欢迎登录材料期刊网

材料期刊网

高级检索

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.

参考文献

[1] J.T.DeMasi-marcin,D.K.Gupta,Protective coatings in the gas turbine engine,Surface & Coatings Technology,68-69(1-3),1(1994)
[2] LIU Suwei,LI Shu,LIU Yang,Seal coating and evaluation of its abradability,China Surface Engineering,22(1),12(2009)(刘夙伟,李曙,刘阳,封严涂层材料及其可刮削性的评价,中国表面工程,22(1),12(2009)1
[3] A.F.Emery,J.Wolak,S.Etemad,S.R.Choi,An experimental investigation of temperatures due to rubbing at the blade-aeal interface in an aircraft compressor,Wear,91(2),117(1983)
[4] M.O.Borel,A.R.Nicoll,H.W.Sch pfer,R.K.Schmid,The wear mechanisms occurring in abradable seals of gas turbines,Surface & Coatings Technology,39-40(1-3),117(1989)
[5] D.E.Chappel,L.Vo,H.W.Howe,in: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)p.1
[6] K.Hajmrle,P.Fiala,A.P.Chilkowich,L.T.Shiembob,in:ASME Turbo Expo.(vol.4),Abradable seals for gas turbines and other rotary equipment(Vienna,Australia,ASME,2004) p.673
[7] F.E.Kennedy,N.P.Hine,Single-pass rub testing of abradable seal materials,Journal of the ASLE,38(9),557(1982)
[8] Y.N.Liang,S.Z.Li,S.Li,Evaluation of abradability of porous seal materials in a single pendulum scratch device,Wear,177(2),167(1994)
[9] R.C.Bill,L.P.Ludwig,Wear of seal materials used in aircraft propulsion system,Wear,59(1),165(1980)
[10] W.F.Laverty,Rub energetics of compressor blade tip seals,Wear,75(1),1(1982)
[11] E.Novinski,J.Harrington,J.Klein,Modified zirconia abradable seal coating for high temperature gas turbine applications,Thin Solid Films,95,255(1982)
[12] YI Maozhong,ZHANG Xianlong,HU Naisai,HE Jiawen,Abradability evaluation of seal coating by impact-scraping test machine,Acta Aeronautica et Astronautica Sinica,20(3),249(1999)(易茂中,张先龙,胡奈赛,何家文,冲击刮削法评价封严涂层的可磨耗性,航空学报,20(3),249(1999))
[13] M.Z.Yi,J.W.He,B.Y.Huang,H.J.Zhou.Friction and wear behavior and abradability of abradable seal coating,Wear,231(1),47(1999)
[14] G.Barbezat,R.Clarke,A.R.Nicoll,in: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,edited by Y.S.Jin(Beijing,China,International Academic Publishers,1993)p.756
上一张 下一张
上一张 下一张
计量
  • 下载量()
  • 访问量()
文章评分
  • 您的评分:
  • 1
    0%
  • 2
    0%
  • 3
    0%
  • 4
    0%
  • 5
    0%