公开(公告)号：US08016239B2

公开(公告)日：2011-09-13

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: B64D17/00

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.

Abstract translation: 用于各种运输工具的安全预冲击减速系统包括由气体膨胀的气囊形成的降落伞结构。 或者，降落伞结构包括具有孔的顶盖。 降落伞结构中的空气间隙或冠层中的孔口具有可调节和选择性尺寸以控制车辆的操作参数。 该系统包括具有连续循环记录的传感器和快速曝光率摄像机，以测量车辆的操作参数并预测可能的碰撞。 一旦检测到碰撞条件，音频/视频图像被存储在存储介质上。 气囊被部署和充气。 除了构成降落伞结构的气囊之外，还设置有多个安全气囊，以便在车辆的外部展开以帮助安全着陆。

公开(公告)号：US07980799B1

公开(公告)日：2011-07-19

申请号：US12128204

申请日：2008-05-28

Applicant: Paul A. Rioux ,  Marcia B. Rioux

Inventor： Paul A. Rioux ,  Marcia B. Rioux

IPC: B61D45/00

CPC classification number: B63B25/24 ,  B60P7/065 ,  B61D45/00 ,  B64D2201/00 ,  B65D90/004

Abstract: This patent discloses a freight dunnage bag to accommodate discrete units of freight that have been loaded on board a freight carrier for transportation. The freight dunnage bag may include a first layer dividing a freight dunnage bag interior from a freight dunnage bag exterior. An adaptor having a capsule attached between a cap and a valve body may be attached to the first layer so that the first layer may be positioned between the capsule and the cap. A gas cartridge containing compressed gas may be attached to valve body within the freight dunnage bag interior.

Abstract translation: 该专利公开了一种货运衬垫袋，以容纳已经装载在货运运输工具上的运输的分离单位。 货运衬垫袋可以包括将货运衬垫袋内部与货物衬垫袋外部分开的第一层。 具有附接在盖和阀体之间的胶囊的适配器可以附接到第一层，使得第一层可以位于胶囊和盖之间。 包含压缩气体的气瓶可以附接到货物衬垫袋内部的阀体上。

公开(公告)号：US07975963B2

公开(公告)日：2011-07-12

申请号：US12087199

申请日：2006-12-15

Applicant: Ludger Merz ,  Roland Fuhrmann

Inventor： Ludger Merz ,  Roland Fuhrmann

IPC: B64D1/10

CPC classification number: B64C27/006 ,  B64C1/062 ,  B64D9/00 ,  B64D9/003 ,  B64D2201/00 ,  Y02T50/46

Abstract: A safety system for reducing the impact energy of a container for an aircraft includes an aircraft cargo hold with at least one safety wall; an accommodation device; and at least one airbag. The accommodation device can be affixed to the safety wall, wherein the accommodation device is designed to accommodate the at least one airbag. In the case of a movement of the container, the at least one airbag can be activated so that air can be injected into the airbag so that some of the impact energy of the container can be absorbed by the at least one activated airbag, with the remaining forces then being distributed over an area of the at least one safety wall.

Abstract translation: 用于减少用于飞机的容器的冲击能量的安全系统包括具有至少一个安全壁的飞机货舱; 住宿设备; 和至少一个气囊。 住宿装置可以固定到安全墙上，其中住宿装置被设计成容纳至少一个气囊。 在容器移动的情况下，可以启动至少一个气囊，使得空气可以被注入到气囊中，使得容器的一些冲击能量能够被至少一个活动的气囊吸收， 然后剩余的力分布在至少一个安全墙的一个区域上。

公开(公告)号：US07954752B2

公开(公告)日：2011-06-07

申请号：US12089884

申请日：2006-11-08

Applicant: Michael R. Smith ,  Somen Chowdhury ,  Cheng-Ho Tho

Inventor： Michael R. Smith ,  Somen Chowdhury ,  Cheng-Ho Tho

IPC: B64C25/56 ,  B64D25/18

CPC classification number: B64D25/18 ,  B64C27/006 ,  B64D2201/00

Abstract: A crash attenuation system for an aircraft, the system having an airbag carried by the aircraft and inflatable generally adjacent an exterior of the aircraft. The airbag has at least one vent for releasing gas from the interior of the airbag. A first gas source is in fluid communication with the interior of the airbag for inflating the airbag with gas generated provided by the first gas source. A vent valve is provided for controlling a flow of gas through each vent, each vent valve being selectively configurable between an open state, in which gas can pass through the associated vent from the interior of the airbag, and a closed state, in which gas is retained within the interior of the airbag. A second gas source is provided for at least partially re-inflating the airbag after venting of gas through the at least one vent.

Abstract translation: 一种用于飞行器的碰撞衰减系统，该系统具有由飞机携带并且大体上邻近飞机外部充气的气囊。 气囊具有至少一个用于从气囊的内部释放气体的通气口。 第一气体源与气囊的内部流体连通，以便由第一气体源产生的气体使气囊充气。 提供排气阀以控制通过每个排气口的气体流动，每个排气阀可选择性地配置在打开状态之间，气体可以从气囊的内部通过相关联的排气口，而关闭状态，气体 保持在气囊的内部。 第二气源被提供用于在通过至少一个通气口排出气体之后至少部分地重新充气气囊。

公开(公告)号：US07934682B2

公开(公告)日：2011-05-03

申请号：US11825758

申请日：2007-07-09

Applicant: Dario P. Manfredi ,  Savia N. Giarraffa

Inventor： Dario P. Manfredi ,  Savia N. Giarraffa

IPC: B64D17/00

CPC classification number: F41H11/02 ,  B64D25/00 ,  B64D25/12 ,  B64D2201/00 ,  F42B3/006 ,  F42B15/36

Abstract: A system for enabling the safe landing of an aircraft during an in-flight emergency is provided. The system includes a plurality of onboard devices for releasably securing a plurality of wings to a fuselage, and a non-electric module for activating said onboard devices. Said onboard devices are released to separate said wings from the fuselage.

Abstract translation: 提供了一种用于在飞行中紧急情况下使飞机安全着陆的系统。 该系统包括多个用于将多个翼片可释放地固定到机身的车载装置，以及用于启动所述车载装置的非电动模块。 所述车载装置被释放以将机翼与机身分开。

公开(公告)号：US20100044507A1

公开(公告)日：2010-02-25

申请号：US12089884

申请日：2006-11-08

Applicant: Michael R. Smith ,  Somen Chowdhury ,  Cheng-Ho Tho

Inventor： Michael R. Smith ,  Somen Chowdhury ,  Cheng-Ho Tho

IPC: B64C25/56 ,  B64D25/00

CPC classification number: B64D25/18 ,  B64C27/006 ,  B64D2201/00

Abstract: A crash attenuation system for an aircraft, the system having an airbag carried by the aircraft and inflatable generally adjacent an exterior of the aircraft. The airbag has at least one vent for releasing gas from the interior of the airbag. A first gas source is in fluid communication with the interior of the airbag for inflating the airbag with gas generated provided by the first gas source. A vent valve is provided for controlling a flow of gas through each vent, each vent valve being selectively configurable between an open state, in which gas can pass through the associated vent from the interior of the airbag, and a closed state, in which gas is retained within the interior of the airbag. A second gas source is provided for at least partially re-inflating the airbag after venting of gas through the at least one vent.

Abstract translation: 一种用于飞行器的碰撞衰减系统，该系统具有由飞机携带并且大体上邻近飞机外部充气的气囊。 气囊具有至少一个用于从气囊的内部释放气体的通气口。 第一气体源与气囊的内部流体连通，以便由第一气体源产生的气体使气囊充气。 提供排气阀以控制通过每个排气口的气体流动，每个排气阀可选择性地配置在打开状态之间，气体可以从气囊的内部通过相关联的排气口，并且气体可以在气体 保持在气囊的内部。 第二气源被提供用于在通过至少一个通气口排出气体之后至少部分地重新充气气囊。

公开(公告)号：US07644739B1

公开(公告)日：2010-01-12

申请号：US11712121

申请日：2007-02-28

Applicant: Jonathan Vezzosi ,  Thomas W. Swierkocki

Inventor： Jonathan Vezzosi ,  Thomas W. Swierkocki

IPC: B65B1/08

CPC classification number: B64C25/56 ,  B64C25/52 ,  B64C2025/325 ,  B64D2201/00

Abstract: A pressurized actuator system for independent deployment of at least two inflatable structures having a first primary section adapted for deployment of a primary inflatable structure and second section for deployment of a secondary inflatable structure and an auxiliary source of pressurized fluid for operating said device. A control assembly for controlling a flow of pressurized fluid from the auxiliary source of pressurized into the second system is provided. Thus, the system assures independent deployment of the primary and secondary inflatable structures.

Abstract translation: 一种用于独立展开至少两个充气结构的加压致动器系统，其具有适于展开主充气结构的第一主要部分和用于展开二次可充气结构的第二部分和用于操作所述装置的加压流体辅助源。 提供了用于控制加压流体从加压辅助源流入第二系统的控制组件。 因此，该系统确保主要和次要充气结构的独立部署。

公开(公告)号：US20090212160A1

公开(公告)日：2009-08-27

申请号：US11827146

申请日：2007-09-17

Applicant: Michael Lawrence Beauchamp

Inventor： Michael Lawrence Beauchamp

IPC: B64D25/108

CPC classification number: B64D25/10 ,  B64D2201/00

Abstract: An aircraft fuselage, with a seat chassis mounted on a set of track and guide rails. Any ejection seat chassis with an occupant attached to a guide track is ejectable along a lateral trajectory, perpendicular to the horizontal longitudinal axis of an aircraft fuselage interior, and can be guided out of the field of an imperiled aircraft during ejection by a rocket catapult system. A seat, framework, bed or chassis is enabled to eject laterally from an aircraft fuselage since a conventional hinged door is operational within a greater sliding emergency door panel which pneumatic rockets at the top and bottom of the emergency sliding door transverse the greater emergency sliding door panel including an interior fixed conventional hinge operational door along a set of tracks attached to the frame and outer fuselage of said aircraft, out of the path of the lateral ejection seat chassis or chassis', towards the rear of an aircraft where the sliding greater panel is prevented from recoiling by spring loaded latch catches; and which emergency door can also drop-slide down by pneumatic rocket assist for some aircraft where the weight, time and spatial difference between a drop-down and a slide-back emergency door or exit opening can in many instances is a benefit to use a drop-down emergency door or exit, pneumatically propelled; so that an aircraft has less nascent drag from rocket weight, and can result in a fractionally quicker or faster rate of acceleration and removal of the door, panel or canopy from the lateral ejection pathway when feasible. Wing struts can also be removed from the emergency lateral ejection exit pathway by pneumatic or other explosive charge means. Additional supporting fuselage struts and slender tempered glass panes are constructed into the fuselage for increased rigidity for the enlarged fuselage structure incorporating a same near relative number of aircraft seats for pilots and passengers, equipped with lateral ejection apparattii, and has an improved field of view. Dual airbags for positioning the legs and torso of an occupant for a safe emergency exit lateral ejection are embedded or attached to a structure directly in front of a seat chassis. A second set of pressure sensitive airbags, head, neck, spine and organ concave-convex protector are attached on both sides of a seat chassis. Three compartments for altitude appropriate parachutes and a sensor fuse box for opening said desired chute are located inside an ejection seats rigid framework back section. The invention includes an interior side mounted blast shield which a rocket catapult systems rocket nozzles face, and which rocket or rockets are locked by collar seal(s) to a said blast shields, alloy or metallic, ceramic tile backing. A track support launcher platform, column, columns or center console support the lateral ejection apparattii at a functional and comfortable level and height for the occupant or occupants. Otherwise, the tracks or guide rails can be attached directly on an aircraft fuselage floor frame or attached to a wall frame structure in an aircraft fuselage, and can be constructed within rows with aisles on a chain motor reloading laterally aligned guide track for lateral rotor positioning lateral ejection apparattii.

公开(公告)号：US20080179462A1

公开(公告)日：2008-07-31

申请号：US11699277

申请日：2007-01-29

Applicant: Peter J. Murphy

Inventor： Peter J. Murphy

IPC: B64D17/02

CPC classification number: B64D17/025 ,  A41D13/02 ,  A62B1/22 ,  B64D10/00 ,  B64D2201/00

Abstract: The present invention is a fast inflating parasail jump suit combining an inflatable parasail, an inflatable jump suit with outside and inside coupled at edges to provide an inflatable pressurized gas volume, at least one inflator device for storing and swiftly releasing pressurized gas into the parasail and suit upon activation, a suit harness coupling outside of suit to inside liner to body center of mass, and attachments coupling to parasail providing sail support to suit in suspension.

Abstract translation: 本发明是一种快速充气式跳伞套件，其组合了可充气的伞杆，一种可膨胀的跳伞，其外侧和内侧在边缘处耦合以提供可膨胀的加压气体容积，至少一个用于储存并迅速将加压气体释放到伞架中的充气装置， 适用于激活，西装线束耦合到衣服外部到内衬到体重中心，以及连接到吊架的附件，提供帆支撑以适应悬挂。

公开(公告)号：US06892983B2

公开(公告)日：2005-05-17

申请号：US10753550

申请日：2004-01-08

Applicant: Philip Kneisl

Inventor： Philip Kneisl

IPC: B64D45/00 ,  G08B15/00 ,  B64D25/00

CPC classification number: G08B15/00 ,  B64D45/0015 ,  B64D2045/002 ,  B64D2201/00

Abstract: The present invention provides an anti-hijacking system. In one embodiment, the anti-hijacking system is used in an airplane to provide forceful contact to disarm, disable, immobilize or otherwise incapacitate a hostile intruder who has entered the cockpit. The anti-hijacking system includes one or more inflation devices, such as deployable air bags.

Abstract translation: 本发明提供一种防劫持系统。 在一个实施例中，防劫持系统在飞机中用于提供有力的接触以解除武装，禁止，固定或以其他方式使入境驾驶舱的敌对入侵​​者丧失能力。 防劫系统包括一个或多个充气装置，例如可部署的气囊。