Fully Reversible Bending Test Apparatus for Characterization of Material Fatigue Behavior and Performance
INSTITUTION
NASA Marshall Space Flight Center
PRINCIPAL INVESTIGATOR
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FUNDING
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YEAR
2026
MOONBASE SCORE
Still being scored
LOADING MOONBASE SCORE
Abstract
The instrument uses two synchronized fixtures that rotate in equal and opposite directions, imparting fully reversible bending so the same surface experiences alternating tension and compression, mitigating buckling and alignment sensitivities common in uniaxial fatigue setups. A single motor, reduction gearbox, and shaft translate drive motion into counter rotation at both ends, while round tip, width spanning clamps distribute pressure to minimize corner stress concentrations and protect delicate specimens. Users can select pure bending or four point bending modes and adjust rotation amplitude and torque through an integrated controller, delivering repeatable cyclic loading in a compact, standalone system. Distinctive advantages include reliable testing of asymmetric geometries (laps, fillets), thin sheets, additively manufactured parts, and brittle ceramics without large dual actuator frames. This can consolidate multiple flexure methods into one benchtop mechanism. Its modular layout and adjustable fixtures integrate smoothly with common lab workflows and OEM platforms, helping teams accelerate evaluations without major reconfiguration of existing equipment. Potential commercial markets include instrument OEMs and suppliers of materials testing systems and accessories serving aerospace, automotive, academic, and contract laboratories. This technology is assessed at a TRL 6 and is ready for patent licensing. Traditional uniaxial fatigue systems require precise alignment and symmetric specimen geometries, limiting their effectiveness for asymmetric cross-sections (e.g., lap welds), thin-walled structures, additively manufactured parts, and brittle materials such as ceramics. Testing these materials often requires cumbersome or custom fixtures and workarounds, which slow evaluations and add cost, delay, and uncertainty. In response to this issue, researchers at NASA's Marshall Space Flight Center have developed a compact bending fatigue apparatus that applies fully reversed flexural loading, generating alternating tensile and compressive strains on the same specimen face through pure bending (no shear forces). This approach eliminates the need for symmetric specimens and enables reliable fatigue characterization of geometries and materials that are difficult to test with conventional methods. It has been advanced through prototyping and early evaluations to help teams assess materials faster and inform design decisions across numerous specimen types.
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