2019
DOI: 10.1016/j.jestch.2019.10.004
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New conceptual design of the adaptive compliant aircraft wing frame

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Cited by 7 publications
(2 citation statements)
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“…In [53] A. V. Ivchenko et al discusses two proposed design solutions for creating an adaptive compliant aircraft wing frame using a reconfigurable honeycomb core with hidden topological surfaces. The first solution involves lever actuators integrated into the honeycomb structure, while the second solution utilizes mechatronic nodes as actuators.…”
Section: Structural Approachmentioning
confidence: 99%
“…In [53] A. V. Ivchenko et al discusses two proposed design solutions for creating an adaptive compliant aircraft wing frame using a reconfigurable honeycomb core with hidden topological surfaces. The first solution involves lever actuators integrated into the honeycomb structure, while the second solution utilizes mechatronic nodes as actuators.…”
Section: Structural Approachmentioning
confidence: 99%
“…Sahin and Yaman [53] introduced a scissorstructural mechanism for the trailing edge of a morphing wing. Ivchenko et al [54] proposed reconfigurable honeycomb core, based on a network of joints for an adaptive, compliant wing frame morphing concept. However, such concepts did not progress to the manufacturing and testing stage [55][56][57][58][59][60].…”
Section: Material-based Camber Morphing Mechanisms a Material-based Camber Morphing Mechanism Features Materials Anisotropy And Tools Likmentioning
confidence: 99%