Design, Manufacturing and Testing of a Morphing Winglet for a Regional Turboprop Aircraft

被引:0
|
作者
Dimino, Ignazio [1 ]
Pellone, Lorenzo [1 ]
Ameduri, Salvatore [1 ]
Concilio, Antonio [1 ]
Mercurio, Umberto [1 ]
Colella, Eugenio [2 ]
Giuliani, Michelangelo [2 ]
Capuano, Vincenzo [2 ]
机构
[1] Ctr Italiano Ric Aerospaziali, I-81043 Capua, Italy
[2] Costruzioni Aeronautiche Tecnam, I-81043 Capua, Italy
基金
欧盟地平线“2020”;
关键词
Morphing; Adaptive Winglet;
D O I
10.1117/12.2674193
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
In this paper, the design, manufacturing and testing of a morphing winglet concept, developed in the framework of the Clean Sky 2 REG IADP AIRGREEN 2 Project is presented. Such an adaptive device is being developed by CIRA and manufactured by TECNAM to enhance wing aerodynamic efficiency in off-design conditions and reduce maneuver loads. The concept is based on two individual (asynchronous) morphing surfaces consisting of two "finger-like" mechanisms driving the same number of moveable surfaces (the upper and lower tabs), controlled by dedicated electromechanical actuators.
引用
收藏
页数:12
相关论文
共 50 条
  • [41] THEORETICAL DESIGN OF ACOUSTIC TREATMENT FOR NOISE CONTROL IN A TURBOPROP AIRCRAFT.
    Vaicaitis, R.
    Mixson, J.S.
    Journal of Aircraft, 1985, 22 (04): : 318 - 324
  • [42] THEORETICAL DESIGN OF ACOUSTIC TREATMENT FOR NOISE-CONTROL IN A TURBOPROP AIRCRAFT
    VAICAITIS, R
    MIXSON, JS
    JOURNAL OF AIRCRAFT, 1985, 22 (04): : 318 - 324
  • [43] DESIGN AND MANUFACTURE OF A FLUID-ACTUATED MORPHING WINGLET TRAILING EDGE CONTROL SURFACE
    Vasista, Srinivas
    Nolte, Felix
    Schaefer, Michael
    Riemenschneider, Johannes
    PROCEEDINGS OF ASME 2022 CONFERENCE ON SMART MATERIALS, ADAPTIVE STRUCTURES AND INTELLIGENT SYSTEMS, SMASIS2022, 2022,
  • [44] DESIGN AND TESTING OF A LATTICE MORPHING WING
    Keidel, Dominic
    Lienhard, Marc
    Fasel, Urban
    Ermanni, Paolo
    PROCEEDINGS OF THE ASME 2020 CONFERENCE ON SMART MATERIALS, ADAPTIVE STRUCTURES AND INTELLIGENT SYSTEMS (SMASIS2020), 2020,
  • [45] Flexural testing of shape memory polymers for morphing aircraft applications
    Gross, Korey
    Weiland, Lisa
    PROCEEDINGS OF THE ASME INTERNATIONAL MECHANICAL ENGINEERING CONGRESS AND EXPOSITION 2007, VOL 10, PTS A AND B: MECHANICS OF SOLIDS AND STRUCTURES, 2008, : 299 - 303
  • [46] Benefits and design challenges of adaptive structures for morphing aircraft
    Moorhouse, D
    Sanders, B
    von Spakovsky, M
    Butt, J
    AERONAUTICAL JOURNAL, 2006, 110 (1105): : 157 - 162
  • [47] Robust Controller Design for a Morphing Aircraft Based on SRAD
    Zhang Jie
    Wu Sen-Tang
    26TH CHINESE CONTROL AND DECISION CONFERENCE (2014 CCDC), 2014, : 473 - 478
  • [48] Performance based multidisciplinary design optimization of morphing aircraft
    Afonso, Frederico
    Vale, Jose
    Lau, Fernando
    Suleman, Afzal
    AEROSPACE SCIENCE AND TECHNOLOGY, 2017, 67 : 1 - 12
  • [49] TOPOLOGY OPTIMIZATION METHODS FOR MORPHING AIRCRAFT DESIGN: A REVIEW
    Mena-Arciniega, Carlos
    Criollo, Linker
    Xing, Shen
    Aviation, 2024, 28 (04) : 292 - 305
  • [50] Application of an improved RBF neural network on aircraft winglet optimization design
    Bai, J. (junqiang@nwpu.edu.cn), 1865, Chinese Society of Astronautics (35):