公开(公告)号：US09643725B2

公开(公告)日：2017-05-09

申请号：US14801959

申请日：2015-07-17

Applicant: The Boeing Company

Inventor： Thomas E. Dowhower ,  Peter M. Heinrich ,  John A. Lepore

IPC: B60R21/01 ,  B60R22/00 ,  B64D11/00 ,  B64D25/00 ,  B64D11/06 ,  B60R22/02

CPC classification number: B64D11/06205 ,  B60R2021/01177 ,  B60R2022/021 ,  B64D11/0621 ,  B64D25/00 ,  B64D2201/00

Abstract: A safety device has a lower portion and an upper portion. The lower portion defines a cavity for receiving a seat belt buckle assembly and has at least one rear wall portion extending between opposing sidewalls that partially define the cavity. The rear wall portion forms a slot area to permit a strap attached to the seat belt buckle assembly to extend from the cavity when the seat belt buckle assembly is positioned in the cavity. The rear wall portion is configured to prevent the seat belt buckle assembly from moving laterally out of the cavity. The upper portion is hingedly coupled to the lower portion such that the upper portion completely covers the cavity of the lower portion when the upper portion is rotated into engagement with the lower portion.

公开(公告)号：US20170106982A1

公开(公告)日：2017-04-20

申请号：US15050866

申请日：2016-02-23

Applicant: AMI Industries, Inc.

Inventor： Poly Puthur John ,  S. Shyam Sundar Iyer ,  Manjunatha Prabhudevaiah

IPC: B64D11/06

CPC classification number: B64D11/0647 ,  A47C27/10 ,  B60N2/914 ,  B64D2201/00

Abstract: A pressure control system for an aircraft seat includes a base plate and a plurality of cells attached to the base plate, each cell having a bellows and a top inflatable diaphragm and defines a pressure chamber therein. Charging apertures are formed in the base plate such that each cell has an associated charging aperture such that each charging aperture is in fluid communication with a pressure chamber. Discharging apertures are formed in the base plate such that each cell has an associated discharging aperture such that each discharging apertures is in fluid communication a pressure chamber. A charging valve and a discharging valve is in fluid communication with the pressure chambers and configured to supply or extract air to or from the chambers through the apertures. A pump is configured to supply pressurized air to the at least one charging valve.

公开(公告)号：US20170016702A1

公开(公告)日：2017-01-19

申请号：US15211407

申请日：2016-07-15

Applicant: Benteler Steel/Tube GmbH

Inventor： Thomas Vietoris ,  Jozef Balun ,  Olivier Depierreux

IPC: F42B3/04 ,  C22C38/14 ,  C22C38/12 ,  C22C38/08 ,  C22C38/06 ,  A62C3/08 ,  C22C38/02 ,  C22C38/00 ,  B60R21/264 ,  B64D25/10 ,  B64G1/40 ,  F02K9/60 ,  C22C38/16 ,  C22C38/04

CPC classification number: F42B3/04 ,  B60R21/264 ,  B60R21/268 ,  B60R2021/26082 ,  B64D11/0621 ,  B64D25/10 ,  B64D2201/00 ,  B64G1/26 ,  B64G1/40 ,  C22C38/001 ,  C22C38/002 ,  C22C38/02 ,  C22C38/04 ,  C22C38/06 ,  C22C38/08 ,  C22C38/12 ,  C22C38/14 ,  C22C38/16 ,  F02K9/60 ,  Y02T50/46

Abstract: The present invention relates to a gas generator, comprising a comprising a tubular element (10) with high low-temperature toughness. The gas generator is characterized in that the tubular element (10) has a ductile fracture behavior at temperature to at least −196° C., the tubular element (10) has a minimal tensile strength of 650 MPa, the tubular element (10) has a cubic face-centered austenitic structure with at least 90 area percentage and the tubular element (10) consists of a steel alloy which has a manganese content of at least 14.0 wt %

Abstract translation: 气体发生器技术领域本发明涉及一种气体发生器，其包括具有高低温韧性的管状元件（10）。 气体发生器的特征在于，管状元件（10）在至少-196℃的温度下具有延性断裂性能，管状元件（10）的拉伸强度最小为650MPa，管状元件（10） 具有至少90面积百分比的立方面中心奥氏体结构，并且管状元件（10）由锰含量为至少14.0重量％的钢合金组成，

公开(公告)号：US20170015425A1

公开(公告)日：2017-01-19

申请号：US14801994

申请日：2015-07-17

Applicant: The Boeing Company

Inventor： John A. Lepore ,  Thomas E. Dowhower ,  Peter M. Heinrich

IPC: B64D11/06 ,  B64D25/00

CPC classification number: B64D11/06205 ,  A44B11/2526 ,  A44B11/2569 ,  B60R21/18 ,  B60R2021/01177 ,  B60R2022/021 ,  B64D25/00 ,  B64D2201/00

Abstract: A safety device for preventing accidental discharge of an airbag. A lower portion of the safety device includes two opposing sidewalls at least partially defining a cavity for holding a seat belt buckle assembly. An upper portion of the safety devices is hingedly coupled to the lower portion. The safety device also includes a mechanism for securely latching the upper portion to the lower portion and a mechanism for releasing the upper portion from the lower portion when the upper portion is securely latched to the lower portion to allow the upper portion to rotate away from the lower portion.

Abstract translation: 一种用于防止意外排出气囊的安全装置。 安全装置的下部包括两个相对的侧壁，其至少部分地限定用于保持安全带扣组件的空腔。 安全装置的上部铰接地联接到下部。 安全装置还包括用于将上部牢固地锁定到下部的机构，以及用于当上部被牢固地锁定到下部时将上部从下部释放的机构，以允许上部从远离 下部。

公开(公告)号：US20160368610A1

公开(公告)日：2016-12-22

申请号：US14850642

申请日：2015-09-10

Applicant: Alan Jamal ERICKSON

Inventor： Alan Jamal ERICKSON

IPC: B64D17/72 ,  B64C39/02 ,  B64D17/80

CPC classification number: B64D17/72 ,  B64C39/024 ,  B64C2201/027 ,  B64C2201/185 ,  B64D17/80 ,  B64D25/00 ,  B64D2201/00

Abstract: A system and method for resisting an uncontrolled descent or uncontrolled flight condition of an aerial vehicle. The system includes a control system, sensors, an inflation device, and a deployable, inflatable assembly. The control system detects an uncontrolled condition using the sensors, and subsequently initiates the inflation device to inflate the inflatable assembly. The assembly includes an inflatable cage stored on and deployed from the aerial vehicle upon detection of an uncontrolled condition. The inflatable cage includes a hub, a perimeter tube, and support tubes connected between the hub and perimeter tube. Fill tubes enable inflation of the support and perimeter tubes. The assembly includes a parachute-material enclosure connected to the inflatable cage and structured to create drag to reduce a velocity of the aerial vehicle when the inflatable assembly is deployed. The assembly includes weight distribution straps physically coupled between the vehicle and the enclosure or inflatable cage.

Abstract translation: 一种用于抵抗飞行器的不受控制的下降或不受控飞行状态的系统和方法。 该系统包括控制系统，传感器，充气装置和可展开的可充气组件。 控制系统使用传感器检测不受控制的状况，随后启动充气装置以使充气组件膨胀。 该组件包括在检测到不受控制的状态时存储在飞行器上并展开的可充气笼。 可充气笼包括轮毂，周边管和连接在轮毂和周边管之间的支撑管。 填充管可以支撑支架和周边管的膨胀。 组件包括连接到可充气笼的降落伞材料外壳，并被构造成当展开充气组件时产生拖曳以降低飞行器的速度。 组件包括物理耦合在车辆与外壳之间的重量分配带，或者可充气笼。

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。

公开(公告)号：US09428132B2

公开(公告)日：2016-08-30

申请号：US13912937

申请日：2013-06-07

Applicant: Zodiac Seats France

Inventor： Jean-Marc Obadia ,  John Payne ,  Jeremy Cailleteau ,  Nick Lee ,  Nathan Kwok ,  Jean-Marie Daout ,  Jake Story ,  David Knox

IPC: B60R21/20 ,  B64D11/00 ,  B64D25/02 ,  B60R21/00

CPC classification number: B60R21/20 ,  B60R2021/0093 ,  B64D11/00 ,  B64D25/02 ,  B64D2201/00

Abstract: An airbag system assembly configured to be positioned in the interior of a vehicle that includes an aft wall configured to be positioned forward of a passenger seat and an airbag system. The aft wall includes front and aft surfaces and the aft wall includes a first flap that is formed by a plurality of weakness lines in at least the front surface thereof. The airbag system includes at least a first airbag module having a first airbag support plate with front and aft surfaces. The first airbag support plate is secured to the front surface of the aft wall, and the first airbag support plate includes a first airbag that is configured to deploy in the event of a crash condition and that is disposed on the aft surface of the first airbag support plate. The first airbag is positioned adjacent the first flap.

Abstract translation: 一种安全气囊系统组件，其构造成定位在车辆内部，所述气囊系统组件包括构造成位于乘客座椅前方的后壁和气囊系统。 后壁包括前表面和后表面，并且后壁包括在至少其前表面中由多条弱线形成的第一挡板。 所述安全气囊系统至少包括具有前后表面的第一气囊支撑板的第一气囊模块。 第一安全气囊支撑板固定在后壁的前表面上，第一安全气囊支撑板包括第一气囊，其构造成在碰撞状态下展开并且设置在第一气囊的后表面上 支撑板 第一安全气囊邻近第一挡板定位。

公开(公告)号：US20160244173A1

公开(公告)日：2016-08-25

申请号：US15143090

申请日：2016-04-29

Applicant: Takata Protection Systems, Inc.

Inventor： MARK EDWARD DEEVEY ,  MICHAEL H. SCHINDZIELORZ

IPC: B64D25/06 ,  B64D25/02

CPC classification number: B64D25/06 ,  B60R21/18 ,  B60R2021/0093 ,  B64D11/062 ,  B64D11/06205 ,  B64D2201/00 ,  Y10T442/2656 ,  Y10T442/2672 ,  Y10T442/2721

Abstract: The present invention discloses embodiments of an apparatus, systems and related methods for side-facing occupant protection in an aircraft during an abrupt stop—such as in a forward-facing crash event. Embodiments of the present invention disclose a three point air belt that provide superior passenger comfort and retractability, due to inventive construction, by providing enhanced flexibility of the three-point air belt, and more specifically, the shoulder harness portion. The present invention first includes a new airbag material which contributes to the enhanced flexibility, namely, a polyester textile structure treated with a phosphate-phosphonate compound. In further embodiments the material is the coated in a polyurethane mixture. The present invention also includes a new method of compacting the airbag such that it may be disposed in a shoulder harness while remaining substantially unobtrusive and comfortable to a passenger. The invention also includes a new containment material, namely a tubular webbing, to further enhance the flexibility of the shoulder harness over the prior art which generally comprises leather or leather-approximations. The result of the invention also provides enhanced retractability over the prior art, such that the three-point harness may be more easily stowed relative to the prior art.

Abstract translation: 本发明公开了在突然停止期间（例如在前向碰撞事件中）在飞行器中侧面乘员保护的装置，系统和相关方法的实施例。 本发明的实施例公开了一种三点式气动带，其通过提供三点式气动带，更确切地说是肩带配件部分的增强的灵活性，由于本发明的结构，提供了出众的乘客舒适性和伸缩性。 本发明首先包括有助于提高柔性的新型气囊材料，即用磷酸酯 - 膦酸酯化合物处理的聚酯织物结构。 在另外的实施方案中，该材料被涂覆在聚氨酯混合物中。 本发明还包括一种压缩气囊的新方法，使得其可以设置在肩带上，同时对乘客基本上不引人注意并且舒适。 本发明还包括新的容纳材料，即管状织带，以进一步增强肩带的弹性，而现有技术通常包括皮革或皮革近似。 本发明的结果还提供了比现有技术更强的可缩回性，使得相对于现有技术，三点式线束可以更容易地收起。

公开(公告)号：US09260192B2

公开(公告)日：2016-02-16

申请号：US14525947

申请日：2014-10-28

Applicant: BELL HELICOPTER TEXTRON INC.

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

IPC: B64C25/56 ,  B64D25/00

CPC classification number: B64D25/00 ,  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 to a second set of airbags for flotation. 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到用于浮选的第二组安全气囊。 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：US20160001893A1

公开(公告)日：2016-01-07

申请号：US14626838

申请日：2015-02-19

Applicant: SZ DJI TECHNOLOGY CO., LTD

Inventor： Mingyu Wang

IPC: B64D45/00 ,  B64C25/32 ,  B64C25/56 ,  B64D25/00

CPC classification number: B64D25/00 ,  B64C25/32 ,  B64C25/54 ,  B64C25/56 ,  B64C39/024 ,  B64C2201/027 ,  B64D45/00 ,  B64D2201/00

Abstract: An impact protection apparatus is provided, comprising a gas container configured to hold a compressed gas and an inflatable member configured to be inflated by the gas and function as an airbag of a movable object, such as an aerial vehicle. A valve controls flow of gas from the container to the inflatable member in response to a signal from a valve controller. The valve and valve controller are powered by an independent power source than one or more other systems of the movable object. A safety mechanism may also be provided that, unless deactivated, prevents inflation of the inflatable member.