公开(公告)号：US20110260001A1

公开(公告)日：2011-10-27

申请号：US13088804

申请日：2011-04-18

Applicant: Jean-Jacques Ferrier ,  Pierre Prudhomme-Lacroix

Inventor： Jean-Jacques Ferrier ,  Pierre Prudhomme-Lacroix

IPC: B64C25/58 ,  B64C25/56

CPC classification number: B64C27/006 ,  B64C25/52 ,  B64C2025/325 ,  B64D25/00 ,  B64D2201/00

Abstract: Aircraft landing gear (10) provided with at least one contact means (20) for making contact with a contact surface (S). The landing gear includes energy absorber means (30) provided with an inflatable airbag (31) secured to said contact means (20), said energy absorber means (30) being provided with control means (32) and with at least one inflation means (32) for inflating said airbag (31) under the control of said control means (32), said energy absorber means (30) including adjuster means (34) for adjusting the pressure that exists inside (INT) said airbag (31).

Abstract translation: 设置有至少一个用于与接触表面（S）接触的接触装置（20）的飞机起落架（10）。 起落架包括设置有固定到所述接触装置（20）的可充气安全气囊（31）的能量吸收装置（30），所述能量吸收装置（30）设有控制装置（32）和至少一个充气装置 32），用于在所述控制装置（32）的控制下使所述气囊（31）膨胀，所述能量吸收装置（30）包括用于调节存在于所述气囊（31）内部（INT）的压力的调节装置（34）。

公开(公告)号：US20110204606A1

公开(公告)日：2011-08-25

申请号：US13032891

申请日：2011-02-23

Applicant: Thomas Rathmann-Ramlow ,  Ulf Grüne

Inventor： Thomas Rathmann-Ramlow ,  Ulf Grüne

IPC: B60R21/18

CPC classification number: B60R21/18 ,  B60R22/26 ,  B64D11/062 ,  B64D11/06205 ,  B64D2201/00

Abstract: A restraint system for occupants of a vehicle, comprising a belt; an airbag unit arranged on the belt, wherein the positions of the belt and the airbag unit can be shifted with respect to each other; an airbag in the airbag unit; and means for securing the position of the airbag on the belt, i.e., means by which the airbag and the belt can be fastened together upon deployment of the airbag without the possibility of a shift in their relative positions.

Abstract translation: 一种用于车辆乘员的约束系统，包括皮带; 布置在所述带上的气囊单元，其中所述带和所述气囊单元的位置可以相对于彼此移位; 气囊单元中的气囊; 以及用于将气囊的位置固定在皮带上的装置，即，在安全气囊展开时，气囊和皮带可以紧固在一起的装置，而不会有相对位置的变化的可能性。

公开(公告)号：US20110204181A1

公开(公告)日：2011-08-25

申请号：US13125884

申请日：2009-07-27

Applicant: Andrew T. Hill ,  Michael R. Smith ,  Zi Lu ,  Cheng-Ho Tho

Inventor： Andrew T. Hill ,  Michael R. Smith ,  Zi Lu ,  Cheng-Ho Tho

IPC: B64C25/56

CPC classification number: B64D25/00 ,  B64C27/04 ,  B64D2201/00

Abstract: A crash attenuation system for an aircraft includes an airbag carried by the aircraft that is inflatable generally adjacent an exterior of the aircraft. The airbag is in fluid communication with at least one vent passage for channeling gas from within the interior of the airbag to a region external to the airbag that allows the gas to escape without being obstructed by the airbag. A gas source is in fluid communication with the interior of the airbag for inflating the airbag. A vent valve is provided within the vent passage for controlling a flow of gas through the vent passage, thereby controlling deflation of the airbag. The vent valve is continuously adjustable to and between an open state, a closed state, and any number of partially open states.

Abstract translation: 用于飞行器的碰撞衰减系统包括由飞机携带的气囊，该气囊大体上邻近飞行器的外部可充气。 气囊与至少一个通气通道流体连通，用于将气体从气囊的内部引导到气囊外部的区域，允许气体逸出而不被气囊阻挡。 气体源与气囊的内部流体连通，以使气囊膨胀。 在排气通道内设有排气阀，用于控制通过通气通道的气体流，从而控制气囊的放气。 排气阀可连续调节到打开状态，关闭状态和任何数量的部分打开状态之间。

公开(公告)号：US20110133539A1

公开(公告)日：2011-06-09

申请号：US13057442

申请日：2009-08-03

Applicant: Hirokazu Shoji ,  Kazuo Katayama ,  Norio Enomoto ,  Hiroshi Yutani

Inventor： Hirokazu Shoji ,  Kazuo Katayama ,  Norio Enomoto ,  Hiroshi Yutani

IPC: B64D11/06 ,  F16F9/10

CPC classification number: B64D11/0619 ,  B60N2/4242 ,  B64D11/06 ,  B64D11/0647 ,  B64D25/04 ,  B64D2201/00

Abstract: The present invention provides a shock absorbing apparatus for an aircraft seat, that attenuates shock to passengers and crews.The apparatus includes; an airbag 11 being expanded in a plate shape in a state of less than maximum expansion; an upper flat plate 12 arranged on one side of the airbag 11; a lower flat plate 13 arranged on another side of the airbag 11; a gas supply device 15 for supplying a gas to the airbag 11; and a detector sending a signal to activate the gas supply device 15 by a preset condition. The shock is absorbed by expanding the airbag 11 before the shock is applied to the passenger.

Abstract translation: 本发明提供一种用于飞机座椅的减震装置，其减轻对乘客和乘员组的冲击。 该装置包括： 气囊11在小于最大膨胀的状态下膨胀成板状; 布置在气囊11一侧的上平板12; 布置在气囊11的另一侧的下平板13; 用于向气囊11供给气体的气体供给装置15; 以及检测器，其发送信号以使预定条件激活气体供给装置15。 在冲击应用于乘客之前，通过使气囊11膨胀来吸收冲击。

公开(公告)号：US20100206983A1

公开(公告)日：2010-08-19

申请号：US12679563

申请日：2007-10-22

Applicant: Cheng-Ho Tho ,  Michael S. Smith

Inventor： Cheng-Ho Tho ,  Michael S. Smith

IPC: B64C25/56

CPC classification number: B64D25/00 ,  B64C25/52 ,  B64C2025/325 ,  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 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, any number of intermediate states, in which the vent is partially open, and a closed state, in which gas is retained within the interior of the airbag.

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。 气体源与气囊的内部流体连通，用于通过由第一气体源产生的气体使气囊充气。 设置排气阀以控制通过每个通气口的气体流动，每个排气阀可以在打开状态之间选择性地配置，在该状态下，气体可以从气囊的内部通过相关联的通气口，其中任何数量的中间状态，其中 通风口部分打开，并且气体保持在气囊内部的关闭状态。

公开(公告)号：US20090178597A1

公开(公告)日：2009-07-16

申请号：US12381595

申请日：2009-03-12

Applicant: John W. Sliwa, JR.

Inventor： John W. Sliwa, JR.

IPC: E06B9/00

CPC classification number: F41H13/005 ,  B64D45/0015 ,  B64D45/0036 ,  B64D45/0053 ,  B64D2201/00 ,  F41H11/00 ,  F41H13/0006

Abstract: Various novel means are provided to neutralize determined if not fanatical attackers, and in most embodiments to proactively prevent harm to most or all innocent bystanders. In one example, a system offering protection to victims of any one or more of terrorism, criminal behavior and disasters is provided. The system provides protection via one or more of i) immobilization of a perpetrator, if any, ii) protective physical immobilization of potential or actual victims of a disaster, iii) protective physical shielding of actual or potential victims of a disaster, iv) physical blockage of dangerous flying projectiles or debris whether coming from a perpetrator or as a consequence of an actual or potential disaster or v) visual blockage of the perpetrator such that he cannot easily act against victims.

Abstract translation: 提供各种新颖的手段来中和确定的不是狂热的攻击者，并且在大多数实施例中主动地防止对大多数或所有无辜旁观者的伤害。 在一个例子中，提供了向恐怖主义，犯罪行为和灾害中的任何一种或多种受害者提供保护的制度。 该系统通过以下一种或多种方式提供保护：i）固定犯罪者（如果有的话），ii）对潜在或实际遇难的灾民进行保护性物理固定，iii）对灾害的实际或潜在受害者进行保护性物理屏蔽，iv）物理 阻止危险的飞行的射弹或碎片，不论是从犯人身上造成的，还是由于实际或潜在的灾难造成的，或者v）视觉上阻止肇事者，使他不能轻易地对受害者采取行动。

公开(公告)号：US20080315037A1

公开(公告)日：2008-12-25

申请号：US12087199

申请日：2006-12-15

Applicant: Ludger Merz ,  Roland Fuhrmann

Inventor： Ludger Merz ,  Roland Fuhrmann

IPC: B64C1/10

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：US20080142635A1

公开(公告)日：2008-06-19

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: B64C1/32 ,  F42B3/00 ,  B64C1/00 ,  B64D25/00 ,  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：US20080078883A1

公开(公告)日：2008-04-03

申请号：US11463560

申请日：2006-08-09

Applicant: Maxim de Jong

Inventor： Maxim de Jong

IPC: B64G1/00

CPC classification number: B64G1/222 ,  B64D2201/00 ,  B64G1/62 ,  B64G1/646 ,  B64G9/00 ,  B64G2001/224

Abstract: A flexible vessel includes a restraint structure and a barrier structure. The restraint structure further includes a first portion, and a second substantially rounded end cap portion that is attached to the first portion. The restraint structure also includes an array of tendons. The barrier structure is positioned within the restraint structure. When the barrier contains a fluid, a portion of the load is carried by the restraint structure and another portion of the load is carried by the barrier structure. The flexible vessel is collapsible to occupy a first volume and distended to occupy a second volume. The flexible vessel is part of a system when used in various applications with respect to a craft.

Abstract translation: 柔性容器包括约束结构和阻挡结构。 约束结构还包括第一部分和附接到第一部分的第二基本圆形的端盖部分。 约束结构还包括腱阵列。 阻挡结构位于约束结构内。 当挡板包含流体时，负载的一部分由约束结构承载，另一部分负载由阻挡结构承载。 柔性容器可折叠以占据第一体积并膨胀以占据第二体积。 柔性容器是用于相对于工艺的各种应用中的系统的一部分。

公开(公告)号：US20070145193A1

公开(公告)日：2007-06-28

申请号：US11312738

申请日：2005-12-21

Applicant: A-Hamid Hakki ,  Sam Hakki ,  Said Hakky

Inventor： A-Hamid Hakki ,  Sam Hakki ,  Said 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。