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公开(公告)号：EP2305442A1
公开(公告)日：2011-04-06
申请号：EP09400049.4
申请日：2009-09-30
发明人： Meyer-Noack, Sven , Radekopf, Jörg
CPC分类号： B29C43/12 , B29C43/027 , B29C70/443 , B29C70/446 , B29C70/546 , B29C2043/028 , B29L2023/00
摘要： The present invention relates to a device for molding by impregnation of at least one reinforcing layer constituting a piece to be molded or at least one reinforcing layer covering a piece, with a resin (10) in liquid form, said device comprising a mold extending around the reinforcing layer by defining a resin (10) circulation space (5), an end piece (11) for supplying resin (10) in the circulation space (5), an end pieoe for evacuating (12) the surplus resin (10) as well as means for generating a flow of resin in the circulation space (5).
According to the invention, the mold comprises a flexible conduit (80) and means for mechanically deforming said flexible conduit to shape the circulation space (5) according to the impregnation parameters.摘要翻译： 本发明涉及一种通过用液体形式的树脂（10）浸渍至少一个构成待模制件的增强层或至少一个覆盖件的增强层来模制的装置，所述装置包括模具 通过限定树脂（10）循环空间（5）的加强层，用于在循环空间（5）中供应树脂（10）的端部件（11），用于抽空（12）多余树脂（10） 以及用于在循环空间（5）中产生树脂流的装置。 根据本发明，模具包括柔性导管（80）和用于根据浸渍参数机械地使所述柔性导管变形以形成循环空间（5）的装置。
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32.发明公开Filtering device with integrated bypass for an air inlet 有权Filtervorrichtung mit integrierter Nebenleitungfüreinen Lufteinlass
公开(公告)号：EP2282031A1
公开(公告)日：2011-02-09
申请号：EP09400033.8
申请日：2009-07-02
发明人： Krahl, Kornelius
CPC分类号： F02C7/055 , B01D46/0035 , B01D46/0087 , B01D46/2411 , B01D46/46 , B01D2273/14 , B01D2279/60 , B64C27/04 , B64D33/02 , B64D2033/0246 , F02C7/057 , F05D2220/329
摘要： A filtering device for an engine or a for power unit with a radial air intake (2), comprising a ring-shaped filter (3) for covering the radial air intake, characterised in that the ring-shaped filter comprises a first fixed part (3a) and a second mobile part (3b) which is movable with respect of the first fixed part through actuator means (6), from a filtering position in which the whole radial air intake is covered by the ring-shaped filter, to a bypass position in which the second mobile part uncovers at least partly the radial air intake.
摘要翻译： 一种用于发动机的过滤装置或具有径向进气口（2）的功率单元的过滤装置，包括用于覆盖径向进气口的环形过滤器（3），其特征在于，所述环形过滤器包括第一固定部件 3a和第二可移动部件3b，该第二移动部件3b从整个径向进气口被环状过滤器覆盖的过滤位置通过致动器装置相对于第一固定部件移动到旁路 第二移动部件至少部分地露出径向进气口的位置。
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公开(公告)号：EP2246832A1
公开(公告)日：2010-11-03
申请号：EP10400020.3
申请日：2010-03-29
发明人： Bohlender, Peter
摘要： The invention relates to a flight simulator vibration system, particularly to a crew seat (1), a flight control stick (20) and a panel (30) vibration system of a flight simulator with at least one plate of the crew seat (1), the flight control stick (20) and/or the panel (30) being equipped with predefined momentum weights (13, 16) and electric motors driving said respective momentum weights. Speed governors are controlling individually said electric motors (7, 8, 9, 21, 33, 34).
摘要翻译： 本发明涉及一种飞行模拟器振动系统，特别涉及具有机组座椅（1）的至少一个板的飞行模拟器的乘员座椅（1），飞行控制杆（20）和面板（30）振动系统， ，所述飞行控制杆（20）和/或所述面板（30）装备有预定的动量重量（13,16）和驱动所述各个动量重量的电动马达。 调速器分别控制所述电动机（7,8,9,21,33,34）。
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34.发明公开Method and mould tool for producing a component made of fibre-reinforced plastic 审中-公开一种用于生产纤维的部件的方法和模具增强塑料
公开(公告)号：EP2236271A1
公开(公告)日：2010-10-06
申请号：EP09400009.8
申请日：2009-03-30
发明人： Meyer-Noack, Sven , Radekopf, Jörg
CPC分类号： B29C33/308 , B29C70/48 , B29C70/548
摘要： The invention relates to a method for producing a component made of fibre-reinforced plastic by impregnating a fibre mould-blank (11) with a liquid impregnating material (10), comprising at least the following steps:
a) placing the fibre mould-blank (11) into a cavity (2) of a mould tool (1) while generating a temporary free space (9) between the fibre mould-blank (11) and at least one interior surface (19) of the mould tool (1);
b) feeding the impregnating material (10) into this free space (9);
c) closing the free space (9) by narrowing the mould tool (1) so that the impregnating material (10) is displaced from the free space (9) into the fibre mould-blank (11). It is further developed in that the mould tool (1) is gradually subjected to locally different forces (F1; F2; F3; ... Fn, Fa; Fb; Fc) which locally cause the free space (9) to be closed. Furthermore, the invention relates to a mould tool (1) that is designed analogously to this.摘要翻译： 本发明涉及一种用于通过用液体浸渍材料（10）浸渍纤维模具毛坯（11）包括至少以下步骤制造由纤维增强塑料制成的部件：a）将所述纤维模空白 （11）到模具工具的腔体（2）（1），而产生临时的自由空间（9）的纤维之间的模具坯料（11）和所述模具工具中的至少一个内表面（19）（1） ; b）将浸渍材料（10）到该自由空间（9）; C）通过缩小（1）象浸渍材料的模制工具闭合自由空间（9）（10）从所述自由空间（9）成纤维坯模（11）位移。 据进一步的发展，DASS模具模具（1）被逐渐受到局部不同的力（F1; F2; F3; ... Fn的发; Fb的; Fc）的局部地使自由空间（9）被关闭。 进一步，本发明涉及到一个模具（1）没有被设计类似于此。
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35.发明公开VERFAHREN ZUR HERSTELLUNG VON BAUELEMENTEN AUS FASERVERSTÄRKTEN KUNSTSTOFFEN 有权用于生产COMPONENTS纤维增强塑料
公开(公告)号：EP2150397A2
公开(公告)日：2010-02-10
申请号：EP08758130.2
申请日：2008-05-29
发明人： WEIMER, Christian
CPC分类号： B29C70/543 , B29C70/20 , B29C70/22 , B29C70/48 , B29C70/865 , B29L2031/082
摘要： The invention relates to a semifinished textile product composed of a lay of fibres for use as preform for the production of construction elements of fibre-reinforced plastic. According to the invention, the fibres are transferred by means of laying/confectioning/draping into a lay of fibers in the form of a band, characterized in that said lay of fibres is able to absorb the forces acting on the respective construction element that is to be produced, the fibres being provided with the required UD fibre fractions and/or melt fibres and being permanently fixed to the produced fibre architecture of the band by predefined seams.
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公开(公告)号：EP1966045A1
公开(公告)日：2008-09-10
申请号：EP06829420.6
申请日：2006-12-08
IPC分类号： B64C27/615 , B64C13/50
CPC分类号： B64C27/615 , B64C2027/7283 , B64C2027/7288 , Y02T50/34
摘要： A rotor blade (20), especially for a rotary wing aircraft, has an aerodynamically effective rotor blade profile which comprises a profile tip section (21), a profile base (20a) with a profile core (22) and an upper and lower covering skin (30) enclosing the profile core (22), and a profile trailing edge section (23) with a trailing edge (40). A reversibly flexible flection actuator (26) is fastened with a first end to an end section of the profile base (20a) pointing towards the trailing edge (40) and projects with a second end from the profile base (20a) and the end section thereof towards the trailing edge (40). The flection actuator, with the projecting second end, forms a part of the profile trailing edge section (23) of the rotor blade profile and a mobile rotor blade flap (24) which can be deformed to an arched rotor blade flap deflection when the flection actuator (26) is bent.
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公开(公告)号：EP1796960A1
公开(公告)日：2007-06-20
申请号：EP05802354.0
申请日：2005-09-29
IPC分类号： B64C1/14
CPC分类号： B64C1/1407 , B64D13/04
摘要： The invention relates to an aircraft comprising a pressurised cabin with a lockable door, an electrical energy supply network, and a cabin differential pressure warning system (2) provided with an autonomous warning system energy supply device (4, 6, 8) which is independent of the electrical energy supply network.
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38.发明公开Luftfahrzeug-Kommunikationssystem, insbesondere für einen Hubschrauber 有权Luftfahrzeug-Kommunikationssystem，insbesonderefüreinen Hubschrauber
公开(公告)号：EP1793511A1
公开(公告)日：2007-06-06
申请号：EP05400041.9
申请日：2005-12-01
发明人： Lees, Thilo , Stuber, Robert , Seitz, Peter
CPC分类号： H04B7/18508
摘要： Luftfahrzeug-Kommunikations-Verfahren für einen Hubschrauber, sowie Luftfahrzeug-Kommunikationssystem für einen Hubschrauber (15), welches aufweist:
eine Satellitenkommunikationsvorrichtung zum Senden und Empfangen von Sprache und/oder Daten über ein Satellitenkommunikationssystem. Vorteilhaft ist das Satellitenkommunikationssystem ein System mit einem oder mehreren geostationären Satelliten.摘要翻译： 该系统具有通过卫星通信系统发送和接收语音和/或数据的卫星通信设备。 卫星通信系统是具有一套对地静止卫星的系统。 提供加密单元（50a，50b）以对通过卫星通信系统发送的语音和/或数据进行编码，并以编码的方式解码由卫星通信系统接收的语音和/或数据。 直升机的飞机通信方法还包括一项独立的索赔。
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公开(公告)号：EP0980824B1
公开(公告)日：2007-01-10
申请号：EP99111384.6
申请日：1999-06-11
发明人： Pfaller, Rupert , Enenkl, Bernhard
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公开(公告)号：EP1606162A1
公开(公告)日：2005-12-21
申请号：EP03789273.4
申请日：2003-12-13
IPC分类号： B64C27/33
CPC分类号： B64C27/33
摘要： Disclosed is a drilling element (2) for a bearingless rotor, which is made mostly of composite fiber material and the cross section of which has a substantially symmetric, flattened shape that has approximately the contour of a horizontal, central section of a double cone. Also disclosed is a bearingless rotor comprising at least one such drilling element (2). The invention further relates to a rotorcraft, particularly a helicopter, comprising at least one rotor that is provided with at least one such drilling element (2).
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