公开(公告)号：US20080087511A1

公开(公告)日：2008-04-17

申请号：US11580998

申请日：2006-10-16

Applicant: Anthony P. Taylor ,  Robert Sinclair ,  John Sanders ,  Kevin Sweeney

Inventor： Anthony P. Taylor ,  Robert Sinclair ,  John Sanders ,  Kevin Sweeney

IPC: F16F9/04

CPC classification number: F16F9/04 ,  B64D2201/00 ,  B64G1/62

Abstract: An impact attenuation bag has a height-reducing structure in the form of an internal rib that draws the upper and lower surfaces of the bag closer together, reducing the overall height of the bag when inflated as compared with the same bag in the absence of the rib. This gives the bag a flatter resting shape that provides significant performance enhancement by increasing the initial ground contact area and lowering the vehicle assembly center of gravity. As a result, the moment arm is reduced making the payload less likely to roll over. The rib may be a fabric sheet or cord laced in a criss-cross or other lacing pattern that extends from the top of the bag to the bottom.

Abstract translation: 冲击衰减袋具有内肋形式的高度减小结构，其将袋的上表面和下表面更靠近在一起，与没有相同袋时的袋相比，在膨胀时减小袋的整体高度 肋骨。 这使得袋子更平坦的休息形状，通过增加初始接地面积和降低车辆组件的重心来提供显着的性能提升。 因此，力矩臂减小，使得有效载荷不太可能翻滚。 肋条可以是以从十字形或其他带状图案的织物片或绳子，其从袋的顶部延伸到底部。

公开(公告)号：US20080017754A1

公开(公告)日：2008-01-24

申请号：US11491071

申请日：2006-07-24

Applicant: Anthony P. Taylor ,  Debbie Gardinier ,  Michelle Cooper ,  Robert Sinclair

Inventor： Anthony P. Taylor ,  Debbie Gardinier ,  Michelle Cooper ,  Robert Sinclair

IPC: B64C25/56

CPC classification number: B64D1/14 ,  B60R21/239 ,  B64D2201/00

Abstract: A fast acting and low leak rate vent for an impact landing bag in which a vent hole is covered by a gas barrier assembly having a flexible membrane and a low gas permeability layer. A flap assembly positioned around the gas barrier assembly includes flaps that are movable between an open position in which the membrane is exposed and a closed position in which the flaps cover and reinforce the gas barrier assembly. An externally actuated flow initiator is associated with a fastening element that retains the flaps in the closed position. Upon landing, the flow initiator is activated to sever the fastening element and release the flaps and the low gas permeability layer. Thereafter, the internal pressure within the landing bag under landing forces causes the membrane to burst, releasing a flow of gas from within the landing bag to attenuate impact.

Abstract translation: 一种用于冲击着陆袋的快速作用和低泄漏率排气孔，其中通气孔被具有柔性膜和低气体渗透性层的气体阻挡组件覆盖。 围绕气体阻挡组件定位的翼片组件包括可在其中暴露膜的打开位置和打开位置之间移动的挡板，在该位置中，翼片覆盖并加强气体阻挡组件。 外部致动的流动引发器与将襟翼保持在关闭位置的紧固元件相关联。 在着陆时，启动流动引发器以切断紧固元件并释放翼片和低透气性层。 此后，着陆袋内着陆力下的内部压力导致膜破裂，释放来自着陆袋内的气体流，以减少冲击。

公开(公告)号：US20050062274A1

公开(公告)日：2005-03-24

申请号：US10664742

申请日：2003-09-18

Applicant: Brett Snellgrove

Inventor： Brett Snellgrove

IPC: B64D17/30 ,  B60R21/16

CPC classification number: B64D17/30 ,  B64D2201/00

Abstract: An inflatable airbag (by mouth or mechanical pump) that remains continuously inflated and deployed for use in situations where complex impact detection sensors and gas generator inflation, deployment devices are not practical or desirable. It is anticipated this device will have most suitable application in the protection of the vulnerable spinal regions of participants in foot launched and ultralight aviation, in particular paraglider pilots. Participants in this aviation sport suffer from an unacceptably high incidence of vertebral fracture, spinal injury and paralysis due to the semi-reclined, seated position adopted in flight, and in utilizing aircraft subject to turbulence induced deflation and collapse at low altitude with resulting ground impact. This device when fashioned into an aerodynamic, L shaped curve and positioned in the rear of the flying harness, covers and protects the upper thigh, buttock, lumbar, thoracic and cervical spine from dorsal impacts.

Abstract translation: 一种充气安全气囊（通过嘴或机械泵），其在复杂的冲击检测传感器和气体发生器充气，部署装置不实际或不可取的情况下保持连续膨胀和部署。 预计该装置将最适用于保护足部发射和超轻型航空的参与者的脆弱脊椎区域，特别是滑翔伞飞行员。 这个航空运动的参与者由于在飞行中采用的半倾斜的坐姿，以及利用受到湍流引起的低空飞行引起的通风和塌陷的飞机，导致椎骨骨折，脊柱损伤和麻痹的发生率高达不可接受的高度，从而造成地面撞击 。 当这种装置被塑造成一个空气动力学的L形曲线并且位于飞行线束的后部时，覆盖并保护大腿，臀部，腰部，胸部和颈椎从背侧的冲击。

公开(公告)号：US20040226498A1

公开(公告)日：2004-11-18

申请号：US10789407

申请日：2004-02-27

Inventor： Tony W. Mears ,  David G. Walder ,  Thomas Edward Berg

IPC: B63B043/10

CPC classification number: B64D25/18 ,  B63B43/14 ,  B63B2043/145 ,  B64D2201/00

Abstract: A flotation device for maintaining an aircraft in a floating and stable condition is provided. The flotation device comprises at least one flotation bladder mounted to the aircraft and an inflation mechanism for inflating the flotation bladder. A method for maintaining an aircraft in a floating condition is also provided.

Abstract translation: 提供了一种用于将飞机维持在浮动和稳定状态的浮选装置。 浮选装置包括至少一个安装在飞行器上的浮选气囊和用于使浮选气囊充气的充气机构。 还提供了一种将飞机维持在浮动状态的方法。

公开(公告)号：US06817579B2

公开(公告)日：2004-11-16

申请号：US10214396

申请日：2002-08-06

Applicant: Alexander van der Velden ,  Holger Stockfleth

Inventor： Alexander van der Velden ,  Holger Stockfleth

IPC: B64D100

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，模块通过可释放的连接器元件与飞行器分离，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：US06688555B1

公开(公告)日：2004-02-10

申请号：US10209435

申请日：2002-07-30

Applicant: Philip Kneisl

Inventor： Philip Kneisl

IPC: B64D2500

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 cockpit 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，防劫持系统用于飞机驾驶舱以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。

公开(公告)号：US06505890B2

公开(公告)日：2003-01-14

申请号：US09778498

申请日：2001-02-07

Applicant: Michael C. Riley ,  Willard F. Hagan

Inventor： Michael C. Riley ,  Willard F. Hagan

IPC: B60N242

CPC classification number: B64D11/06205 ,  B60R21/207 ,  B60R21/268 ,  B60R21/272 ,  B60R2021/0093 ,  B64D11/0649 ,  B64D25/04 ,  B64D25/06 ,  B64D2201/00 ,  Y02T50/46

Abstract: A passive restraint system in an aircraft utilizing a seat structure of the aircraft to store a source of pressurized gas or solid fuel necessary to expand the passive restraint is disclosed. The seat structure of the aircraft comprises multiple hollow tubes, and these hollow tubes can be utilized to either store pressurized gas or solid fuel directly, or to house a vessel that stores pressurized gas or solid fuel. Thus, no additional aircraft seat space is required to house a pressurized gas vessel. By using the existing seat structure to house the source of pressurized gas or solid fuel, significant space and weight savings can be realized, both of which are important factors in aircraft seat design.

公开(公告)号：US06497389B1

公开(公告)日：2002-12-24

申请号：US09945102

申请日：2001-08-31

Applicant: Blaine K. Rawdon ,  Arthur V. Hawley

Inventor： Blaine K. Rawdon ,  Arthur V. Hawley

IPC: B64D2500

CPC classification number: B66F3/35 ,  B64D25/00 ,  B64D2201/00 ,  Y10S244/905

Abstract: An airbag system for elevating the fuselage of an aircraft off a landing surface a sufficient degree to allow for emergency egress of passengers and crew through ventral emergency exit doors. An airbag assembly made up of a plurality of independent airbags is disposed within the aircraft. When activated, the airbag system deploys the airbags external of the aircraft that elevate the fuselage of the aircraft a sufficient degree to allow for utilizing the ventral emergency exit doors on the fuselage to enable evacuating the passengers and crew. An activation mechanism is connected to the inflation.devices associated with each of the airbags. The activation mechanism generates an electrical signal which activates the inflation devices, which in turn fill the airbags with a compressed fluid, thus expanding the airbags and lifting the fuselage. A crew member initiates the activation of the airbag system through one or more switches.

Abstract translation: 一种气囊系统，用于将飞机的机身从足够的角度提升到足够的程度，以允许乘客和船员通过腹侧紧急出口门的紧急出口。 由多个独立安全气囊组成的气囊组件设置在飞机内。 当活动时，气囊系统部署飞行器外部的安全气囊，以提升机身机身足够的程度，以便利用机身上的腹侧紧急出口门，以使乘客和机组人员能够撤离。 激活机构连接到与每个安全气囊相关联的通风装置。 激活机构产生电信号，其激活充气装置，充气装置又用压缩流体填充安全气囊，从而使安全气囊膨胀并提升机身。 机组人员通过一个或多个开关启动气囊系统的启动。

公开(公告)号：US5692710A

公开(公告)日：1997-12-02

申请号：US676904

申请日：1996-07-08

Applicant: James W. Gee, Sr.

Inventor： James W. Gee, Sr.

IPC: A41D13/015 ,  B64D25/00 ,  B64D11/06

CPC classification number: A41D13/018 ,  B64D25/00 ,  B64D25/02 ,  A41D13/0155 ,  B64D2201/00

Abstract: An inflatable restraint is disclosed, and includes an elongated poncho having therein an air-tight bladder and a cervical aperture for insertion of the head of the individual. A front portion of the poncho is adapted for juxtaposition with a rear surface of a forward seat and a rear portion is adapted for juxtaposition with and between the back of the torso and a forward surface of a rearward seat when inflated. The front portion is longer than the rear portion and has a larger volumetric displacement when inflated and extends over the front torso and lower extremities of the individual. The rear portion extends over the back torso of the individual. An inflation means inflates the bladder and restrains the individual between the forward and rearward seats for protection of the individual during an emergency while traveling in a vehicle.

Abstract translation: 公开了一种可膨胀的约束，并且包括其中具有气密囊和用于插入个人头部的子宫颈孔的细长的斗篷。 雨披的前部适于与前座的后表面并置，并且后部适于在充气时与躯干的后部和后座的前表面并置。 前部比后部长，并且在膨胀时具有较大的体积位移，并且在个体的前躯干和下肢上延伸。 后部延伸到个体的后躯干上。 通气意味着使膀胱膨胀并且限制个体在前后座之间，以在紧急情况下在车辆行驶期间保护个体。

公开(公告)号：US5356097A

公开(公告)日：1994-10-18

申请号：US58328

申请日：1993-05-10

Applicant: Stefan Chalupa

Inventor： Stefan Chalupa

IPC: B64D25/12 ,  B64D1/12 ,  B64D25/18

CPC classification number: B64D25/12 ,  B64D2201/00

Abstract: An aircraft includes a cockpit permanently connected to a fuselage base. At least one fuselage segment is detachably mounted to the support. In case of an imminent crash the segment is detachable from the remainder of the aircraft and can float to safety after being detached by having at least one parachute and an airbag secured to the segment.

Abstract translation: 飞机包括一个永久连接到机身基座的驾驶舱。 至少一个机身段可拆卸地安装到支撑件上。 在即将发生的碰撞的情况下，该段可与飞机的其余部分分离，并且在通过具有至少一个降落伞和安全气囊固定到该段上而可以在分离之后浮起来。