公开(公告)号：US20110225695A1

公开(公告)日：2011-09-22

申请号：US13045647

申请日：2011-03-11

Applicant: Chih-Wei CHENG

Inventor： Chih-Wei CHENG

IPC: B64D10/00 ,  B60R21/26

CPC classification number: B64D10/00 ,  B64D2201/00

Abstract: A life-saving device has a garment and at least one airbag assembly. The at least one airbag assembly is mounted on the garment and each one of the at least one airbag assembly has a gas cylinder, a gas tube, multiple airbag layers and at least one connecting tube. The gas cylinder is attached to the garment. The gas tube is connected between the gas cylinder and the airbag layers. Each one of the at least one connecting tube is connected between two adjacent airbag layers. A user wearing the life-saving device can actuate the gas cylinder when falling from high altitudes to inflate the airbag layers via the gas tube and the at least one connecting tube. The inflated airbag layers will provide an air resistance to slow down the falling speed. Therefore, the user can safely descend to the ground.

Abstract translation: 救生装置具有衣服和至少一个安全气囊组件。 所述至少一个安全气囊组件安装在所述衣服上，并且所述至少一个气囊组件中的每一个具有气瓶，气管，多个气囊层和至少一个连接管。 气瓶附着在衣服上。 气体管连接在气瓶和气囊层之间。 所述至少一个连接管中的每一个连接在两个相邻的气囊层之间。 佩戴救生装置的使用者可以在从高空落下时致动气瓶，经由气管和至少一个连接管使气囊层膨胀。 膨胀的气囊层将提供空气阻力以减慢下落速度。 因此，用户可以安全地下降到地面。

公开(公告)号：US07980590B2

公开(公告)日：2011-07-19

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：US20100276540A1

公开(公告)日：2010-11-04

申请号：US12735176

申请日：2008-04-23

Applicant: Camilo Garcia Rojo

Inventor： Camilo Garcia Rojo

IPC: B64D25/02 ,  B60R21/217

CPC classification number: B60R21/01 ,  B60R21/16 ,  B60R2021/0093 ,  B60R2021/23107 ,  B64D25/00 ,  B64D25/02 ,  B64D2201/00

Abstract: The invention relates to an airbag system for aircraft, intended to protect crew and passengers. The system comprises: inflatable cushions; a supply of air from individual tanks, communal tanks and the aircraft APU; a connection to the landing gear and the altimeter; a manual switch; an approach and contact sensor enabling automatic activation; electric lines, electrovalves and air ducts. The system also includes a second version which is activated using electrochemical batteries which operate on the basis of sharp deceleration.

Abstract translation: 本发明涉及一种用于飞机的气囊系统，旨在保护船员和乘客。 该系统包括：充气垫; 来自各坦克，公共坦克和飞机APU的空气供应; 与起落架和高度计的连接; 手动开关; 一种能够自动激活的方法和接触式传感器; 电线，电动阀和风道。 该系统还包括使用基于急剧减速操作的电化学电池来激活的第二版本。

公开(公告)号：US07523891B2

公开(公告)日：2009-04-28

申请号：US11312738

申请日：2005-12-21

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

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

IPC: B64D17/80

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：US07156033B2

公开(公告)日：2007-01-02

申请号：US10789407

申请日：2004-02-27

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

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

IPC: B63B43/10

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：US20050269452A1

公开(公告)日：2005-12-08

申请号：US10998295

申请日：2004-11-27

Applicant: Glenn Wakefield

Inventor： Glenn Wakefield

IPC: B64C1/10 ,  B64D25/00

CPC classification number: B64D25/00 ,  B64D11/0619 ,  B64D2201/00

Abstract: Toughened airbag systems are applied to the bottom surface of an aircraft to permit the crashing vehicle to land on a cushion of air. Shock absorber systems fitted to aircraft seats allow a more gradual deceleration of the occupant. A bumper system is applied to ground vehicles/trains to allow a more gradual deceleration of the vehicle/train and to minimize injury to pedestrians.

Abstract translation: 增强的气囊系统被应用到飞行器的底面，以允许撞击的车辆落在空气垫上。 安装在飞机座椅上的减震器可以使乘客逐渐减速。 保险杠系统适用于地面车辆/火车，以允许车辆/火车逐渐减速，并尽量减少对行人的伤害。

公开(公告)号：US06708927B2

公开(公告)日：2004-03-23

申请号：US10156127

申请日：2002-05-29

Applicant: Jack Chen

Inventor： Jack Chen

IPC: B64O1700

CPC classification number: B64D17/72 ,  A62B1/22 ,  B64D17/00 ,  B64D2201/00

Abstract: An apparatus for slowing and safely descending from a high-rise building includes a plurality of independent airbags which are connected together to form an airbag jumpsuit, a harness mounted at sternum and back position on an outside layer of the jumpsuit, a pair of triangular wings each connected to one side of the jumpsuit, a first secondary airbag located at an upper chest portion of the jumpsuit and connected to an air pipe, a second secondary airbag located at a lower abdomen portion of the jumpsuit and connected to an air pipe, and a parachute connected to the harness and having a canopy with a plurality of tubular ribs on an outer layer which are communicated with one another and also filled with air, a top of the parachute having an orifice which is connected to the tubular ribs, a flexible air pipe being connected to a top of the parachute, a top of the parachute having two large holes and two small holes, each of the holes being connected to suspension lines of a small parachute.

Abstract translation: 一种用于从高层建筑物放慢安全降落的装置包括多个独立的安全气囊，它们连接在一起以形成气囊连身裤，安装在胸针上的线束和在连身裤的外层上的后部位置，一对三角形的翼 每个连接到连接线的一侧，第一副安全气囊，位于连接针的上胸部并连接到空气管，第二辅助气囊位于连接线的下腹部并连接到空气管，以及 连接到所述线束并且具有彼此连通并且还充满空气的外层上的多个管状肋的顶篷的降落伞，所述降落伞的顶部具有连接到所述管状肋的孔，柔性 空气管连接到降落伞的顶部，降落伞的顶部具有两个大孔和两个小孔，每个孔连接到小parac的悬挂线 静音

公开(公告)号：US06422513B1

公开(公告)日：2002-07-23

申请号：US09644162

申请日：2000-08-22

Applicant: Donald J. Lewis ,  Terry W. Merrifield

Inventor： Donald J. Lewis ,  Terry W. Merrifield

IPC: B64C100

CPC classification number: B64D25/02 ,  B64D25/04 ,  B64D25/06 ,  B64D25/10 ,  B64D2201/00

Abstract: One or more tubular inflatables are mounted in pockets spaced around a flight vest to assist and maintain upper body stiffness during ejection. The inflatables function to maintain the body stiff and prevent its moving from side to side during ejection. By proper positioning of the inflatables around the body, spinal compression may be prevented. In addition, connected to the flight vest is a collar-like inflatable that supports and protects the neck and head of the air crewmember from moving. The collar-like member can encircle the neck like a scarf. In another embodiment, it can also extend above the shoulders and completely encircle the helmet holding the head in a vertical position. In each embodiment, the collar-like member properly maintains the center of gravity of the air crewmember on the aircraft seat.

Abstract translation: 一个或多个管状可充气装置安装在围绕飞行背心间隔开的口袋中，以在排出期间辅助和保持上身刚度。 充气功能用于在弹出时保持身体僵硬并防止其从侧面移动到另一侧。 通过将身体充分定位在身体周围，可以防止脊柱压缩。 此外，连接到飞行背心是一个领子般的充气，支持和保护机组人员的颈部和头部移动。 衣领类的成员可以像围巾一样环绕颈部。 在另一个实施例中，其还可以在肩部上方延伸并且完全围绕将头部保持在垂直位置的头盔。 在每个实施例中，套环状构件适当地将机组人员的重心保持在飞行器座椅上。

公开(公告)号：US6042051A

公开(公告)日：2000-03-28

申请号：US966900

申请日：1997-11-10

Applicant: Jon C. Hagerty

Inventor： Jon C. Hagerty

IPC: B64C3/56 ,  B64D25/12

CPC classification number: B64C3/56 ,  B64D25/12 ,  B64D2201/00

Abstract: An aircraft landing assist system comprised of a preformed and prepacked parawing-bag and fuselage housing and deployment is described. In case of emergency the system can be deployed automatically, manually, or by means of explosive charge. After deployment the open doors and the self inflated parawing-bag catch the on rushing air forcing the nose of the aircraft up. This helps increase the glide ratio and decrease the velocity of the aircraft. Control of the aircraft remains through the use of the upper wing surfaces and tail assembly. Upon landing the system helps extend the time of, and surface area of impact. Drains are provided in the aft section of the parawing-bag(s) to release rain or snow.

Abstract translation: 描述了由预先形成的预包装的解码袋和机身外壳和展开组成的飞机着陆辅助系统。 在紧急情况下，系统可以自动，手动或通过爆炸装置进行部署。 在部署后，敞开的门和自膨胀的解码袋抓住冲击空气迫使飞机的鼻子上升。 这有助于提高飞机的滑行比并降低飞机的速度。 飞机的控制仍然是通过使用上翼面和尾翼组件。 系统着陆后有助于延长时间和表面积的影响。 排水管设在解码袋的后部以释放雨或雪。

公开(公告)号：US5992794A

公开(公告)日：1999-11-30

申请号：US9409

申请日：1998-01-20

Applicant: Israel Rotman ,  Gideon Rosenberg

Inventor： Israel Rotman ,  Gideon Rosenberg

IPC: B64C25/32 ,  B64C25/56 ,  B64C27/00 ,  B64D25/00

CPC classification number: B64D25/00 ,  B64C25/32 ,  B64C25/52 ,  B64C25/56 ,  B64C27/006 ,  B64C2025/325 ,  B64D2201/00

Abstract: An airbag protection system for helicopters. Airbags are inflated either automatically or manually, or a combination of both, prior to the helicopter striking the ground, thus avoiding or ameliorating a crash. Proximity sensors detect a fast descent to trigger inflation of the airbags located beneath the helicopter fuselage so that they can cushion the impact with the ground. Venting of the gas from the airbags is also provided to release the gas from the airbags so as to prevent rebound of the helicopter from the ground.