Skip to main content
Log in

Compliant mechanism based on additive manufacturing

  • Original Paper
  • Published:
CEAS Space Journal Aims and scope Submit manuscript

Abstract

An innovative concept of building compliant mechanisms by additive manufacturing (AM) developed at CSEM is presented. Bringing together CSEM’s experience in the design and development of high-performance flexural elements and mechanisms for more than 30 years has opened the doors to new opportunities. The complete development of compliant structures for AM enables CSEM to develop innovative concepts to drastically reduce the need of machining after AM. Support structures under flexure blades are integrated to the flexures with no need for removal, which makes the overall process becomes more streamlined. Thanks to this concept, CSEM has developed new architectures of compliant mechanisms based on additive manufacturing (COMAM) for the European Space Agency (ESA). These demonstrators will be used as use-case for future high-precision and harsh environment applications such as cryogenic and space. The complete development workflow, starting with the design, topology optimization, manufacturing, post-processes, validation, up to performance and environmental testing will be presented.

This is a preview of subscription content, log in via an institution to check access.

Access this article

Price excludes VAT (USA)
Tax calculation will be finalised during checkout.

Instant access to the full article PDF.

Fig. 1
Fig. 2
Fig. 3
Fig. 4
Fig. 5
Fig. 6
Fig. 7
Fig. 8
Fig. 9
Fig. 10
Fig. 11
Fig. 12
Fig. 13
Fig. 14
Fig. 15

Similar content being viewed by others

Data availability

Not applicable.

Code availability

Not applicable.

References

  1. Merriam, E.G.: Stiffness Reduction Strategies for Additively Manufactured Compliant Mechanisms, All Theses and Dissertations. Paper 5873 (2016)

  2. Saudan, H., Vaideeswaran, K., Kiener, L., Mehdi, D. M.: Additive manufactured metallic flexible structures, a focus on manufacturing strategies, material analysis and fatigue verification. In: ECSSMET 2016, Toulouse, France, 27–30 Sept (2016)

  3. Saudan, H., Kiener, L., Perruchoud, G., Vaideeswaran, K. and Dadras, M.: “Additively manufactured and topologically optimized compliant mechanisms: technological assessment approach, latest achievements and current work in progress” Proceedings of the 17th European Space Mechanisms & Tribology Symposium, Hatfield, United Kingdom, 20–22 Sept (2017)

  4. Rouvinet, J., Ummel, A., Cosandier, F., Nguyen, D., Schaffter, V.: “PULSAR: Development of a mirror tile prototype for future large telescopes robotically assembled in space.” Proc. SPIE 11451, Advances in Optical and Mechanical Technologies for Telescopes and Instrumentation IV, 114512N (2020)

Download references

Funding

This project has been funded by the Swiss Space Office of the State Secretariat for Education, Research and Innovation SERI.

Author information

Authors and Affiliations

Authors

Contributions

Conception or design of the work: LK, HS, FC, GP, AU, PZ. Data collection: LK, HS, FC, VP, YP. Data analysis and interpretation: LK, HS, FC, GP, AU, PZ, ML. Drafting the article: LK. Critical revision of the article: PZ. Final approval of the version to be published: PZ.

Corresponding author

Correspondence to Lionel Kiener.

Ethics declarations

Conflict of interest

The authors declare that they have no conflict of interest/competing interests.

Additional information

Publisher's Note

Springer Nature remains neutral with regard to jurisdictional claims in published maps and institutional affiliations.

Rights and permissions

Reprints and permissions

About this article

Check for updates. Verify currency and authenticity via CrossMark

Cite this article

Kiener, L., Saudan, H., Cosandier, F. et al. Compliant mechanism based on additive manufacturing. CEAS Space J 15, 37–53 (2023). https://doi.org/10.1007/s12567-021-00394-0

Download citation

  • Received:

  • Revised:

  • Accepted:

  • Published:

  • Issue Date:

  • DOI: https://doi.org/10.1007/s12567-021-00394-0

Keywords

Navigation