公开(公告)号：US08888044B2

公开(公告)日：2014-11-18

申请号：US13654576

申请日：2012-10-18

Applicant: Airbus Helicopters

Inventor： Dominique Mailliu ,  Marc Denante

IPC: B64C25/56 ,  B64C11/00 ,  B64C27/26 ,  B64D25/18 ,  B64C27/00 ,  B64C27/28

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：US08818759B2

公开(公告)日：2014-08-26

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: G05B23/02 ,  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：US08800923B2

公开(公告)日：2014-08-12

申请号：US13229909

申请日：2011-09-12

Applicant: Laurent Dock

Inventor： Laurent Dock

IPC: B64C1/00

CPC classification number: B64D25/00 ,  B64D2201/00

Abstract: A system and method of activating protection means (1) in order to protect the physical integrity of an occupant of an aircraft (10) during an accident is provided. The protection means (1) are activated when, firstly the acceleration of said aircraft (10) along a particular axis (X, Y, Z) of the coordinate system of the aircraft (10) is greater than a first variable threshold, and secondly when the speed variation of the aircraft along said particular axis (X, Y, Z) is greater than a second variable threshold. The first variable threshold and the second variable threshold each vary as a function of the stage of flight of the aircraft (10) in such a manner as to be minimized during predetermined accident-prone stages of flight.

Abstract translation: 提供了一种用于在事故期间激活保护装置（1）以便保护飞机（10）的乘客的身体完整性的系统和方法。 当首先沿飞机（10）的坐标系的特定轴线（X，Y，Z）加速所述飞机（10）大于第一可变阈值时，保护装置（1）被激活，其次 当沿着所述特定轴线（X，Y，Z）的飞行器的速度变化大于第二可变阈值时。 第一可变阈值和第二可变阈值各自作为飞行器（10）的飞行阶段的函数以在预定的事故容易发生的阶段期间被最小化的方式变化。

公开(公告)号：US20140027574A1

公开(公告)日：2014-01-30

申请号：US13912937

申请日：2013-06-07

Applicant: SICMA Aero Seat S.A.

Inventor： Jean-Marc OBADIA ,  John PAYNE ,  Jeremy CAILLETEAU ,  Nick LEE ,  Nathan KWOK ,  Jean-Marie DAOUT ,  Jake STORY ,  David KNOX

IPC: B60R21/20

CPC classification number: B60R21/20 ,  B60R2021/0093 ,  B64D11/00 ,  B64D25/02 ,  B64D2201/00

Abstract: An airbag system assembly configured to be positioned in the interior of a vehicle that includes an aft wall configured to be positioned forward of a passenger seat and an airbag system. The aft wall includes front and aft surfaces and the aft wall includes a first flap that is formed by a plurality of weakness lines in at least the front surface thereof. The airbag system includes at least a first airbag module having a first airbag support plate with front and aft surfaces. The first airbag support plate is secured to the front surface of the aft wall, and the first airbag support plate includes a first airbag that is configured to deploy in the event of a crash condition and that is disposed on the aft surface of the first airbag support plate. The first airbag is positioned adjacent the first flap.

Abstract translation: 一种安全气囊系统组件，其构造成定位在车辆内部，所述气囊系统组件包括构造成位于乘客座椅前方的后壁和气囊系统。 后壁包括前表面和后表面，并且后壁包括在至少其前表面中由多条弱线形成的第一挡板。 所述安全气囊系统至少包括具有前后表面的第一气囊支撑板的第一气囊模块。 第一安全气囊支撑板固定在后壁的前表面上，第一安全气囊支撑板包括第一气囊，其构造成在碰撞状态下展开并且设置在第一气囊的后表面上 支撑板 第一安全气囊邻近第一挡板定位。

公开(公告)号：US20140021771A1

公开(公告)日：2014-01-23

申请号：US13551071

申请日：2012-07-17

Applicant: Pete C. Meister ,  Michael Oleson

Inventor： Pete C. Meister ,  Michael Oleson

IPC: B60R22/28 ,  B64D11/06 ,  B60R22/34

CPC classification number: B64D25/06 ,  B60R21/18 ,  B60R2021/0093 ,  B64D11/06205 ,  B64D2201/00

Abstract: An inflatable shoulder harness assembly for an aircraft seat including a shoulder belt, a retractor, an airbag contained within an outer cover, and a belt guide slideably receiving the inflatable airbag and outer cover therein when the shoulder belt is retracted, the belt guide defining an elongate channel for facilitating free movement of the outer cover during belt fastening and retraction. The assembly further includes an exit bezel for finishing the look of the seat and a stiffening element for preventing kinking, bunching and twisting of the outer cover.

Abstract translation: 一种用于飞行器座椅的可充气肩带组件，包括肩带，牵开器，包含在外盖内的气囊，以及当肩带缩回时可滑动地将可充气安全气囊和外盖容纳在其中的皮带引导件， 细长通道，用于在带紧固和收回期间促进外盖的自由运动。 组件还包括用于完成座椅外观的出口挡板和用于防止外盖的扭结，聚束和扭曲的加强元件。

公开(公告)号：US20130075524A1

公开(公告)日：2013-03-28

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: B60R21/16

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：US20130009389A1

公开(公告)日：2013-01-10

申请号：US13428171

申请日：2012-03-23

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: B60R21/16

CPC classification number: B60R21/231 ,  B60R2021/0093 ,  B64D11/0604 ,  B64D11/06205 ,  B64D2201/00

Abstract: Embodiments of the present invention provide an airbag system formed from non-traditional or asymmetric airbag shapes that deflect a vehicle occupant away from an interior vehicle structure.

Abstract translation: 本发明的实施例提供一种由非传统或不对称的安全气囊形状形成的气囊系统，其将车辆乘员偏离内部车辆结构。

公开(公告)号：US20130009009A1

公开(公告)日：2013-01-10

申请号：US13428123

申请日：2012-03-23

Applicant: RAKIBUL ISLAM ,  Robert W. Trimble ,  Raul Daniel Flores Aguirre ,  Frederic Quatanens ,  Jeremy Cailleteau ,  Jeremy Gaudin ,  Vergile Martinez ,  Jean-Marc Obadia

Inventor： RAKIBUL ISLAM ,  Robert W. Trimble ,  Raul Daniel Flores Aguirre ,  Frederic Quatanens ,  Jeremy Cailleteau ,  Jeremy Gaudin ,  Vergile Martinez ,  Jean-Marc Obadia

IPC: B64D25/02 ,  B60R21/21

CPC classification number: B60R21/20 ,  B60R21/23184 ,  B60R2021/0093 ,  B64D11/0604 ,  B64D11/06205 ,  B64D2201/00

Abstract: Embodiments of the present invention provide an airbag system designed to deploy from a privacy wall in a diagonal manner.

Abstract translation: 本发明的实施例提供一种设计成以对角线方式从隐私壁部署的气囊系统。

公开(公告)号：US20120101666A1

公开(公告)日：2012-04-26

申请号：US13380925

申请日：2009-07-27

Applicant: Andrew T. Hill ,  Michael R. Smith ,  Charles E. Covington ,  Nicholas Lappos ,  Walter Sonneborn

Inventor： Andrew T. Hill ,  Michael R. Smith ,  Charles E. Covington ,  Nicholas Lappos ,  Walter Sonneborn

IPC: G05D1/00 ,  G06F19/00

CPC classification number: B64D25/00 ,  B64D2201/00

Abstract: An occupant protection system for an aircraft comprising a sensor system for sensing flight condition information and a control system, which includes an impending crash detection system and an impact detection system. The impending crash detection system receives flight information from the sensors determines whether a crash is likely to occur. If an impending crash is detected, the impending crash detection system activates impact modes of a first group of aircraft systems. The impact detection system receives flight information from the sensor system and determines whether an impact has occurred or is occurring. If an impact is detected, the impact detection system activates impact modes of a second group of aircraft systems.

Abstract translation: 一种用于飞行器的乘员保护系统，包括用于感测飞行情况信息的传感器系统和包括即将发生的碰撞检测系统和冲击检测系统的控制系统。 即将发生的碰撞检测系统从传感器接收飞行信息，确定是否可能发生碰撞。 如果检测到即将发生的碰撞，即将发生的碰撞检测系统激活第一组飞行器系统的冲击模式。 冲击检测系统从传感器系统接收飞行信息，并确定影响是否发生或正在发生。 如果检测到冲击，冲击检测系统激活第二组飞行器系统的冲击模式。

公开(公告)号：US08016239B2

公开(公告)日：2011-09-13

申请号：US12382144

申请日：2009-03-10

Applicant: A-Hamid Hakki ,  Sam Hakki ,  Said I. Hakky

Inventor： A-Hamid Hakki ,  Sam Hakki ,  Said I. Hakky

IPC: B64D17/00

CPC classification number: B64D25/08 ,  B64D17/80 ,  B64D2201/00

Abstract: A safety pre-impact deceleration system for a variety of conveyances includes a parachute structure formed from air bags inflated with gas. Alternatively, the parachute structure includes a canopy with orifices. Air spaces in the parachute structure or orifices in the canopy have adjustable and selective dimensions to control the operational parameters of the vehicle. The system includes sensors and rapid exposure rate cameras with continuous loop recording to measure operational parameters of the vehicle and to predict possible collision. Once a collision condition is detected, audio/video images are stored on storage media. The air bags are deployed and inflated. In addition to air bags constituting the parachute structure, a plurality of air bags are provided to be deployed external the vehicle to aid in a safe landing.

Abstract translation: 用于各种运输工具的安全预冲击减速系统包括由气体膨胀的气囊形成的降落伞结构。 或者，降落伞结构包括具有孔的顶盖。 降落伞结构中的空气间隙或冠层中的孔口具有可调节和选择性尺寸以控制车辆的操作参数。 该系统包括具有连续循环记录的传感器和快速曝光率摄像机，以测量车辆的操作参数并预测可能的碰撞。 一旦检测到碰撞条件，音频/视频图像被存储在存储介质上。 气囊被部署和充气。 除了构成降落伞结构的气囊之外，还设置有多个安全气囊，以便在车辆的外部展开以帮助安全着陆。