某型航空发动机燃油泵性能检测台的研制  

Research and Development of the Performance Test Platform for Aircraft Engine Fuel Pump

作　　者：吕孟军[1] 赵学军[1] 温海涛[1] 郭琪[1] 

机构地区：[1]空军第一航空学院航空机械工程系,河南信阳464000

出　　处：《自动化仪表》2014年第1期77-80,共4页Process Automation Instrumentation

摘　　要：为解决某型航空发动机燃油泵在返厂维修和封存期间的性能检测问题,构建了综合化的燃油泵性能检测平台。为确保功能和指标的实现,依据检测内容,基于安全性和可靠性的设计原则,对平台驱动系统进行了科学搭建、对液压系统和测控系统等进行了试验和修正。检测台实现了对燃油泵的磨合运转、性能参数的准确检测和性能的综合判定,为装备的维护保养和正确使用提供了可靠依据。相关单位应用表明,该平台有效提升了某型航空发动机装备的维护保障效率。In order to solve the performance testing issue during returned for repair and sequestration period of the fuel oil pumps of certain model of aircraft engine, the comprehensive performance test platform of the fuel oil pumps is constructed. To ensure implementation of functions and performance indexes, in accordance with the detection contents, Based on the design principle of reliability and security, the drive system is built scientifically, and the hydraulic system and measurement and control system are tested and revised. The run-in operation, precise detection of the performance parameters, and comprehensive performance judgment for the fuel oil pump are conducted, thus reliable basis of maintenance and proper use of the facility is provided. The application indicates that this platform effectively improves efficiency of maintenance security for facility of this model of aircraft engine.

关 键 词：航空发动机 燃油泵 性能检测 驱动系统 流量测量 

分 类 号：TP216.1[自动化与计算机技术—检测技术与自动化装置]