A5066268927- High-Temperature Coating Behaviors
- Nuclear Materials and Properties
- Advanced ceramic materials synthesis
- Intermetallics and Advanced Alloy Properties
- Catalytic Processes in Materials Science
- Nuclear materials and radiation effects
- Advanced materials and composites
- High Entropy Alloys Studies
- Semiconductor materials and devices
- High Temperature Alloys and Creep
- Particle Dynamics in Fluid Flows
- Metal and Thin Film Mechanics
- Additive Manufacturing Materials and Processes
- Flame retardant materials and properties
- Tribology and Wear Analysis
- Diamond and Carbon-based Materials Research
- Microwave Dielectric Ceramics Synthesis
- Glass properties and applications
- Thermal properties of materials
- Magnesium Oxide Properties and Applications
- MXene and MAX Phase Materials
- Aluminum Alloys Composites Properties
- Luminescence Properties of Advanced Materials
- DNA and Nucleic Acid Chemistry
- Electromagnetic wave absorption materials
Beihang University
2016-2025
Ministry of Industry and Information Technology
2017-2025
State Key Laboratory of Nonferrous Metals and Processes
2023
University of Nottingham Ningbo China
2023
Shaanxi University of Technology
2023
Beijing Advanced Sciences and Innovation Center
2019-2022
University of Massachusetts Lowell
2022
Northwest University
2022
University of Science and Technology Beijing
2011-2020
Shandong Institute of Automation
2017
Abstract Volcanic ash is a major threat to aviation safety. The softening/melting temperatures of volcanic lie far below typical aero‐engine operating temperatures. Thus, molten can accelerate the failure thermal barrier coatings (TBCs). Here, inspired by natural superhydrophobic surfaces (e.g., lotus leaf), molten‐volcanic‐ash‐phobic TBC, which provides large possibility eliminate issues TBCs, developed. A hierarchically structured surface first prepared on (Gd 0.9 Yb 0.1 ) 2 Zr O 7 (GYbZ)...
Abstract Aero-engine is a key part of aircraft, the operating temperature which being pushed to unprecedented levels for higher engine efficiency and performance. To accomplish gas-inlet aero-engines, applying thermal barrier coatings (TBCs) on hot-section metallic components, or even replacing some components in aero-engines with ceramic-matrix composites (CMCs) environmental-barrier (EBCs) them, are effective methods have been widely accepted. On other hand, increasing causes aircraft more...
Thermal barrier coatings (TBCs) with different levels of segmentation crack density were produced by spraying two types ZrO 2 –8Y O 3 powders. The fused and crushed powder has a greater capability forming segmented than the hollow sphere (HOSP) one. highly reveal much lower porosity compared traditionally sprayed coatings, thereby compromising property thermal insulation TBCs. Microstructure conductivity HOSP are more sensitive to changes in spray conditions. Segmentation cracks had strong...