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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。
In order to increase the density of the flight, reduce the flight interval and effectively prevent the collision in the air, the ADS-B retrofit program is developed for the Robinson R44 helicopter widely used in general aviation. The emphasis is put on the mechanism strength, weight and balance, circuit load and electromagnetic Interfere with four aspects of feasibility analysis and demonstration. The results show that the program meets the installation requirements and the inherent airworthiness requirements of the aircraft.