公开(公告)号：US08408494B2

公开(公告)日：2013-04-02

申请号：US12735176

申请日：2008-04-23

Applicant: Camilo Garcia Rojo

Inventor： Camilo Garcia Rojo

IPC: B64C1/10

CPC classification number: B60R21/01 ,  B60R21/16 ,  B60R2021/0093 ,  B60R2021/23107 ,  B64D25/00 ,  B64D25/02 ,  B64D2201/00

Abstract: The invention relates to an airbag system for aircraft, intended to protect crew and passengers. The system comprises: inflatable cushions; a supply of air from individual tanks, communal tanks and the aircraft APU; a connection to the landing gear and the altimeter; a manual switch; an approach and contact sensor enabling automatic activation; electric lines, electrovalves and air ducts. The system also includes a second version which is activated using electrochemical batteries which operate on the basis of sharp deceleration.

Abstract translation: 本发明涉及一种用于飞机的气囊系统，旨在保护船员和乘客。 该系统包括：充气垫; 来自各坦克，公共坦克和飞机APU的空气供应; 与起落架和高度计的连接; 手动开关; 一种能够自动激活的方法和接触式传感器; 电线，电动阀和风道。 该系统还包括使用基于急剧减速操作的电化学电池来激活的第二版本。

公开(公告)号：US08403361B2

公开(公告)日：2013-03-26

申请号：US13227382

申请日：2011-09-07

Applicant: Ronald A. Shields

Inventor： Ronald A. Shields

IPC: B60R21/18

CPC classification number: B60R22/48 ,  B60R21/01546 ,  B60R2022/4816 ,  B64D11/062 ,  B64D11/06205 ,  B64D2201/00

Abstract: Systems for indicating the status of a seatbelt buckle prior to a protective response are disclosed herein. An airbag activation system configured in accordance with one embodiment of the disclosure includes a normally closed magnetically operated reed switch. The reed switch is attached to a connector carried on one portion of a seatbelt, and a magnet is attached to a buckle carried on another portion of the seatbelt. Coupling the connector to the buckle causes the magnetic field of the magnet to move the reed switch from the normally closed position to an open position, thereby enabling the activation system to inflate the airbag in the event of an accident.

Abstract translation: 本文公开了用于在保护性响应之前指示安全带扣的状态的系统。 根据本公开的一个实施例配置的气囊激活系统包括常闭磁性操作的簧片开关。 簧片开关连接到承载在安全带的一部分上的连接器，并且磁体附接到承载在安全带的另一部分上的带扣。 将连接器耦合到带扣将导致磁体的磁场将簧片开关从常闭位置移动到打开位置，从而使得启动系统能够在发生事故时使气囊膨胀。

公开(公告)号：US20130062465A1

公开(公告)日：2013-03-14

申请号：US13696970

申请日：2011-02-23

Applicant: Andrew T. Hill ,  Zi Lu ,  Robert S. Lynds ,  Andrew R. Hansen

Inventor： Andrew T. Hill ,  Zi Lu ,  Robert S. Lynds ,  Andrew R. Hansen

IPC: B64D25/00 ,  C06D5/00

CPC classification number: B64D25/00 ,  B64C25/52 ,  B64C2025/325 ,  B64D2201/00

Abstract: An external airbag for an aircraft includes an inflatable bladder having a top portion and a bottom portion, the top portion being generally adjacent to an exterior of the aircraft. A widthwise panel divides the inflatable bladder into a first cylindrical portion and a second cylindrical portion. The widthwise panel acts to restrict outward bulging of the inflatable bladder. An aperture in the widthwise panel may be used for allowing gas communication between the first cylindrical portion and a second cylindrical portion.

Abstract translation: 一种用于飞行器的外部安全气囊包括具有顶部和底部的可膨胀气囊，所述顶部大体上邻近飞行器的外部。 横向面板将可充气气囊分成第一圆柱形部分和第二圆柱形部分。 横向面板用于限制可膨胀囊的向外膨胀。 宽度方向面板上的孔可以用于允许第一圆柱形部分和第二圆柱形部分之间的气体连通。

公开(公告)号：US20130026803A1

公开(公告)日：2013-01-31

申请号：US13557300

申请日：2012-07-25

Applicant: RAKIBUL ISLAM ,  ROBERT W. TRIMBLE ,  RAUL DANIEL FLORES AGUIRRE ,  FREDERIC QUATANENS ,  JEREMY CAILLETEAU ,  JEREMY GAUDIN ,  VIRGILE MARTINEZ ,  JEAN-MARC OBADIA

Inventor： RAKIBUL ISLAM ,  ROBERT W. TRIMBLE ,  RAUL DANIEL FLORES AGUIRRE ,  FREDERIC QUATANENS ,  JEREMY CAILLETEAU ,  JEREMY GAUDIN ,  VIRGILE MARTINEZ ,  JEAN-MARC OBADIA

IPC: B60R21/207 ,  B60N2/42

CPC classification number: B64D11/06 ,  B60R21/207 ,  B60R21/215 ,  B60R2021/0093 ,  B64D11/0619 ,  B64D11/06205 ,  B64D2201/00

Abstract: Described are airbag modules for a passenger seat having a seat back, a container coupled to the seat back, wherein the container includes at least one airbag, and a structure positioned aft of the seat back, wherein the structure includes a recess configured to receive the at least one airbag in a deployed state. In certain examples, the container also has a cover with a breakable line, and the structure also has a breakable area positioned aft of the recess, wherein the breakable line is configured to form an opening in the cover and the breakable area is configured to form an opening in the aft surface when a force is applied by the at least one airbag in a deployed state.

Abstract translation: 描述了用于具有座椅靠背的乘客座椅的安全气囊模块，联接到座椅靠背的容器，其中容器包括至少一个气囊和位于座椅靠背后部的结构，其中该结构包括凹部， 处于展开状态的至少一个气囊。 在某些实例中，容器还具有带有可断裂线的盖，并且该结构还具有位于凹部后面的可断裂区域，其中该可断裂线构造成在该盖中形成开口，并且该可破坏区域构造成形成 当处于展开状态时由所述至少一个气囊施加力时，所述后表面中的开口。

公开(公告)号：US20120259503A1

公开(公告)日：2012-10-11

申请号：US13228362

申请日：2011-09-08

Applicant: Peter A. Settles

Inventor： Peter A. Settles

IPC: G01M17/00

CPC classification number: G06F11/22 ,  B64D11/062 ,  B64D11/06205 ,  B64D11/0621 ,  B64D2201/00 ,  G05B23/0256

Abstract: A system for testing a number of electronic module assemblies (EMAs) that control one or more personal restraint systems. A programmed processor with a computer system transmits signals that instruct the EMAs to perform a diagnostic self-test. The results of the self-test are received by the computer system and stored in a computer readable memory. In one embodiment, the computer system is a cabin management computer system for use on an aircraft.

Abstract translation: 用于测试控制一个或多个个人约束系统的多个电子模块组件（EMA）的系统。 具有计算机系统的编程处理器传送指示EMA执行诊断自检的信号。 自检结果由计算机系统接收并存储在计算机可读存储器中。 在一个实施例中，计算机系统是用于飞机上的舱室管理计算机系统。

公开(公告)号：US20120259484A1

公开(公告)日：2012-10-11

申请号：US13174659

申请日：2011-06-30

Applicant: Ronald A. Shields ,  Peter A. Settles ,  Willard F. Hagan ,  Joseph Smith

Inventor： Ronald A. Shields ,  Peter A. Settles ,  Willard F. Hagan ,  Joseph Smith

IPC: G06F19/00 ,  G09F9/33 ,  G01M17/00 ,  G08B5/00 ,  B60R22/48 ,  B64D25/02

CPC classification number: B64D11/0621 ,  B64D11/062 ,  B64D11/06205 ,  B64D25/00 ,  B64D25/02 ,  B64D2201/00 ,  G07C5/0808 ,  G07C5/0841

Abstract: An electronic module assembly (EMA) for use in controlling one or more personal restraint systems. A programmed processor within the EMA is configured to determine when a personal restraint system associated with each seat in a vehicle should be deployed. In addition, the programmed processor is configured to perform a diagnostic self-test to determine if the EMA and the personal restraint systems are operational. In one embodiment, results of the diagnostic self-test routine are displayed on a display included on the electronic module assembly. In an alternative embodiment, the results of the diagnostic self-test routine are transmitted via a wireless transceiver to a remote device. The remote device can include a wireless interrogator or can be a remote computer system such as a cabin management computer system.

Abstract translation: 一种用于控制一个或多个个人约束系统的电子模块组件（EMA）。 EMA内的编程处理器被配置为确定何时应该部署与车辆中的每个座椅相关联的个人约束系统。 此外，编程处理器被配置为执行诊断自检，以确定EMA和个人约束系统是否可操作。 在一个实施例中，诊断自检程序的结果被显示在包括在电子模块组件上的显示器上。 在替代实施例中，诊断自检程序的结果通过无线收发器传送到远程设备。 远程设备可以包括无线询问器，或者可以是诸如客舱管理计算机系统的远程计算机系统。

公开(公告)号：US20120256403A1

公开(公告)日：2012-10-11

申请号：US13227382

申请日：2011-09-07

Applicant: Ronald A. Shields

Inventor： Ronald A. Shields

IPC: B60R21/18 ,  B60R21/16

CPC classification number: B60R22/48 ,  B60R21/01546 ,  B60R2022/4816 ,  B64D11/062 ,  B64D11/06205 ,  B64D2201/00

Abstract: Systems for indicating the status of a seatbelt buckle prior to a protective response are disclosed herein. An airbag activation system configured in accordance with one embodiment of the disclosure includes a normally closed magnetically operated reed switch. The reed switch is attached to a connector carried on one portion of a seatbelt, and a magnet is attached to a buckle carried on another portion of the seatbelt. Coupling the connector to the buckle causes the magnetic field of the magnet to move the reed switch from the normally closed position to an open position, thereby enabling the activation system to inflate the airbag in the event of an accident.

Abstract translation: 本文公开了用于在保护性响应之前指示安全带扣的状态的系统。 根据本公开的一个实施例配置的气囊激活系统包括常闭磁性操作的簧片开关。 簧片开关连接到承载在安全带的一部分上的连接器，并且磁体附接到承载在安全带的另一部分上的带扣。 将连接器耦合到带扣将导致磁体的磁场将簧片开关从常闭位置移动到打开位置，从而使得启动系统能够在发生事故时使气囊膨胀。

公开(公告)号：US20120256399A1

公开(公告)日：2012-10-11

申请号：US13516395

申请日：2010-11-08

Applicant: Akira Kokeguchi

Inventor： Akira Kokeguchi

IPC: B60R21/233 ,  B60R21/239 ,  B64D25/00

CPC classification number: B64D11/06205 ,  B60R2021/23382 ,  B60R2021/2395 ,  B64D11/06 ,  B64D2201/00

Abstract: Provided are an aircraft airbag that inflates across a plurality of seats, an airbag device including this airbag, and an aircraft equipped with this airbag device. The airbag has a bag main body extending across three seats and in the left-right direction of the aircraft body, and partition panels that partition the inside of the bag main body into small chambers and corresponding to the seats. Gas from the inflator flows into the small chamber in the middle, and flows into the small chambers through the communication portions above and below the partition panels. When occupants are caught and thereby the pressures in the small chambers reach a predetermined value or more, vent holes open.

Abstract translation: 提供了一种在多个座椅上充气的飞行器安全气囊，包括该气囊的气囊装置和配备有该气囊装置的飞行器。 气囊具有延伸穿过飞机主体的三个座位和左右方向的袋主体，以及将袋主体的内部分隔成小室并对应于座椅的隔板。 来自充气机的气体流入中间的小室，并且通过分隔板上方和下方的连通部分流入小室。 当乘员被卡住时，小室内的压力达到预定值以上时，排气孔打开。

公开(公告)号：US08186625B2

公开(公告)日：2012-05-29

申请号：US11463560

申请日：2006-08-09

Applicant: Maxim De Jong

Inventor： Maxim De Jong

IPC: B64G1/00

CPC classification number: B64G1/222 ,  B64D2201/00 ,  B64G1/62 ,  B64G1/646 ,  B64G9/00 ,  B64G2001/224

Abstract: A flexible vessel includes a restraint structure and a barrier structure. The restraint structure further includes a first portion, and a second substantially rounded end cap portion that is attached to the first portion. The restraint structure also includes an array of tendons. The barrier structure is positioned within the restraint structure. When the barrier contains a fluid, a portion of the load is carried by the restraint structure and another portion of the load is carried by the barrier structure. The flexible vessel is collapsible to occupy a first volume and distended to occupy a second volume. The flexible vessel is part of a system when used in various applications with respect to a craft.

Abstract translation: 柔性容器包括约束结构和阻挡结构。 约束结构还包括第一部分和附接到第一部分的第二基本圆形的端盖部分。 约束结构还包括腱阵列。 阻挡结构位于约束结构内。 当挡板包含流体时，负载的一部分由约束结构承载，另一部分负载由阻挡结构承载。 柔性容器可折叠以占据第一体积并膨胀以占据第二体积。 柔性容器是用于相对于工艺的各种应用中的系统的一部分。

公开(公告)号：US20110315806A1

公开(公告)日：2011-12-29

申请号：US13068601

申请日：2011-05-16

Applicant: John W. Piasecki ,  Frederick W. Piasecki ,  Brian Geiger ,  Douglas Johnson ,  David Pitcairn

Inventor： John W. Piasecki ,  Frederick W. Piasecki ,  Brian Geiger ,  Douglas Johnson ,  David Pitcairn

IPC: B64C37/00 ,  B64C39/00 ,  B64C27/28 ,  B64C27/22 ,  G05D1/00 ,  B64D7/00 ,  B64C25/32 ,  G06F19/00 ,  B64C27/00 ,  B64C27/08 ,  B64C27/10 ,  B64C29/00 ,  B64D17/80

CPC classification number: B64C37/00 ,  B60F5/02 ,  B64C3/385 ,  B64C3/56 ,  B64C11/001 ,  B64C25/58 ,  B64C27/08 ,  B64C27/20 ,  B64C27/22 ,  B64C27/32 ,  B64C27/52 ,  B64C27/57 ,  B64C29/00 ,  B64C29/0033 ,  B64C39/00 ,  B64C39/02 ,  B64D17/80 ,  B64D25/00 ,  B64D2201/00 ,  G05D1/102

Abstract: An unmanned air module includes one or more rotors, engines, a transmission and avionics. Any of several different ground modules may be attached to the air module. The air module may fly with and without the ground module attached. The ground module may be a vehicle ground module and may be manned. The vehicle ground module may transport the attached air module across the ground. The air module may have two rotors, which may be ducted fans, and three different configurations: a tandem rotor configuration, a side-by-side configuration, and a tilted-rotor configuration.

Abstract translation: 无人驾驶的空气模块包括一个或多个转子，发动机，变速器和航空电子设备。 几个不同的接地模块中的任何一个可以连接到空气模块。 空气模块可以在带和不带接地模块的情况下飞行。 接地模块可以是车辆接地模块，并且可以被人操作。 车辆接地模块可以将连接的空气模块运送到地面。 空气模块可以具有两个转子，其可以是导风扇，以及三种不同的配置：串联转子配置，并排配置和倾斜转子配置。