直升机H-V包线拓展飞行试验方法研究  

Research into Helicopter H-V Envelope Expansion Flight Test Method

作　　者：王勇[1] 孙光[1] 陈永禄[2] 

机构地区：[1]中国人民解放军95966部队 [2]中国飞行试验研究院

出　　处：《西安航空学院学报》2016年第3期21-24,共4页Journal of Xi’an Aeronautical Institute

摘　　要：直升机H-V包线是直升机在发动机失效后安全着陆或成功复飞的基础条件。指出了影响H-V包线范围的主要因素是重量相对密度比(W/σ),提出了直升机H-V包线拓展试飞方法,针对某型机进行了H-V包线下边界拓展和上边界拓展飞行试验,分析飞行试验结果,给出了H-V包线图,并明确了H-V包线拓展飞行关键技术和注意事项,有助于其他直升机H-V包线拓展飞行试验的顺利开展。The H-V envelope is the basic condition for the safe landing or successful miss-approach of helicopters after the failure of engine.The paper points out the main factor affecting H-V envelope,namely relative density in weight ratio(W/σ),puts forward the helicopter H-V envelope expansion flight method,and uses a certain type of helicopters to conduct H-V boundary expansion flight test.At last,the paper analyzes the flight test results,presents the H-V package diagram,and clarifies the key technologies and the precautions of H-V envelope expansion flight,which is helpful for the smooth implementation of H-V envelope expansion flight tests of other types of helicopters.

关 键 词：H-V包线 飞行试验 边界拓展 

分 类 号：V217[航空宇航科学与技术—航空宇航推进理论与工程] V275.1