ILDAS - In-flight Lightning Strike Damage Assessment System
Overview
Background & policy context:
Commercial passenger aircraft are on average struck by lightning once a year. The effects of lightning on aircraft and helicopters are minimal for low-amplitude strikes, but higher-amplitude strikes may result in expensive delays and important repair and maintenance.
The present certification threat level is derived from cloud-to-ground lightning strike data measured on instrumented towers. While historically this threat definition has served the purpose of lightning protection adequately on metallic airframes, modern aircraft incorporate an increasing amount of composite materials that make them more susceptible to damage. Moreover, aircraft now employ more high-authority electronic control systems that are susceptible to upset and damage. As a result of the introduction of extra protection measures the advantages of modern materials could be cancelled by the addition of weight and higher cost.
To be able to design appropriate lightning protection, fixed-wing aircraft and helicopter manufacturers have a strong need for a good definition of the threat that lightning poses to aircraft.
Objectives:
The first objective of the ILDAS research project was to develop and validate a concept prototype of an ILDAS, capable of in-flight measurement of the parameters of lightning strikes. Such a system would, in due course, provide better knowledge of these parameters that could be used to improve aircraft lighting protection. Based on the reconstructed attachment points and amplitudes of the in-flight lightning strike in real time, the second objective was to enable the development of tailored and efficient maintenance inspection procedures that must be applied after a recorded strike.
Methodology:
In order to achieve these objectives, it was necessary to develop a measurement system concept prototype. ILDAS uses advanced sensor techniques that enables characterization of lightning strike parameters from the measured electric fields on, and the current flowing in the aircraft skin. For the purpose of measured data interpretation, the development and implementation of an innovative Inverse Method, based on a numerical simulation of the lightning current propagation, was performed. Finally a database concept was realised, enabling subsequent exploitation.
The validation of the various types of sensors and the entire ILDAS Concept Prototype system has been done. The validation comprised simulated lightning tests on a bespoke rig fitted with the system in the UK and its installation and ground testing on an Airbus A320 in France. Characterisation of current flow patterns from simulated strikes to a helicopter has been done in Germany.
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