Smart Structures and Systems

  • 제1권2호
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  • Pages.159-184
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  • 2005
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  • 1738-1584(pISSN)
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  • 1738-1991(eISSN)
테크노프레스 (Techno-Press)
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The future role of smart structure systems in modern aircraft

  • Becker, J. (EADS Deutschland GmbH, Military Aircraft, Technical University of Munich, Institute of Fluidmechanic) ;
  • Luber, W. (EADS Deutschland GmbH, Military Aircraft) ;
  • Simpson, J. (EADS Deutschland GmbH, Military Aircraft) ;
  • Dittrich, K. (EADS Deutschland GmbH, Military Aircraft)
  • 투고 : 2004.07.28
  • 심사 : 2005.03.25
  • 발행 : 2005.04.25
⟨ 이전 논문 다음 논문 ⟩

초록

The paper intends to summarize some guidelines for future smart structure system application in military aircraft. This preview of system integration is based upon a review on approximately one and a half decades of application oriented aerospace related smart structures research. Achievements in the area of structural health monitoring, adaptive shape, adaptive load bearing devices and active vibration control have been reached, potentials have been identified, several feasibility studies have been performed and some smart technologies have been already implemented. However the realization of anticipated visions and previously initial timescales announced have been rather too optimistic. The current development shall be based on a more realistic basis including more emphasis on fundamental aircraft strength, stiffness, static and dynamic load and stability requirements of aircraft and interdisciplinary integration requirements and improvements of integrated actors, actuator systems and control systems including micro controllers.

키워드

참고문헌

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피인용 문헌

  1. Active wing design with integrated flight control using piezoelectric macro fiber composites vol.18, pp.3, 2009, https://doi.org/10.1088/0964-1726/18/3/035010
  2. NEURAL ADAPTIVE CONTROL FOR VIBRATION SUPPRESSION IN COMPOSITE FIN-TIP OF AIRCRAFT vol.18, pp.03, 2008, https://doi.org/10.1142/S0129065708001543