EMI filter design of a three-phase buck-type rectifier for aircraft applications

An EMI filter for a three-phase buck-type medium power pulse-width modulation rectifier is designed. This filter considers differential mode noise and complies with MIL-STD- 461E for the frequency range of 10kHz to 10MHz. In industrial applications, the frequency range of the standard starts at 150kHz and the designer typically uses a switching frequency of 28kHz because the fifth harmonic is out of the range. This approach is not valid for aircraft applications. In order to design the switching frequency in aircraft applications, the power losses in the semiconductors and the weight of the reactive components should be considered. The proposed design is based on a harmonic analysis of the rectifier input current and an analytical study of the input filter. The classical industrial design does not consider the inductive effect in the filter design because the grid frequency is 50/60Hz. However, in the aircraft applications, the grid frequency is 400Hz and the inductance cannot be neglected. The proposed design considers the inductance and the capacitance effect of the filter in order to obtain unitary power factor at full power. In the optimization process, several filters are designed for different switching frequencies of the converter. In addition, designs from single to five stages are considered. The power losses of the converter plus the EMI filter are estimated at these switching frequencies. Considering overall losses and minimal filter volume, the optimal switching frequency is selected

New Considerations in the Input Filter Design of a Three-Phase Buck-Type PWM Rectifier for Aircraft Applications

An EMI filter for a three-phase buck-type medium power pulse-width modulation rectifier is designed. This filter considers differential mode noise and complies with MIL-STD-461E for the frequency range of 10kHz to 10MHz. In industrial applications, the frequency range of the standard starts at 150kHz and the designer typically uses a switching frequency of 28kHz because the fifth harmonic is out of the range. This approach is not valid for aircraft applications. In order to design the switching frequency in aircraft applications, the power losses in the semiconductors and the weight of the reactive components should be considered. The proposed design is based on a harmonic analysis of the rectifier input current and an analytical study of the input filter. The classical industrial design does not consider the inductive effect in the filter design because the grid frequency is 50/60Hz. However, in the aircraft applications, the grid frequency is 400Hz and the inductance cannot be neglected. The proposed design considers the inductance and the capacitance effect of the filter in order to obtain unitary power factor at full power. In the optimization process, several filters are designed for different switching frequencies of the converter. In addition, designs from single to five stages are considered. The power losses of the converter plus the EMI filter are estimated at these switching frequencies. Considering overall losses and minimal filter volume, the optimal switching frequency is selected.

Analysis and optimized design of a distributed multi-stage EMC filter for an interleaved three-phase PWM-rectifier system for aircraft applications

Different possible input filter configurations for a modular three-phase PWM rectifier system consisting of three interleaved converter cells are studied. The system is designed for an aircraft application where MIL-STD-461E conducted EMI standards have to be met and system weight is a critical design issue. The importance of a LISN model on the simulated noise levels and the effect of interleaving and power unbalance between the different converter modules is discussed. The effect of the number of filter stages and the degree of distribution of the filter stages among the individual converter modules on the weight and losses of the input filter is studied and optimal filter structures are proposed.

3-Phase Rectifier System with very demanding dynamic load: Architecture analysis and control strategy

A distributed power architecture for aerospace application with very restrictive specifications is analyzed. Parameters as volume, weight and losses are analyzed for the considered power architectures. In order to protect the 3 phase generator against high load steps, an intermediate bus (based in a high capacitance) to provide energy to the loads during the high load steps is included. Prototypes of the selected architecture for the rectifier and EMI filter are built and the energy control is validated.

Interleaved multi-cell isolated three-phase PWM rectifier system for aircraft applications

Recently there has been an important increase in electric equipment, as well as, electric power demand in aircrafts applications. This prompts to the necessity of efficient, reliable, and low-weight converters, especially rectifiers from 115VAC to 270VDC because these voltages are used in power distribution. In order to obtain a high efficiency, in aircraft application where the derating in semiconductors is high, normally several semiconductors are used in parallel to decrease the conduction losses. However, this is in conflict with high reliability. To match both goals of high efficiency and reliability, this work proposes an interleaved multi-cell rectifier system, employing several converter cells in parallel instead of parallel-connected semiconductors. In this work a 10kW multi-cell isolated rectifier system has been designed where each cell is composed of a buck type rectifier and a full bridge DC-DC converter. The implemented system exhibits 91% of efficiency, high power density (10kW/10kg), low THD (2.5%), and n−1 fault tolerance which complies, with military aircraft standards.

Power Converter Topologies for a High Performance Transformer Rectifier Unit in Aircraft Applications

This paper presents some power converter architectures and circuit topologies, which can be used to achieve the requirements of the high performance transformer rectifier unit in aircraft applications, mainly as: high power factor with low THD, high efficiency and high power density. The voltage and the power levels demanded for this application are: three-phase line-to-neutral input voltage of 115 or 230V AC rms (360 – 800Hz), output voltage of 28V DC or 270V DC(new grid value) and the output power up to tens of kilowatts.

Simulación, construcción y medida de un sistema de telealimentación eficiente

Los sistemas de telealimentación han tomado gran importancia en diferentes campos, incluido el de las telecomunicaciones, algunos ejemplos pueden ser: En la red conmutada telefónica junto con la señal de información y llamada existe una alimentación de 48v que se transmite a través de toda la línea de transmisión hasta los terminales. En algunos ferrocarriles eléctricos, se aprovecha la producción de energía eléctrica cuando un tren baja una cuesta y el motor funciona como generador, devolviendo la energía excedente a la propia catenaria por medio de superposición, y siendo esta recuperada en otro lugar y aprovechada por ejemplo por otro tren que requiere energía. Otro uso en ferrocarriles de la telealimentación es la llamada "tecnología del transpondedor magnético", en la que el tren transmite a las balizas una señal en 27MHz además de otras de información propias, que se convierte en energía útil para estas balizas. En este proyecto pretendemos implementar un pequeño ejemplo de sistema de telealimentación trabajando en 5 MHz (RF). Este sistema transforma una señal de CC en una señal de potencia de CA que podría ser, por ejemplo, transmitida a lo largo de una línea de transmisión o radiada por medio de una antena. Después, en el extremo receptor, esta señal RF se transforma finalmente en DC. El objetivo es lograr el mejor rendimiento de conversión de energía, DC a AC y AC a DC. El sistema se divide en dos partes: El inversor, que es la cadena de conversión DC-AC y el rectificador, que es la cadena de conversión AC-DC. Cada parte va a ser calculada, simulada, implementada físicamente y medida aparte. Finalmente el sistema de telealimentación completo se va a medir mediante la interconexión de cada parte por medio de un adaptador o una línea de transmisión. Por último, se mostrarán los resultados obtenidos. ABSTRACT. Remote powering systems have become very important in different fields, including telecommunications, some examples include: In the switched telephone network with the information signal and call there is a 48v supply that is transmitted across the transmission line to the terminals. In some electric railways, the production of electrical energy is used when a train is coming down a hill and the motor acts as a generator, returning the surplus energy to the catenary itself by overlapping, and this being recovered elsewhere and used by other train. Home TV amplifiers that are located in places (storage, remote locations ..) where there is no outlet, remote power allows to carry information and power signal by the same physical medium, for instance a coax. The AC power signal is transformed into DC at the end to feed the amplifier. In medicine, photovoltaic converters and fiber optics can be used as means for feeding devices implanted in patients. Another use of the remote powering systems on railways is the "magnetic transponder technology", in which the station transmits a beacon signal at 27MHz own as well as other information, which is converted into useful energy to these beacons. In this Project we are pretending to implement a little example of remote powering system working in 5 MHz (RF). This system transform DC into an AC-RF power signal which could be, for instance, transmitted throughout a transmission line or radiated by means of an aerial. At the receiving end, this RF signal is then transformed to DC. The objective is to achieve the best power conversion performance, DC to AC and AC to DC. The system is divided in two parts: The inverter, that is the DC-AC conversion chain and the rectifier that is the AC-DC conversion chain. Each part is going to be calculated, simulated, implemented physically and measured apart. Then the complete remote-powering system is to be measured by interconnecting each part by means of a interconnector or a transmission line. Finally, obtained results will be shown.

Development and improvement of protection-system algorithms for ground-fault detection and location in synchronous machines

Uno de los defectos más frecuentes en los generadores síncronos son los defectos a tierra tanto en el devanado estatórico, como de excitación. Se produce un defecto cuando el aislamiento eléctrico entre las partes activas de cualquiera de estos devanados y tierra se reduce considerablemente o desaparece. La detección de los defectos a tierra en ambos devanados es un tema ampliamente estudiado a nivel industrial. Tras la detección y confirmación de la existencia del defecto, dicha falta debe ser localizada a lo largo del devanado para su reparación, para lo que habitualmente el rotor debe ser extraído del estator. Esta operación resulta especialmente compleja y cara. Además, el hecho de limitar la corriente de defecto en ambos devanados provoca que el defecto no sea localizable visualmente, pues apenas existe daño en el generador. Por ello, se deben aplicar técnicas muy laboriosas para localizar exactamente el defecto y poder así reparar el devanado. De cara a reducir el tiempo de reparación, y con ello el tiempo en que el generador esta fuera de servicio, cualquier información por parte del relé de protección acerca de la localización del defecto resultaría de gran utilidad. El principal objetivo de esta tesis doctoral ha sido el desarrollo de nuevos algoritmos que permitan la estimación de la localización de los defectos a tierra tanto en el devanado rotórico como estatórico de máquinas síncronas. Respecto al devanado de excitación, se ha presentado un nuevo método de localización de defectos a tierra para generadores con excitación estática. Este método permite incluso distinguir si el defecto se ha producido en el devanado de excitación, o en cualquiera de los componentes del sistema de excitación, esto es, transformador de excitación, conductores de alimentación del rectificador controlado, etc. En caso de defecto a tierra en del devanado rotórico, este método proporciona una estimación de su localización. Sin embargo, para poder obtener la localización del defecto, se precisa conocer el valor de resistencia de defecto. Por ello, en este trabajo se presenta además un nuevo método para la estimación de este parámetro de forma precisa. Finalmente, se presenta un nuevo método de detección de defectos a tierra, basado en el criterio direccional, que complementa el método de localización, permitiendo tener en cuenta la influencia de las capacidades a tierra del sistema. Estas capacidades resultan determinantes a la hora de localizar el defecto de forma adecuada. En relación con el devanado estatórico, en esta tesis doctoral se presenta un nuevo algoritmo de localización de defectos a tierra para generadores que dispongan de la protección de faltas a tierra basada en la inyección de baja frecuencia. Se ha propuesto un método general, que tiene en cuenta todos los parámetros del sistema, así como una versión simplificada del método para generadores con capacidades a tierra muy reducida, que podría resultar de fácil implementación en relés de protección comercial. Los algoritmos y métodos presentados se han validado mediante ensayos experimentales en un generador de laboratorio de 5 kVA, así como en un generador comercial de 106 MVA con resultados satisfactorios y prometedores. ABSTRACT One of the most common faults in synchronous generators is the ground fault in both the stator winding and the excitation winding. In case of fault, the insulation level between the active part of any of these windings and ground lowers considerably, or even disappears. The detection of ground faults in both windings is a very researched topic. The fault current is typically limited intentionally to a reduced level. This allows to detect easily the ground faults, and therefore to avoid damage in the generator. After the detection and confirmation of the existence of a ground fault, it should be located along the winding in order to repair of the machine. Then, the rotor has to be extracted, which is a very complex and expensive operation. Moreover, the fact of limiting the fault current makes that the insulation failure is not visually detectable, because there is no visible damage in the generator. Therefore, some laborious techniques have to apply to locate accurately the fault. In order to reduce the repair time, and therefore the time that the generator is out of service, any information about the approximate location of the fault would be very useful. The main objective of this doctoral thesis has been the development of new algorithms and methods to estimate the location of ground faults in the stator and in the rotor winding of synchronous generators. Regarding the excitation winding, a new location method of ground faults in excitation winding of synchronous machines with static excitation has been presented. This method allows even to detect if the fault is at the excitation winding, or in any other component of the excitation system: controlled rectifier, excitation transformer, etc. In case of ground fault in the rotor winding, this method provides an estimation of the fault location. However, in order to calculate the location, the value of fault resistance is necessary. Therefore, a new fault-resistance estimation algorithm is presented in this text. Finally, a new fault detection algorithm based on directional criterion is described to complement the fault location method. This algorithm takes into account the influence of the capacitance-to-ground of the system, which has a remarkable impact in the accuracy of the fault location. Regarding the stator winding, a new fault-location algorithm has been presented for stator winding of synchronous generators. This algorithm is applicable to generators with ground-fault protection based in low-frequency injection. A general algorithm, which takes every parameter of the system into account, has been presented. Moreover, a simplified version of the algorithm has been proposed for generators with especially low value of capacitance to ground. This simplified algorithm might be easily implementable in protective relays. The proposed methods and algorithms have been tested in a 5 kVA laboratory generator, as well as in a 106 MVA synchronous generator with satisfactory and promising results.

Transferencia inalámbrica de energía

El trabajo presentado en este documento se centra en la temática de la transferencia inalámbrica de energía, concretamente en aplicaciones de campo lejano, para llevar a cabo dicho trabajo nos centraremos en el diseño, implementación y medición de una rectenna operando en la banda ISM concretamente a una frecuencia de 2.45GHz, el objetivo primordial de este trabajo será analizar que parámetros intervienen en la eficiencia de conversión en la etapa de RF-DC a fin de lograr la máxima eficiencia de conversión posible. Para llevar a cabo dicho análisis se emplearán herramientas informáticas, concretamente se hará uso del software AWR Microwave Office, a través del cual se realizarán simulaciones SourcePull a fin de determinar la impedancia óptima de entrada que se le debe presentar a la etapa rectificadora RF-DC para conseguir la máxima eficiencia de conversión, una vez realizadas dichas pruebas se implementará físicamente un circuito rectenna a través del cual realizar medidas de SourcePull mediante un Wide Matching Range Slide Screw Tuner de MAURY MICROWAVE para cotejar las posibles diferencias con los resultados obtenidos en las simulaciones. Tras la fase de pruebas SourcePull se extrapolará una red de entrada en base a los datos obtenidos en las mediciones anteriores y se diseñará y fabricará un circuito rectenna con máxima eficiencia de conversión para un conjunto de valores de potencia de entrada de RF y carga de DC, tras lo cual se analizará la eficiencia del circuito diseñado para diferentes valores de potencia de RF de entrada y carga de DC. Como elemento rectificador emplearemos en nuestro trabajo el diodo Schottky HSMS-2820, los diodos Schottky se caracterizan por tener tiempos de conmutación relativamente bajos y pérdidas en directa reducidas los cual será fundamental a la hora de trabajar con niveles reducidos de potencia de RF de entrada, para implementar el circuito se empleará un substrato FR4 con espesor de 0.8mm para disminuir en la mayor medida posible las pérdidas introducidas por el dieléctrico, se analizarán diferentes posibilidades a la hora de implementar el filtro de RF a la salida del diodo rectificador y finalmente se optará por el empleo de un stub radial ya que será este el que mejor ancho de banda nos proporcione. Los resultados simulados se compararán con los resultados medidos sobre el circuito rectenna para determinar la similitud entre ambos. ABSTRACT. The work presented in this paper focuses on the issue of wireless transfer of energy, particularly applied to far-field applications, to carry out this work we focus on the design, implementation and measurement of a rectenna operating in the ISM band specifically at a frequency of 2.45GHz, the primary objective of this study is to analyze any parameter involved in the RF-DC conversion efficiency in order to achieve the maximum conversion efficiency as possible. Computer analysis tools will be used, particularly AWR Microwave Office software, in order to carry out SourcePull simulations to determine the optimal input impedance which must be presented to the rectifier stage for maximum conversion efficiency, once obtained, a rectenna circuit will be implemented to compute SourcePull measurements, and finally simulated results will be compared to measured results. Once obtained the result, an input network impedance is extrapolated based on data from previous measurements to design and implement a rectenna circuit with high conversion efficiency for a set of RF input power and DC load values , after that, the designed circuit efficiency will be analyzed for different values of RF input power and DC load. In this work a HSMS-2820 Schottky diode will be used as the rectifier , Schottky diodes are characterized by relatively low switching times and reduced direct losses, that properties will be essential when working with low RF input power levels , to implement the circuit a FR4 substrate with 0.8mm thickness is used to reduce as much as possible the dielectric losses, different possibilities to implement the RF filter to the output of the rectifier diode will be analyzed, finally we will opt for the use of a radial stub as this will provide the best bandwidth possible. The simulated results are compared with the results measured on the rectenna circuit to determine the similarity between them.

A Wireless Charging System Applying Phase-Shift and Amplitude Control to Maximize Efficiency and Extractable Power

Wireless power transfer (WPT) is an emerging technology with an increasing number of potential applications to transfer power from a transmitter to a mobile receiver over a relatively large air gap. However, its widespread application is hampered due to the relatively low efficiency of current Wireless power transfer (WPT) systems. This study presents a concept to maximize the efficiency as well as to increase the amount of extractable power of a WPT system operating in nonresonant operation. The proposed method is based on actively modifying the equivalent secondary-side load impedance by controlling the phase-shift of the active rectifier and its output voltage level. The presented hardware prototype represents a complete wireless charging system, including a dc-dc converter which is used to charge a battery at the output of the system. Experimental results are shown for the proposed concept in comparison to a conventional synchronous rectification approach. The presented optimization method clearly outperforms state-of-the-art solutions in terms of efficiency and extractable power.

A resistance emulation approach to optimize the wave energy harvesting for a direct drive point absorber

In general, a major challenge for the exploitation of renewable energies is to improve their efficiency. In electricity generation from the energy of ocean waves, not unlike other technologies, the converter must be optimized to make the energy harvesting economically feasible. This paper proposes a passive tuning control strategy of a point absorber in which the power captured is maximized by controlling the electromagnetic force of the generator with a resistance emulation approach. The proposed strategy consists of mapping the optimal values for regular waves and applying them to irregular waves. This strategy is tested in a wave energy converter in which the generator is connected to a boost rectifier converter whose controller is designed to emulate a resistance. The power electronics system implemented is validated by comparing its performance with the case in which the generator is directly connected to a resistive load. The simulation results show the effectiveness of the proposed strategy as the maximum captured power is concentrated around the optimal values previously calculated and with the same behavior for both excitations.