Investigation of electric vehicle EMI

Issued as Monthly progress reports no. 1-16, Expenditures plans no. [1-2], Program schedules no. [1-2], and Technical reports no. [1-4], Project A-308

Assessment and analysis of the electromagnetic profile of prototype high-power-charging units for electric vehicles

This science for policy report discusses and analyses the electromagnetic compatibility (EMC) performance of three High-Power-Charging (HPC) columns at their standby based on IEC 61851-21-2 standard. All laboratory setups and results of the tests that are presented on this work were carried out inside VeLA 9 validated EMC semi-anechoic chamber (SAC) at the Joint Research Centre of the European Commission. The results of more than 150 different measured setups on radiated emissions, conducted emissions and radiated immunity are presented and discussed thoroughly. The applicable test methodologies and instrumentation used for the measurements are fully described. EMC troubleshooting techniques were also successfully carried out for some setups, while novel exploratory work, beyond IEC 61851-21-2 was also conducted. The findings and test data on this study can be a reference material to EMC engineers and contribute to the future policy making of the relevant EMC standards.JRC.C.4-Sustainable Transpor

Electronic systems failures and anomalies attributed to electromagnetic interference

The effects of electromagnetic interference can be very detrimental to electronic systems utilized in space missions. Assuring that subsystems and systems are electrically compatible is an important engineering function necessary to assure mission success. This reference publication will acquaint the reader with spacecraft electronic systems failures and anomalies caused by electromagnetic interference and will show the importance of electromagnetic compatibility activities in conjunction with space flight programs. It is also hoped that the report will illustrate that evolving electronic systems are increasingly sensitive to electromagnetic interference and that NASA personnel must continue to diligently pursue electromagnetic compatibility on space flight systems

Переклад термінології у галузі електроніки, електротехніки та енергетики з англійської на українську мову

У посібнику подано аутентичні матеріали та вправи з письмового та усного перекладу в галузі електротехніки, електроніки та енергетики; тексти для самостійної роботи, контрольні завдання з перекладу, а також англо-український та українсько-англійський словник термінів та понять електротехніки, електроніки та енергетики. Розраховано на студентів спеціальності "Переклад (англійська мова)" і аспірантів технічних спеціальностей.The book presents authentic materials and exercises in written and oral translation in the field of electronics, electrical engineering and power engineering; texts for independent home translation, English–Ukrainian and Ukrainian-English vocabularies of specific terms. For the students of "Translation and Interpreting" departments and post-graduate students of technical specialities

Aircraft electromagnetic compatibility

Illustrated are aircraft architecture, electromagnetic interference environments, electromagnetic compatibility protection techniques, program specifications, tasks, and verification and validation procedures. The environment of 400 Hz power, electrical transients, and radio frequency fields are portrayed and related to thresholds of avionics electronics. Five layers of protection for avionics are defined. Recognition is given to some present day electromagnetic compatibility weaknesses and issues which serve to reemphasize the importance of EMC verification of equipment and parts, and their ultimate EMC validation on the aircraft. Proven standards of grounding, bonding, shielding, wiring, and packaging are laid out to help provide a foundation for a comprehensive approach to successful future aircraft design and an understanding of cost effective EMC in an aircraft setting

Wireless Power Transfer

Wireless power transfer techniques have been gaining researchers' and industry attention due to the increasing number of battery-powered devices, such as mobile computers, mobile phones, smart devices, intelligent sensors, mainly as a way to replace the standard cable charging, but also for powering battery-less equipment. The storage capacity of batteries is an extremely important element of how a device can be used. If we talk about battery-powered electronic equipment, the autonomy is one factor that may be essential in choosing a device or another, making the solution of remote powering very attractive. A distinction has to be made between the two forms of wireless power transmission, as seen in terms of how the transmitted energy is used at the receiving point: - Transmission of information or data, when it is essential for an amount of energy to reach the receiver to restore the transmitted information; - Transmission of electric energy in the form of electromagnetic field, when the energy transfer efficiency is essential, the power being used to energize the receiving equipment. The second form of energy transfer is the subject of this book

Advanced flight control system study

The architecture, requirements, and system elements of an ultrareliable, advanced flight control system are described. The basic criteria are functional reliability of 10 to the minus 10 power/hour of flight and only 6 month scheduled maintenance. A distributed system architecture is described, including a multiplexed communication system, reliable bus controller, the use of skewed sensor arrays, and actuator interfaces. Test bed and flight evaluation program are proposed

Avionics system design for high energy fields: A guide for the designer and airworthiness specialist

Because of the significant differences in transient susceptibility, the use of digital electronics in flight critical systems, and the reduced shielding effects of composite materials, there is a definite need to define pracitices which will minimize electromagnetic susceptibility, to investigate the operational environment, and to develop appropriate testing methods for flight critical systems. The design practices which will lead to reduced electromagnetic susceptibility of avionics systems in high energy fields is described. The levels of emission that can be anticipated from generic digital devices. It is assumed that as data processing equipment becomes an ever larger part of the avionics package, the construction methods of the data processing industry will increasingly carry over into aircraft. In Appendix 1 tentative revisions to RTCA DO-160B, Environmental Conditions and Test Procedures for Airborne Equipment, are presented. These revisions are intended to safeguard flight critical systems from the effects of high energy electromagnetic fields. A very extensive and useful bibliography on both electromagnetic compatibility and avionics issues is included

Technology for large space systems: A bibliography with indexes (supplement 14)

This bibliography lists 645 reports, articles and other documents introduced into the NASA scientific and technical information system between July 1, 1985 and December 31, 1985. Its purpose is to provide helpful information to the researcher, manager, and designer in technology development and mission design according to system, interactive analysis and design, structural and thermal analysis and design, structural concepts and control systems, electronics, advanced materials, assembly concepts, propulsion, and solar power satellite systems