thrust motor的例句大全

The principle of operation for the novel motor, the theoretical expression of thrust and the optimum performance are described.

文章描述了这种电机的运行原理，推力分析，和最佳运行。

The expulsion of the exhaust products through the nozzle at high velocity produces thrust, the "power" of a rocket motor.

驱逐排气产品通过喷嘴高速产生的推力，“权力”的一个火箭发动机。

After calculating the output power of submersible propeller based on thrust, the axial power and the installed power necessary for submersible propeller can be calculated by efficiency of propeller and efficiency of motor which are supplied by the manufactory.

根据推力计算出推动器的输出功率后，可通过厂家提供的产品螺旋桨效率η螺和电机效率η电机来求得推动器所需要的轴功率和装机功率。

It's verified that a series of intense pressure impulses can occur in the combustion chamber after the thrust reversal nozzles of the solid rocket motor are suddenly opened.

实验表明，突然打开固体火箭发动机反向喷管后，燃烧室中可能出现强烈的压力冲击，这种压力冲击来自喷管喉部节流和形成准稳态流动之前的非定常过程。

Magnetically Suspended Rocket Motor Thrust Test Stand

磁悬浮火箭发动机推力测试台

Taking piezoelectric as the core, a novel motor thrust measurement system is developed. Based on this fact, dynamic performance of the new thrust testing stand is studied in this paper. The groundwork of performance studying is mathematical model.

针对研制成功的以压电传感器为核心的新型发动机推力测试系统，本文对其动态性能进行了研究。

Damping on the axial motor thrust bearing structure, hollow shaft and damping winding structure has been analyzed on the electrical test data were analyzed, and combined with the status quo of the market prospects for future analysis.

对电机轴承的轴向阻尼止推结构、空心轴结构和阻尼绕组结构进行了重点分析，对电机的试验数据进行了分析，并结合现状，对今后的市场前景进行分析。

An Exploratory Research of Test Technique for Solid Rocket Motor Thrust Termination

固体火箭发动机推力终止试验技术探讨滚珠式推力终止装置可靠性研究

A cold air experiment on thrust termination of a solid rocket motor with reversal nozzles is described in this paper.

本文介绍一个反向喷管推力终止的冷模拟实验。

Measuring method of opening time and operating synchronism of the reverse nozzle closures of solid rocket motor during thrust termination test was studied.

研究了固体火箭发动机推力终止试验时，反向喷管堵盖打开时间及同步性测量方法。

Dynamic calculation on thrust vector control system for solid rocket motor

固体火箭发动机推力向量控制系统动力学计算

Investigation on secondary gas injection for solid rocket motor based on thrust vector control

基于推力矢量控制的固体火箭发动机气体二次喷射研究

And the research and development of motor energy management and thrust vector control ( TVC) technique are being carried out.

发动机能量管理和向量控制技术的研制与开发工作正在开展之中。

Nozzle is an important part of the thrust vector control system of solid rocket motor and high-performance design of a nozzle plays an important role in the performance of the motor.

喷管是固体火箭发动机推力向量控制系统的重要组成部分，高效能的喷管设计对发动机的性能至关重要。

The effects of the extendible exit cone on stability of the thrust vector control system of largescale solid rocket motor are presented and the measures for improving the system stability are suggested.

介绍了喷管可延伸出口锥对大型固体火箭发动机推力向量控制系统稳定性的影响，并提出了改善其系统稳定性的措施。

For the nuclear pump, it is necessary to provide the motor with sufficient high load support and low friction using the tilting-pad thrust bearing and the mechanical seal, the most two important parts.

可倾瓦推力轴承和机械密封是核主泵和其它核泵中两个最为关键的润滑部件。

Method and Mechanism Analysis of Retraining Thrust Pulsation for Long Stator Linear Synchronous Motor

长定子直线同步电动机抑制推力脉动的新方法及机理分析

In order to satisfy the operation requirement of the rated thrust of the propeller, the propulsion motor performs only in rated torque on the low speed, so the motor power is low.

认为以满足螺旋桨额定推力为目的，推进电动机只需要低速输出额定转矩来实现，即输出功率较低。

In direct thrust control system, flux linkage observation accuracy influences the thrust of linear motor. Therefore, it is offered a theory premises that increase the observation accuracy of flux linkage.

而在直接推力控制系统中，磁链的观测精度直接影响电机输出推力的平稳性，因此，提高磁链观测精度有利于改善直线电机控制系统稳定运行的性能。

Direct thrust control for interior permanent magnet linear synchronous motor ( IPMLSM) with hysteresis causes notable thrust as well as flux and current pulses during steady-state operation or with uncertain switch frequency.

直线永磁同步电机直接推力滞环控制，导致开关频率不定及稳态运行时会有明显的推力和磁链脉动产生。