R44II型直升机加装ADS—B系统的可行性分析  

Feasibility Analysis of Adding ADS-B System to R44 II Helicopter

作　　者：任可[1] 周彬[1] 

机构地区：[1]中国民航飞行学院新津分院

出　　处：《航空制造技术》2015年第23期111-113,共3页Aeronautical Manufacturing Technology

摘　　要：为了增大飞行密度，减小飞行间隔和有效防止空中相撞，针对广泛应用于通用航空的罗宾逊R44II型直升机制定ADS—B加装方案，并重点从机构强度、重量与平衡、电路负载和电磁干扰4个方面开展可行性分析与论证、结果表明，该方案满足加装功能要求以及航空器的固有适航性要求。For increasing the flight density, decreasing flight separation and preventing collision effectively, the ADS-B system addition scheme of the general aviation R44 II helicopter is formulated. Then, the feasibility analysis and demonstration are developed from the four aspects strength of mechanism, weight and balance, circuit load and electromagnetic interference. The results prove that the scheme can meet the additional function and the inherent airworthiness.

关 键 词：直升机 GDL90 可行性分析 

分 类 号：V275.1[航空宇航科学与技术—飞行器设计]