CBL - Campus del Baix Llobregat

Projecte llegit

Títol: Gas Turbine Design & Analysis Tool: Ducting Components.

Estudiants que han llegit aquest projecte:

Director/a: MELLIBOVSKY ELSTEIN, FERNANDO PABLO

Departament: FIS

Títol: Gas Turbine Design & Analysis Tool: Ducting Components.

Data inici oferta: 30-01-2012     Data finalització oferta: 30-09-2012


Estudis d'assignació del projecte:
    Tipus: Coordinat    Títol: Gas Turbine Design & Analysis Tool
     
    Lloc de realització: EETAC
     
    Paraules clau:
    gas, turbine, jet, engine, turbojet, turbofan, turboprop, turboshaft, turbomachinery
     
    Descripció del contingut i pla d'activitats:
    In the design and analysis of gas turbines, these are modeled from individual components that are pieced together. The objective of the project is to define types of modules through the input and output parameters that govern interaction with other types of modules. The different modules should contemplate all possibilities in terms of interrelation with other modules, so that their internal operation can be seen as a black box and, therefore, independently improved as finer modeling becomes possible. Each type of module will initially be implemented in its simpler form so that engine operation can be tested from early on in the project. Finer modeling will then be incorporated to modules in an orderly way.

    This project will concentrate on identifying the input/output parameters needed to model ducting components (intake, nozzle, mixer and general purpose ducting) as well as defining a number of other secondary modules to represent additional components. A simple computational model of each of the aforementioned parts will be produced at the final stage.

    Coordination with at least two other projects focusing on other components is essential, as the various modules will have to be assembled into common applications for simulation. Compatibility among is therefore mandatory.

     
    Overview (resum en anglès):
    This project discusses the modelling of the different components of gas turbine engine for the subsequent programming and numerical simulation. Also, this is part of a larger project, whose goal is the design and implementation of a numerical simulator of turbine engines and all of its applications.
    During this project will be modelled, programmed and tested especially the ducting components, as diffusers, nozzles, mixing chambers and ducts linking components. Furthermore, other types of components will be modelled too, those which are mechanical components, like gearboxes, generators,
    transmission shafts, and more.
    In order to do this work, firstly the different components equations will be presented, dividing them in different difficulties or modelling degrees. Later, every component will be programmed using modular programming and will be tested to check if the obtained results are correct by comparing it with other reliable sources.
    The final objective is the implementation and simulation of different types of gas turbine engines, which we hope to be the first of the many engines that the gas turbine engine numerical simulator will have.

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