公开(公告)号：US06598829B2

公开(公告)日：2003-07-29

申请号：US10114139

申请日：2002-04-02

申请人： Paulus Rein Kamstra

发明人： Paulus Rein Kamstra

IPC分类号： B64D1100

CPC分类号： B64D11/003

摘要： Hand luggage locker assembly for use in an aircraft cabin. The assembly includes a shell-like locker, a track mechanism for moveably connecting the locker to an aircraft structure between a closed position and an open position, and a lifting mechanism for relieving the muscle power required for a user to move the locker between the closed position and the open position. The lifting mechanism includes a moveable lifting body which, on one side, is connected to the track mechanism or to the locker and, on its other side, is connected to the aircraft structure, which lifting body is coupled to a pneumatic system. The pneumatic system includes means for supplying an underpressure compared to the pressure in the cabin, control means being provided for at least supplying the underpressure to the lifting body when the locker is to be moved upwards in a controlled manner with the aid of the underpressure as power source.

公开(公告)号：US06454209B1

公开(公告)日：2002-09-24

申请号：US09591879

申请日：2000-06-12

申请人： Thomas Bock ,  Andrew Muin ,  Markus Schumacher

发明人： Thomas Bock ,  Andrew Muin ,  Markus Schumacher

IPC分类号： B64D1100

CPC分类号： B64D11/00 ,  B60Q3/43 ,  B60Q2500/20 ,  B61D29/00

摘要： A comfort and illumination unit especially for a passenger space in an aircraft is constructed for cooperation with a straight wall panel that can be integrated in or secured to a vertical straight wall and/or a horizontal straight ceiling wall. The unit has a mounting base and a cover with passenger convenience elements mounted to the base under the cover which is provided with cut-outs for access to the convenience elements. Fluorescent bulbs form a frame around the convenience elements.

摘要翻译： 特别适用于飞机乘客空间的舒适和照明单元被构造成与可以集成在或固定到垂直直壁和/或水平直的天花板壁的直壁板协作。 该单元具有安装基座和具有乘客便利元件的盖子，该盖子安装到盖下面的基座上，该基座设置有用于接近便利元件的切口。 荧光灯在方便元件周围形成一个框架。

公开(公告)号：US06318672B1

公开(公告)日：2001-11-20

申请号：US09421199

申请日：1999-10-15

申请人： David L. Traylor

发明人： David L. Traylor

IPC分类号： B64D1100

CPC分类号： B64D11/00

摘要： The invention provides a quick disconnect mounting system for cabinets and partitions which entails only the removal of one or two bolt fasteners on the bottom of the cabinet and a pair of retractable pin fasteners on the upper portions of the cabinet, with an optional retractable pin fastener in the center rear of the cabinet. Each of these acoustical mounts are insulated, thus preventing vibration in the structural portion of the fuselage from entering the passenger compartment.

摘要翻译： 本发明提供了一种用于机柜和隔板的快速拆卸安装系统，其仅需要移除机壳底部上的一个或两个螺栓紧固件，以及在机柜的上部上的一对可缩回的销紧固件，其中可选的可缩回销紧固件 在机柜的中央后部。 这些声学安装座中的每一个都是绝缘的，从而防止机身的结构部分的振动进入乘客舱。

公开(公告)号：US06276634B1

公开(公告)日：2001-08-21

申请号：US09364611

申请日：1999-07-29

申请人： Peter Winstanley Bodle

发明人： Peter Winstanley Bodle

IPC分类号： B64D1100

CPC分类号： G08B7/066 ,  A62B3/00 ,  B60Q3/46 ,  B60Q3/47 ,  B60Q3/68 ,  B60Q3/78 ,  B64D25/00 ,  B64D2011/0038 ,  F21S4/22 ,  G09F13/20 ,  G09F19/22

摘要： An emergency lighting system for an aircraft has photoluminescent strips mounted on the floor rather than a string of electrical lights. This is a better fail-safe since there is no possibility of a failure in power supply. A channel extrusion is secured to the floor of the aircraft and a photoluminescent strip is held between the channel and a transparent cover member. The photoluminescent strip has two thin layers of photoluminescent material rather on a base layer, rather than being a calendered product. This increases the light output.

摘要翻译： 用于飞机的应急照明系统具有安装在地板上的光致发光条，而不是一串电灯。 这是一个更好的故障安全，因为电源不可能发生故障。 通道挤压固定在飞行器的地板上，并且光致发光条保持在通道和透明盖构件之间。 光致发光条具有两层薄的光致发光材料，而不是基底层，而不是压延产品。 这增加了光输出。

公开(公告)号：US06273365B1

公开(公告)日：2001-08-14

申请号：US09523422

申请日：2000-03-10

申请人： Stefan Hiesener ,  Joern Duering ,  Dieter Kasch

发明人： Stefan Hiesener ,  Joern Duering ,  Dieter Kasch

IPC分类号： B64D1100

CPC分类号： B64D11/003 ,  B64C2001/009

摘要： A storage compartment is combined with an air flow channel (5) between a passenger seat and an aircraft side wall in an aircraft cabin. The storage compartment is constructed of five walls forming a box (3) inserted into the air channel that extends longitudinally along the aircraft side wall and along the cabin floor. The box (3) is upwardly closed by a hinged cover (16) forming a tray (17). The aircraft side wall (2) has at least one air filter element (10) facing into the channel. One or more dado panels (7) with air flow passages (6) enclose the channel toward the cabin. A cabin floor (4) closes the channel (5) downwardly. One or more decompression flaps (15) in the floor (4) normally close the channel (5). Under normal operating conditions air flow into and out of the cabin passes around the box through the channel (5) and the filter element (10). Should a decompression occur the flap (15) is opened and pressure equalization is achieved by air flow through the openings in the cabin floor thereby bypassing the air filter element (10) for rapid pressure equalization in different spaces of the aircraft.

摘要翻译： 储藏室与飞机机舱中的乘客座位和飞机侧壁之间的空气流动通道（5）组合。 储藏室由五个壁构成，形成插入空气通道的箱体（3），空气通道沿飞机侧壁纵向延伸并沿着机舱地板延伸。 盒（3）由形成托盘（17）的铰接盖（16）向上封闭。 飞行器侧壁（2）具有面向通道的至少一个空气过滤元件（10）。 具有气流通道（6）的一个或多个Dado面板（7）将通道封闭到舱室。 机舱地板（4）向下关闭通道（5）。 地板（4）中的一个或多个减压襟翼（15）通常关闭通道（5）。 在正常操作条件下，进入和离开舱室的气流通过通道（5）和过滤元件（10）围绕箱体通过。 如果减压发生，则翼片（15）打开，并且通过气流通过机舱地板中的开口实现压力平衡，从而绕过空气过滤器元件（10）以在飞行器的不同空间中进行快速均压。

公开(公告)号：US06241187B1

公开(公告)日：2001-06-05

申请号：US09657372

申请日：2000-09-08

申请人： William R. Apel ,  Thomas C. LeTourneau

发明人： William R. Apel ,  Thomas C. LeTourneau

IPC分类号： B64D1100

CPC分类号： G09F7/00 ,  G09F3/10 ,  G09F15/02 ,  G09F2003/0254

摘要： An advertising placard (20) having a substrate (30) and coloration material (34) is utilized to provide an unobtrusive and nondistracting advertisement on internal viewing surfaces (22) in commercial aircraft passenger cabins (24). The substrate (30) is preferably thin and transparent, and the coloration material (34) preferably has substantially the same color hue as the viewing surface (22) to which it is applied. Further, the coloration material (34) preferably has a color lightness within approximately &Dgr;7 of the color lightness of the viewing surface (22).

摘要翻译： 具有基板（30）和着色材料（34）的广告标牌（20）用于在商用飞机乘客舱（24）中的内部观察表面（22）上提供不引人注意的和不重要的广告。 基材（30）优选为薄且透明的，并且着色材料（34）优选具有与其所施加的观察表面（22）基本相同的色调。 此外，着色材料（34）优选具有在观察表面（22）的颜色亮度的约DELTA7内的亮度。

公开(公告)号：US06772977B2

公开(公告)日：2004-08-10

申请号：US10278717

申请日：2002-10-22

申请人： Paul W. Dees ,  Mithra M.K.V. Sankrithi

发明人： Paul W. Dees ,  Mithra M.K.V. Sankrithi

IPC分类号： B64D1100

CPC分类号： B64C1/0009 ,  B64C1/26 ,  B64C25/04 ,  B64C25/10 ,  B64C2001/0027 ,  B64C2001/0045 ,  B64D9/003 ,  B64D11/00 ,  B64D27/18 ,  B64D37/04 ,  Y02T50/12

摘要： Transport aircraft, such as a transonic transport aircraft, having fuselages with multipurpose lower decks. In one embodiment, the fuselage is an “area-ruled” fuselage having a first fuselage portion, a second fuselage portion positioned aft of the first fuselage portion and at least proximate to a wing, and a third fuselage portion positioned aft of the second fuselage portion. The first fuselage portion can have a first dimension, the second fuselage portion can have a second dimension less than the first dimension, and the third fuselage portion can have a third dimension greater than the second dimension. The fuselage can further include an upper deck extending at least within the first and second fuselage portions, and a lower deck extending within the first fuselage portion. The upper deck can include a first passenger portion and the lower deck can include a second passenger portion, a cargo portion, or a second passenger portion and a cargo portion.

摘要翻译： 运输飞机，如跨音速运输机，具有多用途下甲板机身。 在一个实施例中，机身是具有第一机身部分的第一机身部分，位于第一机身部分后部并且至少靠近机翼的第二机身部分的“区域划分”机身，以及位于第二机身后方的第三机身部分 一部分。 第一机身部分可具有第一尺寸，第二机身部分可具有小于第一尺寸的第二尺寸，并且第三机身部分可具有大于第二尺寸的第三尺寸。 机身还可包括至少在第一和第二机身部分内延伸的上甲板，以及在第一机身部分内延伸的下甲板。 上甲板可以包括第一乘客部分，下甲板可以包括第二乘客部分，货物部分或第二乘客部分和货物部分。

公开(公告)号：US06739551B2

公开(公告)日：2004-05-25

申请号：US10253685

申请日：2002-09-24

申请人： Charles Temple ,  Walter Temple

发明人： Charles Temple ,  Walter Temple

IPC分类号： B64D1100

CPC分类号： G08B15/02 ,  B64C1/1469 ,  B64D45/0015

摘要： An expandable/collapsible enclosure positioned about the existing door of a flight crew compartment of an airliner, which is expanded either manually or automatically by the motion of the aircraft to form an airlock type enclosure about the door to the flight crew compartment, the enclosure having its own outer secondary door controllable from the flight crew compartment, an individual seeking access to the flight crew compartment having to position themselves in front of the outer door and again within the enclosure for observation by the flight crew personnel before entering the flight crew compartment, the enclosure having chemical or gaseous means for immobilizing an individual not authorized to enter the enclosure or the flight crew compartment who may have overwhelmed a properly identified individual that was authorized to enter the enclosure.

摘要翻译： 一个可扩展/可折叠的外壳，围绕客机的飞行机组舱室的现有门定位，手动或自动地通过飞行器的运动来扩展，以形成围绕飞行机组舱的门的气锁式外壳，外壳具有 其自己的外部二级门可以从飞行机组舱室控制，一个个人寻求进入机组人员舱的位置，必须将自己定位在外门前方，并再次在机舱内，以便飞行机组人员在进入飞行机组舱前观察， 外壳具有化学或气体装置，用于固定未被授权进入外壳的个人或可能淹没了被授权进入外壳的正确识别的个体的飞行机组舱。

公开(公告)号：US06698690B2

公开(公告)日：2004-03-02

申请号：US10310217

申请日：2002-12-04

申请人： Miloslav Novak ,  Andrew B. Trageser ,  Russell S. Long ,  Jerri F. McMichael ,  Eric F. M. Winter ,  Kenneth B. Balazic

发明人： Miloslav Novak ,  Andrew B. Trageser ,  Russell S. Long ,  Jerri F. McMichael ,  Eric F. M. Winter ,  Kenneth B. Balazic

IPC分类号： B64D1100

CPC分类号： B64D45/0015 ,  B64C1/1423 ,  B64C1/1469 ,  B64C2001/009

摘要： A two layer door is provided. The first layer is made of a plurality of metallic members with a portion of the metallic members having one or more channels adapted to receive one or more armor panels. The second layer is made of the channels of the metallic members and armor panels disposed within the channels. The door also has one or more pivotally attached panels to the door that are adapted to open at a preselected pressure differential across the door. The door is also available as a kit.

摘要翻译： 提供双层门。 第一层由多个金属构件制成，其中金属构件的一部分具有一个或多个适于接收一个或多个装甲板的通道。 第二层由设置在通道内的金属构件和装甲板的通道制成。 门还具有一个或多个枢转连接的面板到门，其适于以预定的压差在门上打开。 门也可作为工具包使用。

公开(公告)号：US06474599B1

公开(公告)日：2002-11-05

申请号：US09683297

申请日：2001-12-11

申请人： Gerald D. Stomski

发明人： Gerald D. Stomski

IPC分类号： B64D1100

CPC分类号： G08B15/007 ,  B64C1/1469 ,  B64D45/0015

摘要： An aircraft security system comprises a transparent bullet-proof security chamber interposed between the pilot area and the passenger area, and providing the only means of passage to the pilot area. The security chamber has a cockpit door to the cockpit area and passenger door to the passenger area. The passenger door must be closed when the cockpit door is open and vice versa. A third, or entry door, may be used to facilitate boarding the aircraft. All doors are closed and locked when sensors indicate unauthorized entry of a passenger into the security chamber.

摘要翻译： 一种飞机安全系统，包括一个插入在飞行员区域和乘客区域之间的透明防弹安全室，并提供通往试点区域的唯一手段。 安全室具有驾驶舱的驾驶舱门和乘客区域的乘客门。 驾驶舱门打开时乘客门必须关闭，反之亦然。 第三个或进入门可用于方便登机。 当传感器表明未经许可进入安全室时，所有门都关闭并锁定。