力矩的平衡的英文

• equilibrium of moments

• "力矩"英文翻译    force moment; moment; moment ...
• "的"英文翻译    4次方是 The fourth power of 2 i ...
• "平衡"英文翻译    balance; equilibrium
• "力矩的叠加" 英文翻译 :    superposition of moments
• "力矩的拼接" 英文翻译 :    moment splice
• "倾侧力矩的力臂" 英文翻译 :    heeling lever
• "限制力矩的转动盘" 英文翻译 :    mitnehmerscheibe f. drehm-begr. retainer pl. for torque limiter
• "保持…的平衡" 英文翻译 :    keethe balance of
• "初步的平衡" 英文翻译 :    rough balance
• "氮的平衡" 英文翻译 :    nitrogen budgets
• "核的平衡形" 英文翻译 :    equilibrium form of nucleus
• "力的平衡" 英文翻译 :    balance of forces; equilibrium of forces
• "酶的平衡" 英文翻译 :    enzyme balance
• "生理的平衡" 英文翻译 :    physiological equilibrium
• "适度的平衡" 英文翻译 :    optimum balance
• "物种的平衡" 英文翻译 :    alancing act
• "新的平衡型" 英文翻译 :    ccitt v.11/x.27
• "运动的平衡" 英文翻译 :    equilibrium of motion
• "轧辊的平衡" 英文翻译 :    roll balance
• "之间的平衡" 英文翻译 :    balance between
• "不平衡力矩" 英文翻译 :    u alanced moment; unbalance moment; unbalanced moments
• "力矩不平衡" 英文翻译 :    moment unbalance; momentum unbalance
• "力矩平衡" 英文翻译 :    balance of couples; equilibrium of moments; moment balance; moment equilibrium
• "力矩平衡器" 英文翻译 :    moment compensator
• "平衡力矩" 英文翻译 :    balancing moment; balancing torque; counterbalance moment; trimming moment; trimmingmoment

• A discussion has been made on the problems of balance for shocking force and moment of the commonly used crank slider mechanism in machinery
  摘要对机械中常用的曲柄滑块机构的振动力和振动力矩的平衡问题进行了探讨。
• In the procedure , the column is first divided into a finite number of small segments in equal length . the deflection - curvature relation of each segment is determined using the finite - difference method . the final nonlinear algebraic equations are then obtained by means of the equilibrium condition for each segment
  运用这种方法时，先将长柱离散成若干等长的柱段，利用差分方法求得各柱段截面上的挠度与曲率的关系，再根据各截面上力及力矩的平衡条件，得到一组关于荷载与变形关系的非线性代数方程组，本文采用曲率增量法求解该方程组。
• In this application , the lorentz force generated by the interaction between the current in the wire and the geomagnetic field produces an electro - dynamic drag leading to a fast orbital decay . in this paper , we make an intensive study of the process of de - orbiting using electro - dynamic tether system . the concrete work includes : firstly , i have studied the basic principle of how to generate the electro - dynamic drag , modeled via accuracy geomagnetism , made a concrete analysis of the de - orbiting duration , the magnitude and direction of electro - dynamic drag under the action of the dipole and accurate geomagnetic models , set up a counterbalance between electro - dynamic torque and gravity gradient torque , emulate the de - orbiting process of spacecraft , and compared the change of six orbital factors and the de - orbiting duration under the action of the dipole and accurate geomagnetic models
  本文对基于电动力缆绳的航天器离轨过程进行了深入研究,具体工作如下:首先,本文研究了电动力缆绳产生电动力拉力的基本原理,建立了精确地磁场模型;分别在偶极子模型和精确地磁场模型作用下,对电动力拉力的大小、方向、离轨时间及电动力缆绳倾角的大小进行了计算分析;建立了电动力力矩与缆绳系统重力梯度力矩的平衡关系;分析了电动力力矩为系统提供能量的原理;最后分别在偶极子地磁场模型和精确地磁场模型作用下,对受电动力缆绳作用的航天器的离轨过程进行仿真,分析了在不同精度地磁场模型下,航天器离轨过程中各轨道参数的变化情况,并比较了不同模型对离轨时间的影响。