TY - JOUR
T1 - Passive energy balancing design for a linear actuated morphing wingtip structure
AU - Zhang, Jiaying
AU - Wang, Chen
AU - Shaw, Alexander D.
AU - Amoozgar, Mohammadreza
AU - Friswell, Michael I.
PY - 2020/12/1
Y1 - 2020/12/1
N2 - 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.
AB - 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.
KW - Actuator efficiency
KW - Energy balancing
KW - Kinematics tailoring
KW - Morphing aircraft
KW - Morphing wingtip
KW - Negative stiffness mechanism
UR - http://www.scopus.com/inward/record.url?scp=85093959248&partnerID=8YFLogxK
U2 - 10.1016/j.ast.2020.106279
DO - 10.1016/j.ast.2020.106279
M3 - Article
AN - SCOPUS:85093959248
VL - 107
JO - Aerospace Science and Technology
JF - Aerospace Science and Technology
SN - 1270-9638
M1 - 106279
ER -