Abstract
The use of power electronics associated with the drive toward higher voltages in more compact and lighter allelectric aircraft introduces new risks and failure modes. Boards are often coated for added protection; however, the performanceand level of protection provided by various coatings in these environments, after some degree of degradation, is not well characterised. Partial discharge has been identified as a particularly significant and aggressive source of coatingdegradation which can lead to electrical failure.A series of experiments have attempted to characterise the magnitude and nature of damage from partial discharge on a silicone coating as a function of applied voltage above partial discharge inception. Simple coated boards designed aroundindustry test standards (IPC2221A and IEC60664) were left to age and degrade while subjected to partial discharge of a given magnitude and were periodically observed under a microscope. The nature of the damage and its evolution was observed in a range of cases and these observations are presented.
Original language | English |
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Title of host publication | Electrical Insulation Conference (EIC), 2015 IEEE |
Publisher | IEEE |
Pages | 420-423 |
Number of pages | 4 |
DOIs | |
Publication status | Published - Jun 2015 |
Event | Electrical Insulation Conference (EIC), 2015 IEEE - Seattle, Washington, United States Duration: 7 Jun 2015 → 10 Jun 2015 |
Conference
Conference | Electrical Insulation Conference (EIC), 2015 IEEE |
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Country/Territory | United States |
City | Seattle, Washington |
Period | 7/06/15 → 10/06/15 |
Keywords
- Aerospace; Partial Discharge; PCB Coating; All- Electric Aircraft, Power Electronics