以120名CUBA运动员为研究对象，以成就动机测量表ams为工具，分析了CUBA运动员的成就动机水平。
With 120 CUBA players as the subjects of study, and achievement motivation Scale (AMS) as analytic tool, this paper researched into the players' achievement motivation level.
并在此基础上，开发了一套应用于枪械自动机测量的实时数据采集系统，文中还对整个系统的软件和硬件结构作了简介。
A set of real-time system for data acquisition of the measurement of gun automation motion is developed based on this method, and the software and hardware of this system are simply described.
由于有较强的理论建构做基础，因此从测量结果可了解物理学习动机的全貌，从而能有针对性地进行教育。
With a strong theory basic, we can see the panorama of students' physics study motivation, so that we can educate them pertinently.
压电式变送器也可以用来测量发动机内部燃烧压力的测量与真空度的测量。
The piezoelectric sensors can also be used to measure the internal combustion engine measure pressure and vacuum measurement.
本研究主要是对无锡、石嘴山、灵石三地的411名基层党政干部的成就动机及其归因进行测量。
This research mainly carry on the measurement of achievement motivation and the attribution of 411 primary level leader in Wuxi, Shizuishan and Lingshi.
“波浪与海流测量仪器测试装置”依靠机械传动机构带动传感器作相对运动，模拟“波浪”和“海流”测量状态。
The testing equipment for wave and current meters drives the sensors to move, and simulates the wave and current state by mechanical system.
本系统能够完成发动机的转速、转矩的高精度控制与测试，以及发动机温度、压力、油耗等指标参数的测量。
This system can complete the engine rotational speed and torque high accuracy control and the test, also engine temperature, pressure, oil consumption parameters survey.
测量旅游动机：不要尺度问题？
遮阳系统配有传感器，不断测量光和温度，然后再通过一个小型电动机的装置机械调节百叶窗。
The solar shading system is fitted with sensors which continuously measure light and heat levels and regulate the shutters mechanically by means of a small motor.
扳动电动机的转轴是否能自由旋转，测量定子和轴承的空隙。
Turn the electric motor shaft if it rotates freely, Measure the air gap between the stator and the rotor.
在充分理解的基础上，再对CMF系列发动机瞬时油耗测量仪进行安装、操作和维护。
On the basis of full understanding, CMF series dynamical fuel mass flow meters for engine can be installed, operated and maintained.
介绍了某型航空发动机可调导向叶片测量的一般原则和内容。
This paper introduces the general principle and the content of the measurement of the adjustable leading vane of aero_engine.
分析表明，这种双量程测力传感器既可以连续测量发动机两级推力，又提高了其测量灵敏度和精度。
The results show that the sensor designed can continuously measure the two grade thrust of rocket engine, and improve the measuring precision and sensitivity.
本文设计了一种发动机排放测量全流稀释系统，可以满足车用发动机排放测量需要。
This paper describes the design of a total flow dilution system for the engine particle emission measurement. This system meets the requirement of vehicle engine emission measurement.
介绍了发动机的本体结构、实验系统、参数测量系统及小推力测量系统。
The structure of arcjet, experimental system, measurement system and the small thrust measurement system were introduced.
该测量装置突破了目前使用手动机油标尺测量的原始方法，弥补了测量不精确、不能动态监测机油的缺陷。
The measuring device has broken through the currently used method of measuring by mechanical oil rod, thus making up for the original idea's defects of inaccuracy and non-dynamic monitoring.
微处理机可以与一个天平、砝码和量杯一起使用，以实现对发动机燃料消耗率的经济而精确的测量。
Can be used with a balance, weight set, and beaker to provide an economical and accurate measure of engine fuel consumption rate.
为此，描述了一种通过测量和分析发动机的瞬态转速来监测气缸内的压力和压力扭矩的方法。
The objective of this paper is to describe a method of monitoring engine pressure and pressure torque by measuring and analysing engine transient speed.
最后，设计出基于特征点拾取的空间参数测量方法，实现剖切后发动机结构空间距离、角度和体积的精确测量。
Finally, space parameter measurement method based on feature point selection was designed to accurately measure the distance, Angle and volume of cutting motor structure.
对于固体火箭发动机羽焰温度的测量是困难的，了解其温度分布对于研究发动机内燃烧流场的特性有重要价值。
The temperature of a high temperature, high pressure plume solid propellant rocket engine is difficult to measure but is useful for determining the combustion status of the engine.
这些优点已使得电容式传感器成为测量发动机汽缸压力的有效的装置。
These advantages have made the capacitive transducer a valuable device for measurement of engine cylinder pressures.
通过测量发动机的关键特征参数，对提取的特征量进行加权处理，利用模糊数学方法对发动机进行了技术状况评估。
The paper disposed the extracted characteristics, and judged the technical state of engine using the method of fuzzing mathematics, via measuring the key characteristics parameters of engine.
试验系统包括真空模拟系统，供电系统，推进剂供给系统，参数测量系统和发动机本体。
The experimental system includes a vacuum simulation section, power supply section, propellent feed section, parameter measurement section and an arcjet.
最后给出传感器标定结果，并讨论了在航空发动机燃油测量中的应用。
Finally, the application of the sensor is discussed in measuring fuel flow of an aeronautical engine.
叶片振动测量对航空发动机、电站涡轮机及各种压气机的强度设计和研究及安全监测非常重要。
It is important to measure blades vibration for the intensity design and for safely monitor of air engines, turbines of power station and compressors.
利用农林废弃物可控热裂解产生的生物质气作为火花点火发动机的燃料，测量火花点火生物质气发动机的示功图，分析了生物质气的燃烧放热特性。
The biogas produced from the controllable thermal cracking of the farming and forestry disposables was used as the fuel of the spark-ignition biogas engine.
在姿控发动机的瞬态推力测量中，推力测量系统的动态特性是影响推力准确测量的一个至关重要的因素。
In the instantaneous thrust measurement of an attitude control solid rocket motor, dynamic characteristic of thrust measurement system affects the accuracy of thrust measurement.
该系统不仅能测量柴油发动机的瞬态油耗和转速，而且可定时间或定质量测量发动机的稳态油耗。
The system can measure not only the instantaneous fuel consumption but also the steady fuel consumption of the engine on the basis of fixed time and fixed mass.
本文介绍了一典型的涡轮喷气发动机全流程参数测量的试验方案、测试结果及分析。
This paper presents the test plan, the results of the station parameters measurement for a typical turbojet engine and the analysis of measurement results.
本文介绍了一典型的涡轮喷气发动机全流程参数测量的试验方案、测试结果及分析。
This paper presents the test plan, the results of the station parameters measurement for a typical turbojet engine and the analysis of measurement results.
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