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303 条记录 (耗时 0.032 秒)

    Heat control system for consolidation roller
    1.
    发明公开
    Heat control system for consolidation roller 审中-公开
    WärmeregelungssystemfürVerfestigungsrollen

    公开(公告)号：EP2730385A1

    公开(公告)日：2014-05-14

    申请号：EP12400046.4

    申请日：2012-11-09

    申请人： Eurocopter Deutschland GmbH

    发明人： Weimer, Christian ,  Dorn, Florian

    IPC分类号： B29C33/04 ,  B29C70/38 ,  B29C35/16 ,  B32B37/00

    CPC分类号： C08J5/04 ,  B29C35/16 ,  B29C70/388 ,  B29C2035/1616 ,  B29C2035/1625 ,  B29C2035/1633 ,  B29C2035/1658 ,  B32B37/0053 ,  B32B37/06 ,  C08J5/24

    摘要： The invention is related to a heat control system for an adaptive consolidation roller (8) for the production of consolidated layers (2) made of fiber reinforced polymers comprising the adaptive consolidation roller (8) for applying, on an application surface (3), a band (4) formed of at least one resin preimpregnated flat tape (5), and a heating system (6, 7) adapted to emit heat radiation directed towards the band (4). Said adaptive consolidation roller (8) is rotatable on a spindle (9) and comprises a surface made of an elastic deformable, flexible material. At least one additional roller (10) with thermal control means is provided and said at least one additional roller (10) is pressed from radial outside against the surface of the adaptive consolidation roller (8).

    摘要翻译： 本发明涉及一种用于生产由纤维增强聚合物制成的固化层（2）的自适应固结辊（8）的热控制系统，该固化层包括用于在施用表面（3）上施加的自适应固结辊（8） 由至少一个树脂预浸渍扁平带（5）形成的带（4）和适于发射朝向带（4）的热辐射的加热系统（6,7）。 所述自适应固定辊（8）可在心轴（9）上旋转并且包括由弹性可变形的柔性材料制成的表面。 提供至少一个具有热控制装置的附加辊（10），并且所述至少一个附加辊（10）从径向外侧压靠自适应固结辊（8）的表面。

    Monitoring device for lubricant quantities
    5.
    发明授权
    Monitoring device for lubricant quantities 有权
    润滑剂量监测装置

    公开(公告)号：EP2584323B1

    公开(公告)日：2013-12-04

    申请号：EP11400048.2

    申请日：2011-10-20

    申请人： Eurocopter Deutschland GmbH

    发明人： Lees, Thilo ,  Vogel, Dominik ,  Regenfelder, Florian ,  Schida, Silvio

    IPC分类号： G01F23/18 ,  B64D47/00

    CPC分类号： G01F23/18 ,  B64C27/006 ,  B64C27/32 ,  B64C27/82 ,  G01F23/14

    摘要： The invention relates to a monitoring device (1, 30) for lubricant quantities, particularly a monitoring device (1, 30) for lubricant quantities in a rotor head (2) of a helicopter (50) and more particularly a monitoring device (1, 30) for lubricant quantities in a rotor head (2) of a tail rotor (3) of a helicopter (50), comprising a casing (5) to preserve the lubricant quantities for monitoring, a shaft (6) mounted inside said casing to rotationally drive the casing (5), at least one bearing (11-14), said at least one bearing (11-14) being mounted from outside to the casing (5) and/or shaft (6) and said at least one bearing (11-14) being connected to the casing (5) for supply of lubricant, sensor means (19-22, 31-34) to detect the lubricant quantities inside said casing (5), and, interface means for communication of data from said sensor means (19-22, 31-34) to at least one display (54).

    Aerodynamic blade attachment for a bearingless rotor of a helicopter
    7.
    发明公开
    Aerodynamic blade attachment for a bearingless rotor of a helicopter 有权
    转盘式旋转机构AerodynamischeFlügelbefestigungfüreinen lagerlosen

    公开(公告)号：EP2653385A1

    公开(公告)日：2013-10-23

    申请号：EP12400014.2

    申请日：2012-04-18

    申请人： Eurocopter Deutschland GmbH

    发明人： Kuntze-Fechner, Gerald ,  Bauer, Markus ,  Ortner, Martin

    IPC分类号： B64C27/33 ,  B64C27/48 ,  B64C27/50

    CPC分类号： B64C27/33 ,  B64C27/48 ,  B64C27/50

    摘要： The invention relates to an aerodynamic blade attachment (1) for a bearingless rotor, particularly a main rotor, of a helicopter, comprising: an airfoil blade (2) having a tip end and a root end forming opposite ends thereof and having a pitch axis from said tip end to said root end; a flexbeam (3); a control cuff (4, 22) enclosing and extending along at least a predominant portion of said flexbeam (3) and a separable junction arrangement between said flexbeam (3), said control cuff (4) and said root end of said airfoil blade (2), wherein said junction arrangement is mechanical between said flexbeam (3), said control cuff (4) and said root end of said airfoil blade (2) with removable fasteners (5, 6) respectively removable connecting said root end of said airfoil blade (2) and said control cuff (4) with said flexbeam (3). Said junction arrangement comprises fairing means (10, 27, 28, 31, 32 and 39) encompassing the removable fasteners (5, 6) and said flexbeam (3).

    摘要翻译： 本发明涉及一种用于直升机的无轴承转子，特别是主转子的空气动力学叶片附件（1），其包括：翼型叶片（2），其具有形成其相对端的顶端和根端，并具有俯仰轴 从所述尖端到所述根端; 柔性梁（3）; 沿着所述柔性梁（3）的至少主要部分包围并延伸的控制箍（4,22）和所述柔性梁（3），所述控制箍（4）和所述翼型叶片的所述根端之间的可分离的连接装置 2），其中所述连接装置在所述柔性梁（3），所述控制箍（4）和所述翼型叶片（2）的所述根端之间是机械的，具有可移除的紧固件（5,6），其可拆卸地连接所述翼型件 叶片（2）和所述控制袖带（4）与所述挠性束（3）。 所述接合装置包括包围可拆卸紧固件（5,6）和所述柔性梁（3）的整流装置（10,27,28,31,32和39）。

    Emergency opening system for an aircraft cabin door
    10.
    发明公开
    Emergency opening system for an aircraft cabin door 有权
    NotfallöffnungssystemfüreineFlugzeugkabinentür

    公开(公告)号：EP2644495A1

    公开(公告)日：2013-10-02

    申请号：EP12400008.4

    申请日：2012-03-27

    申请人： Eurocopter Deutschland GmbH

    发明人： Kress, Denis ,  Pichlmaier, Claus ,  Kirchner, Marc ,  Wolf, Christian

    IPC分类号： B64C1/14

    CPC分类号： B64C1/1423 ,  B64C1/1407 ,  B64C1/143

    摘要： The invention is related to an emergency opening system (1) of an aircraft cabin door (3) mounted in an aircraft fuselage structure (4) by means of a hinge arm (2). An actuator (7), designed to assist the opening of the aircraft cabin door (3) against the force of gravity by means of a gas operated actuating rod (8) is mounted with its fix end (9) to said hinge arm (2) and said actuating rod (8) is connected to an actuator joint (10). A fork lever (24) is linked to said actuator joint (10). A bell crank (13) is respectively pivotable mounted to said hinge arm (2) and to said actuator joint (10) for the fork lever (24). At least one coupling lever (12) is pivotable joint to said fork lever (24) at at least one coupling joint (14). Said at least one coupling lever (12) is mounted in at least one hinge (18) of the hinge arm (2) by means of a respective bolt (26), said bolt (26) being drivingly connected to said aircraft cabin door (3) for rotation of said aircraft cabin door (3).

    摘要翻译： 本发明涉及通过铰链臂（2）安装在飞行器机身结构（4）中的飞机机舱门（3）的紧急开启系统（1）。 一个致动器（7），其设计成通过气动操作的致动杆（8）抵抗重力来协助飞机机舱门（3）的打开，其固定端（9）安装到所述铰链臂（2） ），并且所述致动杆（8）连接到致动器接头（10）。 叉杆（24）连接到所述致动器接头（10）。 钟形曲柄（13）分别可枢转地安装到所述铰链臂（2）和用于叉杆（24）的所述致动器接头（10）。 至少一个联接杆（12）在至少一个联接接头（14）处可转动地连接到所述叉杆（24）。 所述至少一个联接杆（12）通过相应的螺栓（26）安装在所述铰链臂（2）的至少一个铰链（18）中，所述螺栓（26）被驱动地连接到所述飞机机舱门 3）用于所述飞机机舱门（3）的旋转。