Fully morphing aircraft structures: studies from the Department of Aerospace Engineering, METU, Ankara, Turkey

2018 ◽  
Vol 4 (1) ◽  
pp. 1
Author(s):  
Yavuz Yaman
2011 ◽  
Vol 410 ◽  
pp. 25-25
Author(s):  
Jin Song Leng

Stimulus-active polymers can change their shapes with respect to configuration or dimension upon exposure to a particular stimulus such as heat, electricity, light, magnetic, solvent and pH value. These unique characteristics enable stimulus-active polymers to be used in a myriad of fields, including clothing manufacturing, automobile engineering, medical treatment, and aerospace engineering. Stimulus-active polymers can be applied in smart textiles and apparels, intelligent medical instruments and auxiliaries, artificial muscles, biomimetic devices, heat shrinkable materials for electronics packaging, micro-electro-mechanical systems, self-deployable sun sails in spacecrafts, miniature manipulator, actuators and sensors, and many more. This paper presents some recent progress of soft smart materials and their applications. Special emphasis is focused upon shape memory polymer (SMP), electro-active polymer (EAP) for aerospace engineering such as space deployable structures and morphing aircraft, which has highlighted the need for development of these materials. A detailed overview of development in these smart soft materials, of which the undergoing and future applications are used in adaptive structures and active control, is presented. The paper concludes with a short discussion for multi-functional soft smart materials and their composites that are expected to extend the range of development and applications available to the related researches and engineers.


Author(s):  
J P Bates ◽  
A J Morris ◽  
P N Payne

Aerospace engineering offers a challenging test environment for advanced design systems and methods. Focusing particularly on knowledge-based engineering (KBE) systems, this paper demonstrates their application in automating the solid modelling of aircraft structures. The principles are illustrated through a case study example in which a description is given of the knowledge-based geometric modelling of light alloy fuselage frame sectors. The business benefits of using KBE systems in an aerospace engineering programme are quantified. Recommendations for the extended application of the technology to achieve strategic market advantage are also given.


Author(s):  
Jason Bowman ◽  
Brian Sanders ◽  
Bryan Cannon ◽  
Jayanth Kudva ◽  
Shiv Joshi ◽  
...  

2008 ◽  
Author(s):  
Filippo Mattioni ◽  
Paul M. Weaver ◽  
Kevin D. Potter ◽  
Michael I. Friswell

Author(s):  
David H. Myszka ◽  
James J. Joo

This paper presents an investigation into the structural characterization of tensegrity systems for potential use as aircraft structures, especially for morphing aircraft. Morphing aircraft provide multi-role and multi-mission capabilities by adapting their performance to different in-flight requirements. Flexible elements must be included within the structure to permit morphing capabilities compared to conventional single mission aircraft, which are designed for high rigidity and not ideal for shape morphing applications. Tensegrity systems are structures that consist of a series of connected cables, in tension, and struts, in compression, that exist in a self-equilibrium state. Since the struts and cables are loaded axially, external loads are efficiently distributed throughout the tensegrity components resulting in a strong and stiff structure. Adjusting the pretension of the tensegrity will tailor the structural characteristics as needed without a basic configuration change. By changing the length of the cables or struts, tensegrity systems are capable of movement while maintaining their inherent strength and rigidity. This makes tensegrity systems an attractive candidate for morphing aircraft structures. This paper quantifies the strength and rigidity of a single module of various tensegrity systems along with traditional structures to assess their ability to serve as aircraft wings. Those properties are evaluated after boundary conditions are carefully selected to avoid adding unnecessary stiffness. Lastly, a concept for a tensegrity morphing aircraft wing is presented.


2004 ◽  
Author(s):  
Justin Manzo ◽  
Ephrahim Garcia ◽  
Adam M. Wickenheiser ◽  
Garnett C. Horner

2003 ◽  
Author(s):  
Sridhar Kota ◽  
Joel A. Hetrick ◽  
Russell Osborn ◽  
Donald Paul ◽  
Edmund Pendleton ◽  
...  

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