公开(公告)号：US20160176509A1

公开(公告)日：2016-06-23

申请号：US14757591

申请日：2015-12-23

Applicant: Airbus Operations, S.L.

Inventor： Javier Toral Vazquez ,  Diego Folch Cortes ,  Esteban Martino Gonzalez ,  Pablo Goya Abaurrea ,  Vasilis Votsios ,  Michel Fouinnetau ,  Sylvain Roumegas

IPC: B64C11/20 ,  B64D45/00

CPC classification number: B64C11/26 ,  B64D2201/00

Abstract: The disclosure refers to a propeller blade for an aircraft engine that includes an airbag system contained inside the blade and comprising at least one bag and at least one gas generator, the at least one gas generator in fluid communication with at least one bag for inflating the bag, a detecting system for detecting a rupture of a part of the blade, a trigger for activating the at least one gas generator when the rupture is detected by the detecting system, and the blade skin being configured for allowing the at least one bag to pass through the blade skin for being expanded outside the blade upon the bag inflation by the gas generator.

Abstract translation: 本发明涉及一种用于飞行器发动机的螺旋桨叶片，其包括包含在叶片内部并包括至少一个袋和至少一个气体发生器的气囊系统，所述至少一个气体发生器与至少一个袋流体连通，用于使 袋，用于检测叶片的一部分破裂的检测系统，用于当由检测系统检测到破裂时启动至少一个气体发生器的触发器，并且叶片皮肤被配置为允许至少一个袋子 穿过叶片皮肤，以在气体发生器的袋子充气时在叶片外部膨胀。

公开(公告)号：US20160167793A1

公开(公告)日：2016-06-16

申请号：US14970570

申请日：2015-12-16

Applicant: AIRBUS GROUP SAS

Inventor： Jean-Francois GENESTE

IPC: B64D25/02 ,  B60R21/231

CPC classification number: B64D25/02 ,  B60R19/205 ,  B60R21/231 ,  B64D25/00 ,  B64D2201/00 ,  B64G1/62

Abstract: A protection system (15) includes an inflatable bag (16) connected to inflation elements able and intended to be activated so as to inflate the inflatable bag in the event of and/or upon the prediction of an impact. The inflatable bag (16) has a substantially annular overall shape when inflated. Such a protection system (15) is advantageously intended to protect the passengers in a helicopter.

Abstract translation: 保护系统（15）包括连接到能够且预期被启动的充气元件的充气袋（16），以便在预测碰撞和/或预测碰撞的情况下使充气袋膨胀。 充气袋（16）在膨胀时具有基本环形的整体形状。 这种保护系统（15）有利地用于保护直升机中的乘客。

公开(公告)号：US09176202B2

公开(公告)日：2015-11-03

申请号：US13608959

申请日：2012-09-10

Applicant: Andre Baca ,  Ronald A. Shields ,  Willard F. Hagan

Inventor： Andre Baca ,  Ronald A. Shields ,  Willard F. Hagan

IPC: G01R33/00 ,  G05B23/02 ,  B64D11/06 ,  G05B9/02

CPC classification number: G01R33/0047 ,  B64D11/062 ,  B64D11/06205 ,  B64D2201/00 ,  G05B9/02 ,  G05B23/0256 ,  Y02T50/46

Abstract: Electronics module assemblies (“EMAs”) for inflatable personal restraints and associated systems are described herein. An EMA configured in accordance with an embodiment of the present technology can include, for example, a housing having a body portion, cover portion that attaches to the body portion to form an enclosure, and protrusion extending outwardly from the cover portion. The protrusion can have an outer boundary at which the protrusion projects away from the cover portion. The EMA can further include a crash sensor within the enclosure in an area defined by the outer boundary of the protrusion. The protrusion can form an envelope of space around the crash sensor that defines a minimum distance an external object with a magnetic field can come to the crash sensor without activating it. The EMA can optionally include a magnetic field configured to disable the crash sensor upon the detection of an external magnetic field.

Abstract translation: 本文描述了用于充气个人约束和相关系统的电子模块组件（“EMA”）。 根据本技术的实施例构造的EMA可以包括例如具有主体部分的壳体，附接到主体部分以形成外壳的盖部分和从盖部分向外延伸的突出部。 突出部可以具有突出部远离盖部突出的外边界。 EMA还可以在外壳内的碰撞传感器包括在突起的外边界限定的区域内。 突起可以形成围绕碰撞传感器的空间的包络，其限定具有磁场的外部物体可以到达碰撞传感器而不激活它的最小距离。 EMA可以可选地包括被配置为在检测到外部磁场时禁用碰撞传感器的磁场。

公开(公告)号：US09153080B2

公开(公告)日：2015-10-06

申请号：US14468170

申请日：2014-08-25

Applicant: AmSafe, Inc.

Inventor： Ronald A. Shields ,  Peter Anthony Settles

IPC: G05B23/02 ,  G07C5/08 ,  B64D11/06 ,  B64D25/02

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：US20150232184A1

公开(公告)日：2015-08-20

申请号：US14705915

申请日：2015-05-06

Applicant: AmSafe, Inc.

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

IPC: B64D11/06 ,  B60R21/231 ,  B60R21/26 ,  B60R21/20

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：US20150217613A1

公开(公告)日：2015-08-06

申请号：US14684995

申请日：2015-04-13

Applicant: Piasecki Aircraft Corporation

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

IPC: B60F5/02 ,  B64C27/57 ,  B64C11/00 ,  B64C27/32 ,  B64C3/38 ,  B64C3/56 ,  B64C37/00 ,  B64C27/52

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.

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，其可以是管道式风扇。

公开(公告)号：US20150042078A1

公开(公告)日：2015-02-12

申请号：US14384655

申请日：2013-01-09

Applicant: AmSafe, Inc.

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

IPC: B64D25/00

CPC classification number: B64D11/062 ,  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.

Abstract translation: 结构安装的安全气囊组件和相关联的系统和方法在本文中描述。 根据本公开的实施例配置的气囊系统可以包括例如具有空腔和与空腔连通的开口的壳体，腔内的气囊组件以及可操作地联接到气囊组件的充气器。 安全气囊组件可以包括气囊，其构造成在碰撞事件期间部署穿过壳体的开口。 安全气囊系统还可以包括可拆卸地定位成横跨开口并且构造成在气囊展开期间远离开口移动的门。 外壳可以固定在飞行器的内部，在飞机座前方并偏离飞机座。

公开(公告)号：US20140252166A1

公开(公告)日：2014-09-11

申请号：US13840911

申请日：2013-03-15

Applicant: Bell Helicopter Textron Inc.

Inventor： Michael R. Smith ,  Cheng-Ho Tho

IPC: B64C25/56

CPC classification number: B64C25/56 ,  B64C27/006 ,  B64C2025/325 ,  B64D25/18 ,  B64D2201/00

Abstract: An apparatus comprising a float bag comprising an air bladder configured to inflate when an aircraft lands in the water, a girt coupled to the air bladder and configured to attach the air bladder to the aircraft via at least one airframe fitting, and a load attenuator coupled to the girt and configured to be positioned between the girt and the airframe fitting when the float bag is attached to the aircraft.

Abstract translation: 一种包括浮动袋的装置，包括气囊，其配置成当飞行器落在水中时使其膨胀，连接到空气囊并被构造成通过至少一个机身接头将空气囊附接到飞行器，并且耦合到负载衰减器 并且构造成当浮子袋附接到飞行器时定位在棉纱和机身配件之间。

公开(公告)号：US08746735B2

公开(公告)日：2014-06-10

申请号：US13551071

申请日：2012-07-17

Applicant: Pete C. Meister ,  Michael Oleston

Inventor： Pete C. Meister ,  Michael Oleston

IPC: B60R21/18

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：US20130320144A1

公开(公告)日：2013-12-05

申请号：US13894944

申请日：2013-05-15

Applicant: ARIBUS SAS ,  AIRBUS OPERATIONS S.L.

Inventor： Ludovic GERARD ,  Alejandro GUTIÉRREZ GARCÍA ,  Julián MALDONADO

IPC: B64C23/00

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。