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In addition, some experience formulas for them are regressed. The third chapter establishes a unified S-N curve equation to calculate multi-axial fatigue ultimate strength of concrete considering both the effect of confinement and minimum/maximum stress ratio, based on the triaxial fatigue test data in this paper and the test results under uniaxial and biaxial fatigue loading in previous literatures. Moreover, the consistency of calculating condition fatigue ultimate strength with fatigue life distribution and initial ultimate strength distribution is analyzed.

第二章简要地介绍了本文三轴疲劳试验装置,进行了两向等侧压约束下混凝土立方体试件三轴受压等幅和变幅疲劳试验,分析了三轴受压疲劳破坏机理,给出了相应的疲劳破坏试验判断标准;得到了混凝土在两向侧压约束下单级和多级受压疲劳的变形发展规律,包括最大纵向应变、残余应变、最大纵向应变率和疲劳变形模量等随循环次数的发展规律以及疲劳损伤的演变规律,并给出了相应的经验公式。

It comprises an in-put shaft hinged to its yoke through one axis, and an out-put shaft also hinged to its yoke through another axis, and these two yokes (13) were combined together by only one axis position, perpendicular to that two yoke axes like a cross, so that this combined axis will bend just like the angle bisector of that two shafts to maintain its constant velocity by a few methods, firstly, by using a section of gear teeth mesh at both ends of the shafts' teeth were so polished so that it can turn longitudinally as usual gear, and also sideways, to provide a larger solid angle of turning from ordinary 45 degrees into 60 or even more.

它包括输入轴,其通过一根轴铰链连接于叉形支架,和输出轴,其通过另一根轴也铰链连接于其叉形支架。并且这两个叉形支架(13)只需用一根相对垂直铰链轴相连而组合在一起,使得这种组合的轴总能形成这两个轴的角平分线,以通过少数几种方法保持其恒速,首先,通过用啮合在轴的两端的一段齿轮齿抛光为以能够像普通齿轮一样纵向转动,并且还能够侧向转动,以提供较大的转向立体角,从通常的45度变成60度或更大。

A rotor structure for a rotating wing aircraft having substantially rigid rotor head means and rotor blades or wing means arranged in at least one pair, comprising blade angle bearing means (10, 12, 14, 16) for each rotor blade means, tension bar means (6,8) operatively interconnecting the rotor blade means of a pair which blade means are arranged diametrically opposite each other, said tension bar means having a high bending resistance, whereby transmission of bending moments from the rotor blades to the rotor head means is substantially prevented, each of said blade angle bearing means comprising a structure angularly movable in the wing flap direction and in the wing lead-lag direction, at least one of said blade angle bearing means of a pair comprising means permitting an axial motion of the respective tension bar means supported in said blade angle bearing means, and wherein said blade angle bearing means (10, 12, 14, 16) operatively support said tension bar means (6, 8) on said rotor head means (4) for pitch angle rotation of said tension bar means relative to said rotor head means (4), said rotor structure further comprising means (24) securing said rotor blade means (18) to said tension bar means (6, 8) in a manner rigid against rotation of the blade means about the longitudinal blade axis whereby the securing means prevent flapping, drag and lagging movements of the tension bar means, said tension bar means being constructed as torsion bars which are elastic relative to torsion about said longitudinal blade axis.

1转子结构为旋转翼飞机,有大幅刚性转子头部的手段和转子叶片或机翼的手段安排中至少有一对,组成的叶片角度轴承手段( 10 , 12 , 14 , 16 )为每个转子叶片的手段,拉杆手段( 6,8 )手术互连转子叶片的手段,其中一对刀片的手段都是安排截然相反的对方说,拉杆手段,有一个高弯曲阻力,即传输弯矩从转子叶片向转子头的意思是,大幅防患于未然,每个叶片角度说,轴承的手段组成的一个结构angularly动产在机翼上皮瓣的方向和在机翼导致滞后的方向,至少有一个叶片角度说,轴承是指一对组成的手段,允许轴向的议案,分别紧张酒吧手段,支持在叶片角度说,轴承的手段,其中,叶片角度说,轴承的手段( 10 , 12 , 14 , 16 )手术的支持表示拉杆的手段( 6 , 8 )就表示,转子头部的手段( 4 )为俯仰角轮换说拉杆手段相对说,转子头部的手段( 4 )表示,转子结构进一步组成的手段,( 24 )说,确保转子叶片的手段( 18 )表示,拉杆手段( 6 , 8 )在一个僵化的方式对旋转的叶片即是说,约纵向叶片轴,即确保手段防止扑,拖曳和落后变动的紧张局势,酒吧的手段,说拉杆手段,正在建造的,作为扭杆这是弹性相对扭转约说,纵向叶片轴。

The transverse dynamic stiffness curve of a ship front shaft bracket ,and the transverse and longitudinal dynamic stiffness cruves of a back shaft bracket are obtained by means of experiment measurements.

采用实验方法对某舰尾轴架进行动刚度测量,得到了前尾轴架的横向动刚度曲线,后尾轴架的横向和纵向动刚度曲线;分析尾轴架的动刚度曲线,可得到尾轴架结构的固有频率。

The transverse dynamic stiffness curve of a ship front shaft bracket,and the transverse and longitudinal dynamic stiffness cruves of a back shaft bracket are obtained by means of experiment measurements.Analyses of these curves make the natural frequencies of the shaft brackets available.

采用实验方法对某舰尾轴架进行动刚度测量,得到了前尾轴架的横向动刚度曲线,后尾轴架的横向和纵向动刚度曲线;分析尾轴架的动刚度曲线,可得到尾轴架结构的固有频率。

When the flexible drawgear is used, the peak values both of the dynamics longitudinal force and of its instantaneous PSD have decreased largely, and the distribution status of the instantaneous PSD along both the time axles and the frequency axles have been improved. So the working stability of the tractor-trailer combinations braking process would been improved when the optimized flexible drawgear was used.

仿真分析和试验结果均表明,使用柔性牵引装置后,牵引架动态纵向力峰值及其瞬时功率谱的峰值有了大幅度的降低,动态纵向力瞬时功率谱密度沿时间轴和频率轴的能量分布得到了改善,这说明使用柔性牵引装置后有利于提高挂接车辆制动工况的工作稳定性。

Simulation results also show that saddle-shaped distributed AMF can more effectively inhibit constriction of vacuum arc.

对于小电流扩散态真空电弧,重点仿真分析不同电弧电流与不同纵向磁场对其关键特性的影响,部分仿真结果进行了实验验证;对离子处于超音速流动的收缩态真空电弧的仿真表明,真空电弧的磁收缩主要是由于霍尔效应引起的,离子温度和电子温度沿轴向先增大后减小,马鞍形分布的纵向磁场能够更有效地抑制真空电弧的收缩,而且阴极斑点分布对真空电弧特性也有着显著的影响;对离子处于亚音速流动状态的大电流真空电弧的仿真表明,部分等离子体不能到达阳极而损失,马鞍形分布的纵向磁场能够更有效地抑制电弧等离子体的损失,同时能使阳极电流密度和能流密度的分布更加均匀。

The time to peak systolic longitudinal strain and the time to peak systolic radial strain were derived from the LV apical views , and to peak systolic circumferential strain was derived from the parasternal short axis. The standard deviation for time to peak longitudinal、circumferential and radial strain in the 18 segments (LS-SD18、CS-SD18、RS-SD18) and the maximal temporal difference of any two segments(LS-dif、CS-dif、RS-dif)were calculated as a strain-derived dyssynchrony index.

方法16例慢性心衰患者,获取心尖长轴观测量各节段收缩期纵向应变达峰时间,径向应变达峰时间,胸骨旁短轴观测环向应变达峰时间,计算CRT术后1个月、术后3个月18节段纵向、环向、径向应变达峰时间标准差(LS-SD18、CS-SD18、RS-SD18)、左室各节段收缩期纵向、环向、径向应变达峰时间最大差值(LS-dif、CS-dif、RS-dif)作为应变非同步指标。

A non-singular single integral mathematical model is adopted to calculate the external intermittent and alternative longitudinal magnetic field acquired by single axisymmetrical and cylindrical hollow coil t which is coaxial to electrode and excitated by a revisable pulsed current of square wave t in austenitic stainless steel GTA welding.

针对奥氏体不锈钢外加纵向磁场的气体保护钨极电弧焊接时,与电极同轴的单个轴对称空心圆柱线圈在双向脉冲矩形励磁电流作用下产生的间歇交变纵向磁场,采用无暇点单积分磁场的数学模型,对*TAW焊接外加间歇交变纵向磁场进行了数值计算,该方法具有模型简单、计算速度快和精度高等优点并讨论了该间隙交变纵向磁场的分布、磁场的均匀性及其纵向分量与径向分量的比率等规律及其对焊接行为的影响,认为横磁分量将削弱GTAW外加纵向磁场的有利作用,影响磁控电弧的焊接质量

In order to function as a single compression member, the C-sections should be connected at a close enough spacing to prevent buckling of individual C-sections about their own axes parallel to the web at a load equal to or smaller than the buckling load of the entire section. For this reason, Sec.

为了起到单个抗压构件的作用,两段U型钢要贴得足够紧,以避免各段U型钢对平行于筋的自身轴的纵向弯曲——它是自身轴的荷载等于或小于整个断面的临界纵向荷载而造成的。

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