Design Criteria of a Thermal Mass Flow Sensor for Aircraft Air Data Applications

L. C. Ribeiro, M. L. Oliveira, R. A. Souza, S. P. L. Vieira, W. O. Avelino, C. F. R. Oliveira, S. W. de Lima Monteiro, F. S. Torres, Roana Melina de Oliveira Hansen

Publikation: Konferencebidrag uden forlag/tidsskriftPaperForskningpeer review

Abstrakt

The operating environment of aircraft air-data sensors is extremely aggressive with a wide temperature and humidity variation, suspension particles, icing and etc. The Pitot tube is widely used as air-data sensor on aircrafts, which has had many operational issues reported in the past decades due to ice-crystal obstruction of its aperture. The Microelectromechanical Systems (MEMS) technology associated with Thermal Mass Flow Sensors (TMFS) can establish a reformulation on air-data system instrumentation, since it is possible to create micro heaters and thermal sensors on the same substrate without moving parts, simplifying the operational requirements compliant to the aeronautics specifications. Exploring the simplicity and robustness of MEMS technology, a TMFS is herein designed according to criteria that meet aeronautic performance requirements, selecting adequate dimensions of the various structures in the sensor and materials compatible with semiconductor micromachining processes. This paper also presents the numerical results of the interaction of a thermal mass flowing through the integrated heater element of the sensor.

OriginalsprogEngelsk
Publikationsdatosep. 2018
StatusUdgivet - sep. 2018
Begivenhed31st Congress of the International Council of the Aeronautical Sciences - Belo Horizonte, Brasilien
Varighed: 9. sep. 201814. sep. 2018

Konference

Konference31st Congress of the International Council of the Aeronautical Sciences
LandBrasilien
ByBelo Horizonte
Periode09/09/201814/09/2018

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