摘要
本文分析了民用适航规章当中对于襟缝翼控制计算机的适航要求,提出了针对襟缝翼控制计算机硬件架构和余度设计要求,以及选用复杂电子硬件的额外设计要求。以某型襟缝翼控制计算机硬件架构设计为例,详细阐述了硬件架构和余度设计要求的实现与落实,为襟缝翼控制计算机的设计工作提供了参考与借鉴,也为飞控系统控制计算机的设计提供了思路与指导。
This paper analyzes the airworthiness requirements of Slat Flup Control Computer(SFCC)in civil airworthiness regulations,and put forward the hardware architecture and redundancy design requirements for the SFCC,as well as the additional design requirements for the selection of complex electronic hardware.The realization and implementation of hardware architecture and redundancy design requirements are described in detail by taking the hardware architecture design of a certain type of SFCC as an example,which provides reference for the design of SFCC,and also guidance for the design of flight control system control computer.
作者
张昭
秦怀磊
隋立军
李元元
刘敏
王宇
Zhang Zhao;Qin Huailei;Sui Lijun;Li Yuanyuan;Liu Min;Wang Yu(AVIC China Aero-Polytechnology Establishment,Beijing 100028,China;AVIC Qing’an Group Co.,Ltd.,Xi’an 710077,China;AVIC Xi’an Flight Automatic Control Research Institute,Xi’an 710076,China;Xi’an Aircraft Certification Center,Airworthiness Certification Center of CAAC,Xi’an 710065,China)
出处
《航空科学技术》
2023年第4期61-65,共5页
Aeronautical Science & Technology
