Passive energy balancing design for a linear actuated morphing wingtip structure

被引:12
作者
Zhang, Jiaying [1 ]
Wang, Chen [2 ]
Shaw, Alexander D. [1 ]
Amoozgar, Mohammadreza [1 ,3 ]
Friswell, Michael I. [1 ]
机构
[1] Swansea Univ, Coll Engn, Swansea SA1 8EN, W Glam, Wales
[2] Nanjing Univ Aeronaut & Astronaut, Coll Aerosp Engn, Yudao St 29, Nanjing 210016, Peoples R China
[3] Univ Huddersfield, Sch Comp & Engn, Huddersfield HD1 3DH, W Yorkshire, England
关键词
Negative stiffness mechanism; Kinematics tailoring; Energy balancing; Actuator efficiency; Morphing wingtip; Morphing aircraft; NEGATIVE-STIFFNESS-MECHANISM; TIPS;
D O I
10.1016/j.ast.2020.106279
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
A passive energy balancing concept for linear actuation is investigated in the current work by adopting a negative stiffness mechanism. The proposed negative stiffness mechanism uses a pre-tensioned spring to produce a passive torque and therefore to transfer the passive torque through a crankshaft for linear motion. The proposed passive energy balancing design is supposed to be applied in a morphing wingtip, of which the shape change comes from the elastic deformation of the morphing structure. A significant amount of linear actuation force can be required to deform the structure, and therefore it is important to reduce the required force and the consumed energy by adopting the passive energy balancing design. The kinematics of the negative stiffness mechanism is developed to satisfy the required linear motion and its geometry is then optimised to reduce the energy requirements. The performance of the optimised negative stiffness mechanism is evaluated through the net force and the total required energy, which shows the potential of the design in the morphing wingtip application. (c) 2020 Elsevier Masson SAS. All rights reserved.
引用
收藏
页数:10
相关论文
共 36 条
  • [1] Alabuzhev P., 1989, Vibration Protection and Measuring Systems with Quasi-zero Stiffness
  • [2] Aero-servo-elastic design of a morphing wing trailing edge system for enhanced cruise performance
    Arena, Maurizio
    Concilio, Antonio
    Pecora, Rosario
    [J]. AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 86 : 215 - 235
  • [3] A Review of Morphing Aircraft
    Barbarino, Silvestro
    Bilgen, Onur
    Ajaj, Rafic M.
    Friswell, Michael I.
    Inman, Daniel J.
    [J]. JOURNAL OF INTELLIGENT MATERIAL SYSTEMS AND STRUCTURES, 2011, 22 (09) : 823 - 877
  • [4] Barents R., 2009, ASME C P, P689, DOI DOI 10.1115/DETC2009-86770
  • [5] Static analysis of a passive vibration isolator with quasi-zero-stiffness characteristic
    Carrella, A.
    Brennan, M. J.
    Waters, T. P.
    [J]. JOURNAL OF SOUND AND VIBRATION, 2007, 301 (3-5) : 678 - 689
  • [6] Preliminary investigation of use of flexible folding wing tips for static and dynamic load alleviation
    Castrichini, A.
    Siddaramaiah, V. Hodigere
    Calderon, D. E.
    Cooper, J. E.
    Wilson, T.
    Lemmens, Y.
    [J]. AERONAUTICAL JOURNAL, 2017, 121 (1235) : 73 - 94
  • [7] Nonlinear Folding Wing Tips for Gust Loads Alleviation
    Castrichini, A.
    Siddaramaiah, V. Hodigere
    Calderon, D. E.
    Cooper, J. E.
    Wilson, T.
    Lemmens, Y.
    [J]. JOURNAL OF AIRCRAFT, 2016, 53 (05): : 1391 - 1399
  • [8] Cheung R.C.M., 2017, 58 AIAA ASCE ASHS AS
  • [9] A Single-Degree-of-Freedom Self-Regulated Gravity Balancer for Adjustable Payload1
    Chu, Yu-Lin
    Kuo, Chin-Hsing
    [J]. JOURNAL OF MECHANISMS AND ROBOTICS-TRANSACTIONS OF THE ASME, 2017, 9 (02):
  • [10] Mechanical strain energy shuttle for aircraft morphing via wing twist or structural deformation
    Clingman, D
    Ruggeri, R
    [J]. SMART STRUCTURES AND MATERIALS 2004: INDUSTRIAL AND COMMERCIAL APPLICATIONS OF SMART STRUCTURES TECHNOLOGIES, 2004, 5388 : 288 - 296