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1.发明授权公开(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
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。
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公开(公告)号：US20160096625A1
公开(公告)日：2016-04-07
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
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。
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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
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.
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公开(公告)号：US09925950B2
公开(公告)日：2018-03-27
申请号：US15096158
申请日：2016-04-11
Applicant: AmSafe, Inc.
Inventor： Trenton Dirk Moeller , Daniel Nick Foubert , Todd Joseph Humbert , Peter Anthony Settles , Ronald A. Shields
IPC: B60R21/18 , B60R21/2342 , B60R21/233 , B60R21/239 , B60R21/263 , B64D25/00 , B60R21/01
CPC classification number: B60R21/263 , B60R21/18 , B60R21/233 , B60R21/2342 , B60R21/239 , B60R2021/01231 , B60R2021/23324 , B60R2021/2395 , B64D25/00 , B64D2201/00
Abstract: Active airbag vent systems and associated systems and methods are described herein. An airbag system having an active vent configured in accordance with an embodiment of the present technology can include, for example, a first inflator operably coupled to a first hose for inflating an airbag in response to a rapid deceleration event. The airbag system can further include a second inflator operably coupled to a second hose configured to release a vent or seam on the airbag to rapidly deflate the airbag after initial deployment of the airbag.
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公开(公告)号：US20160133069A1
公开(公告)日：2016-05-12
申请号：US14874694
申请日：2015-10-05
Applicant: AmSafe, Inc.
Inventor： Ronald A. Shields , Peter Anthony Settles
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.
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Patent Agency Ranking
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
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。
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公开(公告)号：US20230373633A1
公开(公告)日：2023-11-23
申请号：US18184541
申请日：2023-03-15
Applicant: AmSafe, Inc.
Inventor： Ronald A. Shields , Peter Anthony Settles , Willard F. Hagan , Giuseppe Gullotto
IPC: B64D11/06 , B64D25/00 , B60R21/015 , B60R21/01 , B60R21/017 , B64D25/02 , G07C5/08
CPC classification number: B64D11/0621 , B64D25/00 , B64D11/06205 , B64D11/062 , B60R21/01546 , B60R21/01 , B60R21/0173 , B64D25/02 , G07C5/0808 , G07C5/0841 , B64D2201/00 , B60R21/0132
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.
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公开(公告)号：US11021123B2
公开(公告)日：2021-06-01
申请号：US16353200
申请日：2019-03-14
Applicant: AmSafe, Inc.
Inventor： Peter Anthony Settles , Scott Fink , Giuseppe Gullotto
IPC: B60R21/0132 , B60R21/017 , B64D25/06 , B64D45/00 , B60R21/015 , B64D11/06 , B60R21/0136 , B60R22/48 , B60R21/00
Abstract: An electronic module assembly for controlling the deployment of one or more airbags in an aircraft includes a power source, a crash sensor configured to produce a signal in response to a crash event and an accelerometer that is configured to produce a signal in response to a crash event. A processor starts a timer upon detection of the signal from the crash sensor. When the processor receives a signal from the crash sensor, the processor is configured to determine if a signal has also been received from the accelerometer and if signals from both the crash sensor and the accelerometer indicate a crash event then the processor reads a memory associated with an inflator. The processor reads a timing value selected for the inflator and fires the inflator when the timer has a value equal to the timing value selected for the inflator.
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公开(公告)号：US20180244229A1
公开(公告)日：2018-08-30
申请号：US15445644
申请日：2017-02-28
Applicant: AmSafe, Inc.
Inventor： Peter Anthony Settles , Scott Fink , Giuseppe Gullotto
IPC: B60R21/0132 , B60R21/017 , B60R22/48 , B64D25/06 , B64D45/00
CPC classification number: B60R21/0132 , B60R21/0136 , B60R21/01546 , B60R21/017 , B60R2021/0093 , B60R2022/4816 , B64D11/0621 , B64D25/06 , B64D45/00 , B64D2045/008
Abstract: An electronic module assembly for controlling the deployment of one or more airbags in an aircraft includes a power source, a crash sensor configured to produce a signal in response to a crash event and an accelerometer that is configured to produce a signal in response to a crash event. A processor starts a timer upon detection of the signal from the crash sensor. When the processor receives a signal from the crash sensor, the processor is configured to determine if a signal has also been received from the accelerometer and if signals from both the crash sensor and the accelerometer indicate a crash event then the processor reads a memory associated with an inflator. The processor reads a timing value selected for the inflator and fires the inflator when the timer has a value equal to the timing value selected for the inflator.
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公开(公告)号：US20160297396A1
公开(公告)日：2016-10-13
申请号：US15096158
申请日：2016-04-11
Applicant: AmSafe, Inc.
Inventor： Trenton Dirk Moeller , Daniel Nick Foubert , Todd Joseph Humbert , Peter Anthony Settles , Ronald A. Shields
IPC: B60R21/263 , B60R21/207 , B60R21/262 , B60R21/2342 , B60R21/239 , B64D25/00 , B60R21/233
CPC classification number: B60R21/263 , B60R21/18 , B60R21/233 , B60R21/2342 , B60R21/239 , B60R2021/01231 , B60R2021/23324 , B60R2021/2395 , B64D25/00 , B64D2201/00
Abstract: Active airbag vent systems and associated systems and methods are described herein. An airbag system having an active vent configured in accordance with an embodiment of the present technology can include, for example, a first inflator operably coupled to a first hose for inflating an airbag in response to a rapid deceleration event. The airbag system can further include a second inflator operably coupled to a second hose configured to release a vent or seam on the airbag to rapidly deflate the airbag after initial deployment of the airbag.
Abstract translation: 主动安全气囊排气系统及相关系统和方法在本文中描述。 具有根据本技术的实施例构造的活动通气孔的气囊系统可以包括例如可操作地联接到第一软管的第一充气器，用于响应于快速减速事件使气囊膨胀。 气囊系统还可以包括可操作地联接到第二软管的第二充气器，该第二软管构造成在气囊的初始展开之后释放气囊上的通气孔或接缝，以使气囊快速放气。
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