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Design of Optimum Torsionally Flexible PropRotors for Tilt-Body MAVs

Mohd Zawawi, Fazila and Morlier, Joseph and Grondin, Gilles and Moschetta, Jean-Marc Design of Optimum Torsionally Flexible PropRotors for Tilt-Body MAVs. (2012) Applied Mechanics and Materials - AEROTECH IV - Recent Advances in Aerospace Technologies, 225. 281-286. ISSN 1660-9336

(Document in English)

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Official URL: http://www.scientific.net/AMM.225.281


This paper presents a methodology to design the optimum proprotor for tilt-body microair-vehicles (TB-MAV) with efficient global propulsion system and long flight endurance in both cruise and hover modes. The TB-MAV developed at ISAE, which is called MAVion, was used as a baseline in the design process. To acquire maximum performance of TB-MAV’s global propulsion system, an efficient optimization process of the proprotor propulsion system was carried out. The optimization process consists of two-step inverse design methods. The first step determines the optimal operating conditions in terms of power and rotational speed of proprotor and the second step designs the optimal blade geometry in terms of twist angle distribution. The optimal blade twist distribution along the blade was computed using the Glauert’s strip theory for minimum energy loss condition. Meanwhile, the optimal operating conditions were determined by the motor outputs corresponding to high motor efficiency. A comparison of performance in terms of total efficiency and flight endurance between the optimized flexible proprotor, the optimized rigid proprotor, optimized propeller and optimized rotor is presented.

Item Type:Article
Additional Information:AEROTECH IV, 21-22 November, 2012, Kuala Lumpur, Malaysia, ISBN des actes de conférence : 978-3-03785-506-5
HAL Id:hal-01853129
Audience (journal):International peer-reviewed journal
Uncontrolled Keywords:
Institution:Université de Toulouse > Ecole nationale supérieure des Mines d'Albi-Carmaux - IMT Mines Albi (FRANCE)
Université de Toulouse > Institut National des Sciences Appliquées de Toulouse - INSA (FRANCE)
Université de Toulouse > Institut Supérieur de l'Aéronautique et de l'Espace - ISAE-SUPAERO (FRANCE)
Université de Toulouse > Université Toulouse III - Paul Sabatier - UT3 (FRANCE)
Other partners > Universiti Teknologi Malaysia - UTM (MALAYSIA)
Laboratory name:
Deposited On:03 Dec 2012 14:30

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