多功能综合液压泵试验台的研制  

The design of multi-functional comprehensive hydraulic pump test-bed

作　　者：许松[1] 陈浩[1] 孙启顺[1] 

机构地区：[1]空军第一航空学院,河南信阳464000

出　　处：《机械研究与应用》2012年第3期118-120,共3页Mechanical Research & Application

摘　　要：研制了飞机液压泵综合测试台,介绍了试验台的组成、工作原理、主要技术方案;主要阐述以计算机控制技术为核心,集状态监测、数据采集处理为一体的液压泵综合测试系统的设计过程,该型试验台工作稳定可靠,能完全满足飞机液压泵性能技术要求。A comprehensive test bed aircraft hydraulic pump is developed, the composition of the test bed, the working principle, the main technical program are introduced; Based on the computer control technology, the design programme is exponded for the hydraulic pump test system which integrated the status monitoring and data acquisition processing, this type of test rig is stable and reliable, and is able to fully meet the technical requirements of the aircraft hydraulic pump performance.

关 键 词：飞机 液压泵 测试台 

分 类 号：TH38[机械工程—机械制造及自动化]