水陆两栖飞机升降舵操纵系统操作试验技术研究及应用  

Research and Application of Operation Test Technology for Elevator Control System of Amphibious Aircraft

作　　者：张柁[1] 张园 何月洲[1] Zhang Tuo;Zhang Yuan;He Yuezhou(Full Scale Aircraft Structural Static/Fatigue Laboratory of Aircraft Strength Research Institute of China,Xi′an 710065,Shaanxi,China;Xi′an Changqing Technology Engineering Co.,Ltd.,Xi′an 710021,Shaanxi,China)

机构地区：[1]中国飞机强度研究所全尺寸飞机结构静力/疲劳实验室,陕西西安710065 [2]西安长庆科技工程有限责任公司,陕西西安710021

出　　处：《工程与试验》2021年第1期33-34,共2页Engineering and Test

摘　　要：为了真实地模拟驾驶员对升降舵的操纵,同时验证TA600飞机升降舵操纵系统对CCAR-25-R4中第683条款的符合性,提出了水陆两栖飞机升降舵操纵系统操作试验技术方法。经大型灭火/水上救援水陆两栖飞机升降舵工况试验验证,表明该方法是可行和有效的。本项目的研究成果,已应用于该型号试验中,取得了良好效果,同时也为后续试验提供了技术支撑。In order to truly simulate the pilot′s control of the elevator,and at the same time verify the compliance of the TA600 aircraft′s elevator control system to Article 683 of CCAR-25-R4,and provide the necessary basis for indicating the compliance of the provisions,an elevator control system for amphibious aircraft is proposed.The operation test technology and method have been verified by the working conditions of the large fire extinguishing/water rescue amphibious aircraft elevator rudder,which shows that the method is feasible and effective.The research results of this project have been applied to this type of test,which has achieved good results and also provided technical support for subsequent tests.

关 键 词：升降舵 操纵系统 操作试验 试验方法 

分 类 号：V216.1[航空宇航科学与技术—航空宇航推进理论与工程]