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    IN-FLIGHT EMERGENCY EVACUATION SYSTEM
    1.
    发明公开
    IN-FLIGHT EMERGENCY EVACUATION SYSTEM 审中-公开

    公开(公告)号：US20230142872A1

    公开(公告)日：2023-05-11

    申请号：US17522962

    申请日：2021-11-10

    申请人： Aymen Alfadil

    发明人： Aymen Alfadil

    IPC分类号： B64D25/10 ,  B64D11/06

    CPC分类号： B64D25/10 ,  B64D11/0616 ,  B64D11/0696

    摘要： The invention provides an in-flight emergency evacuation system in an aircraft which has a seating area comprising of plurality of rows of passenger seats which are positioned on plurality of rails. The passenger seats are slidably movable on the rails. The system further discloses at least one emergency room which is configured to accommodate the passenger seats inside it during an emergency condition for safely ejecting the passengers outside of the emergency rooms. During an emergency condition, the crew members of the aircraft can hit the evacuation button which automatically starts the evacuation process. Once the evacuation button is pressed, the slidably movable motorized passenger seats which are positioned on the rails starts moving in a sequential manner into the emergency room which is capable of accommodating one row of passenger seats at a time and ejecting it outside the aircraft.

    TEMPORARILY-INSTALLED AIRCRAFT OBSERVER DOOR PLUG, CHAIR, SONOTUBE EJECTION AND CONTROL SYSTEM
    2.
    发明申请
    TEMPORARILY-INSTALLED AIRCRAFT OBSERVER DOOR PLUG, CHAIR, SONOTUBE EJECTION AND CONTROL SYSTEM 审中-公开
    经过安装的飞机观察门插座，椅子，SONOTUBE喷射和控制系统

    公开(公告)号：US20160347478A1

    公开(公告)日：2016-12-01

    申请号：US15232661

    申请日：2016-08-09

    申请人： 1281329 Alberta Ltd.

    发明人： Richard L.K. Woodland ,  Ross J. Neyedly

    IPC分类号： B64F5/00 ,  B64D1/02 ,  B64C1/20 ,  B64D11/06 ,  B64C1/14

    CPC分类号： B64C1/1407 ,  B64C1/1484 ,  B64C1/18 ,  B64C1/20 ,  B64D1/02 ,  B64D11/06 ,  B64D11/0616 ,  B64D11/062

    摘要： In one embodiment, a non-dedicated, temporarily-installed, aircraft observer bubble door, chair, sonotube ejection system, mission electronics LRU rack and workstation assembly are affixed to a host aircraft, thereby precluding the requirement for dedicated airframe modifications. One embodiment of the present invention also utilizes a multi-axis, articulated, foldable chair temporarily-installed in conjunction with a segmented or one piece pressurized observer bubble door plug and door retraction system. Once installed the subject apparatus can be stowed outboard of the fuselage cargo transit envelope to permit use of the ADS rail system in-flight, without affecting normal air drop operations, crew egress, the flight performance envelope, or emergency procedures of the host aircraft.

    摘要翻译： 在一个实施例中，非专用的，暂时安装的飞行器观察者气泡门，椅子，超声波管喷射系统，任务电子装置LRU机架和工作站组件被固定到主机上，从而排除了对专用机身修改的要求。 本发明的一个实施例还使用与分段或单件加压观察者气泡门塞和门退缩系统暂时安装的多轴，铰接的可折叠椅子。 一旦安装，主体设备可以被存放在机身货物运输信封的外侧，以允许在飞行中使用ADS轨道系统，而不影响主机飞机的正常降落操作，机组人员出口，飞行性能包络或应急程序。

    Temporarily-installed aircraft observer door plug, chair, sonotube ejection and control system
    4.
    发明授权
    Temporarily-installed aircraft observer door plug, chair, sonotube ejection and control system 有权
    临时安装的飞机观察者门插头，椅子，超声波发射和控制系统

    公开(公告)号：US09567058B2

    公开(公告)日：2017-02-14

    申请号：US13738935

    申请日：2013-01-10

    申请人： 1281329 Alberta Ltd.

    发明人： Richard L. K. Woodland ,  Ross James Neyedly

    IPC分类号： B64C1/22 ,  B64C1/14 ,  B64D11/06 ,  B64D1/02 ,  B64C1/18 ,  B64C1/20

    CPC分类号： B64C1/1407 ,  B64C1/1484 ,  B64C1/18 ,  B64C1/20 ,  B64D1/02 ,  B64D11/06 ,  B64D11/0616 ,  B64D11/062

    摘要： The system and apparatus of the present invention is generally comprised of a non-dedicated, temporarily-installed, aircraft observer bubble door, chair, sonotube ejection system, mission electronics LRU rack and workstation assembly which are affixed to the Air Deployment System (ADS) rails, cargo tie down “D” rings, seat belt restraint ring bolt sockets, and litter bar of a host aircraft, thereby precluding the requirement for dedicated airframe modifications. One embodiment of the present invention also utilizes a multi-axis, articulated, foldable chair temporarily-installed in conjunction with a segmented or one piece pressurized observer bubble door plug and door refraction system. Once installed the subject apparatus can be stowed outboard of the fuselage cargo transit envelope to permit use of the ADS rail system in-flight, without affecting normal air drop operations, crew egress, the flight performance envelope, or emergency procedures of the host aircraft.

    摘要翻译： 本发明的系统和装置通常包括固定在空中部署系统（ADS）上的非专用的，暂时安装的飞行器观察者气泡门，椅子，超声波发射系统，任务电子装置LRU机架和工作站组件， 轨道，货物捆扎“D”环，安全带约束环螺栓插座和主机飞机的垃圾条，从而排除了对专用机身修改的要求。 本发明的一个实施例还使用与分段或单件加压观察器气泡门塞和门折射系统暂时安装的多轴，铰接的可折叠椅子。 一旦安装，主体设备可以被存放在机身货物运输信封的外侧，以允许在飞行中使用ADS轨道系统，而不影响主机飞机的正常降落操作，机组人员出口，飞行性能包络或应急程序。

    Temporarily-installed aircraft observer door plug, chair, sonotube ejection and control system
    9.
    发明授权
    Temporarily-installed aircraft observer door plug, chair, sonotube ejection and control system 有权
    临时安装的飞机观察者门插头，椅子，超声波发射和控制系统

    公开(公告)号：US09567060B2

    公开(公告)日：2017-02-14

    申请号：US15232661

    申请日：2016-08-09

    申请人： 1281329 Alberta Ltd.

    发明人： Richard L. K. Woodland ,  Ross J. Neyedly

    IPC分类号： B64C1/22 ,  B64C1/14 ,  B64C1/20 ,  B64D1/02 ,  B64C1/18 ,  B64D11/06

    CPC分类号： B64C1/1407 ,  B64C1/1484 ,  B64C1/18 ,  B64C1/20 ,  B64D1/02 ,  B64D11/06 ,  B64D11/0616 ,  B64D11/062

    摘要： In one embodiment, a non-dedicated, temporarily-installed, aircraft observer bubble door, chair, sonotube ejection system, mission electronics LRU rack and workstation assembly are affixed to a host aircraft, thereby precluding the requirement for dedicated airframe modifications. One embodiment of the present invention also utilizes a multi-axis, articulated, foldable chair temporarily-installed in conjunction with a segmented or one piece pressurized observer bubble door plug and door retraction system. Once installed the subject apparatus can be stowed outboard of the fuselage cargo transit envelope to permit use of the ADS rail system in-flight, without affecting normal air drop operations, crew egress, the flight performance envelope, or emergency procedures of the host aircraft.

    摘要翻译： 在一个实施例中，非专用的，暂时安装的飞行器观察者气泡门，椅子，超声波管喷射系统，任务电子装置LRU机架和工作站组件被固定到主机上，从而排除了对专用机身修改的要求。 本发明的一个实施例还使用与分段或单件加压观察者气泡门塞和门退缩系统暂时安装的多轴，铰接的可折叠椅子。 一旦安装，主体设备可以被存放在机身货物运输信封的外侧，以允许在飞行中使用ADS轨道系统，而不影响主机飞机的正常降落操作，机组人员出口，飞行性能包络或应急程序。

    PASSENGER CONTROL CENTER
    10.
    发明申请
    PASSENGER CONTROL CENTER 审中-公开
    乘客控制中心

    公开(公告)号：US20160137301A1

    公开(公告)日：2016-05-19

    申请号：US14546506

    申请日：2014-11-18

    申请人： Anthony J. Jackson

    发明人： Anthony J. Jackson

    IPC分类号： B64D11/06

    CPC分类号： B64D11/0602 ,  B64D11/0616 ,  B64D25/12 ,  Y02T50/55

    摘要： A passenger control center for an airplane comprising: a pair of seats; a dome enclosing the pair of seats; a base supporting the dome and the pair of seats; a solar panel on a top surface of the dome; a back panel for the dome, where the back panel stores a parachute; a hinge along a rear edge of the base; and a beacon warning indicator in the center of the solar panel. The passenger control center serves as means to survive an accident or emergency on an aircraft. The passenger control center is preferably ejectable and thus provides a means for safe escape and survival of an air disaster

    摘要翻译： 一种用于飞机的乘客控制中心，包括：一对座位; 一个包围这对座位的圆顶; 一个支撑圆顶和一对座位的基座; 在圆顶的顶面上的太阳能电池板; 后面板用于圆顶，后面板存放降落伞; 沿着基座的后边缘的铰链; 以及太阳能电池板中心的信标警告指示灯。 乘客控制中心作为在飞机上事故或紧急情况下生存的手段。 乘客控制中心优选是可弹出的，因此提供了安全逃生和空难的生存手段