The invention relates to a rescue system of a fixed-wing aircraft, which comprises a hardware component and a software component, the hardware component is composed of an emergency automatic control system, a multifunctional communication system, a sensor combination suite, a life support system and an AI auxiliary system; the software assembly is composed of an environment sensing unit, a data analysis unit, a rescue operation management unit, a real-time monitoring unit, an emergency track calculation unit and an emergency communication unit. According to the system, various technologies are integrated, the system is used for flight protection and assistance in emergency situations, the system integrates the capabilities of hardware and software, and real-time flight monitoring, automatic navigation, multi-channel communication, automatic emergency program processing and surrounding environment sensing are provided. The flight safety can be greatly improved, the accident risk is reduced, an effective solution can be provided in an emergency state, and the safety of passengers is improved.

    本发明涉及一种固定翼飞机的救援系统,包括硬件组件和软件组件,所述硬件组件由紧急自动控制系统、多功能通信系统、传感器组合套件、生命支撑系统和AI辅助系统组成;所述软件组件由环境感知单元、数据分析单元、救援操作管理单元、实时监测单元、紧急航迹计算单元和紧急通信单元组成。本发明集成了各项技术,用于应对紧急情况下的飞行保护和协助,系统融合了硬件和软件的能力,提供实时的飞行监控、自动导航、多渠道通信、自动处理紧急程序和感知周围环境,总得来说,本系统通过将各种技术融为一体,不仅可以极大的提升飞行安全、降低事故风险,并在紧急状态下可以提供有效的解决方案,提高乘员的安全性。


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    Titel :

    Rescue system of fixed-wing aircraft


    Weitere Titelangaben:

    一种固定翼飞机的救援系统


    Beteiligte:
    FU QIANG (Autor:in) / WANG JIAN (Autor:in) / ZHANG XIA (Autor:in)

    Erscheinungsdatum :

    2024-05-28


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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