公开(公告)号：US20130147242A1

公开(公告)日：2013-06-13

申请号：US13710538

申请日：2012-12-11

Applicant: EUROCOPTER ,  EUROCOPTER DEUTSCHLAND GMBH ,  SCHROTH SAFETY PRODUCTS GMBH ,  FISCHER + ENTWICKLUNGEN GMBH & CO KG

Inventor： Tomas Santana-Gallego ,  Ulf Gruene ,  Roland Bauer

IPC: B60R21/231 ,  B60R22/00

CPC classification number: B60R21/23138 ,  B60R21/18 ,  B60R21/207 ,  B60R22/00 ,  B60R22/26 ,  B60R2021/0093 ,  B60R2021/2074 ,  B60R2021/2615 ,  B60R2022/027 ,  B60R2022/1843 ,  B64D11/062 ,  B64D11/06205 ,  B64D25/04 ,  B64D2201/00

Abstract: A protection device (10) having a set (11) of protection inflatable members (15, 20, 25) including left and right inflatable lateral means (20, 25) that are suitable for co-operating respectively with the left and right shoulder straps (6, 7), said device (10) possessing an inflator (30) for inflating said protection inflatable members (15, 20, 25). The device includes a headrest (35) carrying a nape airbag (15) of said set of inflatable members (15, 20, 25), the nape airbag (15) including one passage (16, 17) per inflatable lateral means (20, 25) in order to convey fluid to each inflatable lateral means (20, 25), said headrest (35) being provided with a hollow support (40) carrying said inflator (30) and with a fluid diffusion box (50) arranged in the nape airbag (15) so as to convey a fluid from the inflator (30) to the nape airbag (15) and to the inflatable lateral means (20, 25).

Abstract translation: 一种保护装置（10），其具有包括左和右可膨胀侧向装置（20,25）的保护性可充气构件（15,20,25）的组合（11），所述左右可膨胀横向装置适于与左肩肩带和右肩带 （6,7），所述装置（10）具有用于使所述保护性可充气构件（15,20,25）膨胀的充气器（30）。 该装置包括承载所述一组充气构件（15,20,25）的颈部安全气囊（15）的头枕（35），所述颈部安全气囊（15）包括每个可充气横向装置（20,20）的一个通道（16,17） 为了将流体输送到每个可膨胀的侧向装置（20,25），所述头枕（35）设置有承载所述充气器（30）的中空支撑件（40）和布置在所述充气器中的流体扩散箱（50） 从而将来自充气器（30）的流体输送到油包安全气囊（15）和可膨胀的横向装置（20,25）。

公开(公告)号：US20130106080A1

公开(公告)日：2013-05-02

申请号：US13284004

申请日：2011-10-28

Applicant: Patrick Jarboe ,  Douglas Werth ,  Raj Valera

Inventor： Patrick Jarboe ,  Douglas Werth ,  Raj Valera

IPC: B60R21/16 ,  B64D25/02

CPC classification number: B64D11/06205 ,  B60R21/207 ,  B60R2021/0093 ,  B64D11/06 ,  B64D11/0604 ,  B64D11/064 ,  B64D11/0646 ,  B64D2201/00

Abstract: An airbag arrangement is accommodated in an armrest between angled seats. A gas generator inflates an airbag cushion in the path of inertia of each seat occupant of an angled seat. The airbag may have a lamella structure to inflate to a cushioning curtain or wall with a stiffness that resists bending and folding. The airbag may alternatively be provided with wider channels to provide a thicker cushion.

Abstract translation: 安全气囊装置容纳在倾斜座椅之间的扶手上。 气体发生器在倾斜座椅的每个座椅乘员的惯性路径中使气囊垫膨胀。 安全气囊可以具有薄片结构以膨胀到缓冲帘或壁，具有抵抗弯曲和折叠的刚度。 安全气囊可以替代地设置有更宽的通道以提供较厚的垫。

公开(公告)号：US20130105625A1

公开(公告)日：2013-05-02

申请号：US13654576

申请日：2012-10-18

Applicant: EUROCOPTER

Inventor： Dominique Mailliu ,  Marc Denante

IPC: B64D45/06

CPC classification number: B64D25/18 ,  B64C11/001 ,  B64C27/006 ,  B64C27/26 ,  B64C27/28 ,  B64D2201/00

Abstract: The present invention relates to an aircraft (1) provided with at least one rotary element (10) provided with blades (11) liable to come into contact with a liquid surface (100) on ditching, said aircraft including a buoyancy system. The aircraft includes a fairing (15) surrounding at least part of said rotary element (10), the fairing (15) including an inflatable emergency float (20) of the buoyancy system for preventing said blades (11) from coming into contact with the liquid surface when in an inflated position.

Abstract translation: 本发明涉及一种设置有至少一个旋转元件（10）的飞行器（1），该旋转元件（10）设置有在开沟时容易与液体表面（100）接触的叶片（11），所述飞行器包括浮力系统。 飞行器包括围绕所述旋转元件（10）的至少一部分的整流罩（15），整流罩（15）包括浮力系统的可充气紧急浮子（20），用于防止所述叶片（11）与所述旋转元件 处于充气位置时的液面。

公开(公告)号：US20130009430A1

公开(公告)日：2013-01-10

申请号：US13543933

申请日：2012-07-09

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 ,  B60N2/427

CPC classification number: B64D11/06205 ,  B60R21/04 ,  B60R21/16 ,  B60R21/215 ,  B60R2021/0093 ,  B60R2021/21512 ,  B60R2021/21525 ,  B64D11/0015 ,  B64D11/00151 ,  B64D11/0619 ,  B64D11/0624 ,  B64D2201/00 ,  Y02T50/46

Abstract: Described are energy absorbers for a structure within a vehicle cabin having at least one airbag, an inflator, a control module, and an outer surface positioned adjacent the airbag. The outer surface may include a plurality of mechanical energy absorbers positioned adjacent the airbag and coupled to the outer surface, wherein the outer surface comprises a surface area that is greater than an inflated surface area of the airbag. The outer surface may also include a breakable area positioned adjacent the airbag, wherein the breakable area has a weaker coupling to the outer surface on at least a first side and a stronger coupling to the outer surface on at least a second side.

Abstract translation: 描述了用于车厢内的结构的能量吸收器，其具有至少一个气囊，充气机，控制模块和邻近安全气囊定位的外表面。 外表面可以包括邻近安全气囊定位并联接到外表面的多个机械能吸收器，其中外表面包括大于气囊膨胀的表面积的表面积。 外表面还可以包括邻近安全气囊定位的可断裂区域，其中可破裂区域在至少第一侧上具有与外表面的较弱耦合，并且在至少第二侧上具有与外表面更强的联接。

公开(公告)号：US08348192B2

公开(公告)日：2013-01-08

申请号：US12679563

申请日：2007-10-22

Applicant: Cheng-Ho Tho ,  Michael R. Smith

Inventor： Cheng-Ho Tho ,  Michael R. Smith

IPC: B64C25/56

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

Abstract: A crash attenuation system for an aircraft, the system having an airbag carried by the aircraft and inflatable generally adjacent an exterior of the aircraft. The airbag has at least one vent for releasing gas from the interior of the airbag. A gas source is in fluid communication with the interior of the airbag for inflating the airbag with gas generated provided by the first gas source. A vent valve is provided for controlling a flow of gas through each vent, each vent valve being selectively configurable between an open state, in which gas can pass through the associated vent from the interior of the airbag, any number of intermediate states, in which the vent is partially open, and a closed state, in which gas is retained within the interior of the airbag.

Abstract translation: 一种用于飞行器的碰撞衰减系统，该系统具有由飞机携带并且大体上邻近飞机外部充气的气囊。 气囊具有至少一个用于从气囊的内部释放气体的通气口。 气体源与气囊的内部流体连通，用于通过由第一气体源产生的气体使气囊充气。 设置排气阀以控制通过每个通气口的气体流动，每个排气阀可以在打开状态之间选择性地配置，在该状态下，气体可以从气囊的内部通过相关联的通气口，其中任何数量的中间状态，其中 通风口部分打开，并且气体保持在气囊内部的关闭状态。

公开(公告)号：US20120259586A1

公开(公告)日：2012-10-11

申请号：US13228333

申请日：2011-09-08

Applicant: Ronald A. Shields ,  Peter A. Settles

Inventor： Ronald A. Shields ,  Peter A. Settles

IPC: G06F19/00

CPC classification number: G07C5/0808 ,  B64D11/062 ,  B64D11/06205 ,  B64D25/02 ,  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：US20120193899A1

公开(公告)日：2012-08-02

申请号：US13353790

申请日：2012-01-19

Applicant: Tomas Santana-Gallego

Inventor： Tomas Santana-Gallego

IPC: B60R21/26 ,  B60R22/12 ,  B60N2/42

CPC classification number: B60R21/18 ,  B60R21/017 ,  B60R21/268 ,  B60R2021/0016 ,  B60R2021/23382 ,  B60R2021/23386 ,  B60R2021/2395 ,  B60R2021/2765 ,  B64D11/062 ,  B64D11/06205 ,  B64D2201/00

Abstract: A protective device (10) for protecting an occupant (7) of a vehicle (1), said protective device comprising an airbag (11) and inflation means (12) for inflating said airbag (11), the inflation means (12) being connected to the airbag (11) via a feed pipe (13) for feeding inflation fluid for the purpose of inflating the airbag (11) under predetermined conditions. This protective device further comprises expulsion means (20) for expelling said fluid, which expulsion means cooperate with at least one water detection means (15) so as to act when water is detected to remove said fluid resulting from inflation of the airbag (11), said airbag (11) being provided with a peripheral elastic strap (50) for optimizing the deflation of said airbag (11) when said expulsion means (20) allow said fluid to be removed from the airbag (11).

Abstract translation: 一种用于保护车辆（1）的乘员（7）的保护装置（10），所述保护装置包括用于使所述气囊（11）膨胀的气囊（11）和充气装置（12），所述充气装置 经由用于在预定条件下使气囊（11）膨胀的充气流体的供给管（13）连接到气囊（11）。 该保护装置还包括用于排出所述流体的排出装置（20），所述排出装置与至少一个水检测装置（15）配合，以便当检测到水以除去由气囊（11）的膨胀导致的所述流体时起作用 所述气囊（11）设置有周边弹性带（50），用于当所述排出装置（20）允许所述流体从气囊（11）移除时，优化所述气囊（11）的放气。

公开(公告)号：US20110272523A1

公开(公告)日：2011-11-10

申请号：US13144313

申请日：2009-01-18

Applicant: Kenji Uegaki

Inventor： Kenji Uegaki

IPC: B64C25/56

CPC classification number: B64C1/062 ,  B64D17/80 ,  B64D2201/00

Abstract: An air bag 4 is inflated in a shock absorption system 1 by a high pressure air cylinder 5 at the time of a collision between an aircraft and the ground that is caused by inability to fly or the like, so that a cover body 2 is unfolded to the outside from a bottom portion 11a of a fuselage 11 of the aircraft 10 and the air bag 4 is disposed inside the cover body 2. Accordingly, a sufficient shock absorption stroke is obtained, so that it may be possible to reliably absorb shock that is generated at the fuselage 11 during the collision between the aircraft and the ground caused by an inability to fly or the like. Further, the cover body 2 is unfolded from the bottom portion 11a of the fuselage 11 so as to spread out toward the rear side of the aircraft 10. Accordingly, it may be possible to make the fuselage 11 smoothly slide on the ground during the collision between the aircraft and the ground that is caused by an inability to fly or the like. Therefore, according to the shock absorption system 1, it may be possible to prevent the fuselage 11 of the aircraft 10 from being damaged during the collision between the aircraft and the ground that is caused by an inability to fly or the like.

Abstract translation: 空气囊4在飞行器与地面之间由于不能飞行等引起的碰撞时由高压气缸5在减震系统1中膨胀，使得盖体2展开 从飞机10的机身11的底部11a到外面，并且气囊4设置在盖体2的内侧。因此，获得足够的冲击吸收冲程，使得可以可靠地吸收冲击， 在飞机和地面之间的碰撞期间由于不能飞行等而导致在机身11处产生。 此外，盖体2从机身11的底部11a展开，以便朝向飞机10的后侧展开。因此，可能使机身11在碰撞期间在地面上平滑地滑动 在由于无法飞行等而引起的飞机和地面之间。 因此，根据减震系统1，可以防止飞机10的机身11在由于不能飞行等引起的飞机和地面之间的碰撞期间被损坏。

公开(公告)号：US20110024569A1

公开(公告)日：2011-02-03

申请号：US12788063

申请日：2010-05-26

Applicant: Tom Yandle ,  Brian Ford

Inventor： Tom Yandle ,  Brian Ford

IPC: B64D17/78

CPC classification number: B64D1/14 ,  B64D2201/00

Abstract: Disclosed is an attenuated landing system. The landing system includes one or more inflatable structures that are mounted to the underside of a cargo platform. A terrain sensor is likewise mounted to the underside of the cargo platform and is activated upon being air-dropped. Once terrain is detected, pressurized gas vessels are pyrotechnically activated to inflate the structures. Once fully inflated, the structures effectively cushion the landing of the cargo platform and, thereby, protect sensitive on-board equipment.

Abstract translation: 公开了一种减弱着陆系统。 着陆系统包括一个或多个安装在货物平台下侧的可充气结构。 地形传感器同样安装在货物平台的下侧，并在空气流失时被激活。 一旦检测到地形，加压气体容器被烟火地活化，使结构膨胀。 一旦完全充气，结构有效地缓冲货物平台的着陆，从而保护敏感的车载设备。

公开(公告)号：US20110011973A1

公开(公告)日：2011-01-20

申请号：US12922854

申请日：2009-03-17

Applicant: Rahav Shahar ,  Mordechai Ben-Soussan ,  David Albagli ,  Alon Ben Moshe

Inventor： Rahav Shahar ,  Mordechai Ben-Soussan ,  David Albagli ,  Alon Ben Moshe

IPC: B64C25/58 ,  B60R21/239

CPC classification number: B60R21/239 ,  B64C27/57 ,  B64C2025/325 ,  B64D2201/00

Abstract: An airbag system according to any one individual feature or combination of features as described herein.

Abstract translation: 根据本文所述的任何一个单独特征或特征的组合的气囊系统。