公开(公告)号：US08914188B2

公开(公告)日：2014-12-16

申请号：US13228362

申请日：2011-09-08

Applicant: Peter Anthony Settles ,  Ronald A. Shields

Inventor： Peter Anthony Settles ,  Ronald A. Shields

IPC: G01M17/00 ,  G06F11/22 ,  G05B23/02 ,  B64D11/06

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：US08800919B2

公开(公告)日：2014-08-12

申请号：US13088804

申请日：2011-04-18

Applicant: Jean-Jacques Ferrier ,  Pierre Prudhomme-Lacroix

Inventor： Jean-Jacques Ferrier ,  Pierre Prudhomme-Lacroix

IPC: B64C25/56

CPC classification number: B64C27/006 ,  B64C25/52 ,  B64C2025/325 ,  B64D25/00 ,  B64D2201/00

Abstract: Aircraft landing gear (10) provided with at least one contact means (20) for making contact with a contact surface (S). The landing gear includes energy absorber means (30) provided with an inflatable airbag (31) secured to said contact means (20), said energy absorber means (30) being provided with control means (32) and with at least one inflation means (32) for inflating said airbag (31) under the control of said control means (32), said energy absorber means (30) including adjuster means (34) for adjusting the pressure that exists inside (INT) said airbag (31).

Abstract translation: 设置有至少一个用于与接触表面（S）接触的接触装置（20）的飞机起落架（10）。 起落架包括设置有固定到所述接触装置（20）的可充气安全气囊（31）的能量吸收装置（30），所述能量吸收装置（30）设有控制装置（32）和至少一个充气装置 32），用于在所述控制装置（32）的控制下使所述气囊（31）膨胀，所述能量吸收装置（30）包括用于调节存在于所述气囊（31）内部（INT）的压力的调节装置（34）。

公开(公告)号：US20140124620A1

公开(公告)日：2014-05-08

申请号：US13808173

申请日：2011-06-27

Applicant: Giacomo Giovangrossi ,  Pasquale Monteleone

Inventor： Giacomo Giovangrossi ,  Pasquale Monteleone

IPC: B64C25/56

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：US08714589B2

公开(公告)日：2014-05-06

申请号：US13710538

申请日：2012-12-11

Applicant: Eurocopter ,  Eurocopter Deutschland GmbH ,  Schroth Safety Products GmbH ,  Fischer + Entwicklugen GmbH & Co KG

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

IPC: B60R21/18

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可膨胀构件（15,20,25）的颈部安全气囊（15）的头枕（35），所述颈部安全气囊（15）包括每个可充气侧向装置（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：US20140077478A1

公开(公告)日：2014-03-20

申请号：US14054448

申请日：2013-10-15

Applicant: ZODIAC SEATS FRANCE

Inventor： Rakibul Islam ,  Robert W. Trimble ,  Raul Daniel Flores Aguirre ,  Frederic Quatanens ,  Jeremy Cailleteau ,  Jeremy Gaudin ,  Virgile Martinez ,  Jean-Marc Obadia

IPC: B60R21/20

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：US20130327890A1

公开(公告)日：2013-12-12

申请号：US14001238

申请日：2012-02-27

Applicant: Tim Lyons

Inventor： Tim Lyons

IPC: B64C25/56

CPC classification number: B64C25/56 ,  B64C27/006 ,  B64C2025/325 ,  B64D2201/00

Abstract: The present invention provides an aircraft buoyancy system (14) for providing positive buoyancy to an aircraft (15) to keep it afloat at the surface of a body of water (16) after crashing, ditching or landing into a body of water (16). The aircraft buoyancy system (14) comprises at least one inflatable body (1) which, when inflated, increases the buoyancy of the aircraft (14), and a gas generation system (4) to inflate the at least one inflatable body (1). The aircraft buoyancy system (14) also comprises a sensor and activation system (3) to activate the gas generation system (4). Upon activation of the sensor and activation system (3) the gas generation system (4) causes a gas to flow to the at least one inflatable body (1), causing the aircraft (15) to float and remain at the surface of a body of water (16).

Abstract translation: 本发明提供一种飞机浮力系统（14），用于向飞机（15）提供正向浮力，以在撞击，切割或着陆进入水体（16）之后将其浮在水体（16）的表面上， 。 飞机浮力系统（14）包括至少一个可膨胀的主体（1），当充气时，飞行器（14）的浮力增加，并且气体产生系统（4）使至少一个可充气体（1）膨胀， 。 飞机浮力系统（14）还包括一个传感器和激活系统（3），以激活气体发生系统（4）。 在激活传感器和激活系统（3）时，气体产生系统（4）使得气体流动到至少一个可充气体（1），使得飞行器（15）浮起并保持在主体的表面 的水（16）。

公开(公告)号：US08556291B2

公开(公告)日：2013-10-15

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 ,  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: B60R21/20 ,  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.

公开(公告)号：US20130241180A1

公开(公告)日：2013-09-19

申请号：US13424197

申请日：2012-03-19

Applicant: William J. Gehret ,  Joshua Vyrostek ,  Kevin J. Keeslar ,  Daniel N. Foubert

Inventor： William J. Gehret ,  Joshua Vyrostek ,  Kevin J. Keeslar ,  Daniel N. Foubert

IPC: B60R21/16

CPC classification number: B64D11/0621 ,  B60R21/20 ,  B60R21/231 ,  B60R21/26 ,  B60R2021/0093 ,  B64D11/06 ,  B64D11/0604 ,  B64D11/06205 ,  B64D2201/00

Abstract: Structure mounted airbag assemblies and associated systems and methods are described herein. An airbag system configured in accordance with an embodiment of the present disclosure can include, for example, a housing having a cavity and an opening in communication with the cavity, an airbag assembly within the cavity, and an inflator operably coupled to the airbag assembly. The airbag assembly can include an airbag configured to deploy through the opening of the housing during a crash event. The airbag system can further include a door removably positioned across the opening and configured to move away from the opening during airbag deployment. The housing can be affixed to an interior portion of an aircraft, forward of and offset from an aircraft seat.

公开(公告)号：US20130032665A1

公开(公告)日：2013-02-07

申请号：US13641426

申请日：2010-12-29

Applicant: Zi Lu ,  Cheng-Ho Tho ,  Michael R. Smith

Inventor： Zi Lu ,  Cheng-Ho Tho ,  Michael R. Smith

IPC: B64C25/56

CPC classification number: B64C25/56 ,  B64C25/52 ,  B64C2025/325 ,  B64D2201/00

Abstract: A crash attenuation system has an airbag inflatable generally adjacent to an exterior of the aircraft. The system includes a gas generator in fluid communication with an interior of the airbag. The system also includes a vent system having a vent passage supported by the aircraft, the vent passage being configured to allow gas to escape from within the airbag during an impact. The vent system also includes an actuator door for sealing the vent passage, thereby preventing gas from leaving the airbag. The actuator door is actuated by an actuator, the actuator being in fluid communication with the gas generator through an actuator duct. The system operates such that deployment of gas from the gas generator causes the actuator to inflate, thereby causing the actuator door to seal the vent passage. The gas generator is configured to re-inflate the airbag after the actuator door seals the vent passage.

Abstract translation: 碰撞衰减系统具有通常与飞机外部相邻的气囊充气。 该系统包括与气囊的内部流体连通的气体发生器。 该系统还包括具有由飞行器支撑的通气通道的通气系统，该排气通道构造成允许气体在冲击期间从气囊内逸出。 排气系统还包括用于密封通气通道的致动器门，从而防止气体离开气囊。 致动器门由致动器致动，致动器通过致动器导管与气体发生器流体连通。 系统操作使得来自气体发生器的气体展开使致动器膨胀，从而使致动器门密封通气通道。 气体发生器构造成在致动器门密封通气通道之后再次充气气囊。

公开(公告)号：US20110226898A1

公开(公告)日：2011-09-22

申请号：US13110607

申请日：2011-05-18

Applicant: Michael R. Smith ,  Cheng-Ho Tho ,  Somen Chowdhury

Inventor： Michael R. Smith ,  Cheng-Ho Tho ,  Somen Chowdhury

IPC: B64C25/56

CPC classification number: B64D25/00 ,  B64C27/04 ,  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 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, and a closed state, in which gas is retained within the interior of the airbag. The gas source is provided for at least partially re-inflating the airbag after venting of gas through the at least one vent.

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，用气体源产生的气体使气囊充气。 提供排气阀以控制通过每个排气口的气体流动，每个排气阀可选择性地配置在打开状态之间，气体可以从气囊的内部通过相关联的排气口，并且气体可以在气体 保持在气囊的内部。 气源被提供用于在通过至少一个排气口排出气体之后至少部分地重新充气气囊。