公开(公告)号：US20100181421A1

公开(公告)日：2010-07-22

申请号：US12666757

申请日：2008-06-23

Applicant: David Albagli ,  Nathan Libis

Inventor： David Albagli ,  Nathan Libis

IPC: B64D45/04 ,  B60R21/26 ,  F42B3/04 ,  B64C25/00

CPC classification number: B64D25/00 ,  B64C25/56 ,  B64D2201/00

Abstract: A two-stage pyrotechnic gas generator for inflating an airbag has a housing with first and second chambers each having gas release apertures. The chambers are separated by a partition having an opening. Running through the gas generator is an essentially contiguous train of combustible material including a train of fast burning material passing through the first chamber to the opening, a pyrotechnic delay element associated with the opening, and a train of fast burning material within the second chamber. The first and second chambers each include a quantity of propellant deployed to be ignited by the corresponding train of fast burning material. An initiator, associated with the first chamber, is configured to initiate combustion of the essentially contiguous train of combustible material. As a result, the second quantity of propellant is ignited at a predefined delay relative to ignition of the first quantity of propellant to achieve precisely timed two-phase inflation with a single electronic initiator.

Abstract translation: 用于使气囊充气的两级烟火气体发生器具有壳体，其具有分别具有气体释放孔的第一和第二腔室。 室由具有开口的隔板分开。 通过气体发生器运行是基本上连续的可燃材料串，包括通过第一室到开口的快速燃烧材料串，与开口相关联的烟火延迟元件以及在第二室内的快速燃烧材料串。 第一和第二室各自包括一部分被部署以由相应的快速燃烧材料列车点燃的推进剂。 与第一室相关联的引发器被配置为启动基本上相邻的可燃材料串的燃烧。 结果，第二量的推进剂以相对于第一量推进剂的点火的预定延迟点燃，以通过单个电子引发器实现精确定时的两相充气。

公开(公告)号：US20090236828A1

公开(公告)日：2009-09-24

申请号：US12051768

申请日：2008-03-19

Applicant: Daniel Nick Foubert ,  Kevin Keeslar

Inventor： Daniel Nick Foubert ,  Kevin Keeslar

IPC: B60R21/18

CPC classification number: B60R21/18 ,  B60R2021/0093 ,  B60R2022/027 ,  B64D11/062 ,  B64D11/06205 ,  B64D2201/00

Abstract: Inflatable restraint systems for restraining an occupant in a vehicle are disclosed herein. An inflatable restraint system configured in accordance with one embodiment of the invention includes an airbag carried by a web. The web has an end portion coupled to a vehicle and is configured to extend around a portion of the occupant. The restraint system further includes a gas source that is also carried by the web. The gas source is operably coupled to the airbag to inflate the airbag in the event of a rapid deceleration or other dynamic event.

Abstract translation: 本文公开了用于限制车辆中的乘员的充气约束系统。 根据本发明的一个实施例配置的可充气约束系统包括由腹板承载的气囊。 腹板具有联接到车辆的端部，并且构造成围绕乘员的一部分延伸。 约束系统还包括也由腹板承载的气源。 在快速减速或其他动态事件的情况下，气源可操作地联接到气囊以使气囊膨胀。

公开(公告)号：US20090173829A1

公开(公告)日：2009-07-09

申请号：US12382144

申请日：2009-03-10

Applicant: A-hamid Hakki ,  Sam Hakki ,  Said I. Hakky

Inventor： A-hamid Hakki ,  Sam Hakki ,  Said I. Hakky

IPC: B64D17/02 ,  G05D1/00 ,  H04N7/18

CPC classification number: B64D25/08 ,  B64D17/80 ,  B64D2201/00

Abstract: A safety pre-impact deceleration system for a variety of conveyances includes a parachute structure formed from air bags inflated with gas. Alternatively, the parachute structure includes a canopy with orifices. Air spaces in the parachute structure or orifices in the canopy have adjustable and selective dimensions to control the operational parameters of the vehicle. The system includes sensors and rapid exposure rate cameras with continuous loop recording to measure operational parameters of the vehicle and to predict possible collision. Once a collision condition is detected, audio/video images are stored on storage media. The air bags are deployed and inflated. In addition to air bags constituting the parachute structure, a plurality of air bags are provided to be deployed external the vehicle to aid in a safe landing.

公开(公告)号：US20090072077A1

公开(公告)日：2009-03-19

申请号：US11898940

申请日：2007-09-18

Applicant: Chui Wen Chiu

Inventor： Chui Wen Chiu

IPC: B64C1/00 ,  B64D11/00

CPC classification number: B64C39/04 ,  B64C1/22 ,  B64D11/00 ,  B64D25/12 ,  B64D2201/00

Abstract: A high capacity passenger airplane is provided with a plurality of fuselages releasably mounted on it wings section. Each fuselage has an outer shell with a plurality of passenger cabins mounted in tandem with the shell. The passenger cabins are equipped with sliding wheels such that they may be discharged through a rear exit door of the fuselage to separate from the airplane in accident. Each passenger cabin is equipped with safety parachutes and external safety air bags at its underside such that it may be safely landed on ground or on water after having discharged from a fuselage.

Abstract translation: 大容量客机设有多个可拆卸地安装在机翼部分上的机身。 每个机身都有一个外壳，多个客舱与外壳同时安装。 乘客舱配备有滑轮，使得它们可以通过机身的后出口排出，以在事故中与飞机分离。 每个客舱在其下侧配备有安全降落伞和外部安全气囊，以便在从机身出来后可以安全地降落在地面或水面上。

公开(公告)号：US20050279559A1

公开(公告)日：2005-12-22

申请号：US10524146

申请日：2003-08-14

Applicant: Gerard Thevenot

Inventor： Gerard Thevenot

IPC: B60R21/16 ,  A41D13/018 ,  B60K28/00 ,  B60D1/28

CPC classification number: A41D13/018 ,  A62B33/00 ,  B64D2201/00

Abstract: A safety device associated with a transport, or with its pilot's body or the body of any other person practising a sport or a hazardous activity to protect the body, includes an inflatable airbag connected to inflating elements automatically or manually activated upon an impact. The airbag has a frame including at least one tubular element for forming a geometrical frame, when the tubular element is inflated, the latter being initially folded in a container integral, for instance, with the transport and/or the human body and connected to the inflating elements and an outer wall made of a flexible material integral with the frame so as to form a closed chamber filled with air at atmospheric pressure, the outer wall including at least one valve.

Abstract translation: 与运输相关联的安全装置，或其驾驶员的身体或任何其他从事运动或危险活动的人的身体来保护身体，包括在冲击时自动或手动地激活的充气气囊连接到充气元件。 安全气囊具有框架，该框架包括用于形成几何框架的至少一个管状元件，当管状元件膨胀时，该管状元件最初被折叠成一体式的容器，例如与运输工具和/或人体连接， 充气元件和由与框架一体的柔性材料制成的外壁，以形成充满大气压力的空气的封闭室，外壁包括至少一个阀。

公开(公告)号：US20030080250A1

公开(公告)日：2003-05-01

申请号：US10214396

申请日：2002-08-06

Inventor： Alexander van der Velden ,  Holger Stockfleth

IPC: B64D011/00 ,  B64D013/00

CPC classification number: B64D25/12 ,  B64C37/02 ,  B64C39/02 ,  B64D2011/0046 ,  B64D2201/00

Abstract: An autonomous passenger module is releasably carried on a super-sonic aircraft, such as a military fighter jet, for carrying plural passengers on supersonic and near space flights. The passenger module is equipped with passenger service and life support systems to provide oxygen and the like, a parachute system, and a landing airbag or flotation aid system. The module remains mounted on the aircraft throughout a normal flight. In an emergency situation, the module separates from the aircraft by means of releasable connector elements and descends using parachutes. The module provides high passenger capacity at a low cost in a simple manner for commercial supersonic flights using an existing supersonic aircraft as a carrier platform.

Abstract translation: 自主乘客模块可释放地携带在诸如军用战斗机的超声飞行器上，用于在超音速和近空中飞行上携带多个乘客。 乘客模块配备有乘客服务和生命支持系统以提供氧气等，降落伞系统和着陆安全气囊或浮选辅助系统。 模块在正常飞行中保持安装在飞机上。 在紧急情况下，模块通过可拆卸的连接器元件与飞机分离，并使用降落伞下降。 该模块以简单的方式以低成本提供高乘客能力，使用现有的超音速飞机作为载体平台进行商业超音速飞行。

公开(公告)号：US06422512B1

公开(公告)日：2002-07-23

申请号：US09651477

申请日：2000-08-30

Applicant: Donald J. Lewis ,  Terry W. Merrifield ,  Steven R. Hailstone ,  Steven K. Butt ,  Jeffrey Allyn Baker ,  Shyam S. Karigiri

Inventor： Donald J. Lewis ,  Terry W. Merrifield ,  Steven R. Hailstone ,  Steven K. Butt ,  Jeffrey Allyn Baker ,  Shyam S. Karigiri

IPC: B64D2504

CPC classification number: B64D25/02 ,  B64D25/06 ,  B64D25/10 ,  B64D2201/00

Abstract: An inflatable restraint system for holding and securing an aircrew member in his seat during ejection from an aircraft has one or more members forming a shield around him or her. The system is controlled to inflate after the aircrew member has started the sequence of ejection and before the rockets that power the seat from the aircraft are ignited. The forces of windblast are deflected by the inflatable restraint from the aircrew member as the aircrew member enters into and remains in the windblast and in his seat.

Abstract translation: 一种用于在从飞行器弹出期间将空调部件保持并固定在其座椅中的充气约束系统具有一个或多个在其周围形成屏蔽的部件。 在机组成员开始排列顺序之后以及在从飞机上为座椅供电的火箭被点燃之前，该系统被控制为充气。 随着空勤人员进入并保留在喷气式飞机和座椅上，喷气机的力量可以通过充气限制从空勤人员部件偏转。

公开(公告)号：US06371410B1

公开(公告)日：2002-04-16

申请号：US09717047

申请日：2000-11-22

Applicant: Renee Cairo-Iocco ,  Thomas E. Wenzel ,  Eugene C. Fischer

Inventor： Renee Cairo-Iocco ,  Thomas E. Wenzel ,  Eugene C. Fischer

IPC: B64C2556

CPC classification number: B64C25/30 ,  B64D25/00 ,  B64D2201/00

Abstract: Inflation of impact absorbing bags is effected on a portable platform positioned on an emergency landing zone after jettisoning of damaged landing gear from a helicopter fuselage. The impact absorbing bags when inflated form a cradle shape conforming to the bottom of the helicopter fuselage.

Abstract translation: 冲击吸收袋的通货膨胀在位于紧急着陆区上的便携式平台上，在从直升机机身丢弃损坏的起落架之后进行。 冲击吸收袋充气时形成符合直升机机身底部的摇篮形状。

公开(公告)号：US06237875B1

公开(公告)日：2001-05-29

申请号：US09376746

申请日：1999-08-17

Applicant: Stefan Menne ,  Peter Nikolaus Keerl

Inventor： Stefan Menne ,  Peter Nikolaus Keerl

IPC: B64D114

CPC classification number: B64D1/14 ,  B64D2201/00

Abstract: An airbag configuration for braking the landing impact of flying payloads has a central airbag (17) and at least one torus ring (11, 12, 13) surrounding the central airbag. A payload (L) is attachable on the central airbag (17). A stabilizing device (19) is provided which extends from the lowermost portion of the at least one torus ring (11, 12, 13) to the central airbag (17). The central airbag provides primarily vertical braking of the landing impact while the torus ring provides primarily horizontal braking of the landing impact.

Abstract translation: 用于制动飞行有效载荷的着陆冲击的气囊构造具有中央气囊（17）和围绕中央气囊的至少一个环面环（11,12,13）。 有效载荷（L）可附接在中央气囊（17）上。 提供了一种稳定装置（19），其从所述至少一个环形环（11,12,13）的最下部延伸到所述中央气囊（17）。 中央安全气囊主要提供着陆冲击的垂直制动，而环形环主要提供着陆冲击的水平制动。

公开(公告)号：US6029932A

公开(公告)日：2000-02-29

申请号：US32281

申请日：1998-02-27

Applicant: Adalbert Wagner

Inventor： Adalbert Wagner

IPC: B64C25/00 ,  B64G1/62 ,  F16K17/40

CPC classification number: B64G1/62 ,  B64C25/00 ,  F16K13/06 ,  B64D2201/00

Abstract: The detonating valve for releasing openings of air bag landing systems for aircraft and spacecraft has a wedge type charge and a cover closing the opening, which cover is shorn off during the ignition of the wedge type charge. The cover is a thin-walled disk or a membrane, which is integrated either within the aircraft and spacecraft or within the air bag landing system.

Abstract translation: 用于释放用于飞机和航天器的气囊着陆系统的开口的引爆阀具有楔形电荷和封闭开口的盖，该盖在楔形充电点火期间被关闭。 该盖是薄壁盘或膜，它集成在飞机和航天器内或气囊着陆系统内。