In the search of new wear resistant coatings for applications such as cutting tools and turbine refurbishing, a wide range of coatings, belonging to emerging classes of materials, namely, nanocrystalline materials and nanolayered composites, have been produced and tested. These coatings were produced using an rf magnetron sputtering system and include monolithic nanocrystalline metals (Al,Ti,Cu), nanolaminated composites composed of alternating layers of metal/ceramic (Al/Al$sb2$O$sb3$, Ti/TiN) and metal/metal (Ti/Cu). The metal layer thickness in the as-sputtered films of Al/Al$sb2$O$sb3$ ranged from 70 to 500 nm, and 150 to 450 nm in Ti/TiN. The nonmetals (Al$sb2$O$sb3$,TiN) layer thicknesses ranged from 10 to 40 nm and total film thicknesses of 10-15 $mu$m. As-sputtered nanocrystalline aluminum films with an average grain size of 16.4 nm were isothermally annealed at 573 K to increase the grain size up to 98.0. nm. All materials were characterized and tested for their tribological properties. Friction and wear tests were performed under unlubricated sliding conditions using pin-on-disc type tribometer which was designed and constructed for measuring wear rates and coefficients of friction of thin films in air and in vacuum. The coefficient of friction of the materials tested against the stainless steel pin varied with the sliding distance. At the early stages of sliding the coefficient of friction rose to a peak, followed by a decrease to a steady-state value. The transition to the steady-state in the friction curve corresponded to a transition from severe wear to mild wear. In aluminum the value of the peak coefficient of friction decreased from $mmusb{p} = 1.4$ for a coarse grain size of $10sp6$nm to $mmusb{p} = 0.6$ for a grain size of 16.4 nm when tested under ambient conditions. The coefficient of friction of nanocrystalline aluminum showed a 30% increase when tested in vacuum $(10sp{-6}$ torr). Within the grain size range of 15-100 nm, the wear rates were found to be linearly dependent on the square root of the grain size $m(Wsb{s} = 8.5imes 10sp{-4} + (2.44 imes 10sp{-4}). Dsp{1/2}$ for severe wear and $m Wsb{m} = {-}1.9 imes 10sp{-4} + (5.1 imes 10sp{-5}). Dsp{1/2}$ for mild wear). The peak value of the coefficient of friction decreased about 70% in Al/Al$sb2$O$sb3$ (with 200 nm Al layer thickness) while a 60% improvement in the steady-state coefficient of friction was measured in Ti/TiN (with 150 nm Ti layer thickness) in comparison to the as-sputtered monolithic aluminum and titanium films, respectively. An increase in wear resistance with decreasing layer thickness was also observed (for example, $m Wsb{s} = 7.0 imes 10sp{-5} + (2.9 imes 10sp{-7}). lambdasp{0.5}sb{Ti}).$ Mechanical properties (hardness and elastic moduli) of the films were measured using an ultra-microindentation system. Hardness measurement of nanocrystalline aluminum revealed that within the grain size range 15-100 nm the hardness-grain size data obeys a Hall-Petch type relationship (i.e., $m H = 34 lbrack MPabrack + 0.21 lbrack MPacdot msp{0.5}brack Dsp{-0.5} lbrack msp{-0.5}brack).$ The hardness of Al/Al$sb2$O$sb3$ and Ti/TiN could also be described in the formalism of the Hall-Petch type indicating that ceramic layers inhibit slip transfer across metallic layers. (Abstract shortened by UMI.)Dept. of Mechanical, Automotive, and Materials Engineering. Paper copy at Leddy Library: Theses u26 Major Papers - Basement, West Bldg. / Call Number: Thesis1996 .F37. Source: Dissertation Abstracts International, Volume: 59-08, Section: B, page: 4384. Advisers: D. O. Northwood; A. T. Alpas. Thesis (Ph.D.)--University of Windsor (Canada), 1996.
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机译:在寻找用于诸如切削工具和涡轮机翻新之类的应用的新型耐磨涂层时,已经生产并测试了属于新兴材料类别(即纳米晶体材料和纳米层状复合材料)的各种涂层。这些涂层是使用射频磁控溅射系统生产的,包括单片纳米晶金属(Al,Ti,Cu),由金属/陶瓷交替层组成的纳米层压复合材料(Al / Al $ sb2 $ O $ sb3 $,Ti / TiN )和金属/金属(Ti / Cu)。 Al / Al $ sb2 $ O $ sb3 $的溅射膜中的金属层厚度在70/500 nm范围内,在Ti / TiN中为150-450 nm。非金属(Al $ sb2 $ O $ sb3 $,TiN)层的厚度为10至40 nm,总膜厚度为10-15μm。将平均晶粒尺寸为16.4 nm的溅射态纳米晶铝膜在573 K下等温退火,以将晶粒尺寸增加到98.0。纳米对所有材料进行表征并测试其摩擦学性能。使用销盘式摩擦计在未润滑的滑动条件下进行摩擦和磨损测试,该摩擦计的设计和制造用于测量空气和真空中薄膜的磨损率和摩擦系数。被测试材料相对于不锈钢销的摩擦系数随滑动距离而变化。在滑动的早期阶段,摩擦系数上升到峰值,然后下降到稳态值。从摩擦曲线到稳态的过渡对应于从严重磨损到轻度磨损的过渡。在铝中,峰值摩擦系数的值从$ 10 sp6 $ nm的粗晶粒的$ rm mu sb {p} = 1.4 $降低到$ rm mu sb {p} = 0.6 $在环境条件下测试时,晶粒尺寸为16.4 nm。纳米晶铝的摩擦系数在真空($ 10 sp {-6} $托)中测试时显示出30%的增加。在15-100 nm的晶粒尺寸范围内,发现磨损率与晶粒尺寸的平方根成线性关系 rm(W sb {s} = 8.5 乘以10 sp {-4} + (2.44 times 10 sp {-4})。 D sp {1/2} $用于严重磨损,$ rm W sb {m} = {-} 1.9 times 10 sp {-4} +(5.1×10 sp {-5} $。 D sp {1/2} $用于轻度磨损)。在Al / Al $ sb2 $ O $ sb3 $(Al层厚度为200 nm)中,摩擦系数的峰值降低了约70%,而在Ti中测得稳态摩擦系数提高了60% / TiN(Ti层厚度为150 nm),分别与溅射的整体式铝膜和钛膜相比。还观察到耐磨性随层厚度减小而增加(例如,$ rm W sb {s} = 7.0×10 sp {-5} +(2.9×10 sp {-7})。 lambda sp {0.5} sb {Ti})。$薄膜的机械性能(硬度和弹性模量)是使用超微压痕系统测量的。纳米晶铝的硬度测量表明,在15-100 nm的晶粒尺寸范围内,硬度-晶粒尺寸数据符合Hall-Petch类型关系(即,$ rm H = 34 lbrack MPa rbrack + 0.21 lbrack MPa cdot m sp {0.5} rbrack D sp {-0.5} lbrack m sp {-0.5} rbrack)。$ Al / Al $ sb2 $ O $ sb3 $和Ti / TiN也可以用霍尔-帕奇(Hall-Petch)类型的形式描述,表明陶瓷层抑制了跨越金属层的滑动转移。 (摘要由UMI缩短。)机械,汽车和材料工程系。莱迪图书馆的纸质副本:论文主要论文-西楼地下室。 /电话号码:Thesis1996 .F37。资料来源:国际论文摘要,第59卷,第B节,第4384页。 A. T. Alpas。论文(博士学位)-温莎大学(加拿大),1996。
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