2014
DOI: 10.1002/adfm.201401548
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Stepped Moduli in Layered Composites

Abstract: This paper describes adaptive composites that respond to mechanical stimuli by changing their Young's modulus. These composites are fabricated by combining a shorter layer of elastic material (e.g. latex) and a longer layer of stiffer material (e.g., polyethylene and Kevlar), and fixing them together at their ends. Tension along the layered composite increases its length, and as the strain increases, the composite changes the load-bearing layer from the elastic to the stiff material. The result is a step in th… Show more

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Cited by 19 publications
(23 citation statements)
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“…By using a less stretchable silicone formulation (Dragon Skin Ⓡ20 instead of Ecoflex™ 00-30), the stretchability of the harness can be reduced to achieve larger compression against the ASiT hence a larger pressure differential within the air channel during breathing. 51…”
Section: Resultsmentioning
confidence: 99%
“…By using a less stretchable silicone formulation (Dragon Skin Ⓡ20 instead of Ecoflex™ 00-30), the stretchability of the harness can be reduced to achieve larger compression against the ASiT hence a larger pressure differential within the air channel during breathing. 51…”
Section: Resultsmentioning
confidence: 99%
“…The storage modulus E ' of P(nBuA‐BPAEDA), P(nBuA‐PEGDA), and P(nBuA‐TMPTA) is shown in Figure 8 along with the E r (inset) which is the region above the T g and below the melt T m known as the rubbery plateau, its plateau length dependent on the cross‐links. [ 29,30,31 ] All samples had high elastic variances. At the start temperature of −50°C, the E ' values were 5470, 1690, and 245 MPa for polymers containing the crosslinkers TMPTA, BPAEDA, and PEGDA, respectively.…”
Section: Resultsmentioning
confidence: 99%
“…Strain stiffening in layered composites can be used in the future to form contact strain relief islands. 41 This result indicates that each system has a different mode of failure (e.g., failure of the contact-substrate interface, failure of the CB-PDMS layered substrate itself, etc.). To investigate the mode of failure of the CB-PDMS layered composite devices with Cu-pSi and AgEpoxy contacts in more detail, we characterized the mechanical behavior of the devices under shear stress up to 40% strain ( Figure 2B and Figure S7 ).…”
Section: Resultsmentioning
confidence: 99%