Adaptive structural systems and compliant skin technology of morphing aircraft structures

被引:10
|
作者
Manzo, J [1 ]
Garcia, E [1 ]
Wickenheiser, A [1 ]
Horner, GC [1 ]
机构
[1] Cornell Univ, Sibley Sch Mech & Aerosp Engn, Lab Intelligent Machine Syst, Ithaca, NY 14853 USA
关键词
morphing; shape change; HECS; compliant skin; adaptive structure; oblique joint;
D O I
10.1117/12.540348
中图分类号
TM [电工技术]; TN [电子技术、通信技术];
学科分类号
0808 ; 0809 ;
摘要
Morphing aircraft design - the design of aircraft capable of macroscale shape change for drastic in-flight performance variation - is an extremely broad and underdefined field. Two primary means of developing new concepts in morphing exist at Cornell University: design of broad test platforms with generalized motions that can provide future insight into tarcreted ideas. and specifically adapted aircraft and shape change mechanisms attempting to accomplish a particular task, or hybridize two existing aircraft platforms. Working with both schools of thought, Cornell research has developed a number of useful concepts that are currently under independent analysis and experimentation, including three devices capable of drastically modifying wing structure on a testbed aircraft. Additional concerns that have arisen include the desire to implement ornithological concepts such as perching and wingtip control, as well as the necessity for a compliant aerodynamic skin for producing flight-worthy structural mechanisms.
引用
收藏
页码:225 / 234
页数:10
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