Bending stress of rolling element in elastic composite cylindrical roller bearing

A new structure design method of elastic composite cylindrical roller bearing is proposed, in which PTFE is embedded into a hollow cylindrical rolling element, according to the principle of creative combinations and through innovation research on cylindrical roller bearing structure. In order to systematically investigate the inner wall bending stress of the rolling element in elastic composite cylindrical roller bearing, finite element analysis on different elastic composite cylindrical rolling elements was conducted. The results show that, the bending stress of the elastic composite cylindrical rolling increases along with the increase of hollowness with the same filling material. The bending stress of the elastic composite cylindrical rolling element decreases along with the increase of the elasticity modulus of the material under the same physical dimension. Under the same load, on hollow cylindrical rolling element, the maximum bending-tensile stress values of the elastic composite cylindrical rolling element after material filling at 0° and 180° are 8.2% and 9.5%, respectively, lower than those of the deep cavity hollow cylindrical rolling element. In addition, the maximum bending-compressive stress value at 90° is decreased by 6.1%.     

具有弯拱度羽毛片的特性及其应用

主要研究具有弯拱度羽毛片的特性以及建立其转动惯量求解数学模型,通过测量羽毛片的羽毛叶和羽毛杆等相关数据得到了羽毛片质量分布与长度对应关系图.然后考虑羽毛片的弯拱度对其转动惯量的影响,并给出不同弯拱度类型时对应羽毛片质量分布图,从而得到了具有弯拱度的羽毛片转动惯量计算公式.最后根据转动惯量平行轴定理得到了以羽毛球对称中心点为坐标系的各转动轴的羽毛片转动惯量.仿真结果也进一步说明了不同类型弯拱度变化对羽毛片转动惯量的影响.对具有弯拱度羽毛片特性的研究,具有一定的实用意义.     

下坂地水利工程沥青混凝土心墙坝工作性态分析

以新疆下坂地水利枢纽工程中沥青混凝土心墙坝的设计、施工及监测成果为例,对施工期沥青混凝土心墙变形和温度安全监测资料进行了分析,并对下游坝体内部变形的安全监测资料也进行了较详细的分析探讨.结果表明下坂地水利枢纽工程沥青混凝土心墙砂砾石堆石坝的工程质量及结构的稳定安全可靠.此结果可为相关工程提供借鉴.     

千枚岩隧道动态变形及其控制

通过千枚岩隧道实际施工的分析,阐述了隧道动态变形,变形控制施工方式以及关键施工工序,探讨了相关技术在隧道管理中的重要性。     

An index for deformation controllability of small-volume materials

Mechanical tests on small-volume materials show that in addition to the usual attributes of strength and ductility,the controllability of deformation would be crucial for the purpose of precise plastic shaping.In our present work,a"mechanical controllability index"(MCI)has been proposed to assess the controllability of mechanical deformation quantitatively.The index allows quantitative evaluation of the relative fraction of the controllable plastic strain out of the total strain.MCI=0 means completely uncontrollable plastic deformation,MCI=∞means perfectly controllable plastic shaping.The application of the index is demonstrated here by comparing two example cases:0.273 to 0.429 for single crystal Al nanopillars that exhibit obvious strain bursts,versus 3.17 to 4.2 for polycrystalline Al nanopillars of similar size for which the stress-strain curve is smoother.     

Deformation bands in fully pearlitic steel during wire drawing

The deformation of fully pearlitic steels during wire drawing has been investigated for both longitudinal section and transverse section by back-scattered electron imaging(BSEI),electron back-scattered diffraction(EBSD),and transmission electron microscope(TEM).The results show that a large number of deformation bands(DBs)composed of a mixture of kink-like bands and shear-like bands were observed both in the longitudinal section and the traverse section of the drawn wires.The formation of such bands involves two aspects:heterogeneous deformation in the scale of pearlite colonies and instability of ferrite-cementite interfaces due to stress concentration during wire drawing.The development of such bands in fully pearlitic steels dominates the formation of metallographic texture,reduces the pearlite interlamellar spacing and promotes the development of<110>fiber crystalline texture of ferrite matrix during wire drawing.     

Sputtered Si-containing low-friction carbon coatings for elevated temperatures

This work presents a tribological study on three sputtered amorphous carbon-based coatings containing Si and Cr (a-C, a-C:Cr and a-C:Si). Molecular dynamics simulations predict tetrahedral bonds between C and Si in the a-C matrix. Ball-on-disk-tests against Al₂O₃ carried out at room temperature revealed a coefficient of friction of 0.08–0.1 for all films. Between 250 and 325 °C, Si decreases the COF and wear rate to $<0.05$ and $<5\times {10}^{-17}{\mathrm{m}}^3/\mathrm{N}\times \mathrm{laps}$, respectively. The a-C reference shows a COF of 0.15±0.05 and a wear rate of $1\times {10}^{-16}{\mathrm{m}}^3/\mathrm{N}\times \mathrm{laps}$, whereas the a-C:Cr film failed. The improved tribological performance of a-C:Si expands its application temperature to 450 °C and is most probably related to formation of Si-compounds on the film surface, as evidenced by X-ray photoelectron spectroscopy.     

高温高应变率下AM60B镁合金力学性能及失效行为

为了研究镁合金在高温、高应变速率下的变形行为及失效机制,采用分离式Hopkinson压杆在应变速率为1 600~4 500 s^-1、温度为27~150 ℃范围内,对真空压铸AM60B镁合金进行了动态压缩实验,并采用金相显微镜和扫描电子显微镜对压缩后的组织进行了观察.结果表明:在所测试的应变范围内,随着应变率的提高,应力-应变曲线均呈现上升趋势,且最大应变也随之增加,表现出正应变率强化效应.在150 ℃时真空压铸AM60B镁合金变形能力最好; 50 ℃时断裂强度最高.真空压铸AM60B镁合金在高温及高应变率下的断裂方式为以解理断裂为主并伴有韧性断裂的混合断裂方式.当变形温度低于150 ℃时,真空压铸AM60B镁合金在高应变率压缩下的变形机制主要是滑移.     

近场空爆载荷作用下船体板变形估算方法

鉴于目前我国舰船空中爆炸结构响应试验数据的匮乏以及对复杂结构采用理论求得解析解的困难,对船体板结构在空中近场爆炸载荷作用下的破坏估算方法进行研究.根据爆轰波理论及气体膨胀理论计算出空中近场爆炸载荷的形式及其正压作用时间,应用应力波及塑性动力学理论推导船体板结构的变形,得到不同空爆工况下船体板的破口大小及挠度.通过算例进行验证,计算结果与经验值良好吻合.所推导的估算方法应用于舰船结构在空中近场爆炸冲击波作用下产生的毁伤能够满足工程计算精度要求,可作为舰船防护结构的设计依据.     

路堤下盖板涵的竖向土压力分布

由于盖板在填土压力作用下发生挠曲变形,针对盖板涵对竖向土压力分布的影响,推导了盖板涵竖向土压力分布计算公式.假设盖板发生弹性挠曲变形,填土服从Winkler弹性地基条件,对盖板上修正的Marston填土涵洞竖向土压力分布进行了分析.结果表明,该修正公式考虑了盖板涵内外土柱差异沉降的应力集中效应,可计算由于盖板挠曲变形而引起的土压力重分布.通过对鹤大高速公路某盖板涵进行现场测试以及有限元数值模拟分析,结果显示盖板涵土压力的分布特点与本文理论分析相一致,且理论公式计算结果值与现场实测值吻合较好.