摘要
针对新机种对固体膜润滑剂的需求,研制了两种固体膜润滑剂-HR-7201和HR-7101。润滑剂采用国产原材料,具有摩擦系数低,耐高低温及耐介质等优良性能,使用温度HR-7201为-60~300℃,HR-7101为-60~200℃,短期可到250℃。已通过飞机典型零部件试验及长期试车考核,并在飞机上应用。
Two kinds of solid film lubricant,HR-7201 and HR-7101,were prepared to fit new aircraft.Solid film lubricant was made by home-made materials.Different materials including resin,solid lubricant and mixed solvent were selected,the compatibility among all components was studied.The prepared solid film lubricant has such properties: low friction coefficient,heat and cold resistance,fluids resistance,etc.HR-7201 can be used where temperature range from-60℃ to +300℃,and then HR-7101 can be used at temperature ran...
出处
《航空材料学报》
EI
CAS
CSCD
2006年第3期345-346,共2页
Journal of Aeronautical Materials
关键词
环氧树脂
固体润滑剂
固体膜润滑剂
二硫化钼
摩擦系数
飞机
epoxy resin
solid lubricant
solid film lubricant
molybdenum disulfide
friction coefficient
aircraft
