为满足先进航空发动机大推力、轻量化、高可靠的发展需求,亟需提升涡轮叶片的耐温能力和工作可靠性,热障涂层技术作为提高航空发动机涡轮叶片耐温能力的关键技术之一,其综合性能的提升和使用成本的降低受到广泛关注。为充分发挥涡轮叶片热障涂层的使用潜力,本文立足工程实际应用,系统梳理了涡轮叶片热障涂层在结构设计、厚度与组织调控、服役损伤修复三大核心环节的技术控制要点,结合相关调研深入阐述了涂层结构、厚度、孔隙率、柱状组织间隙等对涂层隔热效果、抗冲击性能的影响机制,重点介绍了涡轮叶片热障涂层修复过程中损伤陶瓷层去除的技术原理与实际应用现状,可为提升涡轮叶片热障涂层的隔热效果、抗冲击性能和降低使用成本提供指导。最后,本文从多层结构优化设计、叶身涂层组织分区差异化控制、将可修复性纳入涂层新材料研发需求等方面,提出了涡轮叶片热障涂层综合性能提升和高效修复技术的发展建议,以期促进热障涂层技术在关键热端部件的推广应用,助力先进航空发动机综合性能提升。
Abstract
To satisfy the ever-increasing development requirements of high thrust-to-weight ratio, lightweight structural design and long-term operational reliability for modern advanced aeroengines, it is of great significance and urgency to upgrade the high-temperature resistance and service stability of turbine blades. As the core hot-end components inside aeroengine turbomachinery, turbine blades are subject to harsh service conditions including extreme high-temperature gas flow, complex mechanical loads, thermal-mechanical coupling fatigue and corrosive oxidation environments during long-term operation. Under such severe service circumstances, the performance degradation and premature failure of turbine blades will directly restrict the thrust output, service life and safety margin of the whole propulsion system. As one of the most indispensable thermal protection technologies for aeroengine turbine blades, thermal barrier coatings (TBCs) are widely adopted to reduce the metal substrate temperature, alleviate thermal-mechanical damage and extend the service cycle of high-temperature alloy blades. In recent years, with the continuous improvement of aeroengine performance indicators, researchers and engineering practitioners have paid widespread attention to improving the comprehensive service performance of TBCs and cutting down their full-life-cycle application, maintenance and repair costs. The trade-off between high thermal insulation capacity, excellent mechanical robustness and low-cost maintainability has become a key technical challenge in the research and engineering application of turbine blade thermal barrier coatings.
In order to fully exploit the engineering service potential of thermal barrier coatings applied on aeroengine turbine blades, the work aims to conduct a study on the real-world engineering application scenarios instead of simple laboratory experimental conditions. Based on practical engineering experience and relevant technical investigations, the key technical control points for turbine blade TBCs are systematically summarized, covering three core technical links, namely coating structural design, thickness and microstructure regulation, as well as service-induced damage repair. On the basis of comprehensive literature review and engineering case analysis, the underlying effect mechanisms of multiple critical coating characteristic parameters are further elucidated, including overall coating architecture, coating thickness, internal porosity, and inter-column gaps within the ceramic top-layer, on the thermal insulation effect and impact-resistant performance of the whole thermal barrier coating system. The above-mentioned microstructural features jointly determine the heat-transfer behavior, thermal stress distribution and mechanical failure resistance of TBCs under complex service loads. Special emphasis is placed on the technical principles, typical technical routes and current practical engineering application status of damaged ceramic top-layer removal, which acts as the prerequisite step for TBCs repair of turbine blades. The discussion and analysis presented in this work can provide valuable theoretical reference and practical technical guidance for improving the thermal insulation performance and impact resistance of turbine blade thermal barrier coatings, as well as effectively reducing their engineering application and maintenance expenses.
Furthermore, aiming at the existing bottlenecks in performance improvement and maintainability of turbine blade thermal barrier coatings, this work puts forward targeted development suggestions for comprehensive performance enhancement and efficient repair technologies from multiple technical dimensions. These proposals include the optimization design of multi-layer coating architectures, differentiated zonal microstructure control for coatings deposited on blade airfoils, and the introduction of repairability requirements into the design and development of novel coating materials. It is expected that these technical ideas and development orientations can accelerate the popularization and large-scale engineering application of thermal barrier coating technologies for critical hot-end components of aeroengines. Meanwhile, the research conclusions and proposed strategies can provide meaningful reference for the subsequent development of thermal protection systems, and further contribute to the overall performance upgrading, reliability improvement and cost control of advanced aeroengines.
关键词
涡轮叶片 /
热障涂层 /
结构设计 /
组织控制 /
修复工艺
Key words
turbine blade /
thermal barrier coatings /
structural design /
microstructure control /
repair process
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参考文献
[1] 陈仲光, 张志舒, 李德旺, 等. F119发动机总体性能特点分析与评估[J]. 航空科学技术, 2013, 24(3): 39-42.
CHEN Z G, ZHANG Z S, LI D W, et al.Analysis and Evaluation of F119 Engine Overall Performance[J]. Aeronautical Science & Technology, 2013, 24(3): 39-42.
[2] 任静, 李雪英, 郭欣欣, 等. 燃气涡轮高效冷却技术及设计方法发展趋势[J]. 清华大学学报(自然科学版), 2022, 62(4): 794-801.
REN J, LI X Y, GUO X X, et al.Development Trends in High-Efficiency Gas Turbine Cooling Methods[J]. Journal of Tsinghua University (Science and Technology), 2022, 62(4): 794-801.
[3] 胡壮麒, 刘丽荣, 金涛, 等. 镍基单晶高温合金的发展[J]. 航空发动机, 2005, 31(3): 1-7.
HU Z Q, LIU L R, JIN T, et al.Development of the Ni-Base Single Crystal Superalloys[J]. Aeroengine, 2005, 31(3): 1-7.
[4] 田伟, 郭会明, 刘砚飞. 新型热障涂层在先进航空发动机中的应用研究进展[J]. 航空材料学报, 2025, 45(6): 68-80.
TIAN W, GUO H M, LIU Y F.Research Progress on Application of New Thermal Barrier Coatings in Advanced Aero-Engines[J]. Journal of Aeronautical Materials, 2025, 45(6): 68-80.
[5] 赵云松, 张迈, 戴建伟, 等. 航空发动机涡轮叶片热障涂层研究进展[J]. 材料导报, 2023, 37(6): 77-83.
ZHAO Y S, ZHANG M, DAI J W, et al.Research Progress of Thermal Barrier Coatings for Aeroengine Turbine Blades[J]. Materials Reports, 2023, 37(6): 77-83.
[6] 刘砚飞, 钟燕, 陶稀鹏, 等. 镍基单晶高温合金/热障涂层体系的应用研究进展[J]. 材料工程, 2025, 53(9): 1-10.
LIU Y F, ZHONG Y, TAO X P, et al.Research Progress in Application of Nickel-Based Single Crystal Superalloy/ Thermal Barrier Coating System[J]. Journal of Materials Engineering, 2025, 53(9): 1-10.
[7] 张健, 王莉, 谢光, 等. 镍基单晶高温合金的研发进展[J]. 金属学报, 2023, 59(9): 1109-1124.
ZHANG J, WANG L, XIE G, et al.Recent Progress in Research and Development of Nickel-Based Single Crystal Superalloys[J]. Acta Metallurgica Sinica, 2023, 59(9): 1109-1124.
[8] PADTURE N P, GELL M, JORDAN E H.Thermal Barrier Coatings for Gas-Turbine Engine Applications[J]. Science, 2002, 296(5566): 280-284.
[9] CLARKE D R, OECHSNER M, PADTURE N P.Thermal-Barrier Coatings for More Efficient Gas-Turbine Engines[J]. MRS Bulletin, 2012, 37(10): 891-898.
[10] VAEN R, BAKAN E, MACK D, et al.Performance of YSZ and Gd2Zr2O7/YSZ Double Layer Thermal Barrier Coatings in Burner Rig Tests[J]. Journal of the European Ceramic Society, 2020, 40(2): 480-490.
[11] WEI Z Y, MENG G H, CHEN L, et al.Progress in Ceramic Materials and Structure Design Toward Advanced Thermal Barrier Coatings[J]. Journal of Advanced Ceramics, 2022, 11(7): 985-1068.
[12] 罗敏, 吴杨, 郭磊, 等. 热障涂层的CMAS腐蚀与防护研究进展[J]. 热喷涂技术, 2025, 17(2): 1-18.
LUO M, WU Y, GUO L, et al.Advances in CMAS Corrosion and Protect Method of Thermal Barrier Coatings[J]. Thermal Spray Technology, 2025, 17(2): 1-18.
[13] ZHU D M, MILLER R A.Development of Advanced Low Conductivity Thermal Barrier Coatings[J]. International Journal of Applied Ceramic Technology, 2004, 1(1): 86-94.
[14] GUO L, GUO H B, GONG S K, et al.Improvement on the Phase Stability, Mechanical Properties and Thermal Insulation of Y2O3-Stabilized ZrO2 by Gd2O3 and Yb2O3 Co-Doping[J]. Ceramics International, 2013, 39(8): 9009-9015.
[15] 张华, 寇录文, 王玉锋, 等. CMAS侵蚀环境下YSZ+ GYbZ双陶瓷热障涂层热循环失效机制研究[J]. 燃气涡轮试验与研究, 2025, 38(5): 47-56.
ZHANG H, KOU L W, WANG Y F, et al.Thermal Cycle Failure Mechanism Study of YSZ+GYbZ Double-Ceramic-Layer TBCS under CMAS Erosion Environment[J]. Gas Turbine Experiment and Research, 2025, 38(5): 47-56.
[16] 罗宇晴, 周腾, 刘冠熙, 等. 超高温LaZrCeO热障涂层外观颜色控制研究[J]. 燃气涡轮试验与研究, 2025, 38(5): 68-74.
LUO Y Q, ZHOU T, LIU G X, et al.Color Control of the Ultrahigh Temperature LaZrCeO Thermal Barrier Coating[J]. Gas Turbine Experiment and Research, 2025, 38(5): 68-74.
[17] 李嘉, 谢铮, 何箐, 等. Gd2O3-Yb2O3-Y2O3-ZrO2热障涂层材料的热物理性能[J]. 表面技术, 2015, 44(9): 18-22.
LI J, XIE Z, HE Q, et al.Thermophysical Properties of Gd2O3-Yb2O3-Y2O3-ZrO2 Thermal Barrier Coating Material[J]. Surface Technology, 2015, 44(9): 18-22.
[18] 牟仁德, 申造宇, 刘冠熙. EB-PVD制备LaZrCeO/YSZ热障涂层显微组织结构及火焰热冲击失效行为研究[J]. 表面技术, 2026, 55(7): 264-273.
MU R D, SHEN Z Y, LIU G X.Microstructures and Flame Thermal Shock Failure Behaviors of EB-PVD Deposited LaZrCeO/YSZ Thermal Barrier Coatings[J]. Surface Technology, 2026, 55(7): 264-273.
[19] 潘恒沛, 袁晓冬, 夏申琳, 等. La2Zr2O7厚度对La2Zr2O7-8YSZ双陶瓷热障涂层隔热性能与初始残余应力影响的数值模拟[J]. 铸造技术, 2020, 41(9): 831-834.
PAN H P, YUAN X D, XIA S L, et al.Numerical Simulation of Influence of La2Zr2O7 Thickness on Thermal Insulation Performance and Initial Residual Stress of La2Zr2O7-8YSZ Double Ceramic Thermal Barrier Coating[J]. Foundry Technology, 2020, 41(9): 831-834.
[20] 梅娇, 薛召露, 郑越, 等. 不同厚度比GdYb-YSZ/8YSZ双陶瓷层热障涂层的水淬-热震循环行为及失效机理[J]. 硅酸盐学报, 2025, 53(4): 985-997.
MEI J, XUE Z L, ZHENG Y, et al.Thermal Shock Cycling Behavior and Failure Mechanism of GdYb-YSZ/ 8YSZ Double Ceramic Layer Thermal Barrier Coatings with Different Thickness Ratios[J]. Journal of the Chinese Ceramic Society, 2025, 53(4): 985-997.
[21] 张小伍, 徐佰明. 电子束物理气相沉积热障涂层隔热性能研究[J]. 汽轮机技术, 2020, 62(5): 399-400.
ZHANG X W, XU B M.Thermal Insulating Properties of YSZ TBC Deposited by EB-PVD[J]. Turbine Technology, 2020, 62(5): 399-400.
[22] ZHANG J, GUO X Y, JUNG Y G, et al.Lanthanum Zirconate Based Thermal Barrier Coatings: A Review[J]. Surface and Coatings Technology, 2017, 323: 18-29.
[23] 魏绍斌, 陆峰, 何利民, 等. 热障涂层制备技术及陶瓷层材料的研究进展[J]. 热喷涂技术, 2013, 5(1): 31-37.
WEI S B, LU F, HE L M, et al.Progress in Processing Techniques and Ceramic Materials of Thermal Barrier Coatings[J]. Thermal Spray Technology, 2013, 5(1): 31-37.
[24] SCHULZ U, LEYENS C, FRITSCHER K, et al.Some Recent Trends in Research and Technology of Advanced Thermal Barrier Coatings[J]. Aerospace Science and Technology, 2003, 7(1): 73-80.
[25] 郝洪亮, 龙芸, 杨希刚, 等. 高温服役过程热障涂层隔热性能演变规律[J]. 动力工程学报, 2020, 40(8): 671-677.
HAO H L, LONG Y, YANG X G, et al.Insulation Property Evolution of Thermal Barrier Coatings during High Temperature Services[J]. Journal of Chinese Society of Power Engineering, 2020, 40(8): 671-677.
[26] 刘阳, 蔡洪能, 魏志远, 等. 等离子喷涂热障涂层内孔隙对其隔热性能的影响[J]. 材料保护, 2021, 54(11): 1-9.
LIU Y, CAI H N, WEI Z Y, et al.Influence of the Porosity on the Thermal Insulation Performance of Plasma Sprayed Thermal Barrier Coating[J]. Materials Protection, 2021, 54(11): 1-9.
[27] 牟仁德, 丁宁, 刘冠熙, 等. 不同电子束流EB-PVD制备YSZ热障涂层的组织结构演变、热循环寿命与失效行为分析[J]. 材料工程, 2024, 52(12): 44-52.
MU R D, DING N, LIU G X, et al.Microstructure Evolution, thermal Cycling Lifetime, and Failure Behavior Analysis of YSZ Thermal Barrier Coatings Prepared by EB-PVD with Different Electron Beam Currents[J]. Journal of Materials Engineering, 2024, 52(12): 44-52.
[28] QIU S Y, WU C W, HUANG C G, et al.Microstructure Dependence of Effective Thermal Conductivity of EB- PVD TBCS[J]. Materials, 2021, 14(8): 1838.
[29] LIU J, ZHENG H, HUANG W, et al.Effects of Transient Thermal Shock on the Microstructure and Mechanical Properties of CoCrFeNiMn High-Entropy Alloy Coatings[J]. Frontiers in Materials, 2021, 8: 805296.
[30] ZHOU G, TIAN Y, SHI F, et al.Low-Energy Pulsed Ion Beam Technology with Ultra-High Material Removal Resolution and Widely Adjustable Removal Efficiency[J]. Micromachines, 2021, 12: 1370.
[31] QU J H, GUO C A, ZHANG J. Hot Corrosion Behavior of NiCoCrAlYSiHf Coating Deposited by Arc Ion Plating[J]. Advanced Materials Research, 2012, 472-475: 395-399.
[32] 陈举, 苏倩, 耿永祥, 等. 热障涂层失效行为及其修复再制造研究进展[J]. 航空工程进展, 2021, 12(4): 25-35.
CHEN J, SU Q, GENG Y X, et al.Research Progress on Failure Behavior and Repair Remanufacturing of Thermal Barrier Coatings[J]. Advances in Aeronautical Science and Engineering, 2021, 12(4): 25-35.
[33] 赵婷婷, 张晓东, 李国强, 等. 航空发动机自愈合YSZ基热障涂层的研究进展[J]. 燃气涡轮试验与研究, 2025, 38(5): 11-34.
ZHAO T T, ZHANG X D, LI G Q, et al.Research Progress on Self-Healing YSZ-Based Thermal Barrier Coating of Aero-Engine[J]. Gas Turbine Experiment and Research, 2025, 38(5): 11-34.
[34] 张彬, 蔡妍, 刘嘉曦, 等. 物理法/化学法退除NiCoCrAlYHf涂层对DD6合金表面组织结构的影响[J]. 稀有金属材料与工程, 2024, 53(8): 2200-2204.
ZHANG B, CAI Y, LIU J X, et al.Effect of Physical/ Chemical Removal of NiCoCrAlYHf Coatings on the Surface Microstructure of DD6 Alloy[J]. Rare Metal Materials and Engineering, 2024, 53(8): 2200-2204.
[35] XU W, YANG S L, TAO W, et al.Effect of Al-Si Coating Removal State on Microstructure and Mechanical Properties of Laser Welded 22MnB5 Steel[J]. Journal of Materials Engineering and Performance, 2023, 32(9): 4205-4215.
[36] 蔡妍, 张涛, 赵文君, 等. NiCoCrAlYSiHf涂层退除对DSM11合金性能的影响[J]. 材料工程, 2025, 53(6): 44-51.
CAI Y, ZHANG T, ZHAO W J, et al.Effect of Removal of NiCoCrAlYSiHf Coatings on Performance of DSM11 Alloy[J]. Journal of Materials Engineering, 2025, 53(6): 44-51.
[37] 章易镰, 冯杰才, 郭双全, 等. 航空叶片热障涂层激光清洗工艺及评价研究[J]. 应用激光, 2025, 45(2): 98-113.
ZHANG Y L, FENG J C, GUO S Q, et al.Study on Laser Cleaning Processing and Evaluation of Thermal Barrier Coating of Aero-Blade[J]. Applied Laser, 2025, 45(2): 98-113.
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