Study on Vibration Ezperiment for Aircraft Structure under Static Loads

摘要：

The vibration environment test for aircraft structure under multiform loads is a key technique for examining anti-vibration strength of aircraft structures.This test technique which associates vibration with statie loads was discussed including the general idea of test, the design technique of test system,loading the static pressures, the balance types of static forces and moments, and controlling the static loads.Rubber airbags and rubber-ropes were used to simulate static loads to achieve the vibration environment test for aircraft structure.At same time, the virtual testing technique was used on the vibration response measure for vibration environment test of aircraft structure under vibration load and static loads.

关键词： vibration environment aircraft structure static load shaker dynamic measure

作者: SHAO Chuang FANG Keqiang

作者单位: The 2nd department,Aircraft Strength Research Institute,AVIC Xian,China The 21at department,Aircraft Strength Research Institute,AVIC Xian,China

会议类型: 国际会议

会议名称: 2009 8th International Conference on Reliability,Maintainability and Safety(第八届中国国际可靠性、维修性、安全性会议)

会议地点: 成都

会议语种:英文

页码: 1096-1099

在线出版日期: 2009-08-24（万方平台首次上网日期，不代表论文的发表时间）