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15 条记录 (耗时 0.014 秒)

    A LIFE RAFT SYSTEM FOR AN AIRCRAFT
    1.
    发明公开
    A LIFE RAFT SYSTEM FOR AN AIRCRAFT 审中-公开

    公开(公告)号：EP3904215A1

    公开(公告)日：2021-11-03

    申请号：EP20400006.1

    申请日：2020-04-30

    申请人： AIRBUS HELICOPTERS DEUTSCHLAND GmbH

    发明人： Harms, Stefan

    IPC分类号： B64D25/16 ,  B63C9/22 ,  B64C27/04

    摘要： The invention is related to a life raft system 20 for an aircraft 10, comprising a storage container 21; an inflatable life raft 22 that is stored in the storage container 21 in normal operation mode, an inflation device 23 for inflating the inflatable life raft 22 in an emergency mode, and a control unit 24 for activating the inflation device 23 in the emergency mode; wherein the control unit 24 comprises a floatable control buoy 25 with an activation member that is operable for activating the inflation device 23, wherein the floatable control buoy 25 is provided for operation at a predetermined distance remote from an associated aircraft 10 in an emergency mode.

    METHOD OF CREATING AN EMERGENCY EGRESS IN A VEHICLE, EMERGENCY EGRESS AND VEHICLE
    2.
    发明公开
    METHOD OF CREATING AN EMERGENCY EGRESS IN A VEHICLE, EMERGENCY EGRESS AND VEHICLE 审中-公开

    公开(公告)号：EP4417508A1

    公开(公告)日：2024-08-21

    申请号：EP23156626.6

    申请日：2023-02-14

    申请人： Volocopter GmbH

    发明人： Grimm, Tobias ,  Rodriguez, Javier

    IPC分类号： B64C1/32 ,  B64D25/08 ,  B64D25/12 ,  B64D25/14 ,  B64D25/16

    CPC分类号： B64C1/32

    摘要： We describe a method of creating an emergency egress (1) in a vehicle, in particular in an aircraft, comprising:
    a) providing a vehicle having an emergency egress opening in its chassis or fuselage (3);
    b) attaching at least one cover panel (2) to said chassis or fuselage (3), in particular in an edge region of said emergency egress opening, which cover panel (2) at least partly covers said emergency egress opening;
    c) embedding in a contact region of said cover panel (2) and said chassis or fuselage (3), either in an interface layer (4) between said cover panel (2) and said chassis or fuselage (3) or in said cover panel (2), at least one fluid-tight bag (4b) in a folded-in or deflated state thereof;
    d) inflating said bag (4b) by injecting a fluid under pressure (pi') into said bag (4b);
    e) removing said cover panel (2) from said chassis or fuselage (3).
    Further described are an emergency egress (1) and a vehicle having same.

    A LIFE RAFT SYSTEM FOR AN AIRCRAFT
    4.
    发明公开
    A LIFE RAFT SYSTEM FOR AN AIRCRAFT 审中-公开

    公开(公告)号：EP3907135A1

    公开(公告)日：2021-11-10

    申请号：EP20211003.7

    申请日：2020-04-30

    申请人： AIRBUS HELICOPTERS DEUTSCHLAND GmbH

    发明人： HARMS, Stefan

    IPC分类号： B64D25/16 ,  B63C9/22 ,  B64C27/04

    摘要： The invention is related to a life raft system 20 for an aircraft, comprising a storage container 21; an inflatable life raft that is stored in the storage container 21 in normal operation mode, an inflation device for inflating the inflatable life raft in an emergency mode, and a control unit 24 for activating the inflation device in the emergency mode; wherein the control unit 24 comprises a floatable control buoy 25 with an activation member 27a that is operable for activating the inflation device; wherein the floatable control buoy 25 is provided for operation at a predetermined distance remote from an associated aircraft in an emergency mode; and wherein an ejection device 30 is provided that is configured to eject the floatable control buoy 25 from an associated storage compartment 25b in an emergency mode.

    INTEGRAL LIFE RAFT, SURVIVAL KIT, AND STEP
    8.
    发明公开
    INTEGRAL LIFE RAFT, SURVIVAL KIT, AND STEP 审中-公开

    公开(公告)号：EP3521170A1

    公开(公告)日：2019-08-07

    申请号：EP18165754.5

    申请日：2018-04-04

    申请人： Bell Helicopter Textron Inc.

    发明人： HAUGEBERG, Chad Richard ,  CARR, Timothy ,  DESLATTE, Michael Stephen

    IPC分类号： B64D25/16 ,  B63B7/08 ,  B63B23/62 ,  B63C9/22 ,  B63C9/23

    摘要： An embodiment rotorcraft (101) structure includes a step (201a, 201b) disposed at an exterior of the rotorcraft (101), and an emergency kit (301a, 301b) installed into the recess of the step (201a, 201b). The step is faired into a skin (126) on the exterior of the rotorcraft (101). The emergency kit (301a, 301b) includes a container and a life raft. The container includes a container body that has a storage cavity, a container panel, and a first attachment element. The container body is disposed in the recess of the step, attached to the step, and has a storage cavity. The container panel is disposed at a bottom of the storage cavity, and the life raft is disposed in the storage cavity. The first attachment element releasably couples a first edge of the container panel to the container body, and encloses the life raft in the container under the step (201a, 201b).

    Window mounted raft system
    10.
    发明公开
    Window mounted raft system 有权
    einem Fenster angebrachtes Rettungsinsels系统

    公开(公告)号：EP2484585A1

    公开(公告)日：2012-08-08

    申请号：EP12153729.4

    申请日：2012-02-02

    申请人： Bell Helicopter Textron Inc.

    发明人： Lafton, Brian D. ,  Capwell, Robert G.

    IPC分类号： B64C1/14 ,  B64D25/16

    CPC分类号： B64D25/16 ,  B63C9/04 ,  B63C2009/042 ,  B64C1/1484

    摘要： An inflatable life raft system (215) for an aircraft (201) includes a window (221, 217) coupled to a fuselage portion (223) of the aircraft. A mechanism is used to selectively detach the window (221, 217) from the fuselage. An inflatable life raft (249) is deployable to the exterior of the aircraft upon detachment of the window (221, 217) from the aircraft (201).

    摘要翻译： 用于飞机（201）的可充气救生筏系统（215）包括联接到飞行器的机身部分（223）的窗口（221,217）。 使用机构来选择性地将窗口（221,217）与机身分离。 当窗户（221,217）从飞行器（201）分离时，充气救生筏（249）可部署到飞行器的外部。