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航空发动机磨粒荷电特性研究

Aeroengine Grits Charged Characteristics Research
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摘要 大多数机械系统(航空发动机)失效期的磨粒尺寸多在20 μm^200 μm之间,在这一尺寸范围内研究颗粒的荷电特性对磨粒静电监测技术具有特殊意义。本文采用直接测量的方法获得微米级颗粒不同摩擦时间后产生的静电,实验选用颗粒的材料为金属铝粉末,平均粒径为50 μm、200 μm、3 mm。研究结果表明:铝颗粒的荷电量与振动荷电时间在一定时间范围内存在线性关系,在相同的摩擦振动时间下,颗粒的直径越大,荷电量越多。 Abrasive particle size of most mechanical systems (aeroengine) failure issue is between 20 mi-crons to 200 microns. The study of the charge characteristics of particles in this area has special significance to the technology of abrasive electrostatic monitoring. This paper adopts direct measurement method to obtain the generated static electricity after different friction time of micron particles. The materials used in the experiment are powder of aluminum. The average particle size is 50 um, 200 um and 3 mm. The results show that there is a linear relationship between the charge of aluminum particles and the time of the vibratory load. The greater the diameter of the particle, the more the charge.
机构地区 南昌航空大学
出处 《国际航空航天科学》 2017年第4期182-188,共7页 Journal of Aerospace Science and Technology
基金 国家自然科学基金(51465047) 航空科学基金(2014ZD56009) 江西省研究生创新专项基金(YC2015-S327)。
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  • 1陈奎,杨瑞成,成生伟.蒙脱土填充聚丙烯复合材料的摩擦磨损行为研究[J].摩擦学学报,2006,26(6):561-565. 被引量:7
  • 2王运赣.快速成型技术[M].上海:华中理工大学出版社,1999.251-257.
  • 3Rossner M,Singer H.Measurement of micrometer parti-cles by means of induced charges.IEEE Industry Applica-tions Society Annual Meeting.1989,2:2233-2238.
  • 4Zmarzly D,Boczar T.Measurements of distribution of streaming electrification current inside pipe.IEEE Trans-actions on Dielectrics and Electrical Insulation,2009,16(6):1681-1685.
  • 5Law S E.Electrostatic induction instrumentation for tracking and charge measurement of airborne agricultural particulates.Transactions of the ASAE,1975,18(1):40-45.
  • 6Diaz A F,Felix-Navarro R M.A semi-quantitative tribo-electric series for polymeric materials:the influence of chemical structure and properties.Journal of Electrostat-ics,2004,62(4):277-290.
  • 7李耀华.航空发动机气路静电监测技术研究.南京:南京航空航天大学民航学院,2010.
  • 8Muir D,Howe B.In-line oil debris monitor(ODM)for the advanced tactical fighter engine.SAE Paper961308,1996.
  • 9Hughes I,Muir D.On-line oil debris monitor for aircraft engines.JOAP Conference.1994.
  • 10Byington C S,Schalcosky D C.Advances in real time oil analysis.Practicing Oil Analysis Magazine,2000,11(2):28-34.

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