zldmЗаводская лаборатория. Диагностика материаловIndustrial laboratory. Diagnostics of materials1028-68612588-0187ООО «Издательство «ТЕСТ-ЗЛ»10.26896/1028-6861-2022-88-12-51-63zldm-1818Research ArticleИССЛЕДОВАНИЕ СТРУКТУРЫ И СВОЙСТВ. МЕХАНИКА МАТЕРИАЛОВ: ПРОЧНОСТЬ, РЕСУРС, БЕЗОПАСНОСТЬTESTING OF STRUCTURE AND PARAMETERS. MECHANICAL TESTING METHODSМетоды определения характеристик адгезии в системах с теплозащитными покрытиямиMethods for characterizing the interfacial adhesion in thermal barrier coating systemsФедороваЕ. Н.FedorovaE. N.

Федорова Елена Николаевна.

660041, Красноярск, Свободный просп., д. 79; 660049, Красноярск, просп. Мира, д. 53

Elena N. Fedorova.

79, Svobodny prosp., Krasnoyarsk, 660041; 53, prosp. Mira, Krasnoyarsk, 660049

СуходоеваН. В.SukhodoevaN. V.

Суходоева Надежда Вячеславовна.

660041, Красноярск, Свободный просп., д. 79

Nadezhda V. Sukhodoeva.

79, Svobodny prosp., Krasnoyarsk, 660041

suhodoevanadezda@gmail.comМосквичевВ. В.MoskvichevV. V.

Москвичев Владимир Викторович.

660041, Красноярск, Свободный просп., д. 79; 660049, Красноярск, просп. Мира, д. 53

Vladimir V. Moskvichev.

79, Svobodny prosp., Krasnoyarsk, 660041; 53, prosp. Mira, Krasnoyarsk, 660049

ОгорельцеваН. В.OgoreltcevaN. V.

Огорельцева Нина Валерьевна.

660041, Красноярск, Свободный просп., д. 79

Nina V. Ogoreltceva.

79, Svobodny prosp., Krasnoyarsk, 660041

КлимкинЮ. О.KlimkinYu. O.

Климкин Юрий Олегович.

660041, Красноярск, Свободный просп., д. 79

Yuri O. Klimkin.

79, Svobodny prosp., Krasnoyarsk, 660041

Сибирский федеральный университет; Красноярский филиал Федерального исследовательского центра информационных и вычислительных технологийРоссияSiberian Federal University; Krasnoyarsk Branch of the Federal Research Center for Information and Computational TechnologiesRussian FederationСибирский федеральный университетРоссияSiberian Federal UniversityRussian Federation20222512202288125163Copyright © Федорова Е.Н., Суходоева Н.В., Москвичев В.В., Огорельцева Н.В., Климкин Ю.О., 20222022Федорова Е.Н., Суходоева Н.В., Москвичев В.В., Огорельцева Н.В., Климкин Ю.О.Fedorova E.N., Sukhodoeva N.V., Moskvichev V.V., Ogoreltceva N.V., Klimkin Y.O.Данная работа распространяется под лицензией Creative Commons Attribution 4.0.This work is licensed under a Creative Commons Attribution 4.0 License.https://www.zldm.ru/jour/article/view/1818

Системы теплозащитных покрытий (ТЗП) широко используют в современных высокотемпературных авиационных газовых турбинах для защиты поверхностей лопаток от газовой коррозии и воздействия высоких рабочих температур. Для прогнозирования долговечности систем с ТЗП одним из ключевых является параметр, характеризующий сопротивление отслоению (адгезию) на поверхностях раздела. Цель работы — анализ существующих методов количественного определения характеристик адгезии для многослойных теплозащитных покрытий и защитных оксидных слоев на поверхности жаропрочных сплавов на основе никеля и выявление причин разброса показателей адгезии. Рассмотрены теоретические предпосылки для определения характеристик адгезии. Показано отсутствие национальных стандартов для их оценки и отмечен значительный разброс значений, полученных при использовании международных документов, регламентирующих испытания, и авторских методик. Значения интенсивности высвобождения упругой энергии деформации варьируются 0,3 до 230 Дж/м2 в зависимости от метода определения, условий эксперимента и параметров системы. Причины разброса значений условно разделены на две группы: 1 — внутренние, обусловленные особенностями формирования слоев ТЗП и температурным воздействием, определяющие величину и характер распределения остаточных деформаций и напряжений, а также направление, по которому инициируется разрушение; 2 — внешние, обусловленные особенностями проведения испытаний и обработки результатов. Показана необходимость комплексного подхода к оценке характеристик адгезии, учитывающего влияние внешних и внутренних факторов.

Thermal barrier coatings (TBC) are widely used to protect the hot section structural components, such as aircraft gas turbine, against hot corrosion and large thermal gradients during the service life. The resistance to interfacial debonding (adhesion) is one of the key factors for predicting the TBC durability during operation. The goal of the study is analysis of the existing approaches to quantification of the interfacial adhesion for multi-layered thermal barrier coating systems and thermally-grown oxide on Ni-based superalloys and discussion of the problem regarding the reasons for a large spread of the adhesion characteristics. Theoretical prerequisites for determining the adhesion characteristics are considered to provide a theoretical background for quantification of the interfacial adhesion. The absence of national standard tests applicable to TBC is marked along with a significant scatter of the values obtained using international test-regulating documents and proprietary technologies. The values of the intensity of the strain energy release are found to vary from 0.3 to 230 J/m2 depending on the method for measuring adhesion, experimental details and type of the system considered. The factors that determine a large spread of the interfacial adhesion values were divided into two groups: 1 — intrinsic, attributed to the features of TBC layer formation and temperature affecting the value and distribution of residual strains and stresses and direction of the failure initiation; 2 — extrinsic, which are related to test conditions and technique of experimental data processing. A complex approach involving both intrinsic and extrinsic parameters is required to address the problem of interfacial adhesion quantification.

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