MMT-05 SILICON-BASED FLAPPING WINGS USING SELF-ACTUATED STRESS DISTRIBUTION
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概要
- 論文の詳細を見る
The objective of this project is to develop a battery - powered ornithopter Micro Air Vehicle (MAV) using MEMS technology. The major goal of the MAV project focuses on flapping wing propulsion systems. This paper summarizes the bottom-up design approach involved in new IC-processed micrometer thick silicon wings. The proposed MEMS - based wings have been designed so as to allow two degrees of freedom : flapping and feathering. The wings are actuated through nearly 20,000 elementary actuation cells that are distributed over the upper surface of single crystal silicon structures.
著者
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MOAL Patrice
Laboratoire de Mecanique Appliquee R. Chaleat(LMARC)
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BOURBON Gilles
Laboratoire de Mecanique Appliquee R. Chaleat(LMARC)
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JOSEPH Eric
Laboratoire de Mecanique Appliquee R. Chaleat(LMARC)
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HIBERT Cyrille
EPFL Center of Micro-Nano Technology (CMI)
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MINOTTI Patrice
Laboratoire de Mecanique Appliquee R. Chaleat(LMARC)
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Moal Patrice
Laboratoire De Mecanique Appliquee R. Chaleat(lmarc):institut Des Microtechniques De Franche-comte
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Le Moai
Institut Des Microtechniques De Franche Comte Laboratoire De Mecanique Appliquee Universite De Franc
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Minotti P
Univ. Franche Comte Besancon Fra
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Minotti Patrice
Laboratoire De Mecanique Appliquee R. Chaleat (lmarc)
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Joseph Eric
Laboratoire De Mecanique Appliquee R. Chaleat(lmarc):institut Des Microtechniques De Franche-comte
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Bourbon G
Univ. Franche Comte Besancon Fra
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Bourbon Gilles
Laboratoire De Mecanique Appliquee R. Chaleat(lmarc):institut Des Microtechniques De Franche-comte
関連論文
- MMT-05 SILICON-BASED FLAPPING WINGS USING SELF-ACTUATED STRESS DISTRIBUTION
- (マイクロマシン)
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