This paper presents a procedure to design EMI filters to reduce the electromagnetic disturbances generated by electrical apparatus used in avionic environment. The method proposed can be useful to save weight and size of the attenuation systems, and keep their effectiveness in agreement with the standard requirements. A design of a set of different filters with different topological characteristics is presented for a case study about an electrical actuator used for an aircraft onboard application. Performances and reliabilities of the attenuation systems are assessed by suitable full compliance experimental tests.
|Titolo della pubblicazione ospite||IEEE 4th International Forum on Research and Technologies for Society and Industry, RTSI 2018 - Proceedings|
|Numero di pagine||6|
|Stato di pubblicazione||Published - 2018|
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