Design for additive manufacturing of cryogenic flexible pivot enabling on-demand customization, and reducing failure risks

Abstract Compliant mechanisms achieve motion through elastic deformation rather than contact surfaces, eliminating friction, wear, and lubrication requirements. Historically, conventional manufacturing processes have constrained both the design and adoption of these mechanisms in cryogenic and space applications. This work exploits the design freedom of Laser Powder Bed Fusion (LPBF) to propose a streamlined Design for Additive Manufacturing (DfAM) workflow for optimizing and customizing a flexure pivot operating at 4.2 K within the Mode Selector Mechanism (MSM). The methodology comprises three stages: (i) material selection and post-processing—316L stainless steel combined with stress annealing and HIP—to ensure cryogenic compatibility and fatigue strength; (ii) optimization of the Interlocked Lattice Flexure (ILF) geometry considering performance metrics (stroke, stiffness, guiding accuracy) and AM constraints (overhang, minimum feature size); and (iii) flexure thickness tuning to meet project-specific requirements while mitigating AM-induced variability, enabling rapid customization. Numerical and experimental validation confirmed compliance with design targets: $$\pm \, 3.5^\circ $$ <mml:math xmlns:mml="http://www.w3.org/1998/Math/MathML"> <mml:mrow> <mml:mo>±</mml:mo> <mml:mspace/> <mml:mn>3</mml:mn> <mml:mo>.</mml:mo> <mml:msup> <mml:mn>5</mml:mn> <mml:mo>∘</mml:mo> </mml:msup> </mml:mrow> </mml:math> stroke, stiffness of 3.97 mN m/ $$^\circ $$ <mml:math xmlns:mml="http://www.w3.org/1998/Math/MathML"> <mml:mmultiscripts> <mml:mrow/> <mml:mrow/> <mml:mo>∘</mml:mo> </mml:mmultiscripts> </mml:math> , and fatigue life exceeding $$10^6$$ <mml:math xmlns:mml="http://www.w3.org/1998/Math/MathML"> <mml:msup> <mml:mn>10</mml:mn> <mml:mn>6</mml:mn> </mml:msup> </mml:math> cycles under over-testing conditions (115% of operational range). Failure analysis further demonstrated that the ILF design inherently localizes damage, preventing catastrophic failure and enhancing robustness for aerospace applications. These results underscore the transformative potential of AM for high-performance, customizable compliant mechanisms in extreme environments.

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Publication Details

Journal
CEAS Space Journal
Published
2026-07-02
DOI
https://doi.org/10.1007/s12567-026-00748-6
Primary Topic
Piezoelectric Actuators and Control
Type
article
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article

Design for additive manufacturing of cryogenic flexible pivot enabling on-demand customization, and reducing failure risks

Lionel Kiener, Guilain Lang, Etienne Lallemand, Hervé Saudan et al.
CEAS Space Journal
Piezoelectric Actuators and Control
article

Design for additive manufacturing of cryogenic flexible pivot enabling on-demand customization, and reducing failure risks

Lionel Kiener, Guilain Lang, Etienne Lallemand, Hervé Saudan, Tanguy Thibert, Florent Cosandier, Maxime Lautenbacher
article en

Abstract

Abstract Compliant mechanisms achieve motion through elastic deformation rather than contact surfaces, eliminating friction, wear, and lubrication requirements. Historically, conventional manufacturing processes have constrained both the design and adoption of these mechanisms in cryogenic and space applications. This work exploits the design freedom of Laser Powder Bed Fusion (LPBF) to propose a streamlined Design for Additive Manufacturing (DfAM) workflow for optimizing and customizing a flexure pivot operating at 4.2 K within the Mode Selector Mechanism (MSM). The methodology comprises three stages: (i) material selection and post-processing—316L stainless steel combined with stress annealing and HIP—to ensure cryogenic compatibility and fatigue strength; (ii) optimization of the Interlocked Lattice Flexure (ILF) geometry considering performance metrics (stroke, stiffness, guiding accuracy) and AM constraints (overhang, minimum feature size); and (iii) flexure thickness tuning to meet project-specific requirements while mitigating AM-induced variability, enabling rapid customization. Numerical and experimental validation confirmed compliance with design targets: $$\pm \, 3.5^\circ $$ <mml:math xmlns:mml="http://www.w3.org/1998/Math/MathML"> <mml:mrow> <mml:mo>±</mml:mo> <mml:mspace/> <mml:mn>3</mml:mn> <mml:mo>.</mml:mo> <mml:msup> <mml:mn>5</mml:mn> <mml:mo>∘</mml:mo> </mml:msup> </mml:mrow> </mml:math> stroke, stiffness of 3.97 mN m/ $$^\circ $$ <mml:math xmlns:mml="http://www.w3.org/1998/Math/MathML"> <mml:mmultiscripts> <mml:mrow/> <mml:mrow/> <mml:mo>∘</mml:mo> </mml:mmultiscripts> </mml:math> , and fatigue life exceeding $$10^6$$ <mml:math xmlns:mml="http://www.w3.org/1998/Math/MathML"> <mml:msup> <mml:mn>10</mml:mn> <mml:mn>6</mml:mn> </mml:msup> </mml:math> cycles under over-testing conditions (115% of operational range). Failure analysis further demonstrated that the ILF design inherently localizes damage, preventing catastrophic failure and enhancing robustness for aerospace applications. These results underscore the transformative potential of AM for high-performance, customizable compliant mechanisms in extreme environments.

CEAS Space Journal
University of Liège (BE), ETH Zurich (CH), Observatoire Cantonal de Neuchâtel (CH), École Polytechnique Fédérale de Lausanne (CH)
Openalex Percentile: Top 9%
Piezoelectric Actuators and Control
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