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    EMERGENCY MECHANICAL AND COMMUNICATION SYSTEMS AND METHODS FOR AIRCRAFT
    3.
    发明申请
    EMERGENCY MECHANICAL AND COMMUNICATION SYSTEMS AND METHODS FOR AIRCRAFT 有权
    紧急机械和通信系统和飞机方法

    公开(公告)号：US20170029128A1

    公开(公告)日：2017-02-02

    申请号：US15226176

    申请日：2016-08-02

    Applicant: COMAC AMERICA CORPORATION

    Inventor： Wei Ye ,  Jianhong Sun

    IPC: B64D25/20 ,  G07C5/08 ,  B64D3/00 ,  B64D1/14 ,  B64D47/08 ,  G07C5/00 ,  B64D17/00

    CPC classification number: B64D25/20 ,  B64D1/14 ,  B64D3/00 ,  B64D17/00 ,  B64D45/00 ,  B64D47/08 ,  B64D2045/0065 ,  B65H2701/34 ,  G06F1/18 ,  G07C5/008 ,  G07C5/0858

    Abstract: A system for rapid separation of a flight data recorder from an aircraft comprises a flight data recorder; an emergency detection system comprising a plurality of sensors for detecting flight parameters and at least one computer processor for analyzing the flight parameters and determining, based on the analysis, that an emergency event is occurring; a rapid ejection system comprising a pneumatic system configured to eject the flight data recorder out of an opening in a housing and through the skin of the aircraft when the emergency detection system determines that the emergency event is occurring; and a soft landing system, said soft landing system being attached to the flight data recorder and configured to reduce force of impact upon landing and increase buoyancy of the flight data recorder.

    Abstract translation: 飞行数据记录器与飞机快速分离的系统包括飞行数据记录器; 紧急检测系统，包括用于检测飞行参数的多个传感器和用于分析飞行参数的至少一个计算机处理器，并且基于分析确定发生紧急事件; 一种快速喷射系统，包括气动系统，其构造成当紧急检测系统确定紧急事件发生时，将飞行数据记录器从壳体中的开口中弹出并穿过飞行器的皮肤; 和软着陆系统，所述软着陆系统附接到飞行数据记录器并且被配置为减少着陆时的冲击力并增加飞行数据记录器的浮力。

    Emergency mechanical and communication systems and methods for aircraft
    4.
    发明授权
    Emergency mechanical and communication systems and methods for aircraft 有权
    飞机紧急机械和通信系统和方法

    公开(公告)号：US09452844B1

    公开(公告)日：2016-09-27

    申请号：US15060372

    申请日：2016-03-03

    Applicant: COMAC AMERICA CORPORATION

    Inventor： Wei Ye ,  Jianhong Sun

    IPC: B64D25/20 ,  B64D45/00 ,  G07C5/00 ,  B64D47/08 ,  G07C5/08 ,  B64D1/14

    CPC classification number: B64D25/20 ,  B64D1/14 ,  B64D3/00 ,  B64D17/00 ,  B64D45/00 ,  B64D47/08 ,  B64D2045/0065 ,  B65H2701/34 ,  G06F1/18 ,  G07C5/008 ,  G07C5/0858

    Abstract: A system for quickly locating and retrieving flight data of an aircraft after an aircraft mid-air mishap comprises: a flight data recorder; a tracking device comprising at least one camera; a rapid ejection system for ejecting the flight data recorder and tracking device; a soft landing system; and a tow system, wherein the tow system is configured to continue to transmit flight information from the aircraft to the tracking device via the data communication link for a period of time after the ejection of the tracking device; and wherein the tracking device transmits to the flight data recorder the flight information received from the aircraft after ejection and the images captured by the tracking device immediately following the mid-air mishap, and wherein the flight data recorder is configured to in turn transmit said flight information and images to the remote device.

    Abstract translation: 一种用于在飞机空中事故之后快速定位和检索飞行器的飞行数据的系统包括：飞行数据记录器; 跟踪装置，包括至少一个相机; 用于喷射飞行数据记录器和跟踪装置的快速排出系统; 软着陆系统; 以及牵引系统，其中所述牵引系统被配置为在所述跟踪装置的弹出之后的一段时间内，经由所述数据通信链路继续将飞行信息从所述飞机传送到所述跟踪装置; 并且其中所述跟踪装置向所述飞行数据记录器发送在所述飞行数据记录器之后从所述飞行器接收的飞行信息和由所述跟踪装置在所述空中事故之后立即捕获的图像，并且其中所述飞行数据记录器被配置为依次将所述飞行 信息和图像到远程设备。

    Emergency mechanical and communication systems and methods for aircraft
    5.
    发明授权
    Emergency mechanical and communication systems and methods for aircraft 有权
    飞机紧急机械和通信系统和方法

    公开(公告)号：US09440749B1

    公开(公告)日：2016-09-13

    申请号：US15060367

    申请日：2016-03-03

    Applicant: COMAC AMERICA CORPORATION

    Inventor： Wei Ye ,  Jianhong Sun

    IPC: G06F7/70 ,  B64D45/00 ,  G07C5/00 ,  G07C5/08

    CPC classification number: B64D25/20 ,  B64D1/14 ,  B64D3/00 ,  B64D17/00 ,  B64D45/00 ,  B64D47/08 ,  B64D2045/0065 ,  B65H2701/34 ,  G06F1/18 ,  G07C5/008 ,  G07C5/0858

    Abstract: A system for rapid separation of a flight data recorder from an aircraft comprises a flight data recorder; an emergency detection system comprising a plurality of sensors for detecting flight parameters and at least one computer processor for analyzing the flight parameters and determining, based on the analysis, that an emergency event is occurring; a rapid ejection system comprising a pneumatic system configured to eject the flight data recorder out of an opening in a housing and through the skin of the aircraft when the emergency detection system determines that the emergency event is occurring; and a soft landing system, said soft landing system being attached to the flight data recorder and configured to reduce force of impact upon landing and increase buoyancy of the flight data recorder.

    Abstract translation: 飞行数据记录器与飞机快速分离的系统包括飞行数据记录器; 紧急检测系统，包括用于检测飞行参数的多个传感器和用于分析飞行参数的至少一个计算机处理器，并且基于分析确定发生紧急事件; 一种快速喷射系统，包括气动系统，其构造成当紧急检测系统确定紧急事件发生时，将飞行数据记录器从壳体中的开口中弹出并穿过飞行器的皮肤; 和软着陆系统，所述软着陆系统附接到飞行数据记录器并且被配置为减少着陆时的冲击力并增加飞行数据记录器的浮力。

    EMERGENCY MECHANICAL AND COMMUNICATION SYSTEMS AND METHODS FOR AIRCRAFT
    8.
    发明申请
    EMERGENCY MECHANICAL AND COMMUNICATION SYSTEMS AND METHODS FOR AIRCRAFT 有权
    紧急机械和通信系统和飞机方法

    公开(公告)号：US20160257421A1

    公开(公告)日：2016-09-08

    申请号：US15060367

    申请日：2016-03-03

    Applicant: COMAC AMERICA CORPORATION

    Inventor： Wei Ye ,  Jianhong Sun

    IPC: B64D45/00 ,  G07C5/08 ,  G07C5/00

    CPC classification number: B64D25/20 ,  B64D1/14 ,  B64D3/00 ,  B64D17/00 ,  B64D45/00 ,  B64D47/08 ,  B64D2045/0065 ,  B65H2701/34 ,  G06F1/18 ,  G07C5/008 ,  G07C5/0858

    Abstract: A system for rapid separation of a flight data recorder from an aircraft comprises a flight data recorder; an emergency detection system comprising a plurality of sensors for detecting flight parameters and at least one computer processor for analyzing the flight parameters and determining, based on the analysis, that an emergency event is occurring; a rapid ejection system comprising a pneumatic system configured to eject the flight data recorder out of an opening in a housing and through the skin of the aircraft when the emergency detection system determines that the emergency event is occurring; and a soft landing system, said soft landing system being attached to the flight data recorder and configured to reduce force of impact upon landing and increase buoyancy of the flight data recorder.

    Abstract translation: 飞行数据记录器与飞机快速分离的系统包括飞行数据记录器; 紧急检测系统，包括用于检测飞行参数的多个传感器和用于分析飞行参数的至少一个计算机处理器，并且基于分析确定发生紧急事件; 一种快速喷射系统，包括气动系统，其构造成当紧急检测系统确定紧急事件发生时，将飞行数据记录器从壳体中的开口中弹出并穿过飞行器的皮肤; 和软着陆系统，所述软着陆系统附接到飞行数据记录器并且被配置为减少着陆时的冲击力并增加飞行数据记录器的浮力。

    EMERGENCY MECHANICAL AND COMMUNICATION SYSTEMS AND METHODS FOR AIRCRAFT
    9.
    发明申请
    EMERGENCY MECHANICAL AND COMMUNICATION SYSTEMS AND METHODS FOR AIRCRAFT 有权
    紧急机械和通信系统和飞机方法

    公开(公告)号：US20160257415A1

    公开(公告)日：2016-09-08

    申请号：US15060372

    申请日：2016-03-03

    Applicant: COMAC AMERICA CORPORATION

    Inventor： Wei Ye ,  Jianhong Sun

    IPC: B64D25/20 ,  B64D47/08 ,  G07C5/00 ,  B64D1/14 ,  B64D45/00 ,  G07C5/08

    CPC classification number: B64D25/20 ,  B64D1/14 ,  B64D3/00 ,  B64D17/00 ,  B64D45/00 ,  B64D47/08 ,  B64D2045/0065 ,  B65H2701/34 ,  G06F1/18 ,  G07C5/008 ,  G07C5/0858

    Abstract: A system for quickly locating and retrieving flight data of an aircraft after an aircraft mid-air mishap comprises: a flight data recorder; a tracking device comprising at least one camera; a rapid ejection system for ejecting the flight data recorder and tracking device; a soft landing system; and a tow system, wherein the tow system is configured to continue to transmit flight information from the aircraft to the tracking device via the data communication link for a period of time after the ejection of the tracking device; and wherein the tracking device transmits to the flight data recorder the flight information received from the aircraft after ejection and the images captured by the tracking device immediately following the mid-air mishap, and wherein the flight data recorder is configured to in turn transmit said flight information and images to the remote device.

    Abstract translation: 一种用于在飞机空中事故之后快速定位和检索飞行器的飞行数据的系统包括：飞行数据记录器; 跟踪装置，包括至少一个相机; 用于喷射飞行数据记录器和跟踪装置的快速排出系统; 软着陆系统; 以及牵引系统，其中所述牵引系统被配置为在所述跟踪装置的弹出之后的一段时间内，经由所述数据通信链路继续将飞行信息从所述飞机传送到所述跟踪装置; 并且其中所述跟踪装置向所述飞行数据记录器发送在所述飞行数据记录器之后从所述飞行器接收的飞行信息和由所述跟踪装置在所述空中事故之后立即捕获的图像，并且其中所述飞行数据记录器被配置为依次将所述飞行 信息和图像到远程设备。

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