Thermal prestress in composite compliant shell mechanisms

Stacey, Jonathan P.; O'Donnell, Matthew P.; Schenk, Mark

Abstract

This paper explores the ability to tailor the mechanical properties of composite compliant shell mechanisms, by exploiting the thermal prestress introduced during the composite laminate cure. An extension of an analytical tape spring model with composite thermal analysis is presented, and the effect of the thermal prestress is studied by means of energy landscapes for the cylindrical composite shells. Tape springs that would otherwise be monostable structures become bistable and exhibit greater ranges of low-energy twisting with thermally induced prestress. Predicted shell geometries are compared with finite element (FE) results and manufactured samples, showing good agreement between all approaches. Wider challenges around the manufacture of prestressed composite compliant mechanisms are discussed.

Citation

Stacey, J. P., O'Donnell, M. P., & Schenk, M. (2019). Thermal prestress in composite compliant shell mechanisms. Journal of Mechanisms and Robotics, 11(2), Article 020908. https://doi.org/10.1115/1.4042476

• Journal Article Type: Article
• Acceptance Date: Dec 23, 2018
• Online Publication Date: Feb 22, 2019
• Publication Date: Apr 1, 2019
• Deposit Date: May 5, 2020
• Publicly Available Date: May 11, 2020
• Journal: Journal of Mechanisms and Robotics
• Print ISSN: 1942-4302
• Electronic ISSN: 1942-4310
• Publisher: American Society of Mechanical Engineers
• Peer Reviewed: Peer Reviewed
• Volume: 11
• Issue: 2
• Article Number: 020908
• DOI: https://doi.org/10.1115/1.4042476
• Keywords: Composite materials, Laminates, Shells, Springs, Design, Stiffness, Cylinders, Manufacturing, Compliant mechanisms, Equilibrium (Physics), Finite element analysis
• Public URL: https://uwe-repository.worktribe.com/output/5914765