Al/BN涂层性能及高速刮削下与TA11合金叶片的磨损行为
详细信息 查看官网全文
- 英文论文题名：Performance of Al/BN Coating and Wear Behavior between TA11 blade and Al/BN Coating during High Speed Rubbing
- 论文作者：张佳平 ; 芦国强 ; 李浩宇 ; 李明康 ; 薛伟海
- 英文论文作者：Zhang Jiaping ; Lu Guoqiang ; Li Haoyu ; Li Mingkang ; Xue Weihai ; Institute of Metal Research ; Chinese Academy of Sciences ; LiMing Aero-Engineering(Group) Corporation LTD. ; Shenyang
- 年：2016
- 作者机构：中国科学院金属研究所;沈阳黎明航空发动机(集团)有限责任公司技术中心热表所;
- 论文关键词：封严涂层 ; 相含量 ; 力学性能 ; 刮削机制
- 英文论文关键词：abradabe seal coating ; phase content ; mechanical performance ; rubbing behavior
- 会议召开时间：2016-10-31
- 会议录名称：探索 创新 交流（第7集）——第七届中国航空学会青年科技论坛文集（上册）
- 英文会议录名称：Discovery,Innovation and Communication——Proceedings of 7th CSAA Science and Technology Youth Forum
- 语种：中文
- 分类号：TG174.4
- 学会代码：ZGHU
- 会议名称：探索 创新 交流（第7集）——第七届中国航空学会青年科技论坛
- 会议地点：中国广东中山
- 主办单位：中国航空学会
- 学会名称：中国航空学会
- 页数：7
- 文件大小：2922k
- 原文格式：O
- 会议级别：全国
摘要
在本研究中对Al/BN封严涂层的相含量、拉伸结合强度、硬度以及抗冲蚀性能进行了测定,掌握Al/BN封严涂层相含量分布以及涂层力学性能情况。利用高速刮擦试验机模拟压气机叶片与封严涂层的刮擦行为,研究了Al/BN封严涂层与TA11钛合金模拟叶片体系在线速度250m/s,进给速度在0.002 mm/s和0.01 mm/s范围内的磨损行为。结果表明:较高线速度下涂层的磨损,在较低进给速度下,为涂层剥落和犁削机制以及涂层向叶片转移机制,随着刮削深度的增加涂层向叶片的转移层发生剥落;在较高进给速度下,涂层的磨损机制为剥落和犁削机制,涂层向叶片的转移层在叶片上发生了熔化和涂抹,为犁削和塑性变形机制。
In this research,the phase content,tensile bond strength,hardness and erosion wear of Al/BN abrade seal coating are tested,and the phase distributing and mechanical performance are also investigated.The friction mechanism between Al/BN abrade seal coating and TA11 blade is studied by high rubbing test experiment at line speed of 250m/s with feed speed of 0.002mm/s and 0.01 mm/s.The results reveal that the rubbing behavior of Al/BN abrade seal coating is coating flakes and ploughing,the coating material transfers to blade at lower feed speed and the transfer layer peels off with the' increase of rub depth,while at higher speed,the transfer layer melts and smears with plastic deformation.
In this research,the phase content,tensile bond strength,hardness and erosion wear of Al/BN abrade seal coating are tested,and the phase distributing and mechanical performance are also investigated.The friction mechanism between Al/BN abrade seal coating and TA11 blade is studied by high rubbing test experiment at line speed of 250m/s with feed speed of 0.002mm/s and 0.01 mm/s.The results reveal that the rubbing behavior of Al/BN abrade seal coating is coating flakes and ploughing,the coating material transfers to blade at lower feed speed and the transfer layer peels off with the' increase of rub depth,while at higher speed,the transfer layer melts and smears with plastic deformation.
引文
[1]Chupp R E,Hendricks R C,S B Lattime,et al.Sealing in Turbomachine.2006.
[2]Ludwig L P,Bill R C.Gas Path Sealing in Turbine Engines[J].Asle Transactions,1980,23(1):1-22.
[3]赖师墨.控制航空发动机运转间隙的热喷涂封严涂层[J].航空制造技术,1995(S1):53-55.
[4]Borel M 0,Nicoll A R,Schlapfer H W,et al.The Wear Mechanisms Occurring in Abradable Seals of Gas Turbines[J].Surface and Coatings Technology,1989,39-40,Part 1(0):117-126.
[5]Ghasripoor F,Schmid R,Dorfman M,et al.A Review of Clearance Control Wear Mechanisms for Low Temperature Aluminium Silicon Alloys[C]//Proceeding of the 15th Internation on Thermal Spray Conference.1988:139-144.
[6]Bounazef M,S Guessasma,B Ait Saadi.The Wear,Deterioration and Transformation Phenomena of Abradable Coating BN-SiAl-Bounding Organic Element,Caused by the Friction between the Blades and the Turbine Casing[J].Materials Letters,2004,58(27-28):3375-3380.
[7]薛伟海,高禊洋,张佳平,等.高速刮擦下Ti_6Al_4V叶片与NiAl-BN涂层的磨损行为[J].热喷涂技术,2014,6(3):29-35.
[8]张海存,张彬,李静,等.航空发动机封严涂层试验机控制测量研究[C]//2014航空试验测试技术学术交流会论文集.北京:航空工业出版社,2014:715-720.
[9]张佳平,蔡鑫,张艺馨,等.航空发动机常用热喷涂涂层金相制样关键技术[C]//探索创新交流——第六届中国航空学会青年科技论坛文集(上册).2015.
[10]薛伟海,高禊洋,段德莉,等.刮擦线速度对TC,叶片与Ni-G封严涂层磨损行为的影响[J].摩擦学学报,2013,6(3):31-37.
[2]Ludwig L P,Bill R C.Gas Path Sealing in Turbine Engines[J].Asle Transactions,1980,23(1):1-22.
[3]赖师墨.控制航空发动机运转间隙的热喷涂封严涂层[J].航空制造技术,1995(S1):53-55.
[4]Borel M 0,Nicoll A R,Schlapfer H W,et al.The Wear Mechanisms Occurring in Abradable Seals of Gas Turbines[J].Surface and Coatings Technology,1989,39-40,Part 1(0):117-126.
[5]Ghasripoor F,Schmid R,Dorfman M,et al.A Review of Clearance Control Wear Mechanisms for Low Temperature Aluminium Silicon Alloys[C]//Proceeding of the 15th Internation on Thermal Spray Conference.1988:139-144.
[6]Bounazef M,S Guessasma,B Ait Saadi.The Wear,Deterioration and Transformation Phenomena of Abradable Coating BN-SiAl-Bounding Organic Element,Caused by the Friction between the Blades and the Turbine Casing[J].Materials Letters,2004,58(27-28):3375-3380.
[7]薛伟海,高禊洋,张佳平,等.高速刮擦下Ti_6Al_4V叶片与NiAl-BN涂层的磨损行为[J].热喷涂技术,2014,6(3):29-35.
[8]张海存,张彬,李静,等.航空发动机封严涂层试验机控制测量研究[C]//2014航空试验测试技术学术交流会论文集.北京:航空工业出版社,2014:715-720.
[9]张佳平,蔡鑫,张艺馨,等.航空发动机常用热喷涂涂层金相制样关键技术[C]//探索创新交流——第六届中国航空学会青年科技论坛文集(上册).2015.
[10]薛伟海,高禊洋,段德莉,等.刮擦线速度对TC,叶片与Ni-G封严涂层磨损行为的影响[J].摩擦学学报,2013,6(3):31-37.