陀螺力矩的英文
gyro moment
gyroscoopic torque
gyroscopic couple
gyroscopic moment
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例句与用法
更多例句： 下一页- This dissertation aims to reveal the influence of maneuver load ( including additional centrifugal force and gyroscopic moment ) on the vibration performance of rotors with sfd
本文旨在揭示机动飞机产生的附加离心力和附加陀螺力矩对挤压油膜阻尼器以及发动机转子系统振动特性的影响。 - The counter - rotating dual - rotor system in aeroengines can reduce the influence of rotors ' gyroscopic moments on aircrafts , cut down the torque of cases and improve the flexibility of airplanes
摘要航空发动机采用反向旋转的双转子系统，有助于减小转子整体陀螺力矩对飞机的影响，降低机匣负荷，提高飞机机动性能。 - It is concluded that the influences of maneuver flight on the rotor system of an aero - engine are evident , therefore , they should be taken into account during design of the engine
研究结果表明，机动飞行所产生的附加离心力和附加陀螺力矩对发动机转子振动的影响是明显的。因此，在设计战斗机的发动机转子系统时，必须考虑机动飞行的影响。 - The results for two equations were analyzed and compared , which showed that the gyro effect of the crankshaft system could be ignored for low rotating - speed engine and it should be considered for higher rotating - speed engine
结果表明，对于低转速发动机，曲轴转动的陀螺效应不明显，而对于高转速的发动机，陀螺效应不能忽略，应以考虑陀螺力矩的方程为基础进行设计分析。 - The convert and evolution course of periodical response , quasi - periodical response , double - periodical bifurcation , chaos of the system response is analyzed . ( 3 ) . it is deduced that the general differential equation of bending - torsional - pendular coupling vibration about rotor with the gyroscopic moment
( 3 )推导了一般意义下,考虑陀螺力矩的单盘转子弯扭摆耦合振动非线性方程,基于该方程,推出了不平衡转子和碰摩转子的非线性弯扭摆耦合振动方程。
