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Assessment of arc tracking hazards in high voltage aerospace systems

Project description

Arc tracking in new higher voltage aeroplanes

As we move towards cleaner and more efficient forms of transport, the aviation industry is using more electric technology. Existing electrical wiring systems on aircraft operate at low voltages (115V AC/28V DC). Certain types of faults in the wiring of these systems can cause significant damage to the wiring with a risk of fire. This is managed in existing systems by careful selection of the insulation material and testing. The new aircraft being developed will require the use of higher voltages. The voltage level of their electrical systems may increase to 3kV or above. The EU-funded ARCTRACK project will study whether arc tracking failure poses a significant risk in these new higher voltage systems.

Objective

Electrical wiring systems on aircraft have traditionally operated at low voltages (115V AC / 28V DC). The insulation system used in the wiring systems is not subject to significant levels of electrical stress but thermal and chemical degradation / mechanical damage can allow the insulation to be breached. If two wires / a wire and a ground plane are then breached by a conductive fluid (from a leaking pipe / condensation) or by making contact with a conductive surface (such as a bulkhead), current will then flow. The magnitude of the current is then limited by the electric arc that forms between the wires with the arc voltage being of a similar magnitude to the system voltage. These arcing events are therefore difficult to detect given their intermittent nature and the relatively small levels of current that flow. However, they can cause significant damage. A recent example was the loss of an F35B where an electrical fault caused by an incorrectly installed bracket then caused the failure of a hydraulic line and a fire.

As we development hybrid and all electric aircraft, the voltage level of the on-board electrical systems is expected to climb to 0.75-3kV (the lower voltages being used for VTOL air taxis and the higher voltages being used in regional jet applications such as the E Fan X demonstrator). The use of higher voltages, the change in component technology (such as using screened instead of unscreened cables), system configuration (grounded / ungrounded) and use of composite structures within the aircraft will all impact on arc tracking.

This project aims to deliver a clear understanding of the arc tracking hazard in these new higher voltage systems and describe ways in which it can be quantified and mitigated.

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IA - Innovation action

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(opens in new window) H2020-CS2-CFP09-2018-02

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Coordinator

THE UNIVERSITY OF MANCHESTER
Net EU contribution

Net EU financial contribution. The sum of money that the participant receives, deducted by the EU contribution to its linked third party. It considers the distribution of the EU financial contribution between direct beneficiaries of the project and other types of participants, like third-party participants.

€ 310 947,50
Address
OXFORD ROAD
M13 9PL Manchester
United Kingdom

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Region
North West (England) Greater Manchester Manchester
Activity type
Higher or Secondary Education Establishments
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Total cost

The total costs incurred by this organisation to participate in the project, including direct and indirect costs. This amount is a subset of the overall project budget.

€ 310 947,50

Participants (2)

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