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| Tekkaya, A. Erman |
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| Förster, Peter |
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| Mudimu, George T. |
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| Shibata, Lillian Marie |
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| Talabbeydokhti, Nasser |
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| Laffite, Ernesto Dante Rodriguez |
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| Schöpke, Benito |
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| Gobis, Anna |
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| Alfares, Hesham K. |
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| Münzel, Thomas |
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| Joy, Gemini Velleringatt |
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| Oubahman, Laila |
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| Filali, Youssef |
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| Philippi, Paula |
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| George, Alinda |
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| Lucia, Caterina De |
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| Avril, Ludovic |
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| Belachew, Zigyalew Gashaw |
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| Kassens-Noor, Eva | Darmstadt |
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| Cho, Seongchul |
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| Tonne, Cathryn |
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| Hosseinlou, Farhad |
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| Ganvit, Harsh |
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| Schmitt, Konrad Erich Kork |
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| Grimm, Daniel |
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Pecora, Rosario
in Cooperation with on an Cooperation-Score of 37%
Topics
Publications (15/15 displayed)
- 2019Electro-Actuation System Strategy for a Morphing Flapcitations
- 2019Description of Position Control Laws for Functionality Test of a Bi-modal Morphing Flap
- 2018Electro-Actuation System Strategy for a Morphing Flapcitations
- 2018Structural design of a multifunctional morphing fowler flap for a twin-prop regional aircraft
- 2018Feasibility studies for the installation of Plasma Synthetic Jet Actuators on the skin of a morphing wing flapcitations
- 2017An adaptive trailing edgecitations
- 2017Experimental validation of a true-scale morphing flap for large civil aircraft applicationscitations
- 2017Preliminary aeroelastic assessment of a large aeroplane equipped with a camber-morphing aileroncitations
- 2016An adaptive trailing edge for large commercial aircraftcitations
- 2016Safety and Reliability Aspects of an Adaptive Trailing Edge Device (ATED)citations
- 2016Actuation and control of a novel wing flap architecture with bi-modal camber morphing capabilitiescitations
- 2015Actuation System Design for a Morphing Aileroncitations
- 2014Multi-parametric flutter analysis of a morphing wing trailing edge
- 2014Actuation System Design for a Morphing Wing Trailing Edgecitations
- 2013Trade-off flutter analysis of a morphing wing trailing edge
Places of action
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booksection
Actuation System Design for a Morphing Aileron
Abstract
In the field of European and International morphing structures projects, the CRIAQ MD0-505 enables collaboration among Italian and Canadian research centers and industries paying particular attention to the development of innovative design in the area of adaptive technologies. The main project goals involve the design of a wing trailing edge device capable to improve aerodynamic efficiency in all the flight envelope leading to fuel consumption reduction with positive impact on aircraft weight. This paper deals with the design and modeling of a novel actuation system of a full scale morphing aileron for a regional aircraft wing. The proposed aileron architecture is characterized by segmented adaptive ribs. Each rib is composed of two movable blocks connected by means of rotational hinges in which are housed bearings and bushing in a finger-like mechanism. Rib actuation is guaranteed by an actuation system composed of a dedicated kinematic chain derived from a quick-return mechanism. In order to achieve the aileron target shapes, the system is driven by a set of servo-rotary electro mechanical actuators that permit a highly integrated design which lays the groundwork for the technological transition from the torque shaft to the distributed actuation architecture.
Topics
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