학술논문

Assessment of lightning transients on a de-iced rotor blade with predictive tools and coaxial return measurements
Document Type
Conference
Source
2012 ESA Workshop on Aerospace EMC Aerospace EMC, 2012 Proceedings ESA Workshop on. :1-6 May, 2012
Subject
Aerospace
Communication, Networking and Broadcast Technologies
Components, Circuits, Devices and Systems
Fields, Waves and Electromagnetics
Transportation
Signal Processing and Analysis
Blades
Solid modeling
Computational modeling
Integrated circuit modeling
Frequency measurement
Predictive models
Rotors
Language
Abstract
The increasing use of composite materials in aircrafts primary structures has led to different problematics in the field of safety of flight in lightning conditions. The consequences of this technological mutation, which occurs in a parallel context of extension of electrified critical functions, are addressed by aircraft manufacturers through the enhancement of their available assessment means of lightning transient. On the one hand, simulation tools, provided an accurate description of aircraft design, are today valuable assessment tools, in both predictive and operative terms. On the other hand, in-house test means allow confirmation and consolidation of design office hardening solutions. The combined use of predictive simulation tools and in-house test means offers an efficient and reliable support for all aircraft developments in their various life-time stages. The present paper provides PREFACE research project results that illustrate the above introduced strategy on the de-icing system of the NH90 composite main rotor blade.