A Morphing Composite Air Inlet with Multiple Stable Shapes

被引:87
作者
Daynes, S. [1 ]
Weaver, P. M. [1 ]
Trevarthen, J. A. [1 ]
机构
[1] Univ Bristol, Dept Aerosp Engn, Bristol BS8 1TR, Avon, England
关键词
compliant mechanisms; morphing; multistability; stiffness tailoring; non-linear deformations; PERFORMANCE; PLATES; METAL;
D O I
10.1177/1045389X11399943
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
The morphing air inlet is a structure with shape-changing capability. Shapes include that which is flush with an aerodynamic surface and also a submerged divergent channel suitable for use in an aircraft cooling system. The air inlet structure is multistable in order that it can 'snap' open and closed and not require any external holding force to maintain its geometry. Structural multistability is achieved using a novel combination of material prestress and bending stiffness tailoring. Analytical and finite element models are developed in order to explain how this multistability is achieved and to predict the actuator requirements and bending strains within the structure. The air inlet design is autoclave manufactured from carbon fiber reinforced plastic and tested as a proof-of-concept demonstrator. The bending stiffness tailoring enables the structure to fulfill the conflicting requirements of large deformations, low mass, and high stiffness to withstand external loads. The simple construction also aids ease of maintenance and reliability. The morphing demonstrator behaves as a one degree-of-freedom system enabling simple actuation solutions, such as inflatable bladders, to be feasible.
引用
收藏
页码:961 / 973
页数:13
相关论文
共 32 条
[1]   Manufacture and characterization of high activity piezoelectric fibres [J].
Bowen, CR ;
Stevens, R ;
Nelson, LJ ;
Dent, AC ;
Dolman, G ;
Su, B ;
Button, TW ;
Cain, MG ;
Stewart, M .
SMART MATERIALS AND STRUCTURES, 2006, 15 (02) :295-301
[2]   Initial thoughts on weight penalty effects in shape-adaptable systems [J].
Campanile, LF .
JOURNAL OF INTELLIGENT MATERIAL SYSTEMS AND STRUCTURES, 2005, 16 (01) :47-56
[3]   Aerodynamic and aeroelastic amplification in adaptive belt-rib airfoils [J].
Campanile, LF ;
Anders, S .
AEROSPACE SCIENCE AND TECHNOLOGY, 2005, 9 (01) :55-63
[4]   Thermally-induced deformation behavior of unsymmetric laminates [J].
Dano, ML ;
Hyer, MW .
INTERNATIONAL JOURNAL OF SOLIDS AND STRUCTURES, 1998, 35 (17) :2101-2120
[5]   Bistable Prestressed Symmetric Laminates [J].
Daynes, S. ;
Diaconu, C. G. ;
Potter, K. D. ;
Weaver, P. M. .
JOURNAL OF COMPOSITE MATERIALS, 2010, 44 (09) :1119-1137
[6]   Bistable prestressed buckled laminates [J].
Daynes, S. ;
Potter, K. D. ;
Weaver, P. M. .
COMPOSITES SCIENCE AND TECHNOLOGY, 2008, 68 (15-16) :3431-3437
[7]  
DAYNES S, 2010, Patent No. 10173714
[8]   Analysis of unsymmetric CFRP-metal hybrid laminates for use in adaptive structures [J].
Daynes, Stephen ;
Weaver, Paul .
COMPOSITES PART A-APPLIED SCIENCE AND MANUFACTURING, 2010, 41 (11) :1712-1718
[9]   Concepts for morphing airfoil sections using bi-stable laminated composite structures [J].
Diaconu, Cezar G. ;
Weaver, Paul M. ;
Mattioni, Filippo .
THIN-WALLED STRUCTURES, 2008, 46 (06) :689-701
[10]   Environmental effects on thermally induced multistability in unsymmetric composite laminates [J].
Etches, Julie ;
Potter, Kevin ;
Weaver, Paul ;
Bond, Ian .
COMPOSITES PART A-APPLIED SCIENCE AND MANUFACTURING, 2009, 40 (08) :1240-1247