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1. 发明申请

WO2014186438A3 WINDOW OF AN AIRCRAFT 审中-公开
标题翻译：飞机窗口
公开(公告)号：WO2014186438A3
公开(公告)日：2015-11-26
申请号：PCT/US2014037958
申请日：2014-05-14
申请人： HONDA PATENTS & TECH NORTH AM , FUJINO MICHIMASA , HOMMA YASUHIRO
发明人： FUJINO MICHIMASA , HOMMA YASUHIRO
IPC分类号： B64C1/14 , E06B5/12 , E06B9/24
CPC分类号： B64C1/1484 , B64C1/1492 , B64D11/02
摘要： An aircraft includes a fuselage including a plurality of frame members disposed at predetermined intervals in a longitudinal direction of the fuselage and a plurality of stringers extending substantially linearly in the longitudinal direction. The fuselage defines an aircraft interior. A compartment is located in the interior of the fuselage. The compartment defines an interior area. A first one window assembly is mounted to an upper portion of the fuselage for introducing daylight into the interior area. The first window assembly is flanked by adjacent frame members of the plurality of frame members and adjacent stringers of the plurality of stringers. The first window assembly includes a window pane, an inner cover and a retainer. The inner cover introduces daylight from the window pane into the interior area. The retainer secures the window pane and the inner cover to the fuselage.
摘要翻译：飞机包括机身，其包括沿着机身的纵向方向以预定间隔设置的多个框架构件和沿纵向大致直线延伸的多个桁条。机身定义了飞机内饰。机舱位于机身内部。隔间定义一个内部区域。第一个窗户组件安装到机身的上部，以将日光引入内部区域。第一窗组件的侧面是多个框架构件的相邻框架构件和多个桁条的相邻桁条。第一窗组件包括窗玻璃，内盖和保持架。内盖将日光从窗玻璃引入内部区域。保持架将窗玻璃和内盖固定在机身上。

2. 发明申请

WO2015116439A1 AIRCRAFT TRANSPARENCY WITH PRESSURE SEAL AND/OR ANTI-STATIC DRAIN 审中-公开
标题翻译：具有压力密封和/或防静电排放的飞机透明度
公开(公告)号：WO2015116439A1
公开(公告)日：2015-08-06
申请号：PCT/US2015/012132
申请日：2015-01-21
申请人： PPG INDUSTRIES OHIO, INC.
发明人： HARRISON, Spencer B. , HARTMANN, James V.
IPC分类号： B64C1/14
CPC分类号： B64C1/1492 , B64C1/1484 , B64D45/02 , F16J15/064
摘要： An aircraft transparency assembly includes an aircraft transparency having at least one ply having an outer surface and an extended portion. The assembly also includes a pressure seal configured to engage the extended portion of the ply, wherein the pressure seal includes a pressure seal body and at least one integrated compression stop. The transparency can include an optional anti-static drain assembly including at least one flexible conductive element having a first end in electrical contact with the outer surface of the ply, for example with an optional conductive coating on the outer surface of the ply, and a second end configured to contact the pressure seal.
摘要翻译：飞机透明度组件包括具有至少一个具有外表面和延伸部分的层的航空器透明体。组件还包括构造成接合帘布层的延伸部分的压力密封件，其中压力密封件包括压力密封体和至少一个集成的压缩止挡件。透明度可以包括可选的防静电排放组件，其包括至少一个柔性导电元件，其具有与层的外表面电接触的第一端，例如在层的外表面上具有任选的导电涂层，以及第二端构造成接触压力密封。

3. 发明申请

WO2014183614A1 具防爆缓冲功能的武装直升机透明件紧固结构及紧固方法审中-公开
公开(公告)号：WO2014183614A1
公开(公告)日：2014-11-20
申请号：PCT/CN2014/077243
申请日：2014-05-12
申请人：一禾科技发展(上海)有限公司
发明人：谢晓斌 , 李震 , 谢隽永
IPC分类号： E06B3/58
CPC分类号： B64C1/1492 , B64C27/04 , B64D7/00
摘要：一种具防爆缓冲功能的武装直升机透明件紧固结构及紧固方法，包括安装框体（1）和通过安装框体（1）固定于直升机主体（5）上的座舱透明件（2），安装框体（1）形成有第一安装槽（10），座舱透明件（2）的侧边插设于第一安装槽（10）内，座舱透明件（2）侧边结合有一圈框体（3），框体（3）与第一安装槽（10）之间形成有相互配合的安装结构，框体（3）包括压迫组件（31）和紧固组件（32），通过压迫组件（31）和座舱透明件（2）的配合压迫紧固组件（32）生成预应力进而紧固座舱透明件（2）。该紧固结构强度高，适应面广。

4. 发明申请

WO2012148719A3 OPTICAL DOME BEZEL 审中-公开
标题翻译：光学眼镜
公开(公告)号：WO2012148719A3
公开(公告)日：2014-05-08
申请号：PCT/US2012033756
申请日：2012-04-16
申请人： BAE SYS INF & ELECT SYS INTEG , SINDLEDECKER GLENN , ESPOSITO GERARD A , SHE SIXING
发明人： SINDLEDECKER GLENN , ESPOSITO GERARD A , SHE SIXING
IPC分类号： F21V29/00
CPC分类号： B64C1/1492 , G08B13/19619
摘要： Techniques and architecture are disclosed for implementing an optical dome bezel to interface an optical dome/window and a housing of differing coefficients of thermal expansion (CTEs). In some embodiments, the bezel may comprise a material (e.g., Ti-6A1- 4V) that is CTE-matched to the optical dome material (e.g., silicon, germanium, sapphire, ALON), thereby mitigating temperature effects on system performance. In some embodiments, the bezel may include a radially compliant flexure feature (e.g., flexure blades, spring-form S-channels), which mitigates physical stress effects (e.g., vibration, thermal expansion/contraction, etc.) on system performance. In some embodiments, the bezel may include an integral environmental sealing feature (e.g., O-ring gaskets), which protects internal optics/electronics from external environmental hazards (e.g., moisture, corrosive substances, particulates, debris). In some embodiments, the bezel may be efficiently and repeatedly removed/replaced while preserving optical system performance. Numerous configurations and variations will be apparent in light of this disclosure.
摘要翻译：公开了用于实现光学圆顶挡板以连接光学圆顶罩/窗口和不同热膨胀系数（CTE）的外壳的技术和架构。在一些实施例中，边框可以包括与光学圆顶材料（例如硅，锗，蓝宝石，ALON）CTE匹配的材料（例如，Ti-6A1-4V），从而减轻温度对系统性能的影响。在一些实施例中，边框可以包括径向顺应的弯曲特征（例如，弯曲叶片，弹簧形S通道），其减轻对系统性能的物理应力影响（例如振动，热膨胀/收缩等）。在一些实施例中，边框可以包括整体环境密封特征（例如，O形环垫片），其保护内部光学/电子器件免受外部环境危害（例如，水分，腐蚀性物质，颗粒，碎片）的影响。在一些实施例中，可以有效地和重复地去除/替换边框，同时保持光学系统的性能。鉴于本公开，许多构造和变化将是显而易见的。

5. 发明申请

WO2014022188A2 AEROSPACE INTELLIGENT WINDOW SYSTEM 审中-公开
标题翻译：航空智能WINDOW系统
公开(公告)号：WO2014022188A2
公开(公告)日：2014-02-06
申请号：PCT/US2013052002
申请日：2013-07-25
申请人： PPG IND OHIO INC
发明人： JIAO YU , DUARTE NICOLAS , STONE MONROE A
CPC分类号： B64C1/1484 , B64C1/1476 , B64C1/1492 , B64D2045/0085
摘要： A network system for monitoring and storing data of aircraft intelligent windows or windshields to provide useable life of, provide real life performance of, and/or measure characteristics and/or properties of, the windshields forwards the data from sensors mounting the windshield to a window sensing hub having a microprocessor programed to receive and process the data to determine the performance of the windshield and formatting the data in accordance to a preset program, wherein the program includes providing data from the sensors that measures characteristics and properties of the windshield that are active during the period in which the data is taken. An aircraft central maintenance system connected to the window sensing hub receives the formatted information from the window sensing hub and unfiltered or unformatted information, wherein the unfiltered information from the windshield is acted on by the central maintenance system to provide an estimated useable life of the windshield.
摘要翻译：一种网络系统，用于监控和存储飞行器智能窗或挡风玻璃的数据，以提供挡风玻璃的可用寿命，提供现实生活性能和/或测量特性和/或性能，将数据从安装挡风玻璃的传感器转发到窗口感测集线器具有被编程为接收和处理数据以确定挡风玻璃的性能并根据预设程序格式化数据的微处理器，其中该程序包括提供来自传感器的数据，该传感器测量活动的挡风玻璃的特性和性质在数据采集期间。连接到窗口感测集线器的飞行器中央维护系统接收来自窗口感测集线器的格式化信息和未过滤或未格式化的信息，其中来自挡风玻璃的未过滤信息由中央维护系统作用以提供挡风玻璃的估计使用寿命。

6. 发明申请

WO2012097176A1 SYSTEMS AND METHODS FOR INSTALLING MOTORIZED WINDOW SHADE MECHANISM IN AIRCRAFT 审中-公开
标题翻译：在飞机上安装摩托车窗帘机构的系统和方法
公开(公告)号：WO2012097176A1
公开(公告)日：2012-07-19
申请号：PCT/US2012/021115
申请日：2012-01-12
申请人： AEROSPACE TECHNOLOGIES GROUP, INC. , KNOWLES, Byron, R.
发明人： KNOWLES, Byron, R.
IPC分类号： B64C1/14
CPC分类号： B64C1/1484 , B64C1/1492
摘要： Systems and methods for installing a motorized window shade assembly on an aircraft window panel having fastener receiving elements and an electrical access port. A receptacle frame includes a front face bounded by side walls defining a volume for receiving the window shade assembly. The frame further includes a rear face having window panel fasteners adapted to engage with the fastener receiving elements of the aircraft window panel and adapted to secure the receptacle frame to the aircraft window panel. The frame further includes window shade assembly fasteners positioned on at least a first pair of the side walls and adapted to secure the window shade assembly within the volume for receiving the window shade assembly.
摘要翻译：用于在具有紧固件接收元件和电接入端口的飞机窗口面板上安装电动窗帘组件的系统和方法。插座框架包括由限定用于接收窗帘组件的容积的侧壁限定的正面。框架还包括具有适于与飞行器窗板的紧固件接收元件接合并适于将插座框架固定到飞行器窗板的窗板紧固件的后表面。该框架还包括定位在至少第一对侧壁上的窗帘组件紧固件，并适于将窗帘组件固定在用于容纳窗帘组件的容积内。

7. 发明申请

WO2012020078A1 NON-FOGGING VEHICLE WINDOW 审中-公开
标题翻译：非飞机车窗
公开(公告)号：WO2012020078A1
公开(公告)日：2012-02-16
申请号：PCT/EP2011/063826
申请日：2011-08-11
申请人： AIRBUS OPERATIONS GMBH , MÜLLER, Rainer , ELMERS, Jens
发明人： MÜLLER, Rainer , ELMERS, Jens
IPC分类号： B64C1/14
CPC分类号： B64C1/1484 , B60J1/002 , B64C1/1492
摘要： A vehicle window with a primary window pane arrangement (2, 4, 8, 10, 12), a secondary window pane (14) that is spaced apart from the primary window pane arrangement and a window funnel (16) that extends between the secondary window pane and the primary window pane arrangement comprises an intermediate space (24) that is formed by the window funnel, the secondary window pane and the primary window pane arrangement, wherein said intermediate space is sealed and equipped with an air inlet (6) for introducing dehumidified air into the intermediate space. Due to the seal, humid air leading to condensation and frost in the intermediate space is prevented from flowing into the intermediate space during a pressure compensation flow. The passenger comfort is enhanced due to the improved view through the window.
摘要翻译：具有主窗格布置（2,4,8,10,12）的车窗，与主窗格布置间隔开的次窗玻璃（14）和在第二窗玻璃之间延伸的窗口漏斗（16）窗格和主窗格布置包括由窗口漏斗，副窗玻璃和主窗玻璃布置形成的中间空间（24），其中所述中间空间被密封并配备有空气入口（6），用于向中间空间引入除湿空气。由于密封，在压力补偿流动期间防止在中间空间中导致冷凝和结霜的潮湿空气流入中间空间。乘客的舒适度得到改善，这是因为通过窗户的改进。

8. 发明申请

WO2009008903A1 AIRCRAFT WINDOW EROSION SHIELD 审中-公开
标题翻译：飞机防风罩
公开(公告)号：WO2009008903A1
公开(公告)日：2009-01-15
申请号：PCT/US2008/000307
申请日：2008-01-09
申请人： THE NORDAM GROUP, INC.
发明人： OSTREM, Scott, Ernest , JACKSON, Kevin, Steven , WALLACE, Stephen, Frederick, Joseph
IPC分类号： B64C1/14
CPC分类号： B64C1/1492 , B29C70/345 , B29C70/462 , B29L2031/005 , Y02T50/43
摘要： An erosion shield (54) for an aircraft window (12) includes an annular band (56) having a radially outer brim (58) and a radially inner clip (60). The shield (54) is sized to cover a composite window frame (18) having an outer rim (22) and an inner sash (24) around a central aperture (26) in which is mounted a window pane (20). The clip (60) is asymmetrical around the central aperture (26) to protect the sash (24) and permit assembly of the shield (54) thereto.
摘要翻译：用于飞机窗（12）的侵蚀屏蔽（54）包括具有径向外边缘（58）和径向内夹（60）的环形带（56）。护罩（54）的尺寸被设计成覆盖具有围绕中心孔（26）的外缘（22）和内窗（24）的复合窗框（18），其中安装有窗玻璃（20）。夹子（60）围绕中心孔（26）不对称以保护窗扇（24）并且允许屏蔽件（54）组装到其上。

9. 发明申请

WO2008073150A3 WINDOW ASSEMBLY AND METHOD FOR A MOBILE PLATFORM 审中-公开
标题翻译： WINDOW组装和移动平台的方法
公开(公告)号：WO2008073150A3
公开(公告)日：2008-10-23
申请号：PCT/US2007016045
申请日：2007-07-13
申请人： BOEING CO , DIXON ROBERT D , SWITZER LON E , SIEBERT FREDERICK P , LAVERNE SCOTT , ZIZZO MICHAEL J , NELSON GREGORY W , SHANKOV GENNADY V , TRIMBLE JAMES G
发明人： DIXON ROBERT D , SWITZER LON E , SIEBERT FREDERICK P , LAVERNE SCOTT , ZIZZO MICHAEL J , NELSON GREGORY W , SHANKOV GENNADY V , TRIMBLE JAMES G
IPC分类号： B64C1/14
CPC分类号： B64C1/1492
摘要： A window assembly (10) for a mobile platform, for example, a commercial aircraft. The window assembly includes a reveal member (14) that is retained within an opening (28) in an interior panel (24) of the mobile platform without the use of independent retaining clips or adhesives. In one embodiment the reveal member is generally rectangular in shape and includes a flange adjacent to each of the four corners thereof. The flanges engage the opening in the structural panel (24) so that the reveal member can be held in a precise position within the opening in the interior structural panel without external fastening clips or adhesives. The window assembly is lighter in weight than existing window assemblies, and can also be easily removed without special tools or disassembly procedures, and also is retrofittable to existing mobile platforms.
摘要翻译：一种用于移动平台的窗户组件（10），例如商用飞机。窗户组件包括露出构件（14），该露出构件（14）保持在移动平台的内部面板（24）内的开口（28）内，而不使用独立的固定夹或粘合剂。在一个实施例中，露出构件的形状大致为矩形，并且包括与其四个角中的每一个相邻的凸缘。凸缘与结构面板（24）中的开口接合，使得露出构件能够保持在内部结构面板内的开口内的精确位置，而无需外部紧固夹或粘合剂。窗户组件的重量比现有的窗户组件重，并且也可以在没有特殊工具或拆卸过程的情况下轻松拆卸，也可以改装到现有的移动平台。

10. 发明申请

WO2008097383A2 UNITARY ONE-PIECE WINDSHIELD 审中-公开
标题翻译：单位一体式WINDSHIELD
公开(公告)号：WO2008097383A2
公开(公告)日：2008-08-14
申请号：PCT/US2007/081288
申请日：2007-10-12
申请人： SPECTRUM AERONAUTICAL, LLC , BLUE, Linden, S. , COONEY, Daniel, E.
发明人： BLUE, Linden, S. , COONEY, Daniel, E.
IPC分类号： B64C1/14
CPC分类号： B64C1/1492
摘要： A windshield for a pressurized aircraft includes a single transparent unit that functions structurally to allow pressurization of the aircraft and to support the aircraft's fuselage in response to external loads. The windshield also functions operationally to provide the pilot with an unobstructed field of vision through an extended arc of more than two hundred degrees. For its manufacture, layers of the transparent unit are respectively bent along a straight center line to establish two curved portions that are symmetrical relative to a common plane. The layers are then laminated.
摘要翻译：用于加压飞机的挡风玻璃包括单个透明单元，其在结构上起作用以允许飞行器加压并且响应于外部载荷来支持飞行器的机身。挡风玻璃还通过延伸的弧度超过两百度，在飞行员的作用下为飞行员提供无障碍的视野。为了制造，透明单元的层分别沿直线中心线弯曲以形成相对于公共平面对称的两个弯曲部分。然后层压层。

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