公开(公告)号：US11220341B2

公开(公告)日：2022-01-11

申请号：US16896041

申请日：2020-06-08

Applicant: Textron Innovations Inc.

Inventor： Eric A. Sinusas ,  Olivier Andre Boisvert ,  Guillaume Noiseux-Boucher ,  Steve Loveland ,  Sebastien Duval

IPC: B64D11/06 ,  B64D25/02

Abstract: A modal restraint system for an occupant of a seat of an aircraft having a mechanical failure sensor includes a strap feeder unit and a strap selectively retractable into and extendable from the strap feeder unit. The strap is positionable adjacent to the occupant. The strap feeder unit is adapted to switch between a plurality of modes including an unfixed mode and a fixed mode. The strap is extendable from and retractable into the strap feeder unit in the unfixed mode. The strap is substantially unextendable from the strap feeder unit in the fixed mode. The strap feeder unit is in the unfixed mode by default. The strap feeder unit is operable to switch to the fixed mode in response to a precautionary event including detection of an aircraft mechanical failure by the mechanical failure sensor, thereby reducing freedom of movement of the occupant relative to the seat.

公开(公告)号：US20200307798A1

公开(公告)日：2020-10-01

申请号：US16896041

申请日：2020-06-08

Applicant: Textron Innovations Inc.

Inventor： Eric A. Sinusas ,  Olivier Andre Boisvert ,  Guillaume Noiseux-Boucher ,  Steve Loveland ,  Sebastien Duval

IPC: B64D11/06 ,  B64D25/02

Abstract: A modal restraint system for an occupant of a seat of an aircraft having a mechanical failure sensor includes a strap feeder unit and a strap selectively retractable into and extendable from the strap feeder unit. The strap is positionable adjacent to the occupant. The strap feeder unit is adapted to switch between a plurality of modes including an unfixed mode and a fixed mode. The strap is extendable from and retractable into the strap feeder unit in the unfixed mode. The strap is substantially unextendable from the strap feeder unit in the fixed mode. The strap feeder unit is in the unfixed mode by default. The strap feeder unit is operable to switch to the fixed mode in response to a precautionary event including detection of an aircraft mechanical failure by the mechanical failure sensor, thereby reducing freedom of movement of the occupant relative to the seat.

公开(公告)号：US20200094973A1

公开(公告)日：2020-03-26

申请号：US16138216

申请日：2018-09-21

Applicant: GOODRICH CORPORATION

Inventor： Jaro S. Volny ,  Kassidy L. Carson ,  Scott R. Patterson ,  Drew Hartman

IPC: B64D25/02 ,  B64D17/30 ,  B64D25/10

Abstract: An inflatable head restraint system for a parachute assembly may comprise an inflatable volume configured to inflate in response to a deployment of the parachute assembly. The inflatable volume may be located between a left shoulder riser and a right shoulder riser of the parachute assembly. A conduit may be fluidly coupled to the inflatable volume.

公开(公告)号：US20190023403A1

公开(公告)日：2019-01-24

申请号：US16140684

申请日：2018-09-25

Applicant: THE BOEING COMPANY

Inventor： Darren Carl McIntosh ,  Jeff S. Siegmeth

IPC: B64D11/06 ,  B64D25/02 ,  B64D11/00 ,  B64D11/02 ,  B64D11/04

CPC classification number: B64D11/0606 ,  B64D11/0023 ,  B64D11/02 ,  B64D11/04 ,  B64D25/02

Abstract: A monument is configured to be positioned within an internal cabin of a vehicle. The monument includes a deployable portion. The deployable portion is configured to move from a non-deployed state into a deployed state when a force that meets or exceeds a predetermined threshold is exerted into the monument wall assembly.

公开(公告)号：US20160052636A1

公开(公告)日：2016-02-25

申请号：US14808983

申请日：2015-07-24

Applicant: AmSafe, Inc.

Inventor： Trenton Dirk Moeller ,  Giuseppe Gullotto

IPC: B64D25/02

Abstract: An airbag assembly for leg flail protection and associated systems and methods are described herein. An airbag system configured in accordance with an embodiment of the present technology can include, for example, a housing having a cavity and an opening in communication with the cavity, an airbag stowed within the cavity, and an inflator operably coupled to the airbag. The airbag can be configured to deploy through the opening of the housing during a crash or other significant dynamic event. The airbag can deploy outwardly from the side-facing seat to reduce occupant leg rotation during the crash or other significant dynamic event. The airbag can be pushed out of the housing before it is fully inflated. The airbag can be stowed and include folded first and second opposing side portions such that when the airbag is deployed, the portion nearest the occupant unfurls toward the occupant prior to the other portion farthest from the occupant unfurling in a direction away from the occupant.

Abstract translation: 本文描述了用于腿箍保护的安全气囊组件和相关联的系统和方法。 根据本技术的实施例构造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，存放在空腔内的气囊和可操作地联接到气囊的充气器。 安全气囊可以配置成在碰撞或其他重大动态事件期间通过壳体的开口部署。 安全气囊可以从侧面的座椅向外展开，以减少在碰撞或其他重大动态事件期间的乘员腿部旋转。 气囊在完全充气之前可以从壳体推出。 安全气囊可以被收起并且包括折叠的第一和第二相对侧部分，使得当安全气囊展开时，最靠近乘员的部分在离乘员远离乘员的方向展开的另一部分之前向乘员敞开。

公开(公告)号：US08876205B2

公开(公告)日：2014-11-04

申请号：US13702943

申请日：2011-06-06

Applicant: Mario Maevert

Inventor： Mario Maevert

IPC: B60N2/42 ,  B60N2/427 ,  B60N2/24 ,  B60N2/50 ,  B63B29/04 ,  B64D11/06 ,  B64D25/02 ,  B64D25/06

CPC classification number: B60N2/4242 ,  B60N2/24 ,  B60N2/427 ,  B60N2/503 ,  B63B29/04 ,  B64D11/06 ,  B64D11/062 ,  B64D25/02 ,  B64D25/06

Abstract: A safety seat for land vehicles, aircraft and watercraft, having a seat part frame, and a backrest frame suspended on a restraint or suspension strap firmly attached to the vehicle, wherein the backrest frame has a lateral or transverse strut, and an additional holding strap clamps the lateral strut in. A separate mounting frame is provided to fix the restraint strap and the holding strap, and can be mounted in the vehicle, wherein bushing or guide-through eyes and attachment eyes for stretching the restraint strap and the holding strap are provided on the oppositely disposed lateral or transverse supports of the mounting frame, and wherein the holding strap is formed integrally, is fixed by its two ends to two attachment eyes, and is looped through, and passed back and forth between, a plurality of bushing eyes.

Abstract translation: 用于陆上车辆，飞机和船舶的安全座椅，具有座椅部分框架，以及悬挂在牢固地附接到车辆的约束或悬挂带上的靠背框架，其中靠背框架具有横向或横向支柱和附加的保持带 夹紧横向支柱。设置单独的安装框架以固定约束带和固定带，并且可以安装在车辆中，其中用于拉伸约束带和固定带的衬套或引导眼睛和附着眼睛是 设置在安装框架的相对设置的横向或横向支撑件上，并且其中保持带一体地形成，其两端固定到两个附接眼睛，并且环绕并在多个衬套之间来回传递 眼睛

公开(公告)号：US20130088055A1

公开(公告)日：2013-04-11

申请号：US13583766

申请日：2010-10-12

Applicant: István Gubás

Inventor： István Gubás

IPC: B64D25/02 ,  B60N2/427 ,  B60N2/42 ,  B64D11/06 ,  B64D25/04

CPC classification number: B64D25/02 ,  B60N2/0745 ,  B60N2/42 ,  B60N2/4256 ,  B60N2/427 ,  B60N2/686 ,  B64D11/06 ,  B64D11/0619 ,  B64D11/062 ,  B64D11/06205 ,  B64D11/0621 ,  B64D25/04

Abstract: The safety seat according to the invention contains a lower fastening 5 structure (5), seat surface, squab and head support (9) and safety belt, and further it is provided with a casing (1) surrounding said seat surface (8), squab and head support (9), having an egg shape and being provided with a door (2) form-fitting on said casing (1) and rotatable in horizontal direction. The safety seat is provided with air-bags (10, 11) and there is a weakened part or a releasable lock 10 between the lower fastening structure (5) and the casing (1), releasing in answer to shock like load. (FIG. 1)

Abstract translation: 根据本发明的安全座椅包括下紧固件5结构（5），座椅表面，小腿和头部支撑件（9）和安全带，并且还设置有围绕所述座椅表面（8）的壳体（1） 具有卵形状并且具有形成在所述壳体（1）上并可沿水平方向旋转的门（2）的小腿和头部支撑件（9）。 安全座具有气囊（10,11），并且在下紧固结构（5）和壳体（1）之间存在弱化部分或可释放的锁10，释放以应付诸如负载的冲击。 （图。1）

公开(公告)号：US08286559B2

公开(公告)日：2012-10-16

申请号：US12580827

申请日：2009-10-16

Applicant: Justin Robinson ,  Brian Ford

Inventor： Justin Robinson ,  Brian Ford

IPC: E01B25/22 ,  B64D25/02

CPC classification number: B64D25/06 ,  B64D25/02

Abstract: Disclosed is a trolley assembly that is adapted to be used with a passenger restraint, such as a locking reel. The trolley assembly allows the reel lock to be securely positioned at any of a number of discrete locations along the length of an associated track. A mechanism is included for permitting the user to selectively lock and unlock the trolley as needed.

Abstract translation: 公开了一种适于与诸如锁定卷轴的乘客约束装置一起使用的手推车组件。 手推车组件允许卷轴锁被牢固地定位在沿着相关轨道的长度的多个离散位置中的任何一个处。 包括用于允许用户根据需要选择性地锁定和解锁手推车的机构。

公开(公告)号：US20120259484A1

公开(公告)日：2012-10-11

申请号：US13174659

申请日：2011-06-30

Applicant: Ronald A. Shields ,  Peter A. Settles ,  Willard F. Hagan ,  Joseph Smith

Inventor： Ronald A. Shields ,  Peter A. Settles ,  Willard F. Hagan ,  Joseph Smith

IPC: G06F19/00 ,  G09F9/33 ,  G01M17/00 ,  G08B5/00 ,  B60R22/48 ,  B64D25/02

CPC classification number: B64D11/0621 ,  B64D11/062 ,  B64D11/06205 ,  B64D25/00 ,  B64D25/02 ,  B64D2201/00 ,  G07C5/0808 ,  G07C5/0841

Abstract: An electronic module assembly (EMA) for use in controlling one or more personal restraint systems. A programmed processor within the EMA is configured to determine when a personal restraint system associated with each seat in a vehicle should be deployed. In addition, the programmed processor is configured to perform a diagnostic self-test to determine if the EMA and the personal restraint systems are operational. In one embodiment, results of the diagnostic self-test routine are displayed on a display included on the electronic module assembly. In an alternative embodiment, the results of the diagnostic self-test routine are transmitted via a wireless transceiver to a remote device. The remote device can include a wireless interrogator or can be a remote computer system such as a cabin management computer system.

Abstract translation: 一种用于控制一个或多个个人约束系统的电子模块组件（EMA）。 EMA内的编程处理器被配置为确定何时应该部署与车辆中的每个座椅相关联的个人约束系统。 此外，编程处理器被配置为执行诊断自检，以确定EMA和个人约束系统是否可操作。 在一个实施例中，诊断自检程序的结果被显示在包括在电子模块组件上的显示器上。 在替代实施例中，诊断自检程序的结果通过无线收发器传送到远程设备。 远程设备可以包括无线询问器，或者可以是诸如客舱管理计算机系统的远程计算机系统。

公开(公告)号：US20090212159A1

公开(公告)日：2009-08-27

申请号：US12372658

申请日：2009-02-17

Applicant: Matthew M. O'Brien ,  Christopher C. Culbertson ,  Colin A. Godby ,  Stephen M. King ,  Grant R. McCloud ,  Charles E. Van Druff

Inventor： Matthew M. O'Brien ,  Christopher C. Culbertson ,  Colin A. Godby ,  Stephen M. King ,  Grant R. McCloud ,  Charles E. Van Druff

IPC: B64D25/02 ,  B64D25/06 ,  B60R22/36 ,  B60R22/38 ,  B64D25/00

CPC classification number: B60R22/34 ,  B60R22/00 ,  B64D25/06

Abstract: In a preferred embodiment, a restraint system is described for restraining a standing occupant in a vehicle such as a plane or helicopter. The restraint system includes a webbing strap that winds and unwinds from a spool assembly. The spool assembly includes a trigger assembly that locks a spool from rotation, a manual release assembly for manually releasing the trigger assembly and lock, and an adjustable payout assembly that determines the maximum length that the webbing strap can be pulled out before stopping (i.e., the number of rotations of the spool). The trigger assembly can trigger the lock assembly from one or more sensors. Further, the trigger assembly can be arranged to automatically unlock after a triggering event, manually unlocked after a triggering event or a combination of the two for different sensors.

Abstract translation: 在优选实施例中，描述了约束系统以限制诸如平面或直升机的车辆中的站立乘客。 约束系统包括从卷轴组件卷绕和展开的织带。 阀芯组件包括一个将阀芯从旋转中锁定的触发器组件，用于手动释放触发器组件和锁定的手动释放组件，以及一个可调节的支撑组件，其确定在停止之前能够拉出带状带的最大长度（即， 卷轴的转数）。 触发器组件可以从一个或多个传感器触发锁组件。 此外，触发器组件可以被布置成在触发事件之后自动解锁，在触发事件之后手动解锁或者针对不同传感器的两者的组合。