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TRIMIS

Novel Coating Systems For Power Electronics In Aerospace Environments

PROJECTS
Funding
European
European Union
Duration
-
Status
Complete with results
Geo-spatial type
Other
Total project cost
€484 234
EU Contribution
€363 175
Project Acronym
PECOAT
STRIA Roadmaps
Transport electrification (ELT)
Vehicle design and manufacturing (VDM)
Transport mode
Airborne icon
Transport policies
Safety/Security
Transport sectors
Passenger transport,
Freight transport

Overview

Call for proposal
SP1-JTI-CS-2011-03
Link to CORDIS
Objectives

Power electronic converters used in aircraft have previously been used at reasonably low voltages which have not been associated with a significant risk of electrical discharge. Items such as circuit boards are designed in accordance with standards such as IPC2221A but this is often seen as conservative. Given the drive to the more electric aircraft and the need to increase power density of the electrical sub-systems, power electronic converters are now at increased risk of electrical discharge given the increase in voltage and are under increased pressure to remain as compact and light weight as possible. This project identified a coating that could be applied to power electronic converter components to reduce the risk of electrical discharge and also identified suitable techniques for integrating the application of this coating within a manufacturing environment.

Coatings applied to high voltage equipment can reduce the risk of electrical discharges. Conformal coatings based on polymer films have been applied commercially onto electronic circuit boards. However, they might not be suitable to be used in low pressure operation of high voltage power electronics reliably given the relatively poor performance of such coatings when exposed to tracking / partial discharge.

We examined the options for the deployment of novel and cost-effective coatings to be placed onto the printed circuit boards and power electronic components that may require protection in open box power electronics. Our focus developed:

  • A coating type that can withstand the aerospace environment;
  • A coating that when applied to open box power electronics will inherently reduce the risk of electrical discharge;
  • A coating that is straightforward to apply (ideally using techniques identical to those in present manufacturing);
  • A coating that can withstand damage from electrical discharges should a localised defect occur which allows these to take place.

Funding

Parent Programmes
Institution Type
Public institution
Institution Name
European Commission
Type of funding
Public (EU)
Specific funding programme
JTI-CS - Joint Technology Initiatives - Clean Sky
Other Programme
JTI-CS-2011-3-SGO-02-033 Optimisation of coating for the opeartion of power electronis with "open box" -housing in high altitude and identification of pass and fail criteria for respective corona testing

Results

Executive Summary:

Power electronic converters used in aircraft have previously been used at reasonably low voltages which have not been associated with a significant risk of electrical discharge. Items such as circuit boards are designed in accordance with standards such as IPC2221A but this is often seen as conservative. Given the drive to the more electric aircraft and the need to increase power density of the electrical sub-systems, power electronic converters are now at increased risk of electrical discharge given the increase in voltage, and are under increased pressure to remain as compact and light weight as possible. The drive for this project was to identify a coating that could be applied to power electronic converter components to reduce the risk of electrical discharge and identify suitable techniques for integrating the application of this coating within a manufacturing environment.

The use of any high voltage system on an aircraft introduces a risk of damage from electrical discharge. This risk is exacerbated by low pressure, humid and variable temperature environments. Electrical discharge can be subdivided into three categories; disruptive discharge, partial discharge, and tracking. The risk from all of these must be considered in the design of any insulation system. As aerospace power systems move to higher voltage, these forms of discharge must be considered in their design. At present, there is little guidance in this area and SAE have recognised this through the development of an Aerospace Information Report ‘High Voltage Design Guidelines for Aerospace Systems’. In addition to producing a system for coating open-box power electronic systems, this project intended to provide guidance to the partners in this area and accelerate progress to a standardised method of ensuring power electronic reliability with regards high voltage discharge.

The project therefore sought to develop:

  • A coating type that can withstand the aerospace environment;
  • A coating that when applied to open box power electronics will inherently reduce the risk of electrical discharge;
  • A coating that is straightforward to apply (ideally using techniques identical to those in present manufacturing);
  • A coating that can withstand damage from electrical discharges should a localised defect occur which allows these to take place.

The principal output from the project was a recommendation for the partner on a specific type of coating that, when used with an appropriate thickness and track spacing, would be robust against all form of electrical discharges. The recommendations covered the way in which a printed circuit board should be designed when such a coating is used and the methodology for applying the coating.

Partners

Lead Organisation
Organisation
The University Of Manchester
Address
OXFORD ROAD, MANCHESTER, M13 9PL, United Kingdom
Organisation website
EU Contribution
€363 175
Partner Organisations
EU Contribution
€0

Technologies

Technology Theme
Aircraft design and manufacturing
Technology
Power electronics
Development phase
Research/Invention

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