孙东,王海新,蒲吉斌,刘金玲,曹娜娜,郭武明.碳基薄膜在航空轴承乏油问题中的应用研究[J].表面技术,2019,48(8):218-224.
SUN Dong,WANG Hai-xin,PU Ji-bin,LIU Jin-ling,CAO Na-na,GUO Wu-ming.Application Research of Carbon-based Films in Aeroengine Bearings under Oil Starvation Condition[J].Surface Technology,2019,48(8):218-224
碳基薄膜在航空轴承乏油问题中的应用研究
Application Research of Carbon-based Films in Aeroengine Bearings under Oil Starvation Condition
投稿时间:2018-11-29  修订日期:2019-08-20
DOI:10.16490/j.cnki.issn.1001-3660.2019.08.029
中文关键词:  GLC薄膜  DLC薄膜  磁控溅射  摩擦学  航空轴承  乏油工况
英文关键词:GLC films  DLC films  magnetron sputtering  tribology  aeroengine bearing  oil starvation condition
基金项目:浙江省自然科学基金(LZ17E050004)
作者单位
孙东 1.中国航发哈尔滨轴承有限公司 研发中心,哈尔滨 150000 
王海新 2.中国科学院宁波材料技术与工程研究所 中国科学院海洋新材料与应用技术重点实验室 浙江省海洋材料与防护技术重点实验室,浙江 宁波 315201 
蒲吉斌 2.中国科学院宁波材料技术与工程研究所 中国科学院海洋新材料与应用技术重点实验室 浙江省海洋材料与防护技术重点实验室,浙江 宁波 315201 
刘金玲 1.中国航发哈尔滨轴承有限公司 研发中心,哈尔滨 150000 
曹娜娜 1.中国航发哈尔滨轴承有限公司 研发中心,哈尔滨 150000 
郭武明 2.中国科学院宁波材料技术与工程研究所 中国科学院海洋新材料与应用技术重点实验室 浙江省海洋材料与防护技术重点实验室,浙江 宁波 315201 
AuthorInstitution
SUN Dong 1.R&D Center, AECC Harbin Bearing Co., Ltd, Harbin 150000, China 
WANG Hai-xin 2.Key Laboratory of Marine Materials and Related Technologies, Key Laboratory of Marine Materials and Protective Technologies of Zhejiang, Ningbo Institute of Materials Technology and Engineering, Chinese Academy of Sciences, Ningbo 315201, China 
PU Ji-bin 2.Key Laboratory of Marine Materials and Related Technologies, Key Laboratory of Marine Materials and Protective Technologies of Zhejiang, Ningbo Institute of Materials Technology and Engineering, Chinese Academy of Sciences, Ningbo 315201, China 
LIU Jin-ling 1.R&D Center, AECC Harbin Bearing Co., Ltd, Harbin 150000, China 
CAO Na-na 1.R&D Center, AECC Harbin Bearing Co., Ltd, Harbin 150000, China 
GUO Wu-ming 2.Key Laboratory of Marine Materials and Related Technologies, Key Laboratory of Marine Materials and Protective Technologies of Zhejiang, Ningbo Institute of Materials Technology and Engineering, Chinese Academy of Sciences, Ningbo 315201, China 
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中文摘要:
      目的 研究乏油工况下GLC和DLC两种碳膜在航空轴承上的应用。方法通过磁控溅射技术在单晶硅片P(100)、轴承钢样块和轴承套圈表面分别制备了GLC和DLC两种薄膜。利用扫描电镜(SEM)、拉曼光谱对薄膜的截面和磨痕形貌及结构进行了分析。利用纳米压痕仪、摩擦磨损试验机等对薄膜的力学性能和摩擦学性能进行了研究。利用轴承试验机对镀两种膜的轴承进行了对比研究。结果 GLC和DLC两种碳基薄膜均结构致密,GLC薄膜含有更多的sp2,DLC薄膜含有更多的sp3;两种薄膜硬度分别达到18.2 GPa和22.2 GPa,弹性模量分别达到230.2 GPa和260.8 GPa,干摩擦条件下,薄膜摩擦系数分别低至0.11和0.21。镀膜轴承在运转0~10 h时,温升无明显差异;10~30 h过程中,镀GLC薄膜轴承温升约为40~45 ℃,而镀DLC薄膜轴承温升约为50~55 ℃。运转后,轴承滚子上出现转移膜,镀GLC薄膜的轴承磨损比镀DLC薄膜的轴承严重。结论 在乏油工况下,DLC薄膜具有更加优异的环境适应性。
英文摘要:
      The work aims to study the application of GLC and DLC carbon films in aeroengine bearing under oil starvation condition. GLC and DLC thin films were prepared on the surface of single crystal silicon P(100), bearing steel and bearing ring by magnetron sputtering technique. The cross-section, wear morphology and structure of the films were analyzed by SEM and Raman. The mechanical properties and tribological properties of the films were studied by nano-indentation instrument and friction and wear tester. The bearing test machine was used to compare these two film-coated bearings. The structure of the GLC and DLC films were both compact. The GLC films contained more sp2, but DLC films contained more sp3. The hardness and elastic modulus of the two films were up to 18.2 GPa, 22.2 GPa and 230.2 GPa, 260.8 GPa respectively. Under dry friction conditions, the friction coefficient was as low as 0.11 and 0.21, respectively. There was no significant difference in the temperature rise of the coated bearings between 0 to 10 h. The temperature rise of the GLC films bearing was about 40~45 ℃ during 10~30 h, while the temperature rise of the DLC films bearing was about 50~55 ℃. The transfer film appeared on the bearing rollers and the bearing wear of GLC films was more serious than that of DLC films after the operation. The DLC films have better environmental adaptability under oil starvation condition.
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