文章信息/Info

Title:

Research Progress on Insulation Performance of Thermal Barrier Coatings on Turbine Blade

文章編號:

1674-3962(2020)10-0707-16

作者:

周益春1; 楊麗1;  2; 劉志遠(yuǎn)1; 朱旺1

（1. 湘潭大學(xué)材料科學(xué)與工程學(xué)院, 湖南 湘潭 411105）（2. 西安電子科技大學(xué)先進(jìn)材料與納米科技學(xué)院, 陜西 西安 710126）

Author(s):

ZHOU Yichun1;  YANG Li1; 2;  LIU Zhiyuan1 ;  ZHU Wang1

(1. School of Materials Science and Engineering, Xiangtan University, Xiangtan 411105, China) (2. School of Advanced Materials and Nanotechnology, Xidian University, Xi�餫n 710126, China)

關(guān)鍵詞:

渦輪葉片; 熱障涂層; 隔熱效果; 試驗裝置; 測溫技術(shù)

Keywords:

turbine blade;  thermal barrier coatings;  thermal insulation performance;  test devices;  temperature measuring techniques

分類號:

TG174.4;V231

DOI:

10.7502/j.issn.1674-3962.202007035

文獻(xiàn)標(biāo)志碼:

A

摘要:

隨著航空發(fā)動機(jī)的發(fā)展，熱障涂層已經(jīng)變?yōu)槲磥砀咝阅馨l(fā)動機(jī)不可缺少的技術(shù)，其隔熱效果的準(zhǔn)確評價與預(yù)測是進(jìn)行渦輪葉片優(yōu)化設(shè)計、發(fā)動機(jī)性能提升的關(guān)鍵問題�；仡櫫私�些年來渦輪葉片熱障涂層的隔熱效果研究的理論方法、模擬實驗裝置與測溫技術(shù)的研究進(jìn)展，進(jìn)一步從材料參數(shù)、服役環(huán)境以及渦輪葉片結(jié)構(gòu)3個方面介紹了渦輪葉片熱障涂層隔熱效果的影響因素和有關(guān)規(guī)律發(fā)現(xiàn)。最后展望了熱障涂層隔熱效果研究的發(fā)展趨勢和挑戰(zhàn)。影響熱障涂層隔熱效果的服役環(huán)境和冷卻結(jié)構(gòu)方面因素眾多，當(dāng)前的實驗研究還不充分，未來熱障涂層隔熱效果的研究趨勢是：優(yōu)化熱障涂層與氣膜冷卻相互影響及其服役可靠性相互耦合的評價理論和試驗方法，開發(fā)針對渦輪葉片服役環(huán)境下熱障涂層表面和界面溫度測量技術(shù)，研究高速旋轉(zhuǎn)下燃?xì)�、冷氣等相關(guān)參數(shù)對隔熱效果和可靠性的影響因素。

Abstract:

With the development of aeroengines, thermal barrier coating (TBC) has become one of the key technologies for future high performance aero-engine turbine blade. Evaluation and prediction of thermal insulation performance are the key problems for TBC optimization design of turbine blade and performance improvement of aero-engine. In this paper, the theory analysis methods, testing devices and temperature measuring techniques for TBC thermal insulation performance in recent years are reviewed, and the effects of material parameters, service environment and structure of turbine blade on TBC thermal insulation performance are introduced. Finally, the research development trend and challenges of TBC thermal insulation performance on turbine blades are prospected. There are many factors affecting the thermal insulation effectiveness of TBC from service environment and structure of turbine blade aspects, and the current experimental research is not sufficient. The development trends of the thermal insulation effectiveness of TBC contain: (i) improving evaluation theory of interaction between TBC and film cooling and testing method for reliability of TBC in service; (ii) developing the technology for measuring the surface and interface temperature of TBC in the service condition; (iii) investigating these influence of parameters about gas and coolant on thermal insulation effectiveness and reliability of TBC under high speed rotation.