rigid rotor

基本解釋

Equations of motion are adopted for the symmetrical rigid rotor-bearing system, and the nonlinear oil-film force of finite journal bearings is calculated.
采用單圓盤對稱剛性轉(zhuǎn)子軸承系統(tǒng)的運動模型和四階龍格—庫塔法，利用有限長滑動軸承的非線性油膜力，求解系統(tǒng)運動方程。
The theoretical analysis of the balancing of the rigid rotor is performed by means of 8-coefficient bearing model and on the basis of taking into consideration the influence of the gyroscopic moment.
采用8系數(shù)軸承力學(xué)模型，考慮到陀螺力矩的影響，對剛性轉(zhuǎn)子進行了動平衡理論分析。
This paper briefly describes the principles of balancing and correcting for low-speed spinning satellites that work as rigid rotor on ver- tical dynamic balancing machines provided with hard supports.
著重分析了低速自旋式衛(wèi)星作為剛性轉(zhuǎn)子在立式硬支承平衡機上做平衡的工作原理及校正原理；

剛性轉(zhuǎn)子
First, the characteristics of AMBs’ rigid rotor are studied under the condition of low and high rotation speed respectively. The correlative dynamic functions of the rotor are derived.
首先，本文在分析了剛性轉(zhuǎn)子低速和高速旋轉(zhuǎn)時的動力學(xué)特性基礎(chǔ)上，推導(dǎo)了相關(guān)的動力學(xué)方程，推導(dǎo)過程中，在平衡點處作了線性化處理。
電子、通信與自動控制技術(shù)
剛性轉(zhuǎn)子
In chapter 2, the balance theory of rigid rotor is narrated. And the imbalance type and the expression of imbalance quantity of rotor are introduced.
第二章敘述了剛性轉(zhuǎn)子平衡的力學(xué)原理，并對轉(zhuǎn)子的不平衡類型進行了分類，同時對不平衡量的表示方法作了描述。
政治學(xué)
剛接式旋翼