帮助 关于我们

返回检索结果

NiCrW-BN气路封严涂层的可刮削性评价
Abradability Evaluation of NiCrW-BN Gas Path Seal Coating

查看参考文献14篇

文摘 用销-盘、单摆冲击划痕和高速刮擦三种试验方法,研究了两种NiCrW-BN封严涂层的可刮削性.结果表明:封严涂层的可刮削性不同于耐磨性,即涂层的磨损量、比能耗和硬度等测量结果,不能单独作为其可刮削性的评价判据;评价封严涂层的可刮削性,应该综合涂层磨损、叶片磨损、摩擦系数和磨痕形貌等多方面的信息.封严涂层的可刮削性能受试验条件的影响十分明显,高速刮擦试验可模拟涂层工作参数(刮擦线速度、入侵速率等),可能重现其磨损现象,因此采用高速刮擦试验方法评价封严涂层的可刮削性更为合理
其他语种文摘 The abradability of two NiCrW-BN seal coatings processed by different heat treatments were observed by pin-disk, single-pass scratching, and high-speed wear tests. The results show that seal coating abradability is different from its wear-resistance,i.e.measuring of wear loss, wear-resistance, specific energy consumption and hardness, can not be used as abradability criterion. Coating abradability evaluation should be composed of extensive information, such as coating and blade wear loss, friction coefficient, wear topography. Seal coating abradability is obviously influenced by test condition, while high-speed rubbing test can simulate working variables of seal coating, such as rub linear speed, incursion velocity, probably reproduce its wear phenomena. Therefore the adoption of high-speed test to evaluate seal coating abradability is more reasonable
来源 材料研究学报 ,2010,24(4):406-410 【核心库】
关键词 复合材料 ; 可刮削性 ; 高速刮擦法 ; 封严涂层 ; 可刮削
地址

中国科学院金属研究所, 沈阳, 110016

语种 中文
文献类型 研究性论文
ISSN 1005-3093
学科 金属学与金属工艺;机械、仪表工业
基金 国家自然科学基金
文献收藏号 CSCD:3996824

参考文献 共 14 共1页

1.  DeMasi-marcin J T. Protective coatings in the gas turbine engine. Surface & Coatings Technology,1994,68/69(1/3):1 CSCD被引 35    
2.  刘夙伟. 封严涂层材料及其可刮削性的评价. 中国表面工程,2009,22(1):12 CSCD被引 21    
3.  Emery A F. An experimental investigation of temperatures due to rubbing at the blade-seal interface in an aircraft compressor. Wear,1983,91(2):117 CSCD被引 8    
4.  Borel M O. The wear mechanisms occurring in abradable seals of gas turbines. Surface & Coatings Technology,1989,39/40(1/3):117 CSCD被引 15    
5.  Chappel D E. The International Gas Turbine & Aeroengine Congress & Exhibition. Gas path blade tip seals: abradable seal material testing at utility gas and steam turbine operating conditions(New Orleans, USA, ASME, 2001) CSCD被引 1    
6.  Hajmrle K. Shiembob, in: ASME Turbo Expo.(vol. 4), Abradable seals for gas turbines and other rotary equipment,2004:673 CSCD被引 1    
7.  Kennedy F E. Single-pass rub testing of abradable seal materials. Journal of the ASLE,1982,38(9):557 CSCD被引 1    
8.  Liang Y N. Evaluation of abradability of porous seal materials in a single pendulum scratch device. Wear,1994,177(2):167 CSCD被引 10    
9.  Bill R C. Wear of seal materials used in aircraft propulsion system. Wear,1980,59(1):165 CSCD被引 11    
10.  Laverty W F. Rub energetics of compressor blade tip seals. Wear,1982,75(1):1 CSCD被引 6    
11.  Novinski E. Modified zirconia abradable seal coating for high temperature gas turbine applications. Thin Solid Films,1982,95:255 CSCD被引 9    
12.  易茂中. 冲击刮削法评价封严涂层的可磨耗性. 航空学报,1999,20(3):249 CSCD被引 4    
13.  Yi M Z. Friction and wear behavior and abradability of abradable seal coating. Wear,1999,231(1):47 CSCD被引 20    
14.  Jin Y S. Proceedings of the international symposium on tribology(Vol.2). The importance of tribology in the development and application of abradable plasma sprayed coatings for aircraft engines,1993:756 CSCD被引 1    
引证文献 2

1 雷冰 封严涂层腐蚀检测及评价方法研究 腐蚀科学与防护技术,2017,29(6):651-656
CSCD被引 1

2 张阳 激光熔覆CoNiCrAlY 高温合金格栅的高速刮削性能 中国表面工程,2018,31(2):165-171
CSCD被引 2

显示所有2篇文献

论文科学数据集
PlumX Metrics
相关文献

 作者相关
 关键词相关
 参考文献相关

版权所有 ©2008 中国科学院文献情报中心 制作维护:中国科学院文献情报中心
地址:北京中关村北四环西路33号 邮政编码:100190 联系电话:(010)82627496 E-mail:cscd@mail.las.ac.cn 京ICP备05002861号-4 | 京公网安备11010802043238号