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A Smart Icing Detection System for Any Location on the Outer Aircraft Surface
ISSN: 0148-7191, e-ISSN: 2688-3627
Published June 10, 2019 by SAE International in United States
This content contains downloadable datasetsAnnotation ability available
Given approximately one million small and light aircraft in operation worldwide, icing detection and icing quantification of in-flight icing are still an open research topic. Despite technical means are available to de-ice on ground, there is a lack of a suitable control system based on sensor data to de-ice while the aircraft is airborne. Most often, it is still task of the pilot to visually inspect the icing status of the airfoil and/or other critical parts of the aircraft such as engine air intakes, which distracts the flight crew from flying the aircraft especially in IMC conditions. Based on preliminary simulation and tests in 2014 in a collaborative research project lasting from 2015 until 2018, the technology of energy self-sustaining, wireless, self-adhesive smart sensors for industrial sensing in an aerodynamically critical environment (i.e. wind turbines) was further investigated to fulfil general aviation requirements. Prototype hardware setups have been designed and built for application on aircraft. In test flights carried out in Scotland in late 2017, the functionality of the system could be demonstrated. It could be shown that a wireless, energy self-sustaining detection system for early icing can be implemented based on currently available technologies and components. Additionally, it could be shown that detection sensitivity is sufficient to detect ice at very thin layers.
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CitationSchlegl, T., Moser, M., Loss, T., and Unger, T., "A Smart Icing Detection System for Any Location on the Outer Aircraft Surface," SAE Technical Paper 2019-01-1931, 2019, https://doi.org/10.4271/2019-01-1931.
Data Sets - Support Documents
|[Unnamed Dataset 1]|
- Jackson, D. and Goldberg, J. , “Ice Detection Systems: A Historical Perspective,” SAE Technical Paper 2007-07-3325, 2007, doi:10.4271/2007-01-3325.
- On-Wings Report Summary, FP7-Transport, 2012, http://cordis.europa.eu/publication/rcn/16503_en.html
- U.S. Department of Transportation Federal Aviation Administration, Advisory Circular AC No: 91-74A Pilot Guide: Flight In Icing Conditions, 12/31/07.
- SAE Aerospace Standard AS5498, ‘Minimum Operational Performance Specification for Inflight Icing Detection Systems’, 2001.
- Schlegl, T., Moser, M. and Zangl, H. , ‘Wireless and Flexible Ice Detection on Aircraft’, in Proceedings of the SAE International Conference on Icing of Aircraft, Engines, and Structures, Prague, 2014
- Schlegl, T. and Zangl H. , Chapter ‘Capacitive Sensing for Safety Applications’, In: ‘Technologies for Smart Sensors and Sensor Fusion’, CRC Press, 2014
- Gietler, H., Stetco, C., Leitzke, J.P. and Zangl, H. , “On-Wing Temperature Estimation and Control for Anti-Icing System’, I2MTC 2019, New Zealand (submitted)
- Leitzke, J.P. and Zangl, H. , ‘Feasibility of Wireless Pressure Sensors for Aircraft’, in 2017 IEEE International Instrumentation and Measurement Technology Conference (I2MTC), Torino, 2017, 1-5, doi:10.1109/I2MTC.2017.7969780
- Leitzke, J.P. and Zangl, H. , ‘Wireless Differential Pressure Measurement for Aircraft’, in 2017 IEEE International Workshop on Metrology for AeroSpace (MetroAeroSpace), Padova, 2017, 164-168 doi:10.1109/MetroAeroSpace.2017.7999556
- Leitzke, J. P., Della Mea, A., Faller, L., Muehlbacher-Karrer, S. and Zangl, H. , ‘Wireless Differential Pressure Measurement for Aircraft’, Measurement 122, July 2018, 459-465
- Stocksreiter, W., Zangl, H. , Moser and Moser, M., ‘Environmental Impacts on Antennas for Wireless Sensors on Outer Aircraft Surfaces’, in 2017 IEEE International Workshop on Metrology for AeroSpace, Padova, 2017, 496-501. doi:10.1109/MetroAeroSpace.2017.7999625
- Stocksreiter, W., Zangl, H., Glaser, D., Kaur, M. and Moser, M. , ‘Compact Wireless Ice Detection System with Electrode Used as Antenna’, in IMEKO World Congress 2018, Belfast, UK, Sep. 2018