no-load test
英 [nəʊ ləʊd test]
美 [noʊ loʊd test]
空载试验;无载试验;无负载试验
双语例句
- According to the no-load test results and the locked rotor test results, the equivalent circuit parameters of the prototype motor with copper windings are obtained.
根据空载试验结果和堵转试验结果,得到了铜绕组试制样机的等效电路参数。 - Testing Method with Microcomputer for No-load Test of Transformer
变压器空载试验微机化测试方法 - Developed the device manufacturers, installation, debugging, and then for no-load test and actual field test.
所研制的装置经制造、安装、调试,然后进行空载试车和实际现场应用试验。 - The close-loop test for generator excitation system is done by using RTDS simulation system, including regulator parameters setting, no-load step response test and load PSS test, power system fault simulation.
利用实时数字仿真RTDS进行发电机励磁系统闭环试验,完成了调节参数整定、发电机空载阶跃响应和发电机负载PSS参数整定、系统故障模拟等试验。 - Taking the error occurring in no-load test of three phase AC traction motor in our company as example, analyzing with symmetrical components method, the main cause of error-three phase non-symmetry and corresponding solutions were given in this paper.
根据本公司轨道交通用三相异步电动机在空载试验时所出现的误差,用对称分量法进行分析,找出电源的三相不对称是三相异步电动机空载试验时产生误差的主要原因,并给出了相应对策。 - No-load Test: No-load characteristic curve analyze all kinds of loss;
空载试验,空载特性曲线,分析各种损耗。 - Based on analysis of power source in no-load test of large power transformer, the cause for larger power source capacity in tests are given. The compensation method with parallel capaci-tance to solved the power source problem in no-load tests is presented.
通过对电力变压器空载试验电源的分析,指出了造成试验要求电源容量较大的原因,提出了解决空载试验中电源容量问题的并联电容补偿方法。 - Research on Accurate Measuring Method for Transformer No-load Field Test
现场变压器空载试验的精确测试方法研究 - Temperature data in transformer core during heating up under no-load test are analysed, and mathematical model for temperature rise curves at some test points established, thermal time constant in its expression assumed as a linear function of time.
分析了变压器空载试验时铁心温升过程的温度数据,得出试验点温升曲线的数学模型,其表达式中热时间常数为时间的一次函数,而试验点的极限温升可直接求出。 - The paper provides a simulated mathematics model of the ground to air missile's pneumatic actuator in that some major nonlinear factors were considered, presents three methods, no-load check, simulation test and flight test, to check this model.
本文给出了某种地一空导弹气压舵机的仿真数学模型,此模型计入了一些重要的非线性因素;介绍了空载校准,仿真试验和导弹飞行验证的综合校准此模型的方法。
