The micro air car, it is actually the thermop thanes (TPU), which primarily plays the function of adhesion.Figure five. The vacuum bag. Figure 5. The vacuum bag.The piezoelectric actuation mechanism adopts the procedure of combining composite The piezoelectric actuation mechanism adopts the course of action of combin material vacuum bag technology and laser release [24]. Figure 6a depicts its exceptional structure. The Lanifibranor Technical Information method starts with laser cutting, followed by shape cutting of the piezoelectric material vacuum bag technologies and laser release [24]. Figure 6a depicts its sheet and every single layer with the support material, and then proceeds in sequence. Curing with ture. The method starts with laser cutting, followed by shape cutting of th the vacuum bag, followed by the release in the actuator. The wings are a rigid lexible sheet and each layer of the assistance material, after which proceeds in sequenc composite structure created up of a rigid vein skeleton as well as a flexible film. The processing procedure is related to that with the actuator, as shown in Figure 6b, the solid vein skeleton will be the vacuum bag, followed by the release of your actuator. The wings are a Micromachines 2021, 12, x FOR PEER Evaluation 7 of 13 very first reduce, then the flexible film plus the vein skeleton are combined and cured, and finally, composite structure made up of a rigid vein skeleton and a flexible film. T the release on the wings is performed.approach is related to that on the actuator, as shown in Figure 6b, the strong v 1st cut, then the flexible film and the vein skeleton are combined and cure the release on the wings is performed.Figure six. Actuator and wing manufacture: (a) distinct structure of actuator; (b) the manufacturing Figure 6. Actuator and wing manufacture: (a) precise structure of actuator; (b) the manufacturing process in the wings. course of action of the wings.The developed planar composite sheet structure is processed by adopting the pro cessing technique of rigid lexible composite threedimensional structure, as shown in Fig ure 7a. Then, the processed composite board is L-Kynurenine Epigenetics folded and fixed as outlined by the hinge crease and folding angle, as shown in the figure. Ultimately, the key structure shown in Figure 7b may be obtainedMicromachines 2021, 12,Figure 6. Actuator and wing manufacture: (a) distinct structure of actuator; (b) the manufacturing 7 of 13 process on the wings.The designed planar composite sheet structure is processed by adopting the pro cessing strategy of rigid lexible composite threedimensional structure, as shown in Fig The made planar composite sheet structure is processed by adopting the processing ure 7a. Then, the processed composite board is folded and fixed in accordance with the hinge process of rigid lexible composite three-dimensional structure, as shown in Figure 7a. crease the processedangle, as shown in folded and fixed according to the hinge crease and then, and folding composite board may be the figure. Finally, the key structure shown in Figure 7b may be obtained the figure. Lastly, the key structure shown in Figure 7b could be folding angle, as shown inobtainedFigure 7. Monolithic manufacturing system of air vehicle primary structure: (a) folding and shaping Figure 7. Monolithic manufacturing approach of air car major structure: (a) folding and shaping method; (b) folded main structure. strategy; (b) folded major structure.Finally, the processed drive mechanism, wings, and main structure are assembled Ultimately, the processed drive mechanism, wings, and key structure are assembled.
