公开(公告)号：US20050077429A1

公开(公告)日：2005-04-14

申请号：US10645044

申请日：2003-08-18

申请人： Michael Beauchamp

发明人： Michael Beauchamp

IPC分类号： B64D25/10 ,  B64D17/00

CPC分类号： B64D25/10 ,  B64D2201/00

摘要： An aircraft occupancy, here a helicopter with a seat chassis mounted on a set of rails of any type, ideally as I have demonstrated on load bearing triple monorails with one hundred sixty-eight circumventing roller trucks attached to the inner rails, an outer track box movable along the inner tracks, and a monorail supporting track with eighty-four roller trucks. Shown here in a side view with partial delineation of the mesh end cover Any seat chassis attached to the outer track box is ejectable along a lateral trajectory, perpendicular to the horizontal longitudinal axis of an aircraft, and guided out of the path of a failed aircraft during ejection flight by two bottom positioned tail fins slotted within the ejection monorails launcher platform legs. The seat chassis is enabled to eject laterally since a conventional hinged door is operational within a greater sliding door panel which pneumatic rockets at the top and bottom of the sliding door transverse the greater emergency sliding door panel including the interior fixed conventional hinge operational door out of the path of the seat chassis or chassis', attached to the outer track box towards the rear of the aircraft where the sliding greater panel is prevented from recoiling by a common latch catches. Dual airbags for positioning the legs and torso of an occupant for a safe emergency exit ejection are embedded or attached to the structure directly fore of the seat chassis. A second set of airbags, head, neck and chest protector are connected on both sides of the seat chassis, mandatory for safe lateral equal access emergency exit ejection. Three compartments for altitude appropriate parachutes and sensor fuse box for opening said desired chute. Including an interior side mounted blast shield and monorails inner tracks support to which a couple of rocket catapults are fixed by seals at their ignition points, holding the outer track box and seat chassis stationary between the inner tracks and supporting track.

公开(公告)号：US06845947B1

公开(公告)日：2005-01-25

申请号：US10681499

申请日：2003-10-09

申请人： Milton L. Reese, Jr. ,  Edward G. Tersine

发明人： Milton L. Reese, Jr. ,  Edward G. Tersine

IPC分类号： B64C1/14 ,  B64C1/32 ,  B64C1/00

CPC分类号： B64C1/32 ,  B64C1/1476 ,  B64D2201/00

摘要： A method of removing a canopy from a cockpit of an aircraft comprising providing an airbag in the cockpit adjacent the canopy; inflating the airbag; and as the airbag inflates, applying a force to the canopy from the inflating airbag to thereby jettison the canopy.

摘要翻译： 一种从飞行器驾驶舱中移除冠层的方法，包括：在座舱附近提供安全气囊; 使气囊充气; 并且当安全气囊膨胀时，从充气气囊向冠层施加力，从而排出顶盖。

公开(公告)号：US20040219314A1

公开(公告)日：2004-11-04

申请号：US10425014

申请日：2003-04-29

发明人： Glen J. Brown

IPC分类号： B32B001/02

CPC分类号： F16F7/00 ,  B64D1/14 ,  B64D2201/00 ,  F16F9/0472 ,  Y10T428/13

摘要： Inflating conical legs are mounted on a structure that needs protection against destruction upon impact with the ground as it descends at a potentially destructive velocity. The legs are inflated before impact and they deflate with the pressure caused by the compression forces of impact through an exhaust valve at a rate designed, in conjunction with the conical shape of the legs, to preclude an excessive deceleration rate for the overall structure during impact.

摘要翻译： 膨胀的圆锥形支架安装在一个结构上，当结构以潜在的破坏性速度下降时，需要防止与地面碰撞时的破坏。 腿部在冲击之前膨胀，并且以与腿部的圆锥形状一起设计的速率通过排气阀由冲击压力引起的压力放气，以防止冲击期间整体结构的过度减速率 。

公开(公告)号：US20040188566A1

公开(公告)日：2004-09-30

申请号：US10753550

申请日：2004-01-08

发明人： Philip Kneisl

IPC分类号： B64D011/00

CPC分类号： G08B15/00 ,  B64D45/0015 ,  B64D2045/002 ,  B64D2201/00

摘要： 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.

摘要翻译： 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。

公开(公告)号：US20040021036A1

公开(公告)日：2004-02-05

申请号：US10209435

申请日：2002-07-30

发明人： Philip Kneisl

IPC分类号： B64D011/00 ,  B64D013/00

CPC分类号： G08B15/00 ,  B64D45/0015 ,  B64D2045/002 ,  B64D2201/00

摘要： 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.

摘要翻译： 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：US06682017B1

公开(公告)日：2004-01-27

申请号：US10220977

申请日：2002-09-09

申请人： Pavlos Giannakopoulos

发明人： Pavlos Giannakopoulos

IPC分类号： B64C132

CPC分类号： B64D25/12 ,  B64D17/80 ,  B64D2201/00 ,  Y10S70/06 ,  Y10T70/7051

摘要： An aircraft with a detachable cabin (1) that serves to rescue its passengers as a result of the aircraft's sudden fall either due to its malfunction or fire. The cabin escapes either smoothly or by means of fast ejection and descends slowly to the Earth with the aid of a parachute (13, 14); during a crash on the ground or in the sea external airbags (38a-38f) with which it is equipped and which are located in its lower part are inflated thus absorbing the loads that are developed during the crash. In addition a conventional aircraft (70) of the type being already in use is also described and in which the parachute equipment (71) has already been applied; however, the proposed equipment of the airbag boxes (72a-72c) is adapted to it for the absorption of the energy produced due to its crash on Earth in case of its sudden fall.

摘要翻译： 一架带有可拆卸舱室（1）的飞机，由于其故障或火灾而导致飞机突然下落，从而拯救乘客。 客舱可以顺利进行，也可以通过快速排出，借助降落伞慢慢地下降到地球上（13,14）。 在地面或海上碰撞期间，装备有下部的外部安全气囊（38a-38f）被充气，从而吸收在碰撞期间产生的载荷。 此外，还描述了已经使用的类型的常规飞行器（70），并且已经应用​​了降落伞设备（71）; 然而，所提出的安全气囊箱（72a-72c）的设备适合于在突然坠落的情况下由于其在地球上的碰撞而产生的能量的吸收。

公开(公告)号：US20030222178A1

公开(公告)日：2003-12-04

申请号：US10156127

申请日：2002-05-29

发明人： Jack Chen

IPC分类号： B64D017/00

CPC分类号： B64D17/72 ,  A62B1/22 ,  B64D17/00 ,  B64D2201/00

摘要： 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.

摘要翻译： 用于从高层建筑物减速并安全地下降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背部位置。 一对三角形翼片，各自连接到所述连接线的一侧，第一辅助安全气囊位于所述连帽衫的上胸部并连接到空气管，第二辅助气囊位于所述连身裤的下腹部并连接到 空气管和降落伞，其连接到所述线束并且具有冠层，其具有彼此连通并且还充满空气的外层上的多个管状肋，所述降落伞的顶部具有连接到所述导管的孔， 管状肋，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，每个孔连接到小降落伞的悬挂线。

公开(公告)号：US06227325B1

公开(公告)日：2001-05-08

申请号：US09588679

申请日：2000-06-07

申请人： Reza H. Shah

发明人： Reza H. Shah

IPC分类号： B60K2810

CPC分类号： B63B59/02 ,  B60R19/205 ,  B60R2021/0006 ,  B60R2021/0016 ,  B60R2021/0088 ,  B60R2021/0093 ,  B60R2021/0095 ,  B62J27/00 ,  B64C25/32 ,  B64C25/56 ,  B64D25/00 ,  B64D2201/00

摘要： External inflatable safety bags are provided in this system which is adaptable for a variety of conveyances. A sensing means determines the speed and distance between the conveyance and an obstacle or another conveyance for selectively providing a warning signal to the driver to avoid a collision or to deploy the safety bags automatically when collision is imminent. The safety bags provide impact absorption as well as aerodynamic breaking of the speed of the conveyance.

摘要翻译： 该系统提供外部充气安全气囊，适用于各种运输工具。 感测装置确定运输工具与障碍物或另一运送工具之间的速度和距离，以便在碰撞即将发生时，选择性地向驾驶员提供警告信号以避免碰撞或自动部署安全袋。 安全袋提供冲击吸收以及运输速度的气动破坏。

公开(公告)号：US06213427B1

公开(公告)日：2001-04-10

申请号：US09232620

申请日：1999-01-19

申请人： Edwin Mareska

发明人： Edwin Mareska

IPC分类号： B64D2502

CPC分类号： B64D25/12 ,  B64D11/00 ,  B64D2201/00

摘要： A self-contained airliner passenger safety module. A module is preferably made of a lightweight material, such as fiberglass, capable of absorbing at least some of the energy generated when an airliner inadvertently impacts with the ground. Passenger seat bases are molded into the module and are provided with slots through which passenger safety belts are passed; thus, a passenger is belted directly to each module. Each seat back is further provided with a deployable safety member, such as an airbag. A module is also equipped with electricity, water, air conditioning, and a fire extinguisher at each end. A module is also provided with sealable doorways. The number of modules to be used in a given airliner is governed by the size and type of airliner in which the modules are to be placed. The modules are designed to be positioned in the interior of an airliner fuselage. They are secured to the floor of a fuselage with a series of graduated shear pins and anti-vibration hold down pins. In the event of an inadvertent airliner impact, the shear pins and hold down pins shear as the fuselage disintegrates and the airbags deploy. The energy vector changes caused by the impact permit the modules to be deployed away from the airliner, thereby increasing the chance of survival by the module's occupants.

摘要翻译： 一个独立的客机乘客安全模块。 模块优选地由诸如玻璃纤维的轻质材料制成，其能够吸收当客机无意中与地面碰撞时产生的至少一些能量。 乘客座椅基座模制成模块，并设有通过乘客安全带穿过的槽; 因此，乘客直接绑在每个模块上。 每个座椅靠背还设置有可展开的安全构件，例如气囊。 每个模块还配备有电，水，空调和灭火器。 模块还具有可密封的门口。 在给定客机中使用的模块数量由要安装模块的客机的尺寸和类型决定。 这些模块设计成位于机载机身内部。 它们固定在机身的地板上，配有一系列刻度剪切销和抗振动压脚。 在无意中的客机撞击的情况下，当机身分解并且安全气囊部署时，剪切销和压紧销剪切。 由冲击引起的能量矢量变化允许将模块部署在远离客机的地方，从而增加了模块乘员的生存机会。

公开(公告)号：US4645142A

公开(公告)日：1987-02-24

申请号：US564476

申请日：1983-12-21

申请人： Michael Soelter

发明人： Michael Soelter

IPC分类号： B60V1/00 ,  B60V1/16 ,  B64D1/14 ,  F16F9/04

CPC分类号： B60V1/16 ,  B64D1/14 ,  F16F9/0418 ,  B64D2201/00

摘要： One end of a hose is affixed to the underside of the object which may descend and whose impact has to be cushioned while the other end of the hose is pulled through the first end, the two ends are separately fastened permitting filling of the hose; a second hose may be inserted in the first one to provide separate filling spaces, one being the interior of the second hose and the other one being the gas space between the two hoses whereby different pressures permit selection of the resilient characteristics of the cushion.

摘要翻译： 软管的一端固定到物体的下侧，该下侧可能下降，并且其冲击必须被缓冲，同时软管的另一端被拉过第一端，两端分别固定，允许填充软管; 可以在第一软管中插入第二软管以提供单独的填充空间，一个是第二软管的内部，另一个是两个软管之间的气体空间，由此不同的压力允许选择衬垫的弹性特性。