TRAINING METHOD AND SYSTEM COMPRISING MIXED REAL AND VIRTUAL IMAGES
    11.
    发明公开
    TRAINING METHOD AND SYSTEM COMPRISING MIXED REAL AND VIRTUAL IMAGES 审中-公开
    ÜBUNGSVERFAHRENUND MIT ECHTEN UND VIRTUELLEN BILDERN

    公开(公告)号:EP2460108A1

    公开(公告)日:2012-06-06

    申请号:EP10739351.4

    申请日:2010-07-29

    IPC分类号: G06F19/00 G09B9/042

    CPC分类号: G09B9/042 G09B9/05

    摘要: Training method for the simulation of an operation performed by at least one device which is part of a real apparatus, wherein the method comprises providing to display means (212) overlaid images under controlled depth order of a virtual apparatus, and real images of said device, and providing a simulated response to control means (210), based on data of the position and behavior of said device (205) and on data of the position and behavior of said virtual apparatus (209).

    摘要翻译: 用于模拟由作为实际装置的一部分的至少一个装置执行的操作的训练方法,其中所述方法包括向显示装置(212)提供覆盖在虚拟装置的受控深度顺序下的图像,以及所述装置的真实图像 ,并且基于所述设备(205)的位置和行为的数据以及所述虚拟设备(209)的位置和行为的数据,向控制装置(210)提供模拟响应,

    Method and system for the simulation of the human factor in assembly processes
    12.
    发明公开
    Method and system for the simulation of the human factor in assembly processes 审中-公开
    魔兽世界和系统zur模拟des menschlichen在einem Montageverfahren的faktors

    公开(公告)号:EP2444876A1

    公开(公告)日:2012-04-25

    申请号:EP10382258.1

    申请日:2010-09-29

    IPC分类号: G06F3/03 G06F17/50 G09B23/00

    CPC分类号: G06F3/03

    摘要: System (1) for positioning a virtual dummy (3) according to the positioning of segments (20) of a physical dummy (2) manipulated by a user of the system (1), such that the positioning of these segments (20) is effected by markers (21) in the physical dummy (2) defining the segments (20), the markers (21) providing the coordinates corresponding with the degrees of freedom of such segments (20), the degrees of freedom of the segments (20) in the physical dummy (2) directly mapping the positioning in the virtual dummy (3), by generating the degrees of freedom of the physical dummy (2) and transferring them directly to the virtual dummy (3). The invention also refers to a method for positioning a virtual dummy (3) according to the positioning of segments (20) of a physical dummy (2).

    摘要翻译: 根据由系统(1)的用户操纵的物理虚拟机(2)的段(20)的定位来定位虚拟虚拟机(3)的系统(1),使得这些段(20)的定位是 由限定段(20)的物理虚拟(2)中的标记(21)进行,标记(21)提供与这些段(20)的自由度相对应的坐标,段(20)的自由度 )在物理虚拟(2)中直接映射虚拟虚拟(3)中的定位,通过产生物理虚拟(2)的自由度并将它们直接传输到虚拟虚拟(3)。 本发明还涉及一种用于根据物理虚拟(2)的段(20)的定位来定位虚拟虚拟(3)的方法。

    Wing-mounted refueling pod in a tanker aircraft
    13.
    发明公开
    Wing-mounted refueling pod in a tanker aircraft 审中-公开
    在einem Tankflugzeug的Auf derTragflächemontierter Betankungspod

    公开(公告)号:EP2423109A1

    公开(公告)日:2012-02-29

    申请号:EP11382219.1

    申请日:2011-06-29

    发明人: Hrncir, Zbynek

    IPC分类号: B64D39/00 B64D39/02

    CPC分类号: B64D39/00 B64D39/02

    摘要: A refueling pod (17) for a tanker aircraft (13) used for refueling a receptor aircraft (11) in flight by means of a hose and drogue device (15) comprising a streamlined-shaped first section (33) that houses the main handling equipment of the hose and drogue device (15) and a second section (35) housing the opening (37) for the deployment/retraction of the hose and drogue device (15), in which said second section (35) has an streamlined shape and houses an opening (37) which has a symmetrical shape with respect to an hypothetical X-Z plane by the longitudinal axis (31) of the refueling pod (17) and is placed below an hypothetical X-Y plane by said longitudinal axis (31) for reducing the turbulence behind the refueling pod (17) and improving therefore the stability of the hose and drogue device (15).

    摘要翻译: 用于通过软管和锥形装置(15)在飞行中为飞行中的受理飞机(11)加油的加油机(13)的加油舱(17),包括流线型的第一部分(33),其容纳主要处理 软管和锥形装置(15)的设备和容纳用于软管和脱水装置(15)的展开/缩回的开口(37)的第二部分(35),其中所述第二部分(35)具有流线型 并且通过所述加油荚(17)的纵向轴线(31)容纳相对于假想XZ平面具有对称形状的开口(37),并且通过所述纵向轴线(31)放置在假设XY平面的下方以减少 加油舱(17)后面的湍流,从而改善了软管和锥套装置(15)的稳定性。

    Coiled device
    14.
    发明公开
    Coiled device 审中-公开
    Spiralvorrichtung

    公开(公告)号:EP2339201A1

    公开(公告)日:2011-06-29

    申请号:EP09382295.5

    申请日:2009-12-22

    IPC分类号: F16F1/12 F16F3/02

    摘要: The present invention relates to a coiled device allowing the connection between two points separated by a variable distance. The use of one or more guides improving the mechanical elongation conditions of the coiled device characterizes the invention. The main application of the invention is in electric conductor cables, tubular conduits and others which use a coiled configuration to allow establishing the connection between two points the separation of which is variable.

    摘要翻译: 线圈装置技术领域本发明涉及一种允许以可变距离分开的两点之间的连接的线圈装置。 使用一个或多个引导件改善卷绕装置的机械伸长条件的特征在于本发明。 本发明的主要应用是在电导体电缆,管状导管等中,其使用线圈结构以允许建立两个点之间的连接,其间的分离是可变的。

    DEVICE FOR AN AIRCRAFT PROPULSION UNIT
    15.
    发明公开
    DEVICE FOR AN AIRCRAFT PROPULSION UNIT 有权
    VORRICHTUNGFÜREIN FLUGZEUGTRIEBWERK

    公开(公告)号:EP2314509A2

    公开(公告)日:2011-04-27

    申请号:EP09784126.6

    申请日:2009-07-09

    IPC分类号: B64D29/06

    CPC分类号: B64D29/06

    摘要: Device (3) for providing a warning signal when the fan cowl doors (8, 9) of an aircraft are not properly latched by primary locking means (6), said device (3) comprising a panel (4) the panel (4) being fixed by rotating means (5) on one of the two fan cowl doors (8 or 9), the panel (4) being closed on that one fan cowl doors (8 or 9) by rotating on said rotating means (5) therefore covering at least partially the primary locking means (6), such that all the primary locking means (6) have to be properly latched for the panel (4) to be closed, and at least one of the panel (4) primary locking means (6) not properly latched prevents proper closing of the panel (4).

    摘要翻译: 一种用于当飞行器的风扇整流罩门(8,9)没有被主锁定装置(6)正确锁定时提供警告信号的装置(3),所述装置(3)包括面板(4),面板(4) 通过在两个风扇整流罩门(8或9)中的一个上的旋转装置(5)固定,因此通过在所述旋转装置(5)上转动,面板(4)在该一个风扇整流罩门(8或9)上关闭,因此 至少部分地覆盖主锁定装置(6),使得所有主锁定装置(6)必须被适当地锁定以使面板(4)关闭,并且面板(4)中的至少一个主锁定装置 (6)未正确锁定可防止面板(4)正确关闭。

    DEVICE FOR REMOVING AND INSTALLING AIRCRAFT COMPONENTS
    16.
    发明公开
    DEVICE FOR REMOVING AND INSTALLING AIRCRAFT COMPONENTS 有权
    设备拆卸和安装飞机零部件

    公开(公告)号:EP2287074A2

    公开(公告)日:2011-02-23

    申请号:EP09742181.2

    申请日:2009-04-24

    IPC分类号: B64F5/00

    CPC分类号: B64F5/50

    摘要: The invention relates to a modular device for removing and installing aircraft power plant components comprising a modular frame (41) as main system of the device, common for every component which is to be installed or removed, this modular frame (41) being assembled in attaching points (2,3) of the pylon lugs of the airframe, and this frame (41) comprising: a forward frame (7), at least two lateral frames (8) and a rear structure (9, 10). The invention also relates to a method for installing such a device for removing and installing aircraft power plant components, and to a method for operating said device.

    Refueling boom with a fail-safe roll-pitch device
    18.
    发明公开
    Refueling boom with a fail-safe roll-pitch device 有权
    Luftbetankungssonde mit ausfallsicherem Roll- und Nickscharnier

    公开(公告)号:EP1916186A1

    公开(公告)日:2008-04-30

    申请号:EP06381041.0

    申请日:2006-10-24

    IPC分类号: B64D39/00

    CPC分类号: B64D39/00 B64D39/04

    摘要: A refueling apparatus for interconnecting a tanker aircraft (11) with a receiver aircraft in flight comprising a boom (21) joined to said tanker aircraft (11) by means of a mechanical articulation (41) comprising a first device (43) including a pivot axis (45), a second device (47) including a roll axis (49) and a third device (51) including a pitch axis (53), having at least one of said devices (43, 47, 51) fail-safe means (37, 37') providing a duplication of the load paths (39, 39') along the device, and also comprising a rigid fuel tight coupling (35) connecting the boom fuel line (31) to the tanker aircraft fiuef line (33).

    摘要翻译: 一种用于将油罐飞机(11)与飞行器中的接收器飞机相互连接的加油装置,包括通过机械铰接(41)连接到所述油罐飞行器(11)的悬臂(21),所述机械铰接件包括第一装置(43) 轴(45),包括辊轴(49)的第二装置(47)和包括俯仰轴(53)的第三装置(51),其具有至少一个所述装置(43,47,51)故障安全 装置(37,37'),沿着装置提供负载路径(39,39')的重复,并且还包括将起重臂燃油管线(31)连接到油罐飞机射流管线(28)的刚性燃料密封联接器(35) 33)。

    Lightning protected aircraft telescopic refueling mast
    19.
    发明公开
    Lightning protected aircraft telescopic refueling mast 有权
    Gegen Blitzeinschlaggeschützterteleskopischer BetankungsmastfürFlugzeuge

    公开(公告)号:EP1832513A1

    公开(公告)日:2007-09-12

    申请号:EP06381009.7

    申请日:2006-03-06

    IPC分类号: B64D45/02 B64D39/00

    CPC分类号: B64D39/04 B64D45/02

    摘要: An aircraft telescopic in-flight refueling mast comprising a metallic structural beam (31), electrically connected to the aircraft by flexible conductive means (33), having inside a fixed metallic tube (11) and a metallic telescopic tube (11) providing the fuel conduit, and, attached to said beam (31), flight control surfaces (41) and protection means against electric discharges, specially lightning strikes and electro-static discharges, including insulated means (39, 51) and low conductive means (15, 17) for reducing the lightning currents at a safe level and for draining the static charge created during the refueling, and conductive means (19, 21, 23, 33, 43) providing a safe lightning current path and good electrical bonding for electro-static discharge.

    摘要翻译: 一种飞机伸缩式飞行中加油桅杆,包括金属结构梁(31),其通过柔性导电装置(33)与飞行器电连接,具有固定的金属管(11)和金属伸缩管(11)内部,该伸缩管提供燃料 导管,并且附接到所述梁(31),飞行控制表面(41)和保护装置,以防止放电,特别是雷击和静电放电,包括绝缘装置(39,51)和低导电装置(15,17) ),用于将雷电电流降低到安全水平并且用于排放在加油期间产生的静电荷;以及导电装置(19,21,23,33,43),其提供安全的雷电流路径和用于静电放电的良好电粘合 。

    Assembly for testing panels under shear-compression loads
    20.
    发明公开
    Assembly for testing panels under shear-compression loads 有权
    Anordnung zum Testen von Platten unter Scherdruckbelastung

    公开(公告)号:EP1826550A1

    公开(公告)日:2007-08-29

    申请号:EP06110272.9

    申请日:2006-02-22

    IPC分类号: G01N3/00 G01N19/00

    摘要: Assembly for testing a panel (11) made of composite material under different combinations of shear-compression loads using an universal tension load machine (16), comprising metallic sheets (12) configured to form, together with the panel (11), a frame of rectangular shape in the same plane than the panel (11), being said metallic sheets (12) able to transmit external loads to the panel (11), two loading parts (19), having translatable lugs (20) to be connected with the universal tension load machine (16), joined at two opposed sides of said frame and a structure (18) to prevent displacements out of the panel (11).

    摘要翻译: 用于使用通用张力负载机器(16)测试由不同组合的剪切压缩载荷的复合材料制成的面板(11)的组件,包括被配置为与所述面板(11)一起形成的框架 在与平板(11)相同的平面上具有矩形形状,所述金属片(12)能够将外部载荷传递到面板(11),两个装载部分(19)具有可平移的凸耳(20) 在所述框架的两个相对侧连接的万向张力装载机(16)和用于防止从所述面板(11)移出的结构(18)。