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91. 发明公开

EP2193991A2 Aircraft window assembly 有权
标题翻译： Flugzeugfenster
公开(公告)号：EP2193991A2
公开(公告)日：2010-06-09
申请号：EP10158395.3
申请日：2007-02-16
申请人： The Boeing Company
发明人： Coak, Craig E.
IPC分类号： B64C1/14 , B60J10/02
CPC分类号： B64C1/1492
摘要： A window assembly is provided to prevent the migration of the window seal. The window assembly includes an outer window pane, an inner window pane and a seal. The outer window pane having a geometric feature configured to become parallel relative to another structure while the outer window pane rotates from a first position to a second position. The window assembly may further include a stiffening ring and a clamping ring which act to further secure the window seal in the desired position.
摘要翻译：提供了一种窗组件（200）以防止窗密封件（206）的迁移。窗组件包括外窗玻璃（202），内窗玻璃（204）和密封件（208）。窗组件包括加强环（210）和用于将窗户密封件固定在期望位置的夹紧环（212）。

92. 发明授权

EP1971797B1 DISPOSITIF DE GUIDAGE D ' UN CABLE D ' UN GLACE OUVRANTE 有权转让
标题翻译：装置，保护并保持CABLE飞机机舱的开闭窗
公开(公告)号：EP1971797B1
公开(公告)日：2009-04-22
申请号：EP07717799.6
申请日：2007-01-08
申请人： Airbus France SAS
发明人： BIANCALANA, Olivier
IPC分类号： F16L3/015 , B64C1/14
CPC分类号： B64C1/1492 , F16L3/015 , Y10T74/20462
摘要： The subject of the invention is a device for protecting and guiding at least one cable (22) connecting an openable window (10) for closing an opening of an aircraft cabin to its mounting (14), and is characterized in that it comprises a cable-supporting chain (26) which is deformable within a winding plane and is able to protect and guide said cable (22), and on either side of the cable-supporting chain (26) a first mounting (28) hinged to the openable window (10) in such a way as to be able to pivot about a hinge axis (36) extending approximately parallel to the translational movement of disengagement and a second mounting (30) hinged to the mounting (14) in such a way as to be able to pivot about a hinge axis (38) extending approximately parallel to the translation movement of disengagement, and in that the first and second mountings (28, 30) have an L-shaped cross section.

93. 发明授权

EP1748924B1 WINDOW FRAME FOR AIRCRAFT 有权转让
标题翻译：窗框飞机
公开(公告)号：EP1748924B1
公开(公告)日：2009-03-11
申请号：EP05752736.8
申请日：2005-05-24
申请人： Airbus Deutschland GmbH
发明人： BOLD, Jens
IPC分类号： B64C1/14
CPC分类号： B64C1/1492 , B29C70/48 , B29L2031/005 , Y02T50/43
摘要： The frame (1) includes at least one outer flange (2) attached to the window opening edge of the aircraft fuselage, and at least one inner flange (3) and a vertical flange (4) which support a window piece e.g. glass panel. The frame is made from resin reinforced with fiber webbing semifinished components. An independent claim is also included for a window frame manufacturing method.

94. 发明公开

EP1995046A2 Method of fabricating fiber reinforced composite structure having stepped surface 有权
标题翻译：一种用于生产纤维的方法增强复合结构，台阶面
公开(公告)号：EP1995046A2
公开(公告)日：2008-11-26
申请号：EP08156854.5
申请日：2008-05-23
申请人： The Boeing Company
发明人： Modin, Andrew E. , Woods, Jack A. , Hawkins, Robert D.
IPC分类号： B29C70/34 , B29C70/54
CPC分类号： B32B38/0004 , B29C70/202 , B29C70/34 , B29C70/54 , B29C70/545 , B29L2031/005 , B29L2031/3076 , B32B5/12 , B64C1/1492 , Y02T50/43 , Y10T156/1026 , Y10T156/1028 , Y10T156/1052 , Y10T156/1057 , Y10T156/1062 , Y10T156/1082 , Y10T428/24124 , Y10T428/24628
摘要： Fiber reinforced composite structures having curved stepped surfaces are fabricated by laying up plies (38) of fiber reinforced material over a tool having a stepped tool feature. The plies (38) are rotated about a fixed axis as they are laid up to substantially form a fixed axis rosette pattern. The plies are angularly oriented such that at least certain of the plies have fiber orientations (52) other than 0, +45, -45 and 90 degrees. Potential bridging of the fibers over the stepped tool features is reduced or eliminated by cutting slits (42) in the plies in the area of the stepped features, so that the plies can be fully compacted.
摘要翻译：纤维增强具有弯曲台阶面复合结构通过在具有阶梯状工具特征的工具上铺设的纤维增强材料的层片（38）被制造。帘布层（38）是绕作为它们铺设以形成一个固定的轴线基本莲座图案的固定轴。的帘布层是成角度地定向搜索做至少某些所述层具有纤维取向大于0，45，-45度和90度（52）其他。纤维越过阶梯工具特征的潜在桥接减小或通过在的台阶特征的区域中的帘布层切割狭缝（42）除去，所以没有片层可以是完全压实。

95. 发明公开

EP1991803A2 AIRCRAFT WINDOW ASSEMBLY 有权
标题翻译：机窗安排
公开(公告)号：EP1991803A2
公开(公告)日：2008-11-19
申请号：EP07861241.3
申请日：2007-02-16
申请人： The Boeing Company
发明人： COAK, Craig E.
IPC分类号： F16K5/04 , F16K11/085 , F16K11/076 , A61M39/22
CPC分类号： B64C1/1492
摘要： A window assembly is provided to prevent the migration of the window seal. The window assembly includes an outer window pane, an inner window pane and a seal. The outer window pane having a geometric feature configured to become parallel relative to another structure while the outer window pane rotates from a first position to a second position. The window assembly may further include a stiffening ring and a clamping ring which act to further secure the window seal in the desired position.

96. 发明公开

EP1971797A1 DISPOSITIF DE GUIDAGE D ' UN CABLE D ' UN GLACE OUVRANTE 有权转让
标题翻译：装置，保护并保持CABLE飞机机舱的开闭窗
公开(公告)号：EP1971797A1
公开(公告)日：2008-09-24
申请号：EP07717799.6
申请日：2007-01-08
申请人： Airbus France SAS
发明人： BIANCALANA, Olivier
IPC分类号： F16L3/015 , B64C1/14
CPC分类号： B64C1/1492 , F16L3/015 , Y10T74/20462
摘要： The subject of the invention is a device for protecting and guiding at least one cable (22) connecting an openable window (10) for closing an opening of an aircraft cabin to its mounting (14), and is characterized in that it comprises a cable-supporting chain (26) which is deformable within a winding plane and is able to protect and guide said cable (22), and on either side of the cable-supporting chain (26) a first mounting (28) hinged to the openable window (10) in such a way as to be able to pivot about a hinge axis (36) extending approximately parallel to the translational movement of disengagement and a second mounting (30) hinged to the mounting (14) in such a way as to be able to pivot about a hinge axis (38) extending approximately parallel to the translation movement of disengagement, and in that the first and second mountings (28, 30) have an L-shaped cross section.

97. 发明公开

EP1663776A2 A RESIN INFUSED TRANSPARENT SKIN PANEL AND METHOD OF MAKING SAME 有权
标题翻译：根据上述制造树脂浸渍透明BEPLANKUNGSPLATTE和过程
公开(公告)号：EP1663776A2
公开(公告)日：2006-06-07
申请号：EP04817754.7
申请日：2004-09-02
申请人： The Boeing Company
发明人： ALBERS, Robert, G. , NORDMAN, Paul, S.
IPC分类号： B64C1/12
CPC分类号： B32B15/14 , B29C43/18 , B29C43/203 , B29C70/088 , B29C70/345 , B29C70/885 , B29K2105/0854 , B29K2705/00 , B29L2031/3076 , B29L2031/3082 , B29L2031/778 , B32B3/266 , B32B5/28 , B32B15/20 , B32B2260/021 , B32B2305/38 , B32B2307/412 , B32B2311/18 , B32B2605/18 , B32B2607/00 , B64C1/12 , B64C1/1492 , Y02T50/43 , Y10T428/24331 , Y10T428/24339 , Y10T428/24347 , Y10T428/24364 , Y10T428/24777
摘要： An aircraft that has a structural skin panel. The structural skin panel has: at least one metal sheet having a cutout portion and a perimeter portion, the perimeter portion having a plurality of spaced apart perforations formed therein; and first and second fiber reinforced performs that are generally transparent and that sandwich the at least one metal sheet therebetween and overlay the perimeter portion. An optically transparent resin saturates the first and second fiber reinforced performs and fills the perforations in the at least one metal sheet. Portions of the fiber reinforced preforms that overlay the cutout form a window portion in the structural skin panel.

98. 发明公开

EP1647481A2 Fensterelement eines Luftfahrzeuges 有权
公开(公告)号：EP1647481A2
公开(公告)日：2006-04-19
申请号：EP05022503.6
申请日：2005-10-14
申请人： Airbus Deutschland GmbH
发明人： Paspirgilis, Bernd
IPC分类号： B64C1/14
CPC分类号： B64C1/1492
摘要： Die Erfindung betrifft ein Fensterelement 1 zum Einsetzen in einen Fensterausschnitt 7 in einer Außenhaut 5 eines Verkehrsmittels, insbesondere eines Luftfahrzeuges.
Erfindungsgemäß weist das Fensterelement 1 eine Abdeckscheibe 10 auf, die im Wesentlichen bündig mit der Außenhaut 5 abschließt, um eine strömungstechnisch günstige, weitgehend ebene Gestaltung der Außenhaut zu 5 erreichen.
Infolge des Vorhandenseins einer zusätzlichen, der eigentlichen Außenscheibe 26 des Fensterelementes 1 vorgeordneten und hinterlüfteten Abdeckscheibe 10 wird eine strömungsgünstige Integration des Fensterelementes 1 in die Außenhaut 5 einer Rumpfzelle eines Luftfahrzeuges erreicht.
Eine Deformation, insbesondere eine Ausbeulung der Außenscheibe 26 des Fensterelementes 1 aufgrund einer Druckdifferenz zwischen dem Innenraum der Rumpfzelle des Luftfahrzeuges und des Außenraumes in großen Flughöhen, hat infolge der Abdeckung der Außenscheibe 26 durch die vorgeordnete Abdeckscheibe 10, die sich im Wesentlichen bündig in die Außenhaut 5 der Rumpfzelle des Luftfahrzeuges einfügt, keine strömungstechnisch nachteilige Wirkung. Eine Deformation der Abdeckscheibe 10 wird durch die Hinterlüftung weitgehend ausgeschlossen.
Darüber hinaus lassen sich die Komponenten zur Bildung des erfindungsgemäßen Fensterelementes 1 fertigungstechnisch leicht herstellen und montieren.
摘要翻译：用于插入，特别是在飞行器的外皮中的窗口（7）中的窗元件（1）包括与外皮齐平定位的盖板（10）。

99. 发明公开

EP1642825A1 Injection-molded window panel and related methods 失效
标题翻译：注塑窗板及相关方法
公开(公告)号：EP1642825A1
公开(公告)日：2006-04-05
申请号：EP05077258.1
申请日：2005-10-04
申请人： The Boeing Company
发明人： Wood, Jeffrey H. , Sewell, Terry A.
IPC分类号： B64C1/14
CPC分类号： B64C1/1492
摘要： A window panel (20) adapted for installation relative to a structure (12). The panel includes a single piece of generally transparent injection-molded material (28) configured to span one or more openings (32) in the structure. The panel (20) has panel attachment inserts (44) for attaching the panel relative to the structure. The inserts are embedded in the material alongside at least one edge of the panel. The panel has a curvature that essentially continues a curvature of the structure surrounding the opening(s) when the panel is installed relative to the structure. This panel can be single-pane and can provide an essentially continuous window along an aircraft fuselage.
摘要翻译：适于相对于结构（12）安装的窗板（20）。面板包括构造成跨越结构中的一个或多个开口（32）的单件大体上透明的注塑材料（28）。面板（20）具有用于相对于结构附接面板的面板附接插入件（44）。插入物沿着面板的至少一个边缘嵌入在材料中。当面板相对于结构安装时，面板具有基本上延续围绕开口的结构的曲率的曲率。该面板可以是单面板，并且可以沿着飞机机身提供基本上连续的窗口。

100. 发明公开

EP1614623A1 Porte pour aéronef, et aéronef muni d'au moins une telle porte 有权转让
标题翻译：飞机门和配备至少一个这样的门的飞机
公开(公告)号：EP1614623A1
公开(公告)日：2006-01-11
申请号：EP05300537.7
申请日：2005-06-30
申请人： AIRBUS France
发明人： Baderspach, Jérôme , Rondot, Sébastien
IPC分类号： B64C1/14
CPC分类号： B64C1/1492 , E05D3/12 , E05Y2900/502
摘要： L'invention a pour objet une porte (1) pour aéronef, apte à obturer une ouverture pratiquée sur l'aéronef. Un encadrement (2) de la porte est relié au fuselage par des moyens d'articulation (3). L'encadrement est monté en rotation (11, 12) sur les moyens d'articulation. La porte est apte à prendre deux positions stables opposées, par rotation de 180° autour des moyens d'articulation. La porte comporte des moyens de verrouillage de l'encadrement, dans l'une ou l'autre des positions stables. Une première face de l'encadrement est munie d'un dôme d'observation, une deuxième face comportant un orifice d'accès au dôme.
摘要翻译：用于飞行器的门（1）技术领域本发明涉及一种用于飞行器的门（1），其能够关闭飞机上形成的开口门的框架（2）通过铰链装置（3）连接到机身。框架可旋转地安装在铰链装置上（11,12）。通过围绕铰链装置旋转180°，门适于采取两个相反的稳定位置。门包括用于将框架锁定在一个或另一个稳定位置的装置。框架的第一面设置有观察圆顶，具有圆顶入口的第二面。

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