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51. 发明授权

US5800225A Aviation auto-inflatable life raft 失效
标题翻译：航空自动充气救生筏
公开(公告)号：US5800225A
公开(公告)日：1998-09-01
申请号：US890279
申请日：1997-07-09
申请人： Frederick B. Shoaff, III
发明人： Frederick B. Shoaff, III
IPC分类号： B63C9/02 , B63C9/04 , B64D25/16 , B63B35/58
CPC分类号： B63C9/04 , B63C9/02 , B64D25/16 , B63C2009/042 , B63C2009/044
摘要： The present invention involves an inflatable life raft for use in an aircraft. The life raft comprises an air providing device, a floor, a buoyancy tube, and a canopy. The buoyancy tube is disposed about the floor. The canopy protects survivors located on the floor, and includes a cover and an inflatable support having at least three inflatable legs attached to the buoyancy tube. The air providing device inflates the buoyancy tube and the inflatable support. The canopy cover may be positioned in at least three arrangements: a closed position, a sailing position, and a convertible position. The two layered canopy cover includes two zippered doors allowing for ingress and egress, and has a plurality of radar reflective portions. The floor has a generally round shape or a polygonal shape with at least ten sides. A second buoyancy tube is disposed on the first buoyancy tube, and both have approximately the same size. The floor comprises an insulated double floor, and is attached to a plurality of ballast bags disposed around to the outer under perimeter of the floor for stabilizing the life raft in water. A sea anchor is coupled to the lower buoyancy tube by an adjustable swiveled line. A grab handle is attached to the buoyancy tube. The floor comprises an upper floor, a lower floor, and a plurality of reeds defining a buoyancy chamber. A righting line with hand grips is mounted on the underside of the floor.
摘要翻译：本发明涉及一种用于飞行器的充气救生筏。救生筏包括空气提供装置，地板，浮力管和罩。浮力管围绕地板设置。顶篷保护位于地板上的幸存者，并且包括盖子和可充气的支撑件，其具有连接到浮力管的至少三个可充气的腿。空气提供装置使浮力管和可充气支撑件膨胀。顶篷盖可以定位在至少三种布置中：关闭位置，航行位置和可转换位置。两层天篷盖包括允许入口和出口的两个拉链门，并且具有多个雷达反射部分。地板具有至少十个边的大致圆形或多边形。第二浮力管设置在第一浮力管上，并且两者具有大致相同的尺寸。该地板包括一个绝缘的双层地板，并且附接到围绕地板的外部下边缘设置的多个安定袋，以稳定水中的救生筏。海锚通过可调节的旋转线连接到下浮体管。一把抓手连接在浮力管上。地板包括上层，下层和限定浮力室的多个簧片。在地板底部安装了一个带手柄的直线。

52. 发明公开

EP3907135A1 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.

53. 发明授权

EP2987727B1 HEATED INFLATION SYSTEM 有权
标题翻译：加热充气系统
公开(公告)号：EP2987727B1
公开(公告)日：2017-10-04
申请号：EP15181368.0
申请日：2015-08-18
申请人： Goodrich Corporation
发明人： DESHPANDE, Jayant V. , MCBURNETT III, Wilfred Ray
IPC分类号： B64D25/14 , F17C1/00 , B64D25/16 , B64F5/00 , B60R21/26 , F17C5/06
CPC分类号： B64D25/14 , B64D25/16 , B64F5/60 , F17C5/06 , F17C2201/0109 , F17C2205/0338 , F17C2205/0394 , F17C2221/013 , F17C2221/014 , F17C2221/03 , F17C2223/0123 , F17C2223/036 , F17C2227/0304 , F17C2227/0379 , F17C2250/0439 , F17C2260/026 , F17C2270/0772

54. 发明授权

EP2484585B1 Window mounted raft system 有权
标题翻译：附加到一个窗口救生筏系统
公开(公告)号：EP2484585B1
公开(公告)日：2013-04-10
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).

55. 发明授权

EP3521170B1 INTEGRAL LIFE RAFT, SURVIVAL KIT, AND STEP 有权
公开(公告)号：EP3521170B1
公开(公告)日：2020-08-19
申请号：EP18165754.5
申请日：2018-04-04
申请人： Textron Innovations 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

56. 发明公开

EP3521170A1 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).

57. 发明公开

EP2987727A1 HEATED INFLATION SYSTEM 有权
标题翻译：系统ZUM BEHEIZTEN AUFBLASEN
公开(公告)号：EP2987727A1
公开(公告)日：2016-02-24
申请号：EP15181368.0
申请日：2015-08-18
申请人： Goodrich Corporation
发明人： DESHPANDE, Jayant V. , MCBURNETT III, Wilfred Ray
IPC分类号： B64D25/14 , F17C1/00 , B64D25/16 , B64F5/00 , B60R21/26
CPC分类号： B64D25/14 , B64D25/16 , B64F5/60 , F17C5/06 , F17C2201/0109 , F17C2205/0338 , F17C2205/0394 , F17C2221/013 , F17C2221/014 , F17C2221/03 , F17C2223/0123 , F17C2223/036 , F17C2227/0304 , F17C2227/0379 , F17C2250/0439 , F17C2260/026 , F17C2270/0772
摘要： A system (100) for inflating an inflatable device (108) includes an inflation cylinder (102) configured to hold a gas mixture (104) under pressure, a heating element (110) configured to selectively heat the gas mixture (104) and a temperature sensor (112) configured to measure a temperature of the gas mixture (104). A control module (114) is coupled to the heating element (110) and the temperature sensor (112). The control module (114) controls heating of the gas mixture (104) based on the measured temperature, a mass of the gas mixture (104) and a volume of the inflation cylinder (102).
摘要翻译：用于使可膨胀装置（108）膨胀的系统（100）包括构造成在压力下保持气体混合物（104）的充气圆筒（102），配置成选择性地加热气体混合物（104）的加热元件（110）温度传感器（112）被配置为测量气体混合物（104）的温度。控制模块（114）耦合到加热元件（110）和温度传感器（112）。控制模块（114）基于所测量的温度，气体混合物（104）的质量和膨胀气缸（102）的体积来控制气体混合物（104）的加热。

58. 发明公开

EP2484585A1 Window mounted raft system 有权
标题翻译： 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。

59. 发明公开

EP4201808A1 EMERGENCY DEVICE ACTUATION ASSEMBLIES AND AIRCRAFT INCLUDING SAME 审中-公开
公开(公告)号：EP4201808A1
公开(公告)日：2023-06-28
申请号：EP22215607.7
申请日：2022-12-21
申请人： Embraer S.A.
发明人： LIVORATTI, João Carlos , MARASTONI, Carlo Rodrigo de Faria , DOS REIS, Mariana Camargo , RODRIGUES, Juliana Fabricio
IPC分类号： B64C1/14 , B64D25/16 , B63C9/01
摘要： Actuation assemblies for emergency devices (e.g., inflatable life rafts carried on-board an aircraft) are provided with enhanced (preferably multiple) levels of security to preclude inadvertent unlatching and/or deployment but also allow access to an on-board emergency device removably positioned within a device bay of the vehicle which is normally covered by an access panel. The actuation assembly may be provided with a rotatable actuation shaft, a manually operated actuation lever fixed to the actuation shaft so as to rotate the actuation shaft in response to movement of the actuation lever between stowed and deployed conditions thereof, and a safety locking system operably connected to the rotatable shaft and having a locked condition which prevents operation of the actuation lever to thereby maintain the actuation assembly in a safe mode during normal vehicle operation, and an armed mode which allows the actuation lever to be moved into the deployed condition thereof.

60. 发明授权

EP3904215B1 A LIFE RAFT SYSTEM FOR AN AIRCRAFT 有权
公开(公告)号：EP3904215B1
公开(公告)日：2022-12-28
申请号：EP20400006.1
申请日：2020-04-30
发明人： Harms, Stefan
IPC分类号： B64D25/16 , B63C9/22 , B64C27/04

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