六方蝰蛇发动机试验台，不仅是一份文件，设计，它是真实的！
The six-engine viper test rig, not only a paper design, it's real!
在此基础上，建立了火箭发动机试验台液氢供应系统的健康评价体系。
Base on these, the health condition evaluation system of the liquid hydrogen supplying system of a rocket engine testing platform was set up.
本实用新型属于发动机维修调试设备领域，具体涉及一种发动机试验台。
The utility model in particular relates to an engine test-bed which belongs to the field of the maintaining and debugging equipment for engines.
本文论述了车用发动机试验台排气系统中的三节扩张式消声坑的设计和试验结果。
In this paper the design and performance of expanding silencing exhaust duct for the test bed of automotive engines are discussed.
作者结合发动机试验台，设计了一套对活塞环-缸套动态摩擦力进行采集的装置。
Based on the bench test, a system is developed for measuring the variation of the friction between piston ring and cylinder liner.
本实用新型提供一种发动机试验台的油门执行机构，包括电机，该电 机的转轴上固定有可牵拉发动机油门的拉块；
The utility model provides a throttle implementing mechanism of an engine test bed, which includes a motor, a pull block that can pull the engine throttle is fixed on the rotating axis of the motor;
本文介绍了最新引进的发动机动态试验台，对其配置、特点、功能作了叙述。
The latest imported engine dynamic test stand is introduced in this paper, Its allocation, characteristics and functions are also stated.
阐述了模拟汽车运行工作的发动机动态性能试验台的采样与控制系统。
This paper describes the sampling and control system of an engine dynamic performance test bed simulating the running conditions of motor vehicles.
研究了火箭发动机高速旋转试验台高速轴在工作激振频率内的振型。
The mode shapes of the high-speed shaft in rotating test-bed for rocket engine within working excited frequencies were studied.
介绍了汽车发动机冷却水泵密封性能试验台系统设计方法，实现汽车冷却水泵密封性能测试系统的自动化、智能化。
This paper introduced the system design methodology used for automobile water pump seal performance testing, and realized of automation, intelligent for testing it.
日本斥巨资建立发动机模拟高空试验台。
Japan has invested a huge sum on building up a simulated altitude test facility.
该试验台可模拟汽车发动机的道路工况及传动系统，可用于汽车发动机的匹配研究和排放研究。
This test stand can simulate the road condition of engine and transmission system, it can be used in researching match of the engine and the emission.
以D6114型增压柴油机为基础，开发了增压系统瞬态特性与发动机性能试验台。
The test stand-by for studying the transient performance of the diesel engine's turbo-charging system was established based on D6114 diesel engine.
本试验台可以反复模拟发动机在不同工况下各传感器、执行器、电控单元以及线路的各种故障。
The experimental rig can continuously produce various kinds of failure of the sensors, actuators, electronic controlled unit and circuits.
设计制造了发动机冷却风扇噪声性能测试专用试验台，用于冷却风扇的台架试验。
A specialized noise test bench of automobile cooling fan was designed to carry out the bench test and the outer vehicle acceleration noise test also was conducted.
本文详细讨论了航空发动机滑油系统试验台计算机控制系统的软、硬件设计的过程和方法。
In this paper, the design of both the software and the hardware of the computer control system for the test-bed of lubricating oil system for aeroengine are discussed explicitly.
串行通信是发动机电控试验台实时监控软件的主要功能之一。
Serial communications is one of the main functions of real-time control software used in the electronic controlled engine test-bed.
基于振动系统质量周期法，设计了一种测试发动机质量参数的双簧倒立摆试验台。
Based on the mass-period method, a measuring device named double spring inversion pendulum was designed, which could measure the center of mass and moment of inertia of an engine.
研究建立了一个模拟多种发动机尾气热源的试验台。
In the paper, an experimental bench which simulating multiengine tail gas heat source is researched and built.
设计并安装了专用的齿轮箱试验台，并在台架上进行了模拟发动机与螺旋桨扭振激励状况下的试验。
A special gearbox test device was made to simulate the excitation of the engine and the propeller.
将电磁悬浮技术用于火箭发动机推力测试试验台是一次新的尝试。
It is a new experience to apply magnetic levitation technique to thrust measurement for rocket engine.
本文用最大误差方法，对固体火箭发动机六分力立式试验台的静态误差进行了分析。
By using the method of maximum error, the paper deals with the analysis of the static error of the six-component force test stand of solid rocket motors.
该火箭发动机和试验台是如图3所示。
该火箭发动机成立，在试验台是如图3所示。
The rocket motor set up in the test rig is shown in Figure 3.
该火箭发动机成立，在试验台是如图2所示。
The rocket motor set up in the test rig is shown in Figure 2.
当需要考察一台航空发动机的高空性能时，可以利用三种型式的设备，即高空风洞、高空试验台和飞行试验台。
When it becomes necessary to examine the altitude performance of an aircraft engine, three types of facilities may be used-altitude wind tunnels, altitude test beds and flying test beds.
针对亚燃冲压发动机燃烧室内部流动特点，结合二元稳定器试验台高速气流场燃油雾化特性试验，建立试验件三维模型并对其喷雾两相流动进行数值模拟。
Based on experimental investigation of the liquid fuel atomization in high speed airflow and the flow characteristics of ramjet combustion chamber, a three-dimensional model was established.
高速旋转试验台是模拟底排一火箭复合增程炮弹内的固体火箭发动机实验设计的。
The estimation of extend-range solid rocket motor in high speed rotation is a key technique.
高速旋转试验台是模拟底排一火箭复合增程炮弹内的固体火箭发动机实验设计的。
The estimation of extend-range solid rocket motor in high speed rotation is a key technique.
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