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高压高剪切率下润滑剂剪切弹性模量的确定

王燕霜 杨伯原 王黎钦

王燕霜, 杨伯原, 王黎钦. 高压高剪切率下润滑剂剪切弹性模量的确定[J]. 航空动力学报, 2006, 21(1): 181-185.
引用本文: 王燕霜, 杨伯原, 王黎钦. 高压高剪切率下润滑剂剪切弹性模量的确定[J]. 航空动力学报, 2006, 21(1): 181-185.
WANG Yan-shuang, YANG Bo-yuan, WANG Li-qin. Determination of Lubricant Elastic Shear Modulus under Conditions of High Pressure and High Shear Rates[J]. Journal of Aerospace Power, 2006, 21(1): 181-185.
Citation: WANG Yan-shuang, YANG Bo-yuan, WANG Li-qin. Determination of Lubricant Elastic Shear Modulus under Conditions of High Pressure and High Shear Rates[J]. Journal of Aerospace Power, 2006, 21(1): 181-185.

高压高剪切率下润滑剂剪切弹性模量的确定

基金项目: 国家“十五”重大科技攻关项目(HK-2002-043/6);河南科技大学青年基金资助(2003QN05)

Determination of Lubricant Elastic Shear Modulus under Conditions of High Pressure and High Shear Rates

  • 摘要: 在自行研制的球盘式拖动力试验台上,测得了HKD-1型航空润滑油的拖动力;给出了高压高剪切率下滚子-润滑膜系统有效剪切弹性模量的计算公式;推导出了系统有效剪切弹性模量与润滑剂剪切弹性模量之间的关系式;以HKD-1型航空润滑油为例,计算了多种工况条件下系统有效剪切弹性模量及润滑剂本身的剪切弹性模量。结果表明:系统有效剪切弹性模量和润滑剂剪切弹性模量随压力的增大而增大,随入口油温和滚动速度的增大而减小;压力越大,入口油温和滚动速度越小,滚子的柔量对剪切变形的贡献越大。

     

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出版历程
  • 收稿日期:  2005-01-18
  • 修回日期:  2005-08-22
  • 刊出日期:  2006-02-28

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