公开(公告)号：US09272680B1

公开(公告)日：2016-03-01

申请号：US12816221

申请日：2010-06-15

Applicant: Abbas Mirzazadeh

Inventor： Abbas Mirzazadeh

IPC: B60R21/207 ,  B60R21/231

CPC classification number: B60R21/207 ,  B60R21/231 ,  B60R2021/0093 ,  B60R2021/23107 ,  B60R2021/23169 ,  B64D11/0619 ,  B64D2201/00

Abstract: The different advantageous embodiments comprise an apparatus comprising an airbag. The airbag is configured to inflate into a configuration that covers a region around a seat in which a top of a head, a front of a head, upper body region, knees, and shins of a passenger in the seat is expected to be located when an event occurs in which the airbag is deployed.

Abstract translation: 不同的有利实施例包括包括气囊的装置。 安全气囊构造成膨胀成覆盖围绕座椅的区域的构造，其中头部的顶部，头部的前部，上部身体区域，膝盖以及座椅中的乘客的襟翼预期将位于何处 发生气囊展开的事件。

公开(公告)号：US09248905B2

公开(公告)日：2016-02-02

申请号：US13894944

申请日：2013-05-15

Applicant: AIRBUS OPERATIONS S.L. ,  AIRBUS SAS

Inventor： Ludovic Gerard ,  Alejandro Gutiérrez García ,  Julián Maldonado

IPC: B64C23/00 ,  B64C25/16 ,  B64D41/00 ,  B64C25/00

CPC classification number: B64C23/005 ,  B64C25/16 ,  B64C2025/003 ,  B64D41/007 ,  B64D2201/00

Abstract: An aircraft (11) with at least an inflatable device (41) installed in a cavity (21) in its external surface which is equipped with a door (25) for opening/closing said cavity (21) is provided. The inflatable device (41), comprising a cushion (45) and a gas generator is configured for filling the cavity (21) with the cushion (45) when it is inflated with the gas supplied by said gas generator, without protruding from the cavity (21) for reducing the downstream air flow disturbances generated by said cavity (21) when the door (25) is open. The inflatable device (41) includes control means for inflating the cushion (45) in predetermined circumstances, being the door (25) open. The invention is particularly applicable to the cavities of the Main Landing Gear (31) for avoiding power losses to a Ram Air Turbine (51) placed behind it.

Abstract translation: 提供一种具有安装在其外表面中的空腔（21）中的至少一个可充气装置（41）的飞行器（11），其配备有用于打开/关闭所述空腔（21）的门（25）。 包括衬垫（45）和气体发生器的充气装置（41）构造成当用气体发生器供应的气体充气时，利用衬垫（45）填充空腔（21），而不会从空腔 （21），用于当门（25）打开时减小由所述空腔（21）产生的下游空气流动干扰。 充气装置（41）包括控制装置，用于在门（25）打开的情况下在预定情况下使垫子（45）充气。 本发明特别适用于主起落架（31）的空腔，用于避免向放置在其后面的拉姆空气涡轮机（51）的功率损失。

公开(公告)号：US09242737B2

公开(公告)日：2016-01-26

申请号：US13626912

申请日：2012-09-26

Applicant: Rakibul Islam ,  Adrianus W. N. Ruiter ,  Maurice Pinault ,  Jean-Marc Obadia

Inventor： Rakibul Islam ,  Adrianus W. N. Ruiter ,  Maurice Pinault ,  Jean-Marc Obadia

IPC: B64C1/14 ,  B64D25/14 ,  B64D25/00

CPC classification number: B64D25/14 ,  B64D25/00 ,  B64D2201/00

Abstract: Described are airbag modules for a passenger door having a door bustle, an airbag positioned adjacent the door bustle, and an inflator positioned adjacent the door bustle. As examples, a pneumatic system is coupled to the inflator and the airbag, wherein the pneumatic system includes a slide lock that is configured to couple a girt bar of an escape slide to a passenger door sill when the inflator is activated. As additional examples, a valve is coupled to an inlet of the airbag, wherein the valve is configured to prevent the pressurized gas from flowing from the inflator to the airbag when the valve is closed and is configured to allow the pressurized gas to flow from the inflator to the airbag when the valve is open.

Abstract translation: 描述的是具有门喧嚣的乘客门的气囊模块，邻近门喧嚣的气囊以及邻近门喧嚣定位的充气机。 作为示例，气动系统联接到充气机和气囊，其中气动系统包括滑动锁，其构造成当充气机被启动时将逃生滑块的衬垫杆联接到乘客门槛。 作为另外的示例，阀联接到气囊的入口，其中阀被配置为当阀关闭时防止加压气体从充气器流动到气囊，并且构造成允许加压气体从 当阀门打开时，充气器到气囊。

公开(公告)号：US20160001735A1

公开(公告)日：2016-01-07

申请号：US14854605

申请日：2015-09-15

Applicant: Zodiac Seats France

Inventor： Frederic Quatanens ,  Jeremy Cailleteau ,  Jean-Marc Obadia

IPC: B60R21/233 ,  B60R21/207 ,  B64D11/06 ,  B60R21/26

CPC classification number: B60R21/233 ,  B60R21/231 ,  B60R2021/23107 ,  B60R2021/23115 ,  B60R2021/23308 ,  B60R2021/23386 ,  B64D11/06205 ,  B64D2201/00 ,  Y02T50/46 ,  Y10T29/49826

Abstract: Embodiments of the present invention provide an airbag system formed of a plurality of tubular structures.

公开(公告)号：US09216818B1

公开(公告)日：2015-12-22

申请号：US14626838

申请日：2015-02-19

Applicant: SZ DJI TECHNOLOGY CO., LTD

Inventor： Mingyu Wang

IPC: B64C25/00 ,  B64C25/32 ,  B64D25/00

CPC classification number: B64D25/00 ,  B64C25/32 ,  B64C25/54 ,  B64C25/56 ,  B64C39/024 ,  B64C2201/027 ,  B64D45/00 ,  B64D2201/00

Abstract: An impact protection apparatus is provided, comprising a gas container configured to hold a compressed gas and an inflatable member configured to be inflated by the gas and function as an airbag of a movable object, such as an aerial vehicle. A valve controls flow of gas from the container to the inflatable member in response to a signal from a valve controller. The valve and valve controller are powered by an independent power source than one or more other systems of the movable object. A safety mechanism may also be provided that, unless deactivated, prevents inflation of the inflatable member.

公开(公告)号：US20150217713A1

公开(公告)日：2015-08-06

申请号：US14542887

申请日：2014-11-17

Applicant: Zodiac Seats France

Inventor： Alexandre Vasseur ,  Jean-Marc Obadia

IPC: B60R21/2155 ,  B60R21/231 ,  B60R21/237

CPC classification number: B60R21/2155 ,  B60R21/216 ,  B60R21/231 ,  B60R21/237 ,  B64D2201/00

Abstract: Embodiments of the present invention provide an airbag door assembly for use in a vehicle. The door assembly includes a moving door panel that deforms under pressure of an airbag as it deploys. The airbag system employing this airbag door assembly may be installed in a cavity in a structure on-board the vehicle, or it may be independently mounted to a vehicle structure.

Abstract translation: 本发明的实施例提供一种用于车辆的气囊门组件。 门组件包括移动的门板，其在展开时在气囊的压力下变形。 使用该安全气囊门组件的气囊系统可以安装在车辆上的结构中的空腔中，或者可以独立地安装在车辆结构上。

公开(公告)号：US20150199856A1

公开(公告)日：2015-07-16

申请号：US14468170

申请日：2014-08-25

Applicant: AmSafe, Inc.

Inventor： Ronald A. Shields ,  Peter Anthony Settles

IPC: G07C5/08 ,  B64D25/02 ,  B64D11/06

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：US09010682B2

公开(公告)日：2015-04-21

申请号：US13808173

申请日：2011-06-27

Applicant: Giacomo Giovangrossi ,  Pasquale Monteleone

Inventor： Giacomo Giovangrossi ,  Pasquale Monteleone

IPC: B64C25/56 ,  B64D25/00 ,  B64C25/32

CPC classification number: B64C25/56 ,  B64C2025/325 ,  B64D25/00 ,  B64D2201/00

Abstract: A method for emergency landing of a vehicle, such as a helicopter or like, is described. The vehicle has at least one airbag provided with a respective opening valve for allowing the outflow of the gas therein contained. The airbag is suitable to cushion the impact of the vehicle with ground, and is inflated for an emergency landing. The method checks the conditions for the emergency landing of the vehicle, detects the maximum or impact speed of the vehicle, and opens the opening valve after the detection of an activation speed of the vehicle, so as to deflate the airbag. A system for controlling airbags of a vehicle, such as a helicopter or like, is also described.

Abstract translation: 描述了诸如直升机等的车辆的紧急着陆的方法。 该车辆具有至少一个安全气囊，该安全气囊具有相应的开启阀，用于允许其中包含的气体的流出。 安全气囊适用于缓冲车辆撞击地面，并为紧急着陆而充气。 该方法检查车辆的紧急着陆的条件，检测车辆的最大或冲击速度，并且在检测到车辆的启动速度之后打开开启阀，以便使气囊膨胀。 还描述了用于控制诸如直升机等车辆的安全气囊的系统。

公开(公告)号：US08979023B1

公开(公告)日：2015-03-17

申请号：US14257930

申请日：2014-04-21

Applicant: SZ DJI Technology Co., Ltd

Inventor： Mingyu Wang

IPC: B64C25/56 ,  B64C25/32

CPC classification number: B64D25/00 ,  B64C25/32 ,  B64C25/54 ,  B64C25/56 ,  B64C39/024 ,  B64C2201/027 ,  B64D45/00 ,  B64D2201/00

Abstract: An impact protection apparatus is provided, comprising a gas container configured to hold a compressed gas and an inflatable member configured to be inflated by the gas and function as an airbag of a movable object, such as an aerial vehicle. A valve controls flow of gas from the container to the inflatable member in response to a signal from a valve controller. The valve and valve controller are powered by an independent power source than one or more other systems of the movable object. A safety mechanism may also be provided that, unless deactivated, prevents inflation of the inflatable member.

Abstract translation: 提供了一种冲击保护装置，包括构造成保持压缩气体的气体容器和构造成由气体膨胀并充当诸如飞行器的可移动物体的气囊的充气构件。 响应于来自阀控制器的信号，阀控制气体从容器到可膨胀构件的流动。 阀和阀门控制器由与可移动物体的一个或多个其它系统相独立的电源供电。 还可以提供一种安全机构，除非被去激活，否则防止可膨胀构件的膨胀。

公开(公告)号：US20140367514A1

公开(公告)日：2014-12-18

申请号：US14307673

申请日：2014-06-18

Applicant: Eric FRADET

Inventor： Eric FRADET

IPC: B64D17/78

CPC classification number: B64D17/78 ,  B64D1/14 ,  B64D17/30 ,  B64D2201/00

Abstract: A device for absorbing impacts of a parachutist or airdropped package upon landing, which can equip a harness, and/or a skydiver or dropping pallet for performing the aircraft jump without any risk of interferences, allows, during the aircraft exit and free fall, to hold, neutralized in a reduced volume, an air-inflatable airbag, for deployment during the canopy descent. It includes a container back pad hooked to the harness and/or to the user or to the dropping pallet, which can be made removable by straps and bridles, in which an airbag is arranged such that its air scoop is closed by flaps locked by a cutaway cable. When the user exerts an action on the opening handle or when the parachute opens, the cable separates the flaps, allowing to unballast the airbag and open the air scoop to the air flow from the movement of the harness during the descent.

Abstract translation: 用于吸收爬升器或空中投放的包装物在着陆时的冲击的装置，其可以装备线束，和/或用于执行飞行器跳跃的跳伞者或落料托盘而没有任何干扰的风险，允许在飞行器出口和自由落体期间 保持，减小体积的中空，充气的气囊，用于在冠层下降期间展开。 它包括钩在线束上和/或与用户或落下的托盘上的容器背垫，该托盘可以通过带子和马口将其卸下，其中气囊被布置成使得其空气勺被由 切断电缆 当使用者对开启手柄施加动作时，或者当降落伞打开时，电缆分离襟翼，允许不安全气囊，并且在下降期间将气勺从线束的运动打开到空气流中。