Determinación paramétrica para el análisis de la viabilidad técnico económica de la implantación de un parque de aprovechamiento energético de corrientes marinas mediante un generador en inmersión con rotor de eje horizontal

La presente Tesis se ha centrado en un análisis de la tecnología para la generación de energía eléctrica utilizando las corrientes marinas. El contenido desarrollado ha consistido en un análisis de las distintas alternativas para poder aprovechar la energía oceánica con especial interés en los desarrollos tecnológicos de las corrientes marinas. Posteriormente se ha descrito un nuevo prototipo, basado en un diseño de un generador en inmersión con rotor de eje horizontal con estructura en Y, denominado proyecto GESMEY. Se han analizado diversas localizaciones para poder implantar un prototipo experimental del proyecto GESMEY, así como las posibles localizaciones para implementar un parque de explotación comercial basado en esta tecnología, llegando a conclusiones importantes referidas a la costa española, y definiendo localizaciones muy interesantes en la costa Escocesa. Finalmente se han analizado diversos parámetros de definición de estos parques de aprovechamiento de la energía, clasificándolos como parámetros técnicos, de ubicación, de utilización, medioambientales y económicos. A la vista de la investigación realizada se ha concluido que hay muchas líneas de investigación que desarrollar, y que desde un punto de vista estratégico hay muchas actuaciones que poner en marcha para potenciar la tecnología de las energías renovables marinas mediante corrientes marinas. ABSTRACT This thesis has focused on an analysis of technology for generating electrical power using ocean currents. The content developed consisted of an analysis of the alternatives to take advantage of ocean energy with special emphasis on the technological developments of ocean currents. Subsequently it described a new prototype, based on a design of a generator rotor immersion horizontal axis Y structure, called GESMEY project. We analyzed different locations to implement an experimental prototype GESMEY project and possible locations to deploy a fleet of commercial exploitation based on this technology, reaching important conclusions regarding the Spanish coast, and defining interesting locations on the coast Scottish. Finally, we have analyzed various parameters defining these parks use of energy, classifying them as technical parameters, location, utilization, environmental and economic. In view of the conducted research has concluded that there are many lines of research to develop, and that from a strategic point of view there are many actions to implement to enhance the technology of marine renewable energies by sea currents.

Deviations of cup anemometer rotational speed measurements due to steady state harmonic accelerations of the rotor

The measurement deviations of cup anemometers are studied by analyzing the rotational speed of the rotor at steady state (constant wind speed). The differences of the measured rotational speed with respect to the averaged one based on complete turns of the rotor are produced by the harmonic terms of the rotational speed. Cup anemometer sampling periods include a certain number of complete turns of the rotor, plus one incomplete turn, the residuals from the harmonic terms integration within that incomplete turn (as part of the averaging process) being responsible for the mentioned deviations. The errors on the rotational speed due to the harmonic terms are studied analytically and then experimentally, with data from more than 500 calibrations performed on commercial anemometers.

New Fault-Resistance Estimation Algorithm for Rotor-Winding Ground-Fault Online Location in Synchronous Machines With Static Excitation

New Fault-Resistance Estimation Algorithm for Rotor-Winding Ground-Fault Online Location in Synchronous Machines With Static Excitation

Electrostatic interactions between rotor and stator in the bacterial flagellar motor

Bacterial flagellar motors rotate, obtaining power from the membrane gradient of protons or, in some species, sodium ions. Torque generation in the flagellar motor must involve interactions between components of the rotor and components of the stator. Sites of interaction between the rotor and stator have not been identified. Mutational studies of the rotor protein FliG and the stator protein MotA showed that both proteins contain charged residues essential for motor rotation. This suggests that functionally important electrostatic interactions might occur between the rotor and stator. To test this proposal, we examined double mutants with charged-residue substitutions in both the rotor protein FliG and the stator protein MotA. Several combinations of FliG mutations with MotA mutations exhibited strong synergism, whereas others showed strong suppression, in a pattern that indicates that the functionally important charged residues of FliG interact with those of MotA. These results identify a functionally important site of interaction between the rotor and stator and suggest a hypothesis for electrostatic interactions at the rotor–stator interface.

Molecular dynamics of a grid-mounted molecular dipolar rotor in a rotating electric field

Classical molecular dynamics is applied to the rotation of a dipolar molecular rotor mounted on a square grid and driven by rotating electric field E(ν) at T ≃ 150 K. The rotor is a complex of Re with two substituted o-phenanthrolines, one positively and one negatively charged, attached to an axial position of Rh\documentclass[12pt]{minimal} \usepackage{amsmath} \usepackage{wasysym} \usepackage{amsfonts} \usepackage{amssymb} \usepackage{amsbsy} \usepackage{mathrsfs} \setlength{\oddsidemargin}{-69pt} \begin{document} \begin{equation*}{\mathrm{_{2}^{4+}}}\end{equation*}\end{document} in a [2]staffanedicarboxylate grid through 2-(3-cyanobicyclo[1.1.1]pent-1-yl)malonic dialdehyde. Four regimes are characterized by a, the average lag per turn: (i) synchronous (a < 1/e) at E(ν) = |E(ν)| > Ec(ν) [Ec(ν) is the critical field strength], (ii) asynchronous (1/e < a < 1) at Ec(ν) > E(ν) > Ebo(ν) > kT/μ, [Ebo(ν) is the break-off field strength], (iii) random driven (a ≃ 1) at Ebo(ν) > E(ν) > kT/μ, and (iv) random thermal (a ≃ 1) at kT/μ > E(ν). A fifth regime, (v) strongly hindered, W > kT, Eμ, (W is the rotational barrier), has not been examined. We find Ebo(ν)/kVcm−1 ≃ (kT/μ)/kVcm−1 + 0.13(ν/GHz)1.9 and Ec(ν)/kVcm−1 ≃ (2.3kT/μ)/kVcm−1 + 0.87(ν/GHz)1.6. For ν > 40 GHz, the rotor behaves as a macroscopic body with a friction constant proportional to frequency, η/eVps ≃ 1.14 ν/THz, and for ν < 20 GHz, it exhibits a uniquely molecular behavior.

Cálculo da força contra eletromotriz em máquinas síncronas com ímãs na superfície do rotor

O presente trabalho trata do cálculo da força contra eletromotriz em carga de uma máquina síncrona com ímãs na superfície do rotor (cuja forma de onda de força contra eletromotriz é não senoidal) sendo esta alimentada por correntes de fase cujas forma de onda são quadradas. Para conduzir esta investigação e calcular a força contra eletromotriz da máquina em estudo, faz-se uma revisão sobre o Método da Permeabilidade Fixa, método este que permite a linearização do ponto de operação da máquina. Dessa forma, as simulações são conduzidas por meio do método dos elementos finitos e do Método da Permeabilidade Fixa, levando-se em conta a forma de onda da corrente de alimentação. Atenção especial é dada ao modo que se analisa o fluxo concatenado e a forma de obtenção da força contra eletromotriz uma vez que as formas de onda do fluxo concatenado sofrem variações abruptas a cada 60º elétricos. Além destes parâmetros, analisa-se também cada uma das parcelas do torque eletromagnético, i.e., torque mútuo, torque de relutância e torque de borda, sendo realizado ao final do trabalho, uma comparação entre a soma da estimativa de cada parâmetro com o valor do torque eletromagnético obtido por meio de uma simulação não linear.

Summary of studies of helicopter rotor icing.

"Contract No. AF 33(616)-2859."

A method for predicting the aerodynamic loads and dynamic response of the rotor blades of a tandem-rotor helicopter.

"USAAVLABS technical report 67-38."

Computed moisture interception on helicopter rotor blades,

"Contract no. AF 33(616)-2859."

Horizontal-axis wind system rotor performance model comparison : a compendium /

"February 1983."

Investigation of helicopter rotor blade flutter and flapwise bending response in hovering

"Propulsion Laboratory, Contract no. AF33(616)-5210, Project no. 3137, Task no. 33113."

Boundary layer and wake modifications to compressor design systems : the effect of blade-to-blade flow variations on the mean flow field of a transonic rotor : final report, 01 September 1976-31 August 1978 /

"AFAPL-TR-79-2010."

Aerodynamic characteristics of helicopter rotors; rotor contributions to helicopter stability parameters

Mode of access: Internet.

Bestimmung latenter Verdampfungswärmen beziehungsweise molekularer Siedepunktserhöhungen nach der Siedemethode /

Thesis (doctoral)--Friedrich-Alexander Universität, Erlangen, 1893.

Computed induced velocity, induced drag, and angle of attack distributions for a two-bladed rotor

Cover title.