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A process of forming a Si-containing ceramic comprises forming a Si-based polymeric composition. The process includes forming a Si-based polymeric composition; functionalizing said Si-based polymeric composition through covalent bond formation with an ionizable side group; and adding thermal energy under a controlled atmosphere to said Si-based polymeric composition. A turbine engine component (100) comprises an airfoil (120) and the airfoil comprises a Ceramic Matrix Composite (CMC) material.
A process of forming a Si-containing ceramic comprises forming a Si-based polymeric composition. The process includes forming a Si-based polymeric composition; functionalizing said Si-based polymeric composition through covalent bond formation with an ionizable side group; and adding thermal energy under a controlled atmosphere to said Si-based polymeric composition. A turbine engine component (100) comprises an airfoil (120) and the airfoil comprises a Ceramic Matrix Composite (CMC) material.
PRECERAMIC IONIC SYSTEMS
PRÄKERAMISCHE IONISCHE SYSTEME
SYSTÈMES IONIQUES PRÉCÉRAMIQUES
SCHMIDT WAYDE R (author)
2020-05-06
Patent
Electronic Resource
English