Our goal is to develop and demonstrate a MEMS-based methodology for evaluating time-dependent mechanical properties of materials that undergo exposure to extreme and harsh environments (e.g., temperature extremes, high radiation, corrosive chemistries, etc.). Such test methods hold promise for providing a high throughput route to thoroughly measuring the remaining lifetime of highly irradiated materials present in today's nuclear power plants, as well as the suitability of new alloys for next generation nuclear plants.
MEMS-based fatigue test instrument and fatigue testing of micro aluminum specimens
We leveraged MEMS technology to develop a silicon micromachined fatigue load frame which includes an on-chip actuator and displacement sensor. The device is operated under an optical microscope, and performs bending fatigue tests on micro sized metal specimens inserted into it. The specimens have gauge widths of about 100 μm and gauge thickness of about 25 μm. Fatigue failure is detected by the on-chip sensor, and specimen strains are obtained via digital image correlation. The specimens themselves are made separately. The chips can be re-used after specimens have fractured.
A micro specimen of 25 mm-thickAluminum 1145 H19 undergoes quasi-stress controlled bending fatigue testing ina MEMS chip. The MEMS test instrument is a silicon electrostatic comb driveactuator. The longest part of the aluminum specimen, the lever arm, isdisplaced by the silicon actuator to produce bending stresses in the gaugesection, which is the narrowest part of the specimen and has width of about 130mmand length of about 180 mm. The stress can be variedeither by adjusting the input voltage to the MEMS actuator, or by varying theindexed position of the specimen in the MEMS chip to vary the effective leverarm length. Silicon microfabricated grips hold and align the specimen to theactuator. The failure criterion is when the fatigue crack exceeds more thanhalf the width of the gauge section. Fatigue failure is detected by on-chip capacitivesensors. A typical test is run at a frequency of 70 - 130 Hz and MEMS voltagesof 80 – 220 V. The silicon actuator has a maximum force capacity of about 8 mNat no displacement, and displacement range of about 100 mm.Following specimen failure, the MEMS device and grip are reused.
This is a time lapse video – taken with an opticalmicroscope – showing the fatigue crack initiation, growth and failure of anAluminum 1145 H19 micro specimen tested in the MEMS chip. The gauge width (topto bottom of the video screen) is about 130 mm, the gauge width(spanning the horizontal length of the screen) is about 180 mm,and the out-of-plane thickness is about 25 mm. This video spans a totaltime of about 7 hours.
We demonstrated this technique by generating an S-N curve for Al 1145 H19 micro specimens, and measuring the bending stiffness of stainless steel micro specimens. In particular, since generating an S-N curve requires testing of many specimens and with each test being time consuming, a potential advantage of this MEMS approach is low-cost batch fabrication of the silicon devices and the potential to run many chips/specimens in parallel, which would enable highly efficient generation of large data sets. Another advantage is the small size of the actuator which could allow in-situ fatigue testing in harsh environments.
Micro tensile testing on stainless steel micro specimens
We used silicon micromachining techniques to fabricate frames into which micro stainless steel tensile specimens are placed. The silicon frame consists of a stationary outer structure connected by tethers to a movable central platform. Grips consist of etched recesses with the same geometry as the specimen’s ends. One end of the specimen is gripped in the stationary structure and the other end is gripped in the movable platform. The silicon chip is then placed under an optical microscope, and the movable platform is pulled by a custom external actuator to apply tensile loads to the specimen. Force is measured with a load cell and strains are obtained via digital image correlation.
We obtained engineering stress-strain curves of stainless steel 302 micro specimens with gauge section dimensions of 360 μm long x 70 μm wide x 25 μm thick. The specimens were fabricated separately, by a commercial vendor, from stainless steel foils. The properties obtained from our micro tensile tests are in agreement with those specified by the material vendor, and with properties we measured using nanoindentation. This technique allows for tensile testing of extremely small volumes of material – smaller than the state of the art for bulk materials testing – and would be advantageous for testing of in-service traditional structural materials and materials that have been subjected to harsh environments.
structural materials, mechanical testing, MEMS, microsystems, materials characterization, energy, infrastructure, electronics, manufacturing, microscale
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