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Viewing 1 to 30 of 114
2016-09-20
Technical Paper
2016-01-2031
Michal Sztykiel, Steven Fletcher, Patrick Norman, Stuart Galloway, Graeme Burt
There is a well-recognized need for robust simulation tools to support the design and evaluation of future More-Electric Engine and Aircraft (MEE/MEA) design concepts. Design options for these systems are increasingly complex, and normally include multiple power electronics converter topologies and machine drive units. In order to identify the most promising set of system configurations, large number of existing technology variants need to be rapidly evaluated. This paper will describe a method of MEE/MEA system design with the use of a newly developed transient modelling, simulation and testing tool aimed at accelerating the identification process of optimal components, testing novel technologies and finding key solutions at an early development stage. The developed tool is a Matlab/Simulink library consisting of functional sub-system units, which can be rapidly integrated to build complex system architectures.
2016-09-20
Technical Paper
2016-01-1990
Nisha Kondrath, Nathaniel Smith
In aerospace applications, it is important to have efficient, small, affordable, and reliable power conversion units with high power density to supply a wide range of loads. Use of wide-band gap devices, such as Silicon Carbide (SiC) and Gallium Nitride (GaN) devices, in power electronic converters is expected to reduce the device losses and needs for extensive thermal management systems in power converters, as well as facilitate high-frequency operation, thereby reducing the passive component sizes and increasing the power density. A performance comparison of state-of-the art power devices in a 10 kW full-bridge buck converter operating in continuous conduction mode (CCM) and at switching frequencies above 100 kHz will be presented in this manuscript. Power devices under consideration will include Si IGBT with Si antiparallel diodes, Si IGBT with SiC antiparallel diodes, Si MOSFETs, SiC MOSFETs, and enhancement-mode GaN transistors.
2016-09-20
Technical Paper
2016-01-1987
Mingming Yin, Serhiy Bozhko, Seang Shen Yeoh
The paper will deal with the control design for an electric generation system which for future aircrafts. The future on-board systems are expected to be more efficient, safer, simpler in servicing and easier in maintenance. As a result, many existing hydraulic and pneumatic power driven systems are being replaced by their electrical counterparts. This trend is known as a move towards the More-Electric Aircraft (MEA). As a result, a large number of new electrical loads have been introduced in order to power many primary functions including actuation, de-icing and anti-icing, cabin air-conditioning, and engine start. Therefore electric power generation systems have a key role in supporting this technological trend. The state-of-the-art generation technology typically employs a three-stage wound-field synchronous machine. Advances in modern power electronics now allow the developers to consider including other machine types within the S/G.
2016-09-20
Technical Paper
2016-01-1985
Fei Gao, Serhiy Bozhko, Patrick Wheeler
The paper will deal with the problem of establishing a desirable power sharing in multi-feed electric power system for future More-Electric Aircraft (MEA) platforms. The MEA is one of the major trends in modern aerospace engineering aiming for reduction of the overall aircraft weight, operation cost and environmental impact. Electrical systems are employed to replace existing hydraulic, pneumatic and mechanical loads. Hence the onboard installed electrical power increases significantly and this results in challenges in the design of Electrical Power Systems (EPS). One of the key paradigms for future MEA EPS architectures assumes high-voltage dc distribution with multiple sources, possibly of different physical nature, feeding the same bus(es). In our study we investigate control approaches to guarantee that the total electric load is shared between the sources in a desirable manner.
2016-09-20
Technical Paper
2016-01-1982
Michelle Bash, Steven Pekarek, Jon Zumberge
The cost and complexity of aircraft power systems often limits the ability to evaluate system performance using fully integrated aircraft hardware. As a result, evaluations are typically performed using emulators to mimic components or subsystems. As an example, aircraft generation systems are often tested using an emulator that consists of a bank of resistors that are switched to represent the power draw of one or more actuators. The limitation of this approach is that the switched resistive load falls short of representing the dynamic load characteristics of aircraft actuators or other power electronic loads, and thus the true integrated performance cannot be evaluated. In this research, consideration is given to modern emulators that use power electronics and digital controls to obtain wide bandwidth control of power, current, or voltage.
2016-09-20
Technical Paper
2016-01-1991
Syed J. Khalid
Engine bleed and power extraction are required by the aircraft to operate the various onboard subsystems which are necessary for the proper functioning of the aircraft. These extractions are parasitic for engine performance and operation. The engine companies make large investments in technology to achieve a couple of percent in engine efficiency. These gains can be quickly negated if bleed and power extraction are not judiciously managed for minimizing the amounts of extractions. Permission has been obtained from Boeing to use their public domain information on subsystem architecture to articulate the message in this paper. Help from Boeing and from Specific Range Solutions Ltd of Canada in the preparation of this paper is acknowledged. The paper will first quantify the detrimental effects of bleed and power extraction on engine performance and operation using the proven GasTurb 12 performance software. The engine modelled is similar to a modern transport aircraft turbofan.
2016-09-20
Technical Paper
2016-01-2029
Rolf Loewenherz, Francisco Gonzalez-Espin, Laura Albiol-Tendillo, Virgilio Valdivia-Guerrero, Ray Foley
The present work targets a Modelica-based holistic model and simulation approach. The targeted example considers a three phase converter which is divided into the control domain, the converter electrical and thermal domains (based on losses calculation), the heat transfer domain the electromechanical domain (motor and pump) and the fluid dynamics. In this paper, only the control, converter (electrical) and converter (thermal/losses) are described in detail, while the other domains are yet to be explored in future investigation. An averaged model is utilised for the electrical domain of the three phase converter, and a power balance method is used for linking the DC and AC sides. The thermal domain focuses in determining the converter losses by deriving the analytical equations of the space vector modulation to derive a function for the duty cycle of each converter leg.
2016-09-20
Technical Paper
2016-01-2030
Jon Zumberge, Michael Boyd, Raul Ordonez
Cost and performance requirements are driving military and commercial systems to highly integrated, optimized systems which require more sophisticated, highly complex controls. To realize benefits of those complex controls and make confident decisions, the validation of both plant and control models becomes critical. To quickly develop controls for these systems, it is beneficial to develop plant models and determine the uncertainty of those models to predict performance and stability of the control algorithms. A process of model and control algorithm validation for a dc-dc boost converter circuit based on acceptance sampling is presented here. The validation process described in this paper is based on MIL-STD 3022 with emphasis on requirements settings and the testing process. The key contribution of this paper is the process for model and control algorithm validation specifically a method for decomposing the problem into model and control algorithm validation stages.
2016-09-20
Technical Paper
2016-01-2042
Chad N. Miller, Michael Boyd
This paper introduces a method for conducting experimental hardware in the-loop (xHIL) in which an advanced power emulator (APE) is used to emulate an electrical load on an electrical power system (EPS). The emulator, in this case, is commanded using an advanced real-time target which can leverage CPUs and field programmable gate arrays (FPGA) to meet strict real-time execution requirements. The paper will be broken into three challenge problems (1) develop a solution to target behavioral level models to an advanced computational device (2) develop a high-bandwidth power emulation capability and (3) integrate these two solutions into an xHIL experiment. Challenge (1) will be addressed by targeting a behavioral level model of a brushless DC motor drive with a pulsedwidth modulated inverter to a real-time system. The results of the real-time model will be compared to that of a non-real-time gold standard.
2016-09-20
Technical Paper
2016-01-1986
Qian Li, Balakrishnan Devarajan, Xuning Zhang, Rolando Burgos, Dushan Boroyevich, Pradeep Raj
The More Electric Aircraft (MEA) concept has continued evolving with the development of new electrical power conversion technology. As such, one of the main building blocks in advanced aircraft power systems are multi-converter power electronics systems that have demonstrated significant advantages in terms of reliability, efficiency and weight reduction. These power conversion units must provide energy under challenging mission profiles, which includes feeding pulsed power loads. The latter have been increasingly adopted—especially in military applications—demanding high peak power from these systems. Due to the nonlinear characteristic of a pulsed power load, when the load is on it consumes large amounts of power in a short period of time, which is subsequently followed by periods of low power consumption.
2016-09-20
Technical Paper
2016-01-2023
Timothy Deppen, Brian Raczkowski, Marco Amrhein, Jason Wells, Eric Walters, Mark Bodie, Soumya Patnaik
Future aircraft systems are projected to have order of magnitude greater power and thermal demands, along with tighter constraints on the performance of the power and thermal management subsystems. This trend has led to the need for a fully integrated design process where power and thermal systems, and their interactions, are considered simultaneously. To support this new design paradigm, the power quality analysis framework, developed previously, has been augmented to include thermal specifications. MIL-STD-2218 defines thermal design and cooling analysis requirements for airborne electrical equipment, while MIL-STD-704 defines transient, steady-state, and frequency-domain metrics for power quality. The proposed framework augments the power quality analysis framework developed for MIL-STD-704 and others, with a mathematical interpretation of the requirements given in MIL-STD-2218.
2016-09-20
Technical Paper
2016-01-2064
Shashank Krishnamurthy, Stephen Savulak, Yang Wang
The emergence of wide band gap devices has pushed the boundaries of power converter operations and high power density applications. It is desirable to operate a power inverter at high switching frequencies to reduce passive filter weight and at high temperature to reduce the cooling system requirement. The paper describes the design and test of a power electronic converter that converts a fixed input DC voltage to a variable voltage variable frequency three phase output. The component selection and design were constrained such that the converter can operate at and ambient temperature of 170C. The design of the key functional components such as the gate drive, power module, controller and communication will be discussed in the paper. Test results for the converter at high temperature will also be presented.
2016-09-20
Technical Paper
2016-01-2051
Andreas Himmler, Lars Stockmann, Dominik Holler
The application of a communication infrastructure for hybrid test systems is currently a topic in the aerospace and automotive industries. The demand for such a communication infrastructure is driven by the users’ need to run tests on hybrid test systems. These consist of individual, coupled test systems, each dedicated to different, even diverse needs. In the aerospace industry, there is a growing demand for modularity. Future laboratory tests means (LTM) must be scalable and exchangeable for maximum flexibility. Due to their very nature, hybrid test systems are used as integration test systems for large portions of the electronics of an aircraft (e.g., avionics, cabin) or even the complete aircraft electronics. Thus, these integration test systems need to handle high numbers of I/O channels and bus data. In order to make such test systems manageable and to enable a flexible use (e.g., to use only parts of such a system for dedicated tasks), using modular test systems makes sense.
2016-05-01
Journal Article
2015-01-9145
Abdullah AL-Refai, Osamah Rawashdeh, Rami Abousleiman
Abstract Lithium-Ion batteries are the standard portable power solution to many consumers and industrial applications. These batteries are commonly used in laptop computers, heavy duty devices, unmanned vehicles, electric and hybrid vehicles, cell phones, and many other applications. Charging these batteries is a delicate process because it depends on numerous factors such as temperature, cell capacity, and, most importantly, the power and energy limits of the battery cells. Charging capacity, charging time and battery pack temperature variations are highly dependent on the charging method used. These three factors can be of special importance in applications with strict charging time requirements or with limited thermal management capabilities. In this paper, three common charging methods are experimentally studied and analyzed. Constant-current constant-voltage, the time pulsed charging method, and the multistage constant current charging methods were considered.
2016-04-05
Technical Paper
2016-01-0015
Eldad Palachi, Fariz Saracevic, Amit Fisher
Abstract Connected vehicles provide suppliers and OEMs new opportunities to improve their customer experience and offer new services. Yet, in this new era of Internet of Things (IoT), OEMs and suppliers are expected to expand their engineering efforts beyond the vehicle itself. We present a new Rapid Application Development (RAD) service offered by IBM, called IBM Internet of Things Workbench. This is a visual tool, offered as an IBM Bluemix service that allows engineers to design and simulate the overall architecture and interactions between the various IoT entities such as devices, cloud applications and services, mobile clients and asset management systems. IoT Workbench abstracts the messaging details and generates code skeletons for the cloud applications as well as for simulating devices. It also provides the device simulation to allow for the application testing before the actual devices are available and the requirements for the various devices are validated.
2016-04-05
Technical Paper
2016-01-0022
Kenta Morishima, Shigeru Thomas Oho, Satoshi Shimada
Abstract A virtual power window control system was built in order to look into and demonstrate applications of microcontroller models. A virtual ECU simulated microcontroller hardware operations. The microcontroller program, which was written in binary digital codes, was executed step-by-step as the virtual ECU simulation went on. Thus, production-ready codes of ECUs are of primary interest in this research. The mechanical system of the power window, the DC motor to lift the window glass, the H-bridge MOSFET drivers, and the current sensing circuit to detect window locking are also modeled. This means that the hardware system of the control system was precisely modeled in terms of mechanical and circuit components. By integrating these models into continuous and discrete co-simulation, the power window control system was analyzed in detail from the microscopic command execution of the microcontroller to the macroscopic motion of the window mechanism altogether.
2016-04-05
Technical Paper
2016-01-1235
Johannes Gragger, Alessandro Zanon, Michele De Gennaro, Jonathan Juergens, Antonio Fricassè, Luca Marengo, Igor Olavarria, Jutta Kinder
Abstract The widespread of hybrid and battery electric vehicles is vital for the future of low-carbon mobility. In this context the delivery of affordable and efficient electric motor technologies together with high energy density storage devices are key aspects to enable the mass market take-off of electrified vehicles. The objective of this paper is to provide the scientific community with the results and design features of an innovative and rare-earth free electric motor technology based on the synchronous reluctance machine concept. This technology is capable to provide sufficient power density and higher driving cycle energy efficiency compared to the current state-of-the-art rare-earth permanent magnet synchronous machines used for automotive applications. The motor is designed to be integrated within a hatchback rear driving axle vehicle, achieving the maximum energy efficiency in urban operational conditions.
2016-04-05
Technical Paper
2016-01-1229
Douglas Cesiel, Charles Zhu
Abstract The electric vehicle on-board charger (OBC) is responsible for converting AC grid energy to DC energy to charge the battery pack. This paper describes the development of GM’s second generation OBC used in the 2016 Chevrolet Volt. The second generation OBC provides significant improvements in efficiency, size, and mass compared to the first generation. Reduced component count supports goals of improved reliability and lower cost. Complexity reduction of the hardware and diagnostic software was undertaken to eliminate potential failures.
2016-04-05
Technical Paper
2016-01-1232
Peng Yi, Zechang Sun, Xinjian Wang
Abstract Different choices of IGBTs’ switching frequency of the PMSM inverter used in vehicle lead to different energy loss of the inverter. Meanwhile, they lead to different phase current harmonics, which result in different energy loss of the PMSM. Compared with traditional switching frequency design method, the optimal design method considers the loss of the PMSM as well as the inverter, proposing a minimum system loss switching frequency design method. Firstly, by establishing the IGBT model (Hefner Model) and the PMSM analytical model, obtain PMSM phase currents under different switching frequencies through simulating. The inverter energy loss is obtained at the same time. Then, the phase currents under different conditions are applied to the finite element model to obtain the distribution of the magnetic field strength H and the magnetic induction B, so that the PMSM loss can be calculated.
2016-04-05
Technical Paper
2016-01-1220
Sinisa Jurkovic, Khwaja M. Rahman, Peter Savagian, Robert Dawsey
Abstract The Cadillac CT6 plug-in hybrid electric vehicle (PHEV) power-split transmission architecture utilizes two motors. One is an induction motor type while the other is a permanent magnet AC (PMAC) motor type referred to as motor A and motor B respectively. Bar-wound stator construction is utilized for both motors. Induction motor-A winding is connected in delta and PMAC motor-B winding is connected in wye. Overall, the choice of induction for motor A and permanent magnet for motor B is well supported by the choice of hybrid system architecture and the relative usage profiles of the machines. This selection criteria along with the design optimization of electric motors, their electrical and thermal performances, as well as the noise, vibration, and harshness (NVH) performance are discussed in detail. It is absolutely crucial that high performance electric machines are coupled with high performance control algorithms to enable maximum system efficiency and performance.
2016-04-05
Technical Paper
2016-01-1233
Kensuke Sasaki, Apoorva Athavale, Brent Gagas, Takashi Fukushige, Takashi Kato, Robert Lorenz
Abstract Variable flux permanent magnet synchronous machines (VFPMSMs) have been designed by using finite element analysis (FEA) to evaluate speed-torque capability considering requirement for magnetization state (MS) manipulation. However, due to its unique characteristic to change the MS, numerous combinations of design parameters need to be evaluated to achieve a final design. To accelerate the design process, this paper presents a method that consists of an equivalent magnetic circuit model and a process to obtain magnet width and thickness that satisfy target maximum torque and power factor (P.F.) capability. This model includes magnet operating point analysis under given magnet width and thickness condition to achieve target MS and avoid demagnetization at full load. This analysis provides desired stator magnetomotive force, magnet and stator induced flux linkage. Therefore, expected torque and P.F. capability is calculated.
2016-04-05
Journal Article
2016-01-1234
Toshikazu Sugiura, Atsushi Tanida, Kazutaka Tamura
Abstract The adoption of silicon carbide (SiC) power semiconductors is regarded as a promising means of improving the fuel efficiency of all types of electrically powered vehicles, including plug-in, electric, fuel cell, and hybrid vehicles (PHVs, EVs, FCVs, and HVs). For this reason, adoption in a wide variety of vehicles is currently being studied, including in the fuel cell (FC) boost converter of an FC bus. The FC boost converter controls the output voltage of the FC up to 650 V. In this research, SiC Schottky barrier diodes (SiC-SBDs) were adopted in the upper arm of an FC boost converter. Since the forward voltage (Vf) of SiC-SBDs is smaller than conventional Si-PiN diodes (Si-PiNDs), the conduction loss of SiC-SBDs is correspondingly smaller. Recovery loss can also be reduced by at least 90% compared to Si-PiNDs since the recovery current of SiC-SBDs is substantially smaller.
2016-04-05
Technical Paper
2016-01-1223
Yukiya Kashimura, Yuki Negoro
Abstract A second-generation power control unit (PCU) for a two-motor hybrid system is proposed. An optimally designed power module, which is a key component of the PCU, is applied to increase heat-resistant temperature, while the basic structure of the first generation is retained and the power semiconductor chip is directly cooled from the single side. In addition to the optimum design, by decreasing the power loss as well as increasing the heat-resistant temperature of the power semiconductors (IGBT: Insulated Gate Bipolar Transistor and FWD: Free Wheeling Diode), the proposed PCU has attained 25% higher power density and 23% smaller size compared to first-generation units, maintaining PCU efficiency (fuel economy). To achieve a high yield rate in the power module assembly process, a new screening technology is adopted at the initial stage of power module manufacturing.
2016-04-05
Technical Paper
2016-01-1224
Yosuke Osanai, Masaki Wasekura, Hideo Yamawaki, Yusuke Shindo
Abstract Reducing the loss of the power control unit (PCU) in a hybrid vehicle (HV) is an important part of improving HV fuel efficiency. Furthermore the loss of power devices (insulated gate bipolar transistors (IGBTs) and diodes) used in the PCU must be reduced since this amounts to approximately 20% of the total electrical loss in an HV. One of the issues for reducing loss is the trade-off relationship with reducing voltage surge. To restrict voltage surge, it is necessary to slow down the switching speed of the IGBT. In contrast, the loss reduction requires the high speed switching. One widely known method to improve this trade-off relationship is to increase the gate voltage in two stages. However, accurate and high-speed operation of the IGBT gate control circuit is difficult to accomplish. This research clarifies a better condition of the two-stage control and designed a circuit that improves this trade-off relationship by increasing the speed of feedback control.
2016-04-05
Journal Article
2016-01-1221
Kiyoshi Ito, Takumi Shibata, Takashi Kawasaki
Abstract Driving motors for hybrid vehicles and electric vehicles require magnet wires that can endure use at high voltages of 650 V or more. The magnet wire is a main motor component with the electromagnetic steel sheets and magnets. Conventional motors generally assure insulation by using the two parts of the magnet wire and insulate paper. But this increases the motor space factor and hinders weight reduction. A new magnet wire with high insulation performance was used by forming thermoplastic resin onto an enameled layer in order to reduce the number of insulating parts and enhance motor performance. The magnet wire (High-Voltage Wire: HVW) composed of polyetheretherketone (PEEK) resin . HVW can withstand the forming load during motor manufacture, secures durability for the automobile motor operating environment (Automatic Transmission Fluid: ATF), high temperatures) and can maintain high-voltage characteristics.
2016-02-01
Technical Paper
2016-28-0197
Nithin Alex John, Mona Sherki, Sanjay A Patil
Abstract New generation automobiles are equipped with power windows which eases the passenger’s effort in moving the vehicle windows up and down. Many of them are stuffed with advanced features like automatic up/down option for ensuring functionality with a single press of the switch. Even though it adds comfort to driver & passenger, inadvertent use of power window can be fatal if a person’s body part gets trapped inside. An effective solution for this problem is anti-pinch mechanism, which releases the object safely just when it gets trapped. It detects the object trapped and immediately moves the window down so that trapped object will get released easily. The anti-pinch algorithm used in this project is based on the “Method of Monitoring Movable Element”, method monitor traveling distance of a power window pane. In order to achieve this different from conventional techniques we are using Ultrasonic sensor.
2015-09-15
Technical Paper
2015-01-2412
Tao Yang, Serhiy Bozhko, Greg Asher
This paper aims to develop a general functional model of multi-pulse Auto-Transformer Rectifier Units (ATRUs) for More-Electric Aircraft (MEA) applications. The ATRU is seen as the most reliable way readily to be applied in the MEA. Interestingly, there is no model of ATRUs suitable for unbalanced or faulty conditions at the moment. This paper is aimed to fill this gap and develop functional models suitable for both balanced and unbalanced conditions. Using the fact that the DC voltage and current are strongly related to the voltage and current vectors at the AC terminals of ATRUs, a generic functional model has been developed for both symmetric and asymmetric ATRUs. The developed functional models are validated through simulation and experiment. The efficiency of the developed model is also demonstrated by comparing with corresponding detailed switching models. The developed functional model shows significant improvement of simulation efficiency, especially under balanced conditions.
2015-04-14
Technical Paper
2015-01-1202
Weimin Zhang, Saeed Anwar, Daniel J. Costinett, Fred Wang
Abstract A cost-effective SiC based hybrid switch and an improved inductor design procedure for boost converter in electric vehicles (EVs) and hybrid electric vehicles (HEVs) are presented in this paper. The feasibility of a hybrid switch using low power SiC MOSFET and high power Si IGBT is investigated to provide a cost-effective and failure-resistant method to employ the fast switching characteristics of SiC devices. The operation of the hybrid switch is tested in double pulse test experiment and compared with the single IGBT. Additionally, the boost inductor design is discussed, which allows the optimization of weight and power loss across different core materials. An improved powder core inductor design procedure is presented to avoid the iterative design procedure provided by the manufacture. Both the powder material and nanocrystalline material are considered in the inductor design procedure.
2015-04-14
Technical Paper
2015-01-1203
Subhashree Rajagopal, Sebastien Desharnais, Balamurugan Rathinam, Upendra Naithani
Abstract Electromagnetic brakes are found in a variety of applications. They offer tremendous advantages including: absence of fading, high braking torque and controllability. However they suffer from decreasing torque at low and high speeds. In this study, a novel concept of permanent magnet eddy-current brake is proposed that maintains a flat braking torque profile over a broad speed range. The principle is analytically investigated and numerically validated through finite element simulations using MAXWELL. It is demonstrated that a usably flat braking torque profile can be achieved by altering the path of eddy-currents by magnetic field orientation, thereby affecting the apparent rotor resistance.
2015-04-14
Journal Article
2015-01-1201
Mohammad Anwar, Monty Hayes, Anthony Tata, Mehrdad Teimorzadeh, Thomas Achatz
Abstract The Chevrolet Volt is an electric vehicle with extended-range that is capable of operation on battery power alone, and on engine power after depletion of the battery charge. First generation Chevrolet Volts were driven over half a billion miles in North America from October 2013 through September 2014, 74% of which were all-electric [1, 12]. For 2016, GM has developed the second-generation of the Volt vehicle and “Voltec” propulsion system. By significantly re-engineering the traction power inverter module (TPIM) for the second-generation Chevrolet Volt extended-range electric vehicle (EREV), we were able to meet all performance targets while maintaining extremely high reliability and environmental robustness. The power switch was re-designed to achieve efficiency targets and meet thermal challenges. A novel cooling approach enables high power density while maintaining a very high overall conversion efficiency.
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