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陀螺力矩的英文

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"陀螺力矩"怎麼讀用"陀螺力矩"造句
英文翻譯手機版
  • gyro moment
  • gyroscoopic torque
  • gyroscopic couple
  • gyroscopic moment
  • gyroscopic torque
  • gyrostatic moment
例句與用法
  • 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
    本文旨在揭示機動飛機產生的附加離心力和附加陀螺力矩對擠壓油膜阻尼器以及發動機轉子系統振動特性的影響。
  • 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
    摘要航空發動機采用反向旋轉的雙轉子系統,有助于減小轉子整體陀螺力矩對飛機的影響,降低機匣負荷,提高飛機機動性能。
  • 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
    研究結果表明,機動飛行所產生的附加離心力和附加陀螺力矩對發動機轉子振動的影響是明顯的。因此,在設計戰斗機的發動機轉子系統時,必須考慮機動飛行的影響。
  • 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
    結果表明,對于低轉速發動機,曲軸轉動的陀螺效應不明顯,而對于高轉速的發動機,陀螺效應不能忽略,應以考慮陀螺力矩的方程為基礎進行設計分析。
  • 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 )推導了一般意義下,考慮陀螺力矩的單盤轉子彎扭擺耦合振動非線性方程,基于該方程,推出了不平衡轉子和碰摩轉子的非線性彎扭擺耦合振動方程。
  • A method is proposed for the parameter identification of the viscoelastic internal dampers of the multirotor systems in this paper . the multi - rotor system is regarded as a composite structure . the impedance matching method in the substructure method for structural dynamic analysis is used for the dynamic calculation of the structure . the augmented lagrange method is applied to the iteration calculations of the characteristic determinant of eigenvalve equation of the system . and then the results of parameter identification can be obtained . upon the dynamic characteristics of the system , the method can reveal the influence of the gyroscopic moments of force precisely . in process of the analysis , the various properties of multi - rotor systems are made the best use of , so the measure of the modes parameters is avoided , the calculation is simplified . in addition , an efficient method is proposed to establish a dynamic model of multirotor systems with viscoelastic internal dampers . the calculating results are consistent with the experimental results satisfactorily
    提出了多轉子系統的粘彈性中間彈支參數辨識的一種方法.該方法把多轉子系統看作復合結構,用動態子結構分析的阻抗匹配法計算動力學特性,用增廣拉格朗日乘子法迭代計算系統特征方程的系數行列式,獲得系統物理參數的辨識結果.該方法可以準確計入陀螺力矩的影響,避免測量振型參數.在分析中,利用多轉子系統的特性可簡化分析過程.文中還介紹了一種建立粘彈性彈支多轉子系統動力學模型的方法.計算結果與試驗結果基本一致
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