2019
DOI: 10.1016/j.ceramint.2018.12.206
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A new precursor of liquid and curable polysiloxane for highly cost-efficient SiOC-based composites

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Cited by 12 publications
(7 citation statements)
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“…Up to now, several CMCs with different ceramic matrix have been investigated using PIP method for the purpose of structural application in hot section of gas turbine engines, such as C f /SiC [106], C f /SiBCN [107,[310][311][312], C f /SiCN [82,298,313], C f /SiHfBCN [82], C f /SiOC [314,315], C f /SiCON [18], C f /SiBOC [316], SiC f /SiCN [298,317], SiC f /SiC [318,319], and SiC f /SiBCN [320]. These CMCs with polymer-derived ceramic matrix have been demonstrated to exhibit excellent structural properties which are preferable for application in gas turbine engines, such as excellent thermal stability, oxidation resistance, high-temperature www.springer.com/journal/40145 mechanical properties, as well as creep resistance [321][322][323].…”
Section: Ceramic Matrix Compositesmentioning
confidence: 99%
“…Up to now, several CMCs with different ceramic matrix have been investigated using PIP method for the purpose of structural application in hot section of gas turbine engines, such as C f /SiC [106], C f /SiBCN [107,[310][311][312], C f /SiCN [82,298,313], C f /SiHfBCN [82], C f /SiOC [314,315], C f /SiCON [18], C f /SiBOC [316], SiC f /SiCN [298,317], SiC f /SiC [318,319], and SiC f /SiBCN [320]. These CMCs with polymer-derived ceramic matrix have been demonstrated to exhibit excellent structural properties which are preferable for application in gas turbine engines, such as excellent thermal stability, oxidation resistance, high-temperature www.springer.com/journal/40145 mechanical properties, as well as creep resistance [321][322][323].…”
Section: Ceramic Matrix Compositesmentioning
confidence: 99%
“…The exure strength of composite1200 (183 MPa) was higher than the reported values (57.3 MPa) of PDCs fabricated by DLP-printing technology, and is also at the same level with PDCs processed through other methods. [34][35][36][37] A nanoindentation test was undertaken to calculate the hardness and modulus. Composite1200 showed higher hardness (3.4 GPa) and modulus (54.1 GPa) than composite900 and composite1400.…”
Section: Resultsmentioning
confidence: 99%
“…As the ceramic yield rises, fewer gases escape during the pyrolysis process, resulting in fewer pores. Certain modifications are made to the precursors such as Polycarbosilane (PCS)-Allyl-substituted to form AHPCS with 72% yield, polysiloxane-starfire systems resin with 78% yield, boron modified AHPCS with 75% yield, polymer-thysilane added before curing at 320 °C with 91% yield [73][74][75].…”
Section: Polymer Infiltration and Pyrolysismentioning
confidence: 99%