Development of fatigue test technology of aircraft landing gears

1、

Conversion results and error analysis of the level acceleration flight test on an aircraft

某型飞机水平加速性能试飞换算结果及误差分析

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2、

Research on vibration environment test technology of aircraft structure combined with fatigue or static load

飞机结构件复合加载振动环境试验技术研究

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3、

The Actuality and Development of Ground Test Apparatus for Aircraft Hydraulic System

飞机液压系统地面测试设备的现状与发展

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4、

Parameters Test for the Aircraft Power Supply System Based on Personal Computer and Software Engineering

基于PC机下飞机供电系统参数测试及软件设计

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5、

Design and Implementation of Networked Distributed Test System for Aircraft Power Supply System

飞机供电系统的网络化分布式测试系统设计与实现

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6、

Research on Vibration Environment Test Technology of Aircraft Structure

飞机结构件振动环境试验技术初探

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7、

The principle-level test of aircraft hydraulic system is carried out succeeding the component-level test and prior to the system-level test ( known as the iron bird test), in order to verify the principle of the hydraulic system.

飞机液压系统研制试验分为元件级、原理级和系统级三种试验，飞机液压系统原理性试验研究是在元件级试验之后，系统级试验（铁鸟试验）之前，进行原理性探索和验证。

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8、

The full scale ground simulation test of aircraft's pressure refuel system is one of the most important link in system design. The main task is to modulate system parameters, test system performance in order to get the optimal performance of the system.

飞机地面压力加油系统全尺寸1∶1地面模拟试验是该系统研制过程中的重要环节之一，其主要任务是调节系统参数，考核系统性能，使系统达到最优化。

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9、

The data processing and compilation of vibration environmental spectrum is an important part of environmental reliability test for aircraft airborne equipment. It has great significance for guaranteeing the security and reliability of aircraft airborne equipment.

飞机机载设备振动环境谱的数据处理与编制是飞机机载设备环境可靠性试验的重要组成部分，对保障飞机机载设备的安全性和可靠性具有十分重要的意义。

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10、

He simultaneous data acquisition system with multi-channel and large-capacity is the important equipment in the flow-field match test of aircraft inlet/ engine and vibration mode test of aircraft, ships and automobiles.

多通道、大容量同步数据采集系统，是飞机进气道／发动机流场匹配试验，飞机、舰船和汽车的振动模态试验中的重要测试设备。

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11、

Then, the mathematics model of calculating the surface load and point load in the design of aircraft structure static load test using aircraft surface model is established.

其次结合飞机的曲面外形，建立了飞机结构静力试验设计中的分布式载荷和集中式载荷的演算数学模型。

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12、

Considering the influence of corrosive environment, a valuable method for fatigue test of aircraft structures at room temperature and in the air is presented.

考虑腐蚀环境的影响，提出了一种关于飞机结构在一般环境下的疲劳试验方法。

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13、

It was built big to test full-size aircraft, where many wind tunnels are much smaller and test only small-scale models.

它建大考验全尺寸飞机，其中许多风洞试验是小得多，只有小规模的模式。

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14、

The purpose of the test for aircraft with propeller is to obtain the effects due to slipstream.

螺旋桨动力试验的目的在于获得螺旋桨滑流影响（间接影响）。

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15、

Difference GPS Taking-off and Landing Performance Test of Aircraft

基于差分GPS的飞机起飞着陆性能试飞

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16、

The test of aircraft cables is an important technological problem in aircraft final assembling.

飞机电缆检测是飞机总装配的一项重要技术关键。

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17、

Prediction and test of aircraft stall/ spin characteristics

飞机失速/尾旋特性的预测和试验研究

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18、

Random Vibration Test of Aircraft Suspension Equipment

飞机悬挂装置随机振动试验技术

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19、

Automatic Test of Aircraft Failure in Deflected Angle of Horizontal Tail

飞机平尾偏角故障的自动检测

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20、

Design of Computer Control System for Endurance Cycle Loading Test of Aircraft Actuating Cylinder

飞机作动筒耐久循环加载试验计算机控制系统设计

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