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contributor authorPanakarajupally, Ragav P.
contributor authorEl Rassi, Joseph
contributor authorManigandan, K.
contributor authorSingh, Yogesh P.
contributor authorMorscher, Gregory N.
date accessioned2022-02-05T22:22:17Z
date available2022-02-05T22:22:17Z
date copyright3/15/2021 12:00:00 AM
date issued2021
identifier issn0742-4795
identifier othergtp_143_05_051027.pdf
identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4277417
description abstractElectrical resistance (ER) has become a technique of interest for monitoring SiC-based ceramic composites. The typical constituents of SiC fiber-reinforced SiC matrix composites, SiC, Si, and/or C, are semiconducive to some degree resulting in the fact that when damage occurs in the form of matrix cracking or fiber breakage, the resistance increases. For aero engine applications, SiC fiber reinforced SiC, sometimes Si-containing, matrix with a boron nitride (BN) interphase are often the main constituents. The resistivity of Si and SiC is highly temperature dependent. For high temperature tests, electrical lead attachment must be in a cold region which results in strong temperature effects on baseline measurements of resistance. This can be instructive as to test conditions; however, there is interest in focusing the resistance measurement in the hot section where damage monitoring is desired. The resistivity of C has a milder temperature dependence than that of Si or SiC. In addition, if the C is penetrated by damage, it would result in rapid oxidation of the C, presumably resulting in a change in resistance. One approach considered here is to insert carbon “rods” in the form of CVD SiC monofilaments with a C core to try and better sense change in resistance as it pertains to matrix crack growth in an elevated temperature test condition. The monofilaments were strategically placed in two nonoxide composite systems to understand the sensitivity of ER in damage detection at room temperature as well as elevated temperatures. Two material systems were considered for this study. The first composite system consisted of a Hi-Nicalon woven fibers, a BN interphase and a matrix processed via polymer infiltration and pyrolysis (PIP) which had SCS-6 monofilaments providing the C core. The second composite system was a melt-infiltrated (MI) prepreg laminate which contained Hi-Nicalon Type S fibers with BN interphases with SCS-ultramonofilaments providing the C core. The two composite matrix systems represent two extremes in resistance, the PIP matrix being orders of magnitude higher in resistance than the Si-containing prepreg MI matrix. Single notch tension–tension fatigue tests were performed at 815 °C to stimulate crack growth. Acoustic emission (AE) was used along with ER to monitor the damage initiation and progression during the test. Post-test microscopy was performed on the fracture specimen to understand the oxidation kinetics and carbon recession length in the monofilaments.
publisherThe American Society of Mechanical Engineers (ASME)
titleMonitoring Damage in Nonoxide Composites at High Temperatures Using Carbon-Containing CVD SiC Monofilament Fibers as Embedded Electrical Resistance Sensors
typeJournal Paper
journal volume143
journal issue5
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.4048694
journal fristpage051027-1
journal lastpage051027-9
page9
treeJournal of Engineering for Gas Turbines and Power:;2021:;volume( 143 ):;issue: 005
contenttypeFulltext


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