公开(公告)号：US20150034169A1

公开(公告)日：2015-02-05

申请号：US14461989

申请日：2014-08-18

申请人： GOODRICH CORPORATION

发明人： Jayant V. Deshpande ,  Wilfred Ray McBurnett, III

IPC分类号： B64D25/14 ,  F17C13/00 ,  F17C1/00

CPC分类号： B64D25/14 ,  F17C1/00 ,  F17C13/00 ,  Y10T137/0396 ,  Y10T137/3662

摘要： A system and method for inflating an inflatable device is disclosed. The system includes an inflation cylinder configured to hold a gas mixture under pressure, a heating element configured to selectively heat the gas mixture and a temperature sensor configured to measure a temperature of the gas mixture. A control module is coupled to the heating element and the temperature sensor. The the control module controls heating of the gas mixture based on the measured temperature, a mass of the gas mixture and a volume of the inflation cylinder.

摘要翻译： 公开了一种用于使充气装置充气的系统和方法。 该系统包括构造成在压力下保持气体混合物的膨胀圆筒，配置成选择性地加热气体混合物的加热元件和被配置成测量气体混合物的温度的温度传感器。 控制模块耦合到加热元件和温度传感器。 控制模块基于测量的温度，气体混合物的质量和膨胀气瓶的体积来控制气体混合物的加热。

公开(公告)号：US20100258677A1

公开(公告)日：2010-10-14

申请号：US12384703

申请日：2009-04-08

申请人： John O'Donnell ,  Frank Brown ,  Andreas Luethi

发明人： John O'Donnell ,  Frank Brown ,  Andreas Luethi

IPC分类号： B64D25/14

CPC分类号： B64D25/14 ,  Y10S244/905

摘要： Evacuation slide systems having extendable portions are detailed. The extendable portions of slides may be inflated separately from the main portions and actuated manually if desired. Consequently, attitude changes of, for example, an aircraft subsequent to inflation of the main portion of a slide would not necessarily defeat its use, as inflation of the extendable portion could still occur.

摘要翻译： 具有可扩展部分的疏散滑动系统是详细的。 滑动件的可延伸部分可以与主要部分分开充气并且如果需要手动地进行操作。 因此，由于滑块的主要部分的膨胀之后的飞机的姿态变化不一定会使其使用失败，因为可延伸部分的膨胀仍然可能发生。

公开(公告)号：US07159823B1

公开(公告)日：2007-01-09

申请号：US09973005

申请日：2001-10-10

申请人： Paul W. Paustian, Jr. ,  David J. Forrester

发明人： Paul W. Paustian, Jr. ,  David J. Forrester

IPC分类号： B64C1/22 ,  B62D1/08

CPC分类号： B64C1/22 ,  A62B1/20 ,  B64D25/14

摘要： A rapid deployment system has an inflatable landing tube with an inflatable exit slide coupled to an aircraft. Connectors couple the landing tube to the aircraft. Flexible retarders extend inward from the inner surface of the tube for retarding gravitational descent of cargo and/or personnel from the aircraft. The tube has tubular segments, with ribs and reinforcements, forming a continuous descent tube. A spine along the tube is retractable telescopically allowing for the tube to be retracted within the aircraft. The tube is connected to exterior edges of any exit port of the aircraft. A window coaming adapter is positioned around the exterior edges and a membrane extending between sides of the adapter expands with the landing tube as the landing tube is inflated. The membrane is of multiple layers with expansion cells between adjacent layers for allowing independent expansion of the layers. The entry port has a shield behind the membrane and connected to the aircraft for protecting the membrane. The shield has a couple of arms lying in a straight line when the landing tube is inactivated and separating and swinging outward from each other when the landing tube is activated. Another shield extends between edges of the exit port sandwiching the membrane between the two shields. An override lock on the one shield prevents that shield from opening automatically.

摘要翻译： 快速部署系统具有可充气的着陆管，其具有联接到飞行器的可充气出口滑动件。 连接器将着陆管连接到飞机。 柔性缓凝剂从管的内表面向内延伸，用于阻止货物和/或人员从飞行器的重力下降。 该管具有带肋和加强件的管状段，形成连续的下降管。 沿着管的脊柱可伸缩地伸缩，允许管在飞机内缩回。 管连接到飞机的任何出口的外部边缘。 窗户铰链适配器围绕外部边缘定位，并且当着陆管膨胀时，在适配器的两侧之间延伸的膜随着着陆管膨胀。 膜具有多层，在相邻层之间具有扩展单元，用于允许层的独立膨胀。 入口端口在隔膜后面有一个屏蔽层，并连接到飞机上以保护隔膜。 当着陆管被激活时，当着陆管被灭活并且分离并且在着陆管被启动时彼此向外摆动时，护罩具有躺在一条直线上的一对臂。 另一个屏蔽件在两个屏蔽之间夹着膜的出口端口之间延伸。 一个屏蔽上的超驰锁可防止屏蔽自动打开。

公开(公告)号：US20060266888A1

公开(公告)日：2006-11-30

申请号：US11138154

申请日：2005-05-26

申请人： Gary Matsch

发明人： Gary Matsch

IPC分类号： B64C1/22

CPC分类号： B64C1/1423 ,  B64D25/14 ,  Y10S244/905 ,  Y10T292/14

摘要： An inflatable evacuation slide system includes an inflatable evacuation slide stored in a packboard compartment the cover panel of which is retained by a plurality of frangible pneumatic latches. The frangible pneumatic latches each comprise a tension member one end of which is attached to the packboard housing and the other end of which is releasably attached to the cover panel. In normal operation, a pneumatic signal operating on an actuator piston withdraws the piston to allow the latch mechanism to release the cover panel. In the event of a failure of the release mechanism, since the releasable latch secures the cover panel to the frangible tension member rather than to the packboard directly, the force of the inflating evacuation slide breaks the frangible member allowing the cover panel to drop away with only a brief delay in slide deployment.

摘要翻译： 充气抽空滑动系统包括储存在包装板隔室中的可充气抽空滑梯，其盖板由多个易碎的气动闩锁保持。 易碎气动闩锁各自包括张紧构件，其一端附接到包装板壳体，并且其另一端可释放地附接到盖板。 在正常操作中，在致动器活塞上操作的气动信号使活塞收起，以允许闩锁机构释放盖板。 在释放机构发生故障的情况下，由于可释放的闩锁将盖板固定到易碎的张力构件而不是直接地与包装板固定，所以充气抽空滑架的力破坏了易碎构件，允许盖板随着 在幻灯片部署中只是一个短暂的延迟。

公开(公告)号：US07032778B2

公开(公告)日：2006-04-25

申请号：US10354389

申请日：2003-01-30

申请人： Christopher J. Bock ,  Jim Eskildsen

发明人： Christopher J. Bock ,  Jim Eskildsen

IPC分类号： B67D5/00

CPC分类号： F42B3/045 ,  B64D25/14 ,  Y10T137/1647

摘要： A dual stage hybrid inflation device includes a first stage gas source having a pressurized gas stored in a first stage pressure vessel and a second stage gas source having a pyrotechnic gas generator having a gas output directed into the first stage pressure vessel. The first stage pressure vessel is in fluid communication with an inflatable device such as an aircraft emergency evacuation slide via an externally actuated valve upstream of a pressure actuated valve such as a rupturable diaphragm. A control circuit provides a signal to the externally actuated valve to begin a flow of gases from first stage pressure vessel to a chamber on the upstream side of the burst diaphragm. The control circuit also sends a signal to the squib that initiates the pyrotechnic second stage gas source. As the pyrotechnic gas generator of the second stage gas source burns, the hot gaseous products of the second stage gas source mix with the pressurized gas stored in the first stage pressure vessel a predetermined time after the externally actuated valve opens.

摘要翻译： 双级混合式充气装置包括具有存储在第一级压力容器中的加压气体的第一级气体源和具有引导到第一级压力容器中的气体输出的烟火气体发生器的第二级气体源。 第一级压力容器通过诸如可破裂隔膜的压力致动阀上游的外部致动阀与诸如飞机紧急疏散滑块的可充气装置流体连通。 控制电路向外部致动的阀提供信号，以开始从第一级压力容器到爆裂隔膜的上游侧的腔室的气体流。 控制电路还向发起烟火第二级气源的爆管发送信号。 当第二级气体源的烟火气体发生器燃烧时，第二级气体源的热气体产物在外部致动阀打开之后的预定时间内与存储在第一级压力容器中的加压气体混合。

公开(公告)号：US20060029759A1

公开(公告)日：2006-02-09

申请号：US11198621

申请日：2005-08-05

申请人： Mark Hannigan ,  Charles Howland

发明人： Mark Hannigan ,  Charles Howland

IPC分类号： B60R21/16

CPC分类号： D03D1/02 ,  B64D25/14 ,  Y10T428/1362

摘要： A coated, bi-directional substrate design for an aircraft escape slide airbeam, where the longitudinal strength and hoop strength of the substrate and the coating applied thereto are optimized to the application. Less than 45% of the total substrate fiber content is in the longitudinal direction of the substrate, and the longitudinal strength of the substrate is approximately 50% of the hoop strength. The substrate is constructed of nylon, polyester, aramid, para-aramid or liquid crystal polymer fibers, and either polyurethane coatings and adhesives or polyether polyurethane coatings and adhesives. The warp yarns are less than ½ the denier of the fill yarns and are woven in groups of 2 or more yarns to improve the tear strength of the fabric in the warp direction.

摘要翻译： 用于飞机逃逸滑动气动束的涂覆的双向基板设计，其中基底和施加到其上的涂层的纵向强度和箍筋强度被优化至应用。 总基质纤维含量的45％以下是基材的长度方向，基材的纵向强度约为环箍强度的50％。 基材由尼龙，聚酯，芳族聚酰胺，对位芳族聚酰胺或液晶聚合物纤维，以及聚氨酯涂料和粘合剂或聚醚聚氨酯涂料和粘合剂构成。 经纱小于填充纱线的旦尼尔的1/2，并且以2根或多根纱线组织编织，以提高织物在经向上的撕裂强度。

公开(公告)号：US06966414B2

公开(公告)日：2005-11-22

申请号：US10725618

申请日：2003-12-02

申请人： Paul Zonneveld

发明人： Paul Zonneveld

IPC分类号： A62B1/20 ,  A62B3/00 ,  B64D25/14 ,  B65G11/00

CPC分类号： B64D25/14 ,  A62B1/20 ,  A62B3/00

摘要： An inflatable evacuation slide includes a flexible slide surface that is supported by longitudinal main support members. Illumination of the slide surface is provided by a plurality of illumination sources that are supported above the upper surface of the main support members on inflatable stanchions that extend upward from the upper surface of the main support members. The plurality of illumination sources may be high efficiency light emitting diodes or other high efficiency light sources. By providing an illumination source that is elevated above the upper surface of the main support members, a greater portion of the slide surface can be illuminated without shadows.

公开(公告)号：US06786454B2

公开(公告)日：2004-09-07

申请号：US10728050

申请日：2003-12-03

申请人： Jérôme Baderspach ,  Albert Modern ,  Sébastien Rondot

发明人： Jérôme Baderspach ,  Albert Modern ,  Sébastien Rondot

IPC分类号： B64C114

CPC分类号： B64C1/1407 ,  B64D25/00 ,  B64D25/14 ,  F15B1/022 ,  F15B21/10

摘要： The present invention concerns an emergency opening control device for an aircraft door comprising: at least one triggering mechanism (10) for emergency opening, at least one door actuator (8), and means of power supply (14, 16) to the actuator driven by the triggering mechanism. The device also comprises means (20) for modification of the output delivered by the means of power supply to the actuator, to allow the door to be opened more slowly in an initial phase of opening and more rapidly in at least one subsequent opening phase.

摘要翻译： 本发明涉及一种用于飞机门的紧急开启控制装置，包括：用于紧急打开的至少一个触发机构（10），至少一个门致动器（8）和由致动器驱动的致动器的电源（14,16） 触发机构。装置还包括用于修改由致动器供电的装置输出的输出的装置（20），以允许门在开始的初始阶段更加缓慢地打开，并且在至少一个 随后开放阶段。

公开(公告)号：US20030234323A1

公开(公告)日：2003-12-25

申请号：US10177190

申请日：2002-06-21

申请人： GOODRICH COMPANY

发明人： Leibert Danielson ,  William J. Horvath ,  Haiwen Meng

IPC分类号： B64D001/08 ,  B64C001/22 ,  B64D009/00

CPC分类号： B64D25/14 ,  A62B1/20 ,  Y10S244/905

摘要： An inflatable evacuation slide for emergency evacuation of an aircraft comprises a pair of main support tubes supporting a flexible sliding surface. The main support tubes taper from a widest point near the exit opening of the aircraft to a narrowest point at the foot end of the slide. This arrangement of main support tubes, together with the toe end transverse tube and the head end transverse tube, form a quasi-trapezoidal truss structure, which is inherently more stable than the rectangular slides of the prior art.

摘要翻译： 一种用于飞机紧急撤离的可充气疏散滑架包括一对支撑柔性滑动表面的主支撑管。 主支撑管从飞机出口附近的最宽点到幻灯片脚端的最窄点逐渐变细。 主支撑管与趾端横向管和头端横向管的这种布置形成准梯形桁架结构，其本身比现有技术的矩形滑块更稳定。

公开(公告)号：US06659404B1

公开(公告)日：2003-12-09

申请号：US10328557

申请日：2002-12-23

申请人： Lowell W. Roemke

发明人： Lowell W. Roemke

IPC分类号： F16K1714

CPC分类号： B64D25/14 ,  F16K17/048 ,  F16K17/14 ,  Y10S244/905 ,  Y10T137/36

摘要： An inflation system for inflating an inflatable evacuation slide includes an enclosure containing an uninflated, stored evacuation slide. The enclosure is sealed by means of a tightly fitting enclosure door that optionally includes a seal for excluding dirt and moisture. The system also includes a source of pressurized gas comprising a conventional pyrotechnic gas generator, stored pressurized gas, or hybrid inflator. The inflation system includes an overpressure relief vent, which vents inflation gas outside of the inflatable member in the event of an overpressure condition in the gas source. The overpressure relief vent includes a directional vent connected to a conduit. The conduit passes from the overpressure relief vent to an opening in the aircraft fuselage, which allows any vented gas to be safely directed away from the inflation system enclosure.

摘要翻译： 用于对充气抽空滑动件充气的充气系统包括包含未充气的储存的疏散滑块的外壳。 外壳通过紧密配合的外壳门密封，任选地包括用于排除污垢和湿气的密封件。 该系统还包括加压气体源，其包括常规的烟火气体发生器，储存的加压气体或混合式充气机。 膨胀系统包括超压释放口，其在气源中的过压状态下将充气气体排出膨胀气体外部。 超压释放孔包括连接到导管的定向排气孔。 导管从超压释放通道传送到飞行器机身的开口，这允许任何排放的气体被安全地从充气系统外壳导向。