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Aile adaptable : design du système d'actionnement de l'aileron rigide, caractérisation des capteurs de pression et instrumentation pour des tests statiques

Translated title of the thesis: Morphing wing : rigid aileron actuation system design, pressure sensor caracterisation and statique test monitoring
  • Jean-Baptiste Vincent

Student thesis: Master's thesisMaster in Engineering: Engineering

Abstract

This Master’s thesis is part of a multidisciplinary optimisation project initiated by the Consortium for Research and Innovation in Aerospace in Québec (CRIAQ) ; this project is about designing and manufacturing a morphing wing demonstrator. The morphing design adopted in this project is based on airfoil thickness variation applied to the upper skin. This morphing generates a change in the laminar to turbulent boundary layer transition position on top of the wing. The position of this transition area leads to significant changes in the aerodynamic performance of the wing. The study presented here focuses on the design of the conventional aileron actuation system and on the characterization of the high sensitivity differential pressure sensors installed on the upper skin in order to determine the laminar to turbulent transition position. Furthermore, the study focuses on the data acquisition system for the morphing wing structural test validation. The aileron actuation system is based on a linear actuator actuated by a brushless motor. The component choice is presented as well as the command method. A static validation as well as wind tunnel validation is presented. The pressure sensor characterization is performed by installing three of those high sensitivity differential pressure sensors in a bi-dimensional known airfoil. This study goes through the process of determining the sensor position in order to observe the transition area by using a computational fluid dynamics (CFD) statistic approach. The validation of the laminar to turbulent transition position is carried out with a series of wind tunnel tests. A structural test has been executed in order to validate the wing structure. This Master’s thesis shows the data acquisition system for the microstrain measurement installed inside the morphing wing. A hardware and software architecture description is developed and presented as well as the practical results.
Date8 Dec 2015
Original languageFrench
Awarding Institution
  • École de technologie supérieure
SupervisorRuxandra Botez (Supervisor)

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