强化层 meaning in English
strengthening layer
Examples
- Wear resistance of q235 steel surface mo - cr alloy layer by double glow discharge technology
235钢表面双层辉光离子强化层摩擦磨损性能 - The nanometer silicon dioxide ’ s principle is “ micro rolling bearing " effect , and nanometer teflon is due to the film in a surface which has low shear strength and high compressive strength , the nano calcium carbonate is due to the effect cooperate with " micro rolling bearing " effect , sediment film and effect of intensify layer in the surface
其中纳米二氧化硅的减摩抗磨机理是“微滚动轴承”效应,纳米聚四氟乙烯是由于在摩擦副表面形成一层低剪切强度和高抗压强度的沉积膜,而纳米碳酸钙和稀土复合微粒是“微滚动轴承”效应、沉积膜作用和表面强化层作用的协同作用。 - It shows the nanometer particles have automation to make the friction surface in a comparatively even state . 4 ) through tribology chemistry function , the nanometer cacoj and cao particles form a deposited film on the wear scar ' s surface or strengthen the surface through a small amount of metal ca ' s diffusion to improve the friction surface ' s a
（ 4 ）纳米碳酸钙和纳米氧化钙粒子通过摩擦过程中的摩擦化学作用在磨斑表面上形成了沉积膜，少量金属钙通过扩散作用渗透到钢基体表面，形成表面强化层，提高了表面的耐磨性。 - The method employs resin as the base material and fiberglass as reinforcement in forming barrel tank via winding ; resin is selected according to the intended liquid property . the barrel interior is built with anticorrosion coating and additional reinforcement ; the former is capable of withstanding any chemical , whereas the latter is to mend barrel strength
以树脂为基材，以玻璃为补强材，以缠丝成型法缠绕成桶槽，依贮装的液体特性采用不同的树脂，桶槽内部分耐蚀层及强化层，耐蚀可抵抗化学药品，强化层用来补强桶槽强度。 - In this thesis , the strain - hardening model of contact surface layer , the numerical theories and computational methods for shakedown analyses of contact body are systematically studied and applied to the aero - gear . the mentality is that the effects of the surface hardening and contact fatigue on contact surface layer under cycle contact loading are investigated by using shakedown analysis methods considering in a quantitative way the details of stress - inelastic strain responses , residual stress and residual strain computations
在国家“航空基金” 、 “总装预研基金”等课题的资助下，本文以接触体安定分析与接触表面层疲劳裂纹萌生寿命预测一般算法研究为手段，深入、系统研究了接触体安定分析的数值理论和计算方法，全面研究了影响航空齿轮表面强化层失效的原因并提出了齿轮表面强化层裂纹萌生寿命的预测方法。