Multilayered Thermal-Protective HfC-ZrB[2]-SiC-ZrO[2] Ceramic Material; AIP Conference Proceedings; Vol. 2167 : Advanced Materials with Hierarchical Structure for New Technologies and Reliable Structures 2019 (AMHS'19)

Λεπτομέρειες βιβλιογραφικής εγγραφής
Parent link:AIP Conference Proceedings
Vol. 2167 : Advanced Materials with Hierarchical Structure for New Technologies and Reliable Structures 2019 (AMHS'19).— 2019.— [020228, 5 p.]
Συλλογικό Έργο: Национальный исследовательский Томский политехнический университет Школа базовой инженерной подготовки Отделение общетехнических дисциплин, Национальный исследовательский Томский политехнический университет Инженерная школа новых производственных технологий Отделение материаловедения
Άλλοι συγγραφείς: Mirovoy Yu. A. Yury Aleksandrovich, Burlachenko A. G., Buyakova S. P. Svetlana Petrovna, Dedova E. S. Elena Sergeevna, Kulkov S. N. Sergey Nikolaevich
Περίληψη:Title screen
Ultra-high-temperature ceramics based on zirconium diboride and silicon and hafnium carbides are presented as composites with ceramic matrix and oxidation-resistant surface. Relatively low density, high strength at extreme temperatures and operability at oxidative environment with temperature up to 2000°C make these materials useful for aerospace construction and power engineering. HfC-ZrB[2]-SiC-ZrO[2] systems are presented, structural analysis and the results of temperature tests in high-enthalpy gas are provided. It was demonstrated that high resistance of HfC-ZrB[2]-SiCZrO[2] system to high-temperature corrosion is achieved owing to formation of protective oxide layer with variable composition.
Режим доступа: по договору с организацией-держателем ресурса
Γλώσσα:Αγγλικά
Έκδοση: 2019
Θέματα:
Διαθέσιμο Online:https://doi.org/10.1063/1.5132095
Μορφή: Ηλεκτρονική πηγή Κεφάλαιο βιβλίου
KOHA link:https://koha.lib.tpu.ru/cgi-bin/koha/opac-detail.pl?biblionumber=661517
Περιγραφή
Περίληψη:Title screen
Ultra-high-temperature ceramics based on zirconium diboride and silicon and hafnium carbides are presented as composites with ceramic matrix and oxidation-resistant surface. Relatively low density, high strength at extreme temperatures and operability at oxidative environment with temperature up to 2000°C make these materials useful for aerospace construction and power engineering. HfC-ZrB[2]-SiC-ZrO[2] systems are presented, structural analysis and the results of temperature tests in high-enthalpy gas are provided. It was demonstrated that high resistance of HfC-ZrB[2]-SiCZrO[2] system to high-temperature corrosion is achieved owing to formation of protective oxide layer with variable composition.
Режим доступа: по договору с организацией-держателем ресурса
DOI:10.1063/1.5132095