has been investigated. the intergranular corrosion of the base material was observed in the root of the blade, where the corrosion was found to be more severe than the corrosion observed in the tip of the blades. the intergranular corrosion of the base material was studied by the accelerated corrosion test in a corrosive environment. the corrosion was found to be mainly localized in the root region and was not propagated into the tip region. the main mechanism of the intergranular corrosion of the base material was found to be oxidation of the grain boundary, which was confirmed by the eds analysis. in addition, the corrosion was accelerated by the cavitation erosion and the water jet erosion, and the cavitation erosion was found to be the main mechanism for the corrosion acceleration. the corrosion behavior in the cavitation erosion region is not completely understood, but the cavitation erosion region is believed to be associated with the low passivation film at the grain boundary. therefore, it is suggested that the prevention of the cavitation erosion is an effective way to prevent the intergranular corrosion of the base material in the steam turbine blades. 5ec8ef588b
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