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    Circuitry for testing inflatable personal restraint systems
    1.
    发明授权
    Circuitry for testing inflatable personal restraint systems 有权

    公开(公告)号：US10364034B2

    公开(公告)日：2019-07-30

    申请号：US14840916

    申请日：2015-08-31

    Applicant: AmSafe, Inc.

    Inventor： Ronald A. Shields ,  Peter Anthony Settles ,  Willard F. Hagan ,  Giuseppe Gullotto

    IPC: B64D11/06 ,  G07C5/08 ,  B64D25/00 ,  B64D25/02

    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.

    SEATBELT ANCHOR SYSTEMS FOR AIRCRAFT AND OTHER VEHICLES, AND ASSOCIATED METHODS OF MANUFACTURE AND USE
    5.
    发明申请
    SEATBELT ANCHOR SYSTEMS FOR AIRCRAFT AND OTHER VEHICLES, AND ASSOCIATED METHODS OF MANUFACTURE AND USE 有权
    用于飞机和其他车辆的西班牙锚固系统及相关的制造和使用方法

    公开(公告)号：US20150352991A1

    公开(公告)日：2015-12-10

    申请号：US14297457

    申请日：2014-06-05

    Applicant: AmSafe, Inc.

    Inventor： Todd J. Humbert

    IPC: B60N2/68 ,  B64D11/00 ,  B60R21/02

    CPC classification number: B60N2/688 ,  B60R21/02 ,  B60R22/18 ,  B64D11/00 ,  B64D11/062 ,  Y02T50/46 ,  Y10T24/40 ,  Y10T24/45251 ,  Y10T24/45984

    Abstract: The present disclosure describes apparatuses, devices and systems for attaching seatbelts to anchoring structures in aircraft and other vehicles. In some embodiments, such apparatuses include a modular connector having a base configured to be attached to an anchoring structure, a body configured to be attached to a seatbelt, and an annular lock configured to releasably couple the body to the base. In these embodiments, the body carries the lock adjacent to an aperture configured removably receive the base. When the body is pressed over the base, the base passes into the aperture and contacts the annular lock, expanding the lock outwardly around the base. The base continues moving though the aperture in the body until the lock retracts into a groove in base, thereby releasaby locking the body to the base.

    Abstract translation: 本公开描述了用于将安全带附接到飞机和其他车辆中的锚定结构的装置，装置和系统。 在一些实施例中，这样的设备包括具有被配置为附接到锚定结构的基座的模块化连接器，被配置为附接到安全带的主体以及被配置为将主体可释放地连接到基座的环形锁。 在这些实施例中，主体承载与配置成可拆卸地接收底座的孔相邻的锁。 当主体被压在基座上时，基座进入孔口并接触环形锁，将锁定件向外扩展到基座周围。 基座继续移动通过主体中的孔，直到锁缩回到基座中的凹槽中，从而将本体锁定到基座上。

    COMPUTER SYSTEM FOR REMOTE TESTING OF INFLATABLE PERSONAL RESTRAINT SYSTEMS
    6.
    发明申请
    COMPUTER SYSTEM FOR REMOTE TESTING OF INFLATABLE PERSONAL RESTRAINT SYSTEMS 有权
    用于远程测试可充电个人限制系统的计算机系统

    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。

    SEAT HARNESS PRETENSIONER
    7.
    发明申请
    SEAT HARNESS PRETENSIONER 有权
    西雅特线束预制器

    公开(公告)号：US20140167459A1

    公开(公告)日：2014-06-19

    申请号：US13926325

    申请日：2013-06-25

    Applicant: AmSafe, Inc.

    Inventor： David T. Merrill ,  Todd J. Humbert

    IPC: B60R22/195 ,  B60N2/42

    CPC classification number: B60R22/195 ,  B60N2/24 ,  B60N2/4242 ,  B60N2/688 ,  B60R22/1951 ,  B60R22/24 ,  B60R22/26 ,  B60R2022/027 ,  B60R2022/1825

    Abstract: Various embodiments of seat harness pretensioning devices for use in land, air, and sea vehicles are described herein. In one embodiment, a seat unit for use in a military land vehicle or helicopter includes a stroking device that enables the seat to move downwardly in response to sudden movement. The seat unit also includes a seat belt or harness that extends around the occupant in the seat. Sudden movement of the seat in response to an explosion or hard landing causes a tensioning system to automatically pretension the seat harness.

    Abstract translation: 本文描述了用于陆地，空中和海上车辆的座椅线束预张紧装置的各种实施例。 在一个实施例中，用于军用陆地车辆或直升机的座椅单元包括能够使座椅响应于突然移动而向下移动的抚摸装置。 座椅单元还包括围绕座椅中的乘员延伸的安全带或线束。 响应于爆炸或硬着陆而座椅的突然移动导致张紧系统自动地张紧座椅安全带。

    SEAT BELT WEB RETRACTORS AND ASSOCIATED SYSTEMS AND METHODS
    8.
    发明申请
    SEAT BELT WEB RETRACTORS AND ASSOCIATED SYSTEMS AND METHODS 有权

    公开(公告)号：US20240391595A1

    公开(公告)日：2024-11-28

    申请号：US18674344

    申请日：2024-05-24

    Applicant: AmSafe, Inc.

    Inventor： Kenneth Heck ,  Christopher Arnold ,  Todd Humbert

    IPC: B64D25/06

    Abstract: Seat belt web retractors having web locking mechanisms are described herein. In some embodiments, a seat belt web retractor includes an inertial locking mechanism operably coupled to a spool about which a seat belt web is wound. The web retractor further includes a web locking mechanism operably coupled to the inertial locking mechanism. The web locking mechanism can include a driving member that is actuated by engagement of the inertial locking mechanism with the web spool in response to rapid extraction of the web from the retractor. Actuation of the driving member drives first and second clamping portions toward each other, thereby clamping the web in between the clamping members and restraining the web from further movement out of the retractor.

    OCCUPANT RESTRAINT SYSTEMS FOR USE ON AIRCRAFT
    9.
    发明申请
    OCCUPANT RESTRAINT SYSTEMS FOR USE ON AIRCRAFT 有权

    公开(公告)号：US20210229814A1

    公开(公告)日：2021-07-29

    申请号：US16773854

    申请日：2020-01-27

    Applicant: AmSafe, Inc.

    Inventor： Michael Shawn Haycraft ,  Bradley Scott Walker

    IPC: B64D11/06

    Abstract: Occupant restraint systems for use in aircraft and other vehicles are described herein. In some embodiments, the occupant restraint systems include an under-seat airbag positioned below a seat cushion having a separation feature extending laterally therethrough. The separation feature enables a front cushion portion to move upwardly and away from a seat pan by a greater distance than a rear cushion portion upon inflation of the under-seat airbag, thereby favorably positioning the seat occupant's thighs relative to the seat occupant's torso.

    MULTI-CHAMBER AIRBAGS AND ASSOCIATED METHODS OF MANUFACTURE AND USE
    10.
    发明申请
    MULTI-CHAMBER AIRBAGS AND ASSOCIATED METHODS OF MANUFACTURE AND USE 审中-公开

    公开(公告)号：US20170225788A1

    公开(公告)日：2017-08-10

    申请号：US15398977

    申请日：2017-01-05

    Applicant: AmSafe, Inc.

    Inventor： Todd Joseph Humbert

    IPC: B64D11/06 ,  B60R21/2338 ,  B60R21/276 ,  B60R21/235 ,  B60R21/237 ,  B60R21/239 ,  B60R21/18 ,  B60R21/2342

    CPC classification number: B60R21/18 ,  B60R21/233 ,  B60R2021/0044 ,  B60R2021/0093 ,  B60R2021/23115 ,  B60R2021/23308 ,  B60R2021/23386 ,  B64D11/06205 ,  B64D2201/00

    Abstract: Multi-chamber airbag systems for use in aircraft and other vehicles are described herein. In some embodiments, an occupant restraint system includes a multi-chamber airbag that deploys from an occupant restraint (e.g., a lap seat belt) in an aircraft. The multi-chamber airbag can include a first portion that inflates generally upward in front of the occupant's torso, and a second portion that inflates in front of the first portion. The first portion and/or the second portion can include multiple chambers (e.g., generally cylindrical-shaped chambers) that, when inflated, provide the airbag with a shape and/or contact surfaces which can help to maintain the position of the airbag between the occupant and a strike object or hazard. In other embodiments, multi-chamber airbags configured in accordance with the present disclosure can me mounted to a structure (e.g., a monument, console, seat back, etc.) positioned generally in front of the occupant. The structure-mounted airbag can deploy generally toward the occupant in the event of a vehicle impact or other potentially harmful event to protect the occupant from impact injury.

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