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基于正交设计的直升机传动组件磨损影响因素可靠性试验技术研究 被引量:1

Research on the Wear Reliability Test Technique of the Transmission System Assembly Influential Factors of Helicopter based on Orthogonal Test Design
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摘要 以直升机传动系统组件为研究对象,采用正交设计,设计了一套新的磨损影响因素可靠性试验,通过极差分析法和方差分析法对试验数据进行处理分析,比较两者优劣,确定对直升机机械组件磨损的主、次要影响因素,以此证明该可靠性试验技术的实用性与合理性。 In this paper, with helicopter transmission system as its research object, adopted the orthogonal designing method to design a new test for determining the reliability of wear influential factors. To verify the practicability and reasonability of technology test, the test data were processed and analyzed using range analysis method and variance components method to compare the advanta- ges and disadvantages of the two and determine major and secondary influence factors for abrasion of helicopter mechanical components.
作者 刘松宇 沈亚斌 LIU Songyu SHEN Yabin(China Helicopter Research and Development Institute, Jingdezhen 333001, China)
出处 《直升机技术》 2017年第2期56-60,共5页 Helicopter Technique
关键词 正交设计 磨损影响因素 可靠性试验 orthogonal design influential factors reliability test
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  • 1北京大学数学力学系.正交设计[M].北京:石油化学工业出版社,1976..
  • 2Mikael Eriksson,Staffan Jacobson.Tribological surfaces of organic brake pads[J].Tribology International,2000,33:817-827.
  • 3Seong Jin Kim,Kwang Seok Kim,Ho Jang.Optimization of manufacturing parameters for a brake lining using Tagushi method[J].Journal of Materials Processing Technology,2003,136:202-208.
  • 4Luise Gudmand-Hфyer,Allan Bach,Georg T Nielsen,et al.Tribological properties of automotive disc brakes with solid lubricants[J].Wear,1999,232:168-175.
  • 5Ramousse S,Hфj J W,Sфrensen OT.Thermal characterization of brake pads[J].Journal of Thermal Analysis and Calorimetry,2001,64:933-943.
  • 6温诗铸 黄平.摩擦学原理[M].北京:清华大学出版社,2001..
  • 7苏堤,李度成,汪琳,王坪龙.不同温度下半金属摩擦材料的摩擦磨损性能研究[J].摩擦学学报,2000,20(5):383-385. 被引量:11

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