飞机液压系统

飞机液压系统CAI课件的开发与教学

The Development and Teaching of CAI Course Ware of Aircraft Hydraulic System

基于VB6.0平台开发了飞机液压系统CAI课件，并运用于专业核心课程《飞机系统》的教学与实验教学，达到了良好的效果。

The CAI course ware of the aircraft hydraulic system was exploited based on VB6.0 platform and applied to the teaching and experimental teaching of the core specialized course & Aircraft Systems . It has achieved good results .

民用飞机液压系统元件EDP（发动机驱动泵）、ACMP（交流电动泵）、PTU（能量转换单元）为系统提供液压能，是整个液压系统的核心元件。

Commercial aircraft hydraulic components-EDP ( Engine driven pump ), ACMP ( AC-motor driven pump ), PTU ( Power Transfer Unit ) are the key components , supplying the system with hydraulic energy .

飞机液压系统压力脉冲试验波形控制

Controlled Pressure Pulses for Testing Hydraulic Pipes and Components of Aircrafts

飞机液压系统地面测试设备的现状与发展

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

飞机液压系统固体颗粒污染分析与控制

Solid Granule Contamination Analysis and Control for Aircraft Hydraulic Systems

液压油对飞机液压系统性能影响分析研究

Character Analysis of Airplane Hydraulic System Influenced by Hydraulic Fluids

飞机液压系统故障多的原因探讨及对策

The Analysis & Countermeasure of the Reason for Military Aircraft Hydraulic System Fault

基于小波包特征熵的飞机液压系统故障诊断方法研究

Research of Fault Diagnosis of Aircraft Hydraulic System Based on Wavelet Packet-Characteristic Entropy

飞机液压系统污染控制理论研究

Theoretic Study on Contamination Control of Airplane Hydraulic System

飞机液压系统试验数据分析软件的研究与开发

The Research and Development of the Test Data Analysis Software for Aircraft Hydraulic System

某型飞机液压系统相关失效原因分析及其改进方案

The Reason Analysis and Improvement to the Relating Failure of a Airplane Hydraulic System

液压脉冲试验是飞机液压系统设计中的重要环节。

Hydraulic impulse test is the important aspect in the design of airplane hydraulic system .

这对于较精确地分析飞机液压系统损失特性有重要的作用。

It was very important to accurately analyze the loss property of aircraft hydraulic systems .

未来飞机液压系统的特点

Characters of Future Aircraft Hydraulic System

数值分析法在飞机液压系统噪声分析中的应用

The Application of Numeric Analysis Method in the Noise Prodiction of Hydraulic Control System in Airo

这对分析与解决飞机液压系统故障，确保飞机的飞行安全有着重要的意义。

It has much meaning for analyzing and solving aircraft hydraulic systems fault and ensuring aviation safety of aircraft .

综合保障车主要是用来作为液压源向飞机液压系统提供工作所需的液压动力，从而对飞机液压系统进行工作性能检查和试验；

Integrated Service Vehicle ( ISV ) is mainly designed to supply hydraulic oil pressure and provide operation inspecting and testing for airplane hydraulic system .

飞机液压系统由于油压脉动引起的管道振动是近十多年来国内外航空工业界极为重视的工程实际问题。

The pipeline vibration caused by pressure surge in aircraft hydraulic system is an important engineering problem both to domestic and foreign aviation industries in recent decades .

液压油泵车是一种重要的航空地面保障设备，能够为飞机液压系统提供液压动力源、清洁油液和加油等功能。

Hydraulic power carts play an important role in ground handling support because of the function of providing hydraulic energy for airplanes , cleaning and supplying oil .

针对飞机液压系统的工作特点和液压油的工作条件，指出了航空液压油粘度的重要性；

Aiming at working characteristics of hydraulic system and working conditions of aircraft hydraulic oils , the importance of viscosity for the aircraft hydraulic oils is pointed out .

飞机液压系统包括液压源、刹车、起落架收放、飞行控制等子功能系统。

An airplane hydraulic system is composed of different parts including the hydraulic pressure source , brake , landing gear retract and extend , flight control and other sub-function systems .

分动器分流传动装置是一种专用于飞机液压系统和传动系统清洗作业的高压清洗车的取力装置。

The shunt transmission gear of transfer box is a kind of power take off in a heavy pressure cleaning vehicle used to clean hydraulic system and drive line of airplane .

针对飞机液压系统固体颗粒污染，分析了固体颗粒污染物的来源及其危害，进而提出了控制飞机液压系统固体颗粒污染的方法。

The source and endangerment of solid granule pollutant were analyzed on solid granule contamination of aircraft hydraulic systems . A method was proposed to control solid granule contamination of aircraft hydraulic systems .

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。

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 .

重点介绍了民航飞机液压系统伺服控制组件维修所需的液压伺服控制台的系统设计思想、主要技术指标、系统组成和信号标定等内容。

This article analyzes and introduces the design idea , main technologic parameters , constructions and signals indication of a new hydraulic servo control test devices which have been used for repairing the civil aircraft hydraulic servo control assembly .

本课题针对飞机液压系统原理性试验的性能要求，研制开发了某型客机多泵多体制液压系统原理性试验平台，可以针对三种不同压力级别液压系统进行原理性试验探索。

The aircraft hydraulic platform with Multi-pumps and systems , based on the technical requirement of the aircraft hydraulic system principle test , was developed to verify the hydraulic system of an airliner and could test the hydraulic system under three different pressure levels .

随着飞机液压系统中液压舵机和伺服阀等高精度附件的大量应用，为保证系统的可靠性和延长附件寿命，降低全寿命费用，必须大幅度提高液压系统的清洁度。

Because of increasing accuracy of many major accessories , such as servo actuators and servo valves , a raised cleanness must be provided in hydraulic systems to ensure accurate operation of the systems and prolonged service life of the accessories , and to reduce lift cycle costs .

某型飞机液压能源系统频域特性分析

Freqency Characteristic Analysis of an Aeroplane Hydraulic Source System

飞机液压刹车系统数字仿真研究

Research on Digital Simulation of Aircraft Hydraulic Braking System