飞机喷口滑油泵试验台液压系统的设计  

Hydraulic System Design of Test Bed for Aero Spout Hydraulic Oil Pump

作　　者：高昆[1] 陈勇[1] 

机构地区：[1]空军第一航空学院航空修理工程系,河南信阳464000

出　　处：《机电产品开发与创新》2008年第5期33-35,共3页Development & Innovation of Machinery & Electrical Products

摘　　要：分析了飞机喷口滑油泵液压试验台的设计要求与难点,提出了设计方案,有效地解决了大流量、高精度、高温的闭式液压系统设计以及复杂的油泵斜盘角度测量机构的设计难点,该试验台具有精度高、结构紧凑、操作使用方便、维护简易等优点。The difficulty and requirement of test bed design are analyzed, and the design concept is put forward. Big discharge, high accuracy and high temperature of closed - type hydraulic system and complicated angle measurement mechanism of obliqueness plate in oil pump are two design difficulties, but they have been solved effectively. This test bed has the advantage that accuracy is high, structure is severeness, and manipulation is convenience, and maintain is facility, etc.

关 键 词：喷口滑油泵 油泵试验台 液压系统设计 斜盘扭矩检测装置 

分 类 号：TH-39[机械工程]