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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。

This paper first analyses the stress acting on the cable by means of tiny segment analytical methods, establishes cable's stress equation, and finds out the relation between the tethered aerostat's position and its stress acting by cable; then, based on the momentum and moment of momentum theorem, the longitudinal nonlinear dynamic equation is established; Finally a numerical simulation of dynamic responses of the balloon and cable to gust are carried out.

本文首先通过微段分析法对缆绳进行受力分析,建立缆绳的受力方程,找出了系留气球在空中的位置同系留气球所受缆绳拉力的关系;然后根据动量和动量矩定理建立了球体的纵向非线性运动方程;最后通过数值仿真计算,对系留气球的纵向动态响应特性进行了分析。

In order to further understand the effect of deviation angle on the vertical resolution of the compensated neutron log, Monte Carlo simulation method was applied to study the vertical geometrical factors and formation sensitivity under different deviation angle conditions, furthermore the responses of the tool were simulated in laminations.

为了进一步认识井斜角对补偿中子测井纵向分辨率的影响,利用蒙特卡罗模拟方法,分析了在不同井斜角情况下测井仪器的纵向几何因子和地层灵敏度,并模拟了在薄地层中的仪器响应。

The numerical results are analyzed based on the field synergy principle to explain the inherent mechanism of heat transfer enhancement by longitudinal vortex, namely second flow generated by the vortex generators causes the reduction of the intersection angle between the velocity and fluid temperature gradient.

结果发现纵向涡强化管-翅表面换热的内在机理可以用场协同原理进行解释,即纵向涡发生器使全场速度和温度梯度之间的平均夹角减小。

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。

In this paper,a study is given to the relationship between vacuum arc current and axial magnetic field keeping the vacuum arc diffuse,a formula of the relationship is deduced.

本文研究了真空电弧与使其保持扩散型的纵向磁场间的关系,并得出了电弧电流与纵向磁场间的关系式。

The instructive conclusion was: 1 under the vertical loading, the shear-lag effect was produced badly, more severer under concentrated loading than under uniform loading .2 the longitudinal bending deformation of the beam flange was true of the imitating plane assumption of deformation . 3 the width length ratio was confirmed as the first factor working on the shear-lag effect among all the geometric parameters;4 the shear-lag coefficient of simple-supported box-girder was severer than the continuous box-girder, the shear-lag effect in the inner supported section of continuous beam was much more severer, we need paying more attention for it in designing. 5 the non-liner characteristics of material deformation have littlie influence on shear-lag effect in BGCW. 6 the experiential calculating formulation and calculating diagram for the effective flange width was raised with the only factor of the width-span ratio., but the primary location of axis of bending moments should not be changed while calculating the inertial moment .

研究认为:1室内模型试验和空间有限元分析结果均表明波形钢腹板组合箱梁在竖向荷载作用下,翼板出现了典型的纵向应力剪滞效应。2在竖向荷载作用下,截面高度上各点纵向正应变分布认为可符合"拟平截面假定",以此作为波形钢腹板组合箱梁抗弯计算的基本假定。3箱梁宽跨比是影响波形钢腹板组合箱梁翼板剪滞效应的主要因素。4连续波形钢腹板组合箱梁的翼板剪滞系数大于简支梁,且连续箱梁内支点截面翼板剪滞效应相当严重,对此需十分重视。5当混凝土翼板受力由弹性阶段进入弹塑性阶段时,材料的非线性特性对翼板的剪滞效应影响甚微。6提出了根据组合箱梁的宽跨比参数来计算翼板有效宽度比的经验公式和计算图表,但箱梁截面抗弯惯性矩的计算不应改变原先的截面中和轴位置。

Broken or burst apart longitudinally.

纵向破碎或者突然纵向破裂。

The support device (10) having a longitudinally extensive strip having a plurality of sets of transverse corrugations (12) located at successive longitudinal locations along the strip.

该支撑装置(10)具有纵向延伸带,该纵向延伸带具有多个横向皱折组(12),该多个横向皱折组位于沿带的连续纵向位置上。

Numerical control system through research, analysis of the mechanical part of the X52K vertical milling machine, feed servo system design and calculation, and further to the electrical control system for NC transformation, the use of computers to vertical, horizontal feed system for open-loop control, demand In the vertical and horizontal with straight lines and circular interpolation function, and the vertical, horizontal pulses are equivalent 0.01mm / pulse, control X to, Y coordinates of the two.

经过对数控体系的研讨,阐发了X52K立式铣床的机器部门、进给伺服体系等的计划盘算,进一步对电器控制体系举行数控改革,使用微机对纵向、横向进给体系举行开环控制,要求在纵向和横向具有直线和圆弧插补功效,且纵向、横向的脉冲当量均为0.01mm/脉冲,控制X向、Y向两个坐标。

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