某型飞机加装GI275备用仪表系统的可行性分析  

Feasibility Analysis of Installing GI275 Standby Instrument System to Certain Aircraft

作　　者：张一夫 包迪 税远平 彭友 胡凌霄 Zhang Yifu;Bao Di;Shui Yuanping;Peng You;Hu Lingxiao(Xinjin Flight College,Civil Aviation Flight University of China,Chengdu 611430 Sichuan China;Civil Aviation Flight University of China,Guanghan 618307 Sichuan China)

机构地区：[1]中国民用航空飞行学院新津分院,四川成都611430 [2]中国民用航空飞行学院,四川广汉618307

出　　处：《中国民航飞行学院学报》2025年第1期25-27,共3页Journal of Civil Aviation Flight University of China

基　　金：中国民用航空飞行学院面上基金项目(J2023-076)。

摘　　要：针对通用航空领域广泛使用的某型飞机制定GI275备用仪表系统加装方案,并重点从系统兼容性、结构强度、重量与平衡等方面开展可行性分析与论证。经过理论分析和试验验证,该方案满足加装功能要求以及航空器的固有适航性要求。The installation scheme of the GI275 standby instrument system is formulated for a certain aircraft that is widely used in general aviation.Feasibility analysis and demonstration are carried out from the perspectives of system compatibility,structural strength and weight and balance.The results indicate that the scheme meets the functional requirements and the inherent airworthiness requirements of the aircraft.

关 键 词：备用仪表 可行性分析 适航性 

分 类 号：V241[航空宇航科学与技术—飞行器设计]